1. Manuals
  2. Brands
  3. Pilatus Manuals
  4. Aircrafts
  5. PC-12/47E MSN-1001-UP
  6. Maintenance manual

Pilatus PC-12/47E MSN-1001-UP Maintenance Manual

Hide thumbs
1
2
3
4
5
6
7
8
9
10
11
12
13
14
15
16
17
18
19
20
21
22
23
24
25
26
27
28
29
30
31
32
33
34
35
36
37
38
39
40
41
42
43
44
45
46
47
48
49
50
51
52
53
54
55
56
57
58
59
60
61
62
63
64
65
66
67
68
69
70
71
72
73
74
75
76
77
78
79
80
81
82
83
84
85
86
87
88
89
90
91
92
93
94
95
96
97
98
99
100
101
102
103
104
105
106
107
108
109
110
111
112
113
114
115
116
117
118
119
120
121
122
123
124
125
126
127
128
129
130
131
132
133
134
135
136
137
138
139
140
141
142
143
144
145
146
147
148
149
150
151
152
153
154
155
156
157
158
159
160
161
162
163
164
165
166
167
168
169
170
171
172
173
174
175
176
177
178
179
180
181
182
183
184
185
186
187
188
189
190
191
192
193
194
195
196
197
198
199
200
201
202
203
204
205
206
207
208
209
210
211
212
213
214
215
216
217
218
219
220
221
222
223
224
225
226
227
228
229
230
231
232
233
234
235
236
237
238
239
240
241
242
243
244
245
246
247
248
249
250
251
252
253
254
255
256
257
258
259
260
261
262
263
264
265
266
267
268
269
270
271
272
273
274
275
276
277
278
279
280
281
282
283
284
285
286
287
288
289
290
291
292
293
294
295
296
297
298
299
300
301
302
303
304
305
306
307
308
309
310
311
312
313
314
315
316
317
318
319
320
321
322
323
324
325
326
327
328
329
330
331
332
333
334
335
336
337
338
339
340
341
342
343
344
345
346
347
348
349
350
351
352
353
354
355
356
357
358
359
360
361
362
363
364
365
366
367
368
369
370
371
372
373
374
375
376
377
378
379
380
381
382
383
384
385
386
387
388
389
390
391
392
393
394
395
396
397
398
399
400
401
402
403
404
405
406
407
408
409
410
411
412
413
414
415
416
417
418
419
420
421
422
423
424
425
426
427
428
429
430
431
432
433
434
435
436
437
438
439
440
441
442
443
444
445
446
447
448
449
450
451
452
453
454
455
456
457
458
459
460
461
462
463
464
465
466
467
468
469
470
471
472
473
474
475
476
477
478
479
480
481
482
483
484
485
486
487
488
489
490
491
492
493
494
495
496
497
498
499
500
501
502
503
504
505
506
507
508
509
510
511
512
513
514
515
516
517
518
519
520
521
522
523
524
525
526
527
528
529
530
531
532
533
534
535
536
537
538
539
540
541
542
543
544
545
546
547
548
549
550
551
552
553
554
555
556
557
558
559
560
561
562
563
564
565
566
567
568
569
570
571
572
573
574
575
576
577
578
579
580
581
582
583
584
585
586
587
588
589
590
591
592
593
594
595
596
597
598
599
600
601
602
603
604
605
606
607
608
609
610
611
612
613
614
615
616
617
618
619
620
621
622
623
624
625
626
627
628
629
630
631
632
633
634
635
636
637
638
639
640
641
642
643
644
645
646
647
648
649
650
651
652
653
654
655
656
657
658
659
660
661
662
663
664
665
666
667
668
669
670
671
672
673
674
675
676
677
678
679
680
681
682
683
684
685
686
687
688
689
690
691
692
693
694
695
696
697
698
699
700
701
702
703
704
705
706
707
708
709
710
711
712
713
714
715
Table of Contents

Advertisement

Quick Links

Model type - PC-12/47E MSN-1001-UP
Aircraft Maintenance Manual (AMM)
Document Number
12-B-AM-00-00-00-I
Effectivity: All
UNCLASSIFIED
02300
UNCLASSIFIED
©PILATUS AIRCRAFT LTD. CH-6371 STANS, SWITZERLAND
12-B-AM-00-00-00-I
12-B-AM-00-00-00-I

Advertisement

Table of Contents
loading
Need help?

Need help?

Do you have a question about the PC-12/47E MSN-1001-UP and is the answer not in the manual?

Questions and answers

Subscribe to Our Youtube Channel

Related Manuals for Pilatus PC-12/47E MSN-1001-UP

Summary of Contents for Pilatus PC-12/47E MSN-1001-UP

  • Page 1 12-B-AM-00-00-00-I UNCLASSIFIED Model type - PC-12/47E MSN-1001-UP Aircraft Maintenance Manual (AMM) 02300 Document Number 12-B-AM-00-00-00-I Effectivity: All 12-B-AM-00-00-00-I UNCLASSIFIED ©PILATUS AIRCRAFT LTD. CH-6371 STANS, SWITZERLAND...
  • Page 2 12-B-AM-00-00-00-I UNCLASSIFIED Intentionally left blank Effectivity: All 12-B-AM-00-00-00-I UNCLASSIFIED...
  • Page 3 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED PC-12/47E GENERAL - AIRCRAFT MAINTENANCE MANUAL DOCUMENT NO. 02300 LIST OF APPLICABLE DATA MODULES - REVISION 26 Table of Contents Page PC-12/47E GENERAL - AIRCRAFT MAINTENANCE MANUAL DOCUMENT NO. 02300 - LIST OF APPLICABLE DATA MODULES - REVISION 26............
  • Page 4 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Document title Data module code Issue date Effectivity PC-12/47E STRUCTURAL, COMPO- 12-B-04-00-00-00A-000A-A 2021-12-04 NENT AND MISCELLANEOUS LIMITA- TIONS - AMM DOCUMENT NO. 2300 - AIRWORTHINESS LIMITATIONS SCHEDULED / UNSCHEDULED MAIN- 12-B-05-00-00-00A-018A-A 2019-11-19...
  • Page 5 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Document title Data module code Issue date Effectivity HARD LANDING – ELECTRO ME- 12-B-05-50-01-00A-282B-A 2019-11-19 ELECTRO CHANICAL LANDING GEAR - UN- MECHANICAL SCHEDULED INSPECTION LANDING GEAR FLIGHT IN SEVERE TURBULENCE 12-B-05-50-02-00A-282A-A...
  • Page 6 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Document title Data module code Issue date Effectivity LEVELING - MAINTENANCE PRACTI- 12-B-08-20-00-00A-901A-A 2017-07-19 HANDLING AND TAXIING - GENERAL 12-B-09-00-00-00A-040A-A 2019-11-19 - DESCRIPTION AND OPERATION TOWING - MAINTENANCE PRACTI- 12-B-09-10-00-00A-901A-A 2018-11-29...
  • Page 7 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Document title Data module code Issue date Effectivity FUEL - SERVICING 12-B-12-10-01-00A-902A-A 2021-07-08 BRAKES - SERVICING 12-B-12-10-02-00A-902A-A 2019-11-19 ENGINE OIL - SERVICING 12-B-12-10-03-00A-902A-A 2019-11-19 TIRES - SERVICING 12-B-12-10-04-00A-902A-A 2017-07-19 OXYGEN - SERVICING...
  • Page 8 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Document title Data module code Issue date Effectivity STANDARD PRACTICES - NON-DE- 12-B-20-50-00-00A-350A-A 2017-07-19 STRUCTIVE INSPECTION - STRUC- TURE TEST STANDARD PRACTICES - DRILLING, 12-B-20-50-00-00A-901A-A 2017-07-19 CUTTING AND ABRADING MATERIAL COMPOSITE PANELS ANTI–CHAFE...
  • Page 9 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Document title Data module code Issue date Effectivity CABIN PRESSURIZATION CONTROL 12-B-21-30-01-00A-920A-A 2017-07-19 MSN 1001 - UNIT (MSN 1001 - 1719) - REMOV- 1719 AL/INSTALLATION CABIN PRESSURIZATION ELEC- 12-B-21-30-01-00A-920B-A 2019-11-19...
  • Page 10 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Document title Data module code Issue date Effectivity COLD AIR UNIT - REMOVAL/INSTAL- 12-B-21-40-10-00A-920A-A 2019-11-19 LATION CABIN HEATER - REMOVAL/INSTAL- 12-B-21-40-15-00A-920A-A 2019-11-19 CABIN HEAT- LATION ENGINE BAY DUCTS - REPAIR 12-B-21-41-00-00A-904A-A 2018-11-29...
  • Page 11 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Document title Data module code Issue date Effectivity FLIGHT COMPARTMENT TEMPERA- 12-B-21-60-06-00A-920A-A 2019-11-19 TURE SENSOR - REMOVAL/INSTAL- LATION FLIGHT COMPARTMENT TEMPERA- 12-B-21-60-07-00A-920A-A 2019-11-19 TURE SENSOR FAN - REMOVAL/IN- STALLATION UNDERFLOOR TEMPERATURE SEN- 12-B-21-60-08-00A-920A-A...
  • Page 12 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Document title Data module code Issue date Effectivity STICK PUSHER SERVO - REMOV- 12-B-22-20-04-00A-920A-A 2019-11-19 AL/INSTALLATION TORQUE TRANSDUCER - REMOV- 12-B-22-20-05-00A-920A-A 2017-07-19 AL/INSTALLATION STICK PUSHER CAPSTAN - REMOV- 12-B-22-20-06-00A-920A-A 2019-11-19 AL/INSTALLATION...
  • Page 13 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Document title Data module code Issue date Effectivity IRIDIUM SATCOM - DESCRIPTION 12-B-23-16-00-00A-040A-A 2017-07-19 IRIDIUM SAT- AND OPERATION AEROWAVE 100 SATCOM SYSTEM - 12-B-23-16-00-00A-040B-A 2020-11-25 DESCRIPTION AND OPERATION AEROWAVE 100 SATCOM SYSTEM 12-B-23-16-00-00A-903A-A...
  • Page 14 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Document title Data module code Issue date Effectivity DUAL AUDIO INTEGRATING SYSTEM 12-B-23-50-10-00A-903A-A 2021-07-08 DUAL AUDIO - ADJUSTMENT/TEST CONTROL PANELS DUAL AUDIO CONTROL PANEL - RE- 12-B-23-50-11-00A-920A-A 2021-07-08 DUAL AUDIO...
  • Page 15 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Document title Data module code Issue date Effectivity BATTERY AND EXTERNAL POWER 12-B-24-40-01-00A-903A-A 2020-11-25 JUNCTION BOX - ADJUSTMENT/TEST BATTERY AND EXTERNAL POWER 12-B-24-40-01-00A-920A-A 2019-11-19 JUNCTION BOX - REMOVAL/INSTAL- LATION DC ELECTRICAL LOAD DISTRIBU- 12-B-24-50-00-00A-040A-A...
  • Page 16 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Document title Data module code Issue date Effectivity FLIGHT COMPARTMENT CREW 12-B-25-10-01-00A-920A-A 2017-07-19 SEATS - REMOVAL/INSTALLATION CREW SEAT SAFETY HARNESS - RE- 12-B-25-10-02-00A-920A-A 2017-07-19 MOVAL/INSTALLATION FLIGHT COMPARTMENT TRIM - RE- 12-B-25-10-03-00A-920A-A 2021-07-08...
  • Page 17 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Document title Data module code Issue date Effectivity STANDARD TRIM - REMOVAL INSTAL- 12-B-25-22-03-00A-920A-A 2019-11-12 STANDARD LATION INTERIOR STANDARD CARPETS - REMOVAL/IN- 12-B-25-22-04-00A-920A-A 2019-11-19 STANDARD STALLATION INTERIOR BAGGAGE AREA AND TRIM - DE-...
  • Page 18 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Document title Data module code Issue date Effectivity COLD WEATHER PREHEATER SYS- 12-B-25-90-00-00A-040A-A 2017-07-19 COLD TEM - DESCRIPTION AND OPERA- WEATHER TION PREHEATER SYSTEM COLD WEATHER PREHEATER SYS- 12-B-25-90-00-00A-903A-A 2019-05-03 COLD...
  • Page 19 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Document title Data module code Issue date Effectivity AILERON CONTROL SYSTEM - 12-B-27-10-00-00A-307A-A 2017-07-19 PARTS LIST– COCKPIT – KIT P/N 500.50.12.314 AILERON CONTROL SYSTEM - 12-B-27-10-00-00A-307B-A 2017-07-19 PARTS LIST –...
  • Page 20 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Document title Data module code Issue date Effectivity AILERON TRIM - DESCRIPTION AND 12-B-27-15-00-00A-040A-A 2019-11-19 OPERATION AILERON TRIM - ADJUSTMENT/TEST 12-B-27-15-00-00A-903A-A 2019-11-19 AILERON TRIM ACTUATOR - REMOV- 12-B-27-15-01-00A-920A-A 2019-11-19 AL/INSTALLATION...
  • Page 21 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Document title Data module code Issue date Effectivity ELEVATOR CONTROL LEVER - RE- 12-B-27-30-05-00A-920A-A 2019-11-19 MOVAL/INSTALLATION ELEVATOR CONTROL SYSTEM – 12-B-27-30-06-00A-664A-A 2017-07-19 BELLCRANK - SPECIAL REPAIR RM 12–008 HORIZONTAL STABILIZER TRIM - DE- 12-B-27-40-00-00A-040A-A...
  • Page 22 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Document title Data module code Issue date Effectivity FLAP DRIVE SYSTEM - IN SITU EDDY 12-B-27-51-00-00A-353A-A 2019-11-19 CURRENT INSPECTION FLAP DRIVE SYSTEM – WING – LH 12-B-27-51-01-00A-307A-A 2017-07-19 INBOARD MECHANISM - PARTS LIST...
  • Page 23 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Document title Data module code Issue date Effectivity DRAIN VALVE - MAINTENANCE 12-B-28-10-02-00A-901A-A 2021-12-04 PRACTICES DRAIN VALVE - REMOVAL/INSTALLA- 12-B-28-10-02-00A-920A-A 2021-12-04 TION DISTRIBUTION - DESCRIPTION AND 12-B-28-20-00-00A-040A-A 2017-07-19 OPERATION...
  • Page 24 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Document title Data module code Issue date Effectivity FUEL QUANTITY SENSOR AND LOW 12-B-28-40-01-00A-920A-A 2017-07-19 LEVEL SENSOR - REMOVAL/INSTAL- LATION FUEL CONTROL MONITOR UNIT - RE- 12-B-28-40-04-00A-920A-A 2017-07-19 MOVAL/INSTALLATION...
  • Page 25 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Document title Data module code Issue date Effectivity AIRFOIL DE-ICE SYSTEM (TIMER 12-B-30-10-00-00A-040A-A 2018-02-13 MSN 1001 - WITHOUT INHIBIT FUNCTION) - DE- 1751 PRE SB SCRIPTION AND OPERATION 30-013 or PRE SB 30-015 or...
  • Page 26 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Document title Data module code Issue date Effectivity PROBES DE-ICE SYSTEM - ADJUST- 12-B-30-30-20-00A-903A-A 2019-11-19 MENT/TEST AOA PLATE CONTROLLER - REMOV- 12-B-30-30-21-00A-920A-A 2017-07-19 AL/INSTALLATION WINDSHIELD DE–ICE SYSTEM - DE- 12-B-30-40-00-00A-040A-A 2019-11-19 SCRIPTION AND OPERATION...
  • Page 27 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Document title Data module code Issue date Effectivity INDICATING AND RECORDING SYS- 12-B-31-00-00-00A-040A-A 2019-11-19 TEMS - DESCRIPTION AND OPERA- TION OVERHEAD PANEL - DESCRIPTION 12-B-31-10-00-00A-040A-A 2019-11-19 AND OPERATION OVERHEAD PANEL - ADJUST-...
  • Page 28 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Document title Data module code Issue date Effectivity RECORDERS – TEST INSTRUMENTA- 12-B-31-30-05-00A-920A-A 2019-11-20 TION UNIT – LUNCHBOX UNIT - RE- MOVAL/INSTALLATION RECORDERS – TEST INSTRUMENTA- 12-B-31-30-05-00A-920B-A 2019-11-20 TION UNIT –...
  • Page 29 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Document title Data module code Issue date Effectivity MAIN LANDING GEAR AND DOORS 12-B-32-10-00-00A-040A-A 2017-07-19 HYDRAULIC – HYDRAULIC LANDING GEAR - DE- LANDING SCRIPTION AND OPERATION GEAR MAIN LANDING GEAR AND DOORS 12-B-32-10-00-00A-040B-A...
  • Page 30 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Document title Data module code Issue date Effectivity SHOCK ABSORBER – ELECTRO ME- 12-B-32-10-03-00A-920B-A 2019-11-19 ELECTRO CHANICAL LANDING GEAR - REMOV- MECHANICAL AL/INSTALLATION LANDING GEAR MAIN GEAR AND DOORS - FOLDING 12-B-32-10-05-00A-920A-A 2020-11-25...
  • Page 31 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Document title Data module code Issue date Effectivity NOSE LANDING GEAR DOOR – HY- 12-B-32-20-02-00A-920A-A 2017-07-19 HYDRAULIC DRAULIC LANDING GEAR - REMOV- LANDING AL/INSTALLATION GEAR NOSE LANDING GEAR DOOR –...
  • Page 32 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Document title Data module code Issue date Effectivity MAIN LANDING GEAR ACTUATOR – 12-B-32-30-01-00A-920A-A 2019-11-19 HYDRAULIC HYDRAULIC LANDING GEAR - RE- LANDING MOVAL/INSTALLATION GEAR MAIN LANDING GEAR ACTUATOR 12-B-32-30-01-00A-920B-A 2021-07-08 ELECTRO-...
  • Page 33 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Document title Data module code Issue date Effectivity LANDING GEAR RELAY UNIT – ELEC- 12-B-32-30-08-00A-920A-A 2019-11-19 ELECTRO TRO MECHANICAL LANDING GEAR - MECHANICAL REMOVAL/INSTALLATION LANDING GEAR EMERGENCY GEAR EXTENSION 12-B-32-30-10-00A-040A-A...
  • Page 34 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Document title Data module code Issue date Effectivity BRAKE SWIVEL ASSEMBLY (PRE SB 12-B-32-40-06-00A-920A-A 2017-07-19 PRE SB 32–022) - REMOVAL/INSTALLATION 32-022 PARK BRAKE CABLE - REMOVAL/IN- 12-B-32-40-07-00A-920A-A 2018-05-24 STALLATION...
  • Page 35 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Document title Data module code Issue date Effectivity REAR CENTER CONSOLE PANEL 12-B-33-10-02-00A-920A-A 2017-07-19 (PRE SB 46–003 AND MSN 1001 – 1001-1175 1175) - REMOVAL/INSTALLATION REAR CENTER CONSOLE PANEL 12-B-33-10-02-00A-920B-A 2019-11-19...
  • Page 36 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Document title Data module code Issue date Effectivity LED LANDING LIGHT - REMOVAL/IN- 12-B-33-41-01-00A-920B-A 2019-11-19 LED LAND- STALLATION ING LIGHT TAXI LIGHT - DESCRIPTION AND OP- 12-B-33-42-00-00A-040A-A 2017-07-19 ERATION...
  • Page 37 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Document title Data module code Issue date Effectivity LED PULSE RECOGNITION LIGHTS - 12-B-33-44-00-00A-903C-A 2019-11-19 LED PULSE ADJUSTMENT/TEST RECOGNI- TION LIGHTS RECOGNITION LIGHTS - REMOV- 12-B-33-44-00-00A-920A-A 2017-07-19 AL/INSTALLATION...
  • Page 38 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Document title Data module code Issue date Effectivity OUTSIDE AIR TEMPERATURE - DE- 12-B-34-12-00-00A-040A-A 2019-11-19 SCRIPTION AND OPERATION OUTSIDE AIR TEMPERATURE SYS- 12-B-34-12-00-00A-903A-A 2017-07-19 TEM - ADJUSTMENT/TEST ALTITUDE AND VERTICAL SPEED IN- 12-B-34-14-00-00A-903A-A 2021-12-04...
  • Page 39 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Document title Data module code Issue date Effectivity ADAHRS – HEADING/TRACK OVER- 12-B-34-25-04-00A-920A-A 2017-07-19 HEADING/ RIDE SWITCH - REMOVAL/INSTALLA- TRACK TION OVERRIDE SWITCH ELECTRONIC STANDBY INSTRU- 12-B-34-26-40-00A-040A-A 2017-07-19 MSN 1001 -...
  • Page 40 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Document title Data module code Issue date Effectivity WEATHER RADAR - DESCRIPTION 12-B-34-41-00-00A-040A-A 2017-07-19 AND OPERATION WEATHER RADAR - ADJUST- 12-B-34-41-00-00A-903A-A 2020-11-25 MENT/TEST WEATHER RADAR TRANSCEIVER - 12-B-34-41-02-00A-920A-A 2021-07-08 REMOVAL/INSTALLATION...
  • Page 41 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Document title Data module code Issue date Effectivity TRAFFIC ALERT AND COLLISION 12-B-34-44-00-00A-903A-A 2021-07-08 TCAS AVOIDANCE SYSTEM - ADJUST- MENT/TEST TCAS PROCESSOR - REMOVAL/IN- 12-B-34-44-01-00A-920A-A 2017-07-19 TCAS STALLATION...
  • Page 42 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Document title Data module code Issue date Effectivity ADF SYSTEM - DESCRIPTION AND 12-B-34-53-00-00A-040A-A 2021-07-08 OPERATION ADF SYSTEM - ADJUSTMENT/TEST 12-B-34-53-00-00A-903A-A 2020-11-25 ADF ANTENNA - REMOVAL/INSTAL- 12-B-34-53-02-00A-920A-A 2017-07-19 LATION...
  • Page 43 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Document title Data module code Issue date Effectivity SINGLE DIVERSITY AIR TRAFFIC 12-B-34-54-10-00A-040A-A 2017-07-19 SINGLE DI- CONTROL TRANSPONDER SYSTEM VERSITY ATC WITHOUT ADS–B OUT - DESCRIP- TRANSPOND- TION AND OPERATION ER WITHOUT...
  • Page 44 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Document title Data module code Issue date Effectivity OXYGEN (PLUG-IN MASK) SYSTEM - 12-B-35-00-00-00A-903A-A 2019-11-19 PLUG-IN ADJUSTMENT/TEST MASK SYS- OXYGEN (DROP-DOWN MASK) SYS- 12-B-35-00-00-00A-903B-A 2019-11-19 TEM - ADJUSTMENT/TEST CREW OXYGEN SYSTEM - DESCRIP- 12-B-35-10-00-00A-040A-A...
  • Page 45 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Document title Data module code Issue date Effectivity PASSENGER OXYGEN SYSTEM - 12-B-35-20-06-00A-920A-A 2019-11-19 LARGE CA- SHUT-OFF VALVE - REMOVAL/IN- PACITY OXY- STALLATION GEN SYSTEM CENTRAL MAINTENANCE SYSTEM - 12-B-45-00-00-00A-040A-A 2017-07-19...
  • Page 46 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Document title Data module code Issue date Effectivity ASPEN CONNECTED GATEWAY - RE- 12-B-46-21-12-00A-920A-A 2019-11-19 POST SB MOVAL/INSTALLATION 46-004 OR CONNECTED FLIGHT DECK OPTION DISPLAY AND CONTROL - DESCRIP- 12-B-46-30-00-00A-040A-A 2017-07-19 TION AND OPERATION...
  • Page 47 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Document title Data module code Issue date Effectivity REVERSION CONTROL PANEL (3 12-B-46-30-06-00A-040A-A 2017-07-19 THREE SWITCH) - DESCRIPTION AND OPER- SWITCH RE- ATION VERSION CONTROL PANEL REVERSION CONTROL PANEL (3 12-B-46-30-06-00A-903A-A...
  • Page 48 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Document title Data module code Issue date Effectivity PASSENGER/CREW DOOR SKINS - 12-B-52-10-01-00A-353A-A 2017-07-19 EDDY CURRENT INSPECTION PASSENGER DOOR (WITHOUT STAIR 12-B-52-10-01-00A-920A-A 2020-11-25 WITHOUT LIGHTS) - REMOVAL/INSTALLATION STAIR LIGHTS PASSENGER DOOR (WITH STAIR...
  • Page 49 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Document title Data module code Issue date Effectivity CARGO DOOR SEAL - REMOVAL/IN- 12-B-52-30-03-00A-920A-A 2019-11-19 STALLATION CARGO DOOR DRIVE MECHANISM - 12-B-52-30-04-00A-903A-A 2020-11-25 ADJUSTMENT/TEST CARGO DOOR DRIVE MECHANISM - 12-B-52-30-04-00A-920A-A 2019-11-19 REMOVAL/INSTALLATION...
  • Page 50 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Document title Data module code Issue date Effectivity CENTER FUSELAGE FRAMES – CAR- 12-B-53-20-02-00A-307A-A 2019-11-19 RY THROUGH FRAMES - PARTS LIST – KIT P/N 500.50.12.327 CENTER FUSELAGE FRAMES - CAR- 12-B-53-20-02-00A-310A-A 2019-11-19...
  • Page 51 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Document title Data module code Issue date Effectivity VERTICAL STABILZER - DORSAL FIN 12-B-55-30-04-00A-920A-A 2017-07-19 - REMOVAL/INSTALLATION VERTICAL STABILIZER - FAIRING - 12-B-55-30-05-00A-920A-A 2017-07-19 REMOVAL/INSTALLATION RUDDER - EXAMINE 12-B-55-40-00-00A-310A-A 2019-11-19...
  • Page 52 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Document title Data module code Issue date Effectivity LEFT WING - HYDRAULIC LANDING 12-B-57-00-00-00A-720A-A 2021-12-04 HYDRAULIC GEAR - INSTALLATION LANDING GEAR LEFT WING – ELECTRO MECHANI- 12-B-57-00-00-00A-720B-A 2021-12-04 ELECTRO...
  • Page 53 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Document title Data module code Issue date Effectivity WING STRUCTURE – SPARS AND 12-B-57-20-10-00A-307B-A 2019-11-19 AUXILIARY STRUCTURE - PARTS LIST – SECOND OVERSIZE – P/N 500.60.12.020 WING STRUCTURE - SPARS AND 12-B-57-20-10-00A-353A-A...
  • Page 54 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Document title Data module code Issue date Effectivity FIVE-BLADED PROPELLER - AD- 12-B-61-00-00-00A-903B-A 2021-12-04 FIVE-BLADED JUSTMENT/TEST PROPELLER FOUR-BLADED PROPELLER - 12-B-61-00-00-00A-904A-A 2017-07-19 FOUR-BLA- BLADES - REPAIR DED PRO- PELLER FIVE-BLADED PROPELLER - BLADES...
  • Page 55 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Document title Data module code Issue date Effectivity POWER PLANT TEST 7 – EN- 12-B-71-00-00-00A-903H-A 2017-07-19 GINE PERFORMANCE - ADJUST- MENT/TEST POWER PLANT TEST 8 – TOR- 12-B-71-00-00-00A-903I-A 2017-07-19 QUEMETER FUNCTION - ADJUST-...
  • Page 56 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Document title Data module code Issue date Effectivity COWLING - RUBBER SEAL - REMOV- 12-B-71-10-01-00A-920A-A 2019-11-19 AL/INSTALLATION LOWER AFT COWLING ASSEMBLY - 12-B-71-10-10-00A-920A-A 2019-11-19 REMOVAL/INSTALLATION ENGINE - DESCRIPTION AND OPER- 12-B-72-00-00-00A-040A-A 2017-07-19...
  • Page 57 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Document title Data module code Issue date Effectivity EXHAUST - DESCRIPTION AND OP- 12-B-78-00-00-00A-040A-A 2017-07-19 ERATION EXHAUST STUB - REPAIR 12-B-78-10-01-00A-904A-A 2017-07-19 LEFT EXHAUST ASSEMBLY DE–ICE 12-B-78-10-01-00A-904B-A 2018-05-24 BLEED AIR TUBE - REPAIR...
  • Page 58 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Intentionally left blank Effectivity: All 12-B-00-00-00-00A-002A-A UNCLASSIFIED 2021-12-10 Page 56...

  • Page 59: Table Of Contents

    PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED PC-12/47E GENERAL - AIRCRAFT MAINTENANCE MANUAL CHANGE HIGHLIGHTS - REVISION 26 Table of Contents Page PC-12/47E GENERAL - AIRCRAFT MAINTENANCE MANUAL - CHANGE HIGHLIGHTS - REVISION 26..........................

  • Page 60: Dm Reference

    PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED DM Reference Action Change 12-B-05-40-01-02A-000B-A Replaced 23238-3-7 - Editorial updates to various tasks. 23309-3-8 - Edi- torial changes: access panel remove and install tasks split by inspection package and aircraft zone.

  • Page 61: 12-B-00-00-00-00A-003A-A

    PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED DM Reference Action Change 12-B-32-40-01-00A-920A-A Replaced 23216-3-1 - Washer removed and bushes added on illustration and related text. 12-B-32-40-03-00A-920A-A Replaced 21715-3-1 - Illustration updated, AGE and Tools updated, satn- dard sentences used.
  • Page 62 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Intentionally left blank Effectivity: All 12-B-00-00-00-00A-003A-A UNCLASSIFIED 2021-12-10 Page 4...

  • Page 63: 12-B-00-00-00-00A-006A-A

    AMM LIST OF TEMPORARY REVISIONS List of Temporary Revisions Temp Rev No. Date of Issue Date Inserted Signature Date or Revision Signature Removed 05-01 Dec 09/08 Dec 16/08 Pilatus Pilatus 27-01 Dec 09/08 Dec 16/08 Pilatus Pilatus 00-01 Jan 05/09 Jan 23/09 Pilatus Pilatus...
  • Page 64 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Temp Rev No. Date of Issue Date Inserted Signature Date or Revision Signature Removed 05-03 Jul 31/14 Jul 31/14 Pilatus Pilatus 00-07 Mar 09/15 Mar 09/15 Pilatus Pilatus 76-01 Jun 01/15 Jun 01/15 Pilatus Pilatus 33-01 Jun 05/15...
  • Page 65 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Temp Rev No. Date of Issue Date Inserted Signature Date or Revision Signature Removed Effectivity: All 12-B-00-00-00-00A-006A-A UNCLASSIFIED 2021-12-04 Page 3...
  • Page 66 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Temp Rev No. Date of Issue Date Inserted Signature Date or Revision Signature Removed Effectivity: All 12-B-00-00-00-00A-006A-A End of data module UNCLASSIFIED 2021-12-04 Page 4...
  • Page 67 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED GENERAL LIST OF ABBREVIATIONS Table of Contents Page GENERAL - LIST OF ABBREVIATIONS..................Index of Tables Page References......................Abbreviations......................References Table 1 References Data module/Technical publication Title None Description...

  • Page 68: 12-B-00-00-00-00A-005A-A

    PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Table 2 Abbreviations (Continued from previous page) ABBREVIATION DESCRIPTION AHRS Attitude and Reference Heading System AIOP Actuator Input/Output Processor Aircraft Maintenance Manual Angle of Attack Autopilot Aircraft Personality Module (configuration module) As required...
  • Page 69 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Table 2 Abbreviations (Continued from previous page) ABBREVIATION DESCRIPTION Direct Current Difference in Depth Modulation or Deviation from Desired Marker DEOS Digital Engine Operating System Decision Height Data Loading Software Data Module...
  • Page 70 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Table 2 Abbreviations (Continued from previous page) ABBREVIATION DESCRIPTION Flight Management Window Frame Go-around Generator Control Unit Generic Input/Output (module) Generator Line Contactor Greenwich Mean Time GNSSU Global Navigation Sensor System Unit Global Positioning System...
  • Page 71 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Table 2 Abbreviations (Continued from previous page) ABBREVIATION DESCRIPTION Light Emitting Diode Left Line Replacement Unit Low Side Switch Liter Modular Avionics Unit Maximum Megabyte Methyl Ethyl Ketone Multi Function Multi Function Controller...
  • Page 72 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Table 2 Abbreviations (Continued from previous page) ABBREVIATION DESCRIPTION O2/OXY Oxygen Outside Air Temperature Overhead Control Panel Oil Debris Monitoring Overhead Panel OSCMM Operating, Servicing and Component Maintenance Manual PBIT Power-On Built-in Test Power Control Lever...
  • Page 73 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Table 2 Abbreviations (Continued from previous page) ABBREVIATION DESCRIPTION Square Structural Repair Manual SSEC Static Source Error Correction STBY Standby Software Traffic Advisory System TAWS Terrain Awareness &...
  • Page 74 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Intentionally left blank Effectivity: All 12-B-00-00-00-00A-005A-A UNCLASSIFIED 2021-12-04 Page 8...

  • Page 75: General - Amm Introduction

    PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED GENERAL AMM INTRODUCTION Table of Contents Page GENERAL - AMM INTRODUCTION................... General........................Effectivity........................ Responsibilities....................... Spares, Approved Parts, Materials, Processes............Copyright and Legal Statement................Occurrence Reporting Requirement............... Publication Revisions.....................

  • Page 76: General

    If it is necessary to contact Pilatus Aircraft Ltd. about your aircraft, it is important to include the aircraft serial number in any correspondence. The serial number can be found on the manufacturer’s Identification Plate installed aft of the cargo door.

  • Page 77: Copyright And Legal Statement

    No part of this document may be copied, reproduced or translated to other languages without the prior written consent of Pilatus Aircraft Ltd. In connection with the use of this document, Pilatus does not provide any express or implied warranties and expressly disclaims any warranty of merchantability or fitness for a particular purpose. This document contains trade secrets, confidential and/or proprietary information of Pilatus and technical data subject to export control laws and regulations, including the U.S.

  • Page 78: 12-B-00-00-00-00A-018A-A

    PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED NOTE: Used to give details of hints or tips which make the task easier for maintenance personnel. Data Module Code The Data Module Code (DMC) has 17 alpha numeric characters. YY-YY-YY refer to refer to...
  • Page 79 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED − 000 - Airworthiness Limitations − 000 - Function, Data for Plans and Description − 002 - List of Applicable Data Modules − 003 - Change Highlights −...

  • Page 80: Information Code Variant

    PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED − 552 - Data Erasing − 553 - Change the Settings − 720 - Installation − 901 - Maintenance Practices − 902 - Servicing − 903 - Adjustment/Test −...
  • Page 81 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED YY-Y-YY-YY-YY-YYY-YYYY-Y The unit or assembly is identified in the DMC by the highlighted characters. The AMM has the following SNS breakdown to show the systems, subsystems and sub-subsystems: Chapter Section Title...
  • Page 82 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Chapter Section Title System Subsystem/Sub-subsystem Placards and Markings General Exterior Placards and Markings Interior Placards and Markings Servicing General Replenishing and Depleting Scheduled Servicing Standard Practices General Locking and Retaining Devices Consumable Materials List...
  • Page 83 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Chapter Section Title System Subsystem/Sub-subsystem General DC Generation External Power Load Distribution DC Load Distribution 110 VAC Auxiliary Power Equipment and Furnishings General Flight Compartment Passenger Compartment Executive Interior Standard Interior...
  • Page 84 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Chapter Section Title System Subsystem/Sub-subsystem Hydraulic Power General Main Emergency Ice and Rain Protection General Airfoil Wing De-icing Boots Horizontal Stabilizer De-icing Boots Air Intake Pitot and Static Windshield Propeller...
  • Page 85 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Chapter Section Title System Subsystem/Sub-subsystem Exterior Landing Lights Taxi Lights Navigation and Strobe Lights Recognition Lights Logo Lights Red Flashing Beacons Navigation General Flight Environment Data Pitot Static System Altitude and Vertical Speed Indication Angle of Attack...
  • Page 86 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Chapter Section Title System Subsystem/Sub-subsystem Systems Integration and Display General Wireless Data Loading System (Connected Flight Deck) Display Doors General Passenger/Crew Emergency Exit Cargo Service Door Warning Fuselage General...
  • Page 87 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Chapter Section Title System Subsystem/Sub-subsystem Power Plant General Cowling Engine General Power Section Engine Fuel and Control General Controlling Indicating Ignition General Electrical Power Supply Distribution Engine Controls General...

  • Page 88: Punctuation In Units Of Weight And Measurement

    Refer to AMM 12-B-00-00-00-00A-005A-A for the list of abbreviations. Publication Revision Request If operators have suggestions for improvements to the content of the manual or errors are found, please submit the proposed changes (use this form, AMM 12-B-00-00-00-00A-030A-A) by email to publications@pilatus-aircraft.com Effectivity: All 12-B-00-00-00-00A-018A-A...

  • Page 89: 12-B-00-00-00-00A-106A-A

    PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED GENERAL LIST OF SOFTWARE Table of Contents Page GENERAL - LIST OF SOFTWARE..................... Index of Tables Page References......................References Table 1 References Data module/Technical publication Title 12-B-00-00-00-10A-030A-A.PDF Description...
  • Page 90 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Intentionally left blank Effectivity: All 12-B-00-00-00-00A-106A-A UNCLASSIFIED 2021-12-04 Page 2...
  • Page 91 PC-12/47E Software and Hardware Compatibility Component Description Part Number Supplier Partnumber Primus Apex Software Primus Apex System Build 7 Software EB7037248-00104 Primus Apex Option File, PC-12E TT60000664-xxx Primus Apex Settings File, PC-12E use B7 settings.def to create file Loadable Diagnostic Interface (LDI) PC12_LDI_7_1_14 Build 7 PC-APEX Simulation Tool (not installed on a/c)
  • Page 92 PC-12/47E Software and Hardware Compatibility Component Description Part Number Supplier Partnumber Primus Apex Databases 888.309.7555 or 303.328.6948 Purple Disk Green Disk 888.309.7555 or 303.328.6948 Blue Disk 888.309.7555 or 303.328.6948 Checklist Database Apex FMS Performance Database MM60000461-002 (or -001) ADAHRS Dual Channel ADAHRS & 065-00188-5103 (SW/MOD_03/01) &...
  • Page 93 PC-12/47E Software and Hardware Compatibility Valid MAU Hardware/System combinations Description Part Number Supplier Partnumber Power Supply Module PWR-200 Power Supply Module 7024440-1901 PWR-200 Power Supply Module 7024440-1901 (HW/MOD_G) PWR-210 Power Supply Module 7038248-1901 PWR-210 Power Supply Module 7038248-1901 (HW/MOD_A or HW/MOD_B) PWR-210 Power Supply Module 7038248-1901 (HW/MOD_A_B_C)

  • Page 94: Index Of Tables Page

    PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED PC-12/47E STRUCTURAL, COMPONENT AND MISCELLANEOUS LIMITATIONS - AMM DOCUMENT NO. 2300 AIRWORTHINESS LIMITATIONS Table of Contents Page PC-12/47E STRUCTURAL, COMPONENT AND MISCELLANEOUS LIMITATIONS - AMM DOCUMENT NO.

  • Page 95: 12-B-04-00-00-00A-000A-A

    PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Data module/Technical publication Title 12-B-27-10-08-00A-352B-A AILERON CONTROL SYSTEM - FUSELAGE BELLCRANK - MAGNETIC PARTICLE INSPECTION 12-B-27-10-08-00A-353A-A AILERON CONTROL SYSTEM - OUTER WING BELLCRANK - EDDY CURRENT INSPECTION 12-B-27-10-08-00A-353B-A AILERON CONTROL SYSTEM - FUSELAGE BELLCRANK - EDDY CURRENT INSPECTION...
  • Page 96 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Data module/Technical publication Title 12-B-52-10-00-00A-310A-A PASSENGER DOOR - EXAMINE 12-B-52-20-00-00A-310A-A EMERGENCY EXIT - EXAMINE 12-B-52-30-00-00A-310A-A CARGO DOOR - EXAMINE 12-B-53-00-00-00A-310A-A FUSELAGE - ANTENNA STRUCTURE – EXAMINE 12-B-53-00-00-00A-353A-A FUSELAGE - ANTENNA STRUCTURE –...

  • Page 97: General

    532.10.12.049 with serial numbers AM 001 thru 053 (Ref. Pilatus Service Bulletin 32-015/016/018). 532.10.12.050 with serial numbers AM 001 thru 053 (Ref. Pilatus Service Bulletin 32-015/016/018). 532.10.12.077 with serial numbers AM 001 thru 229 and all without primer and painted head (Ref. Pilatus Service Bulletin 32-012/018).

  • Page 98: Structural Limitations

    PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED 532.10.12.175 with serial numbers AM 001 thru 107 (Ref. Pilatus Service Bulletin 32-016). Main Landing Gear Actuators 960.30.01.103 with serial numbers 830E thru 881E (Ref. Pilatus Service Bulletin 32-017). Flaps FCWU 99-3 with serial numbers lower than 10000 and all Vickers Flap Actuators (P/N's 978.73.20.301,...
  • Page 99 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Table 3 Component Limitations (Continued from previous page) Task number Component Life 27-40/3 Pitch trim actuator 20,000 FH / 27,000 LDG 27-40/307 Pitch trim actuator attachment parts, 10,000 FH fail safe plates and their attachment parts (IPD 12-20-00-07)

  • Page 100: Miscellaneous Limitations

    PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Miscellaneous Limitations Table 4 Miscellaneous Limitations Task number Component Procedure Limitation Reference 21-20/317 ECS emergency shut- Attach a spring bal- 3,000 FH / 12 Months off system ance to the ECS See Note 2...
  • Page 101 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Table 4 Miscellaneous Limitations (Continued from previous page) Task number Component Procedure Limitation Reference 32-10/436 Main landing gear Examine 12 Months 12-B-32-10-00-00A- shock absorber top See Note 2 310A-A and bottom attach-...
  • Page 102 353D-A No cracks are permit- 22,500 wing landings. ted. If you find cracks, All wings with no contact Pilatus Cus- landing records must tomer Support for ad- apply a calculated vice, www.pilatus-air- applicable landings craft.com -> contact.
  • Page 103 Contact Pilatus for the lead time of the Pilatus support activities as listed in Para 5.2 and Para 5.3 , www.pilatus-aircraft.com -> contact.
  • Page 104 For the part of the STC itself the STC holder(s) only must do this assessment. On request, Pilatus can do the assessments for items (b) and the first part of (c) in addition to (a) above, provided sufficient information is given.

  • Page 105: Supplemental Structural Inspection Program

    PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Table 5 Supplemental Structural Inspection Program SUPPLEMENTAL STRUCTURAL INSPECTION PROGRAM Task number Inspection/Reference Threshold (whichev- Repeated Interval (whichever er comes first) comes first) Flying Flying Landings Landings Years...
  • Page 106 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Table 5 Supplemental Structural Inspection Program (Continued from previous page) SUPPLEMENTAL STRUCTURAL INSPECTION PROGRAM Task number Inspection/Reference Threshold (whichev- Repeated Interval (whichever er comes first) comes first) Flying Flying...
  • Page 107 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Table 5 Supplemental Structural Inspection Program (Continued from previous page) SUPPLEMENTAL STRUCTURAL INSPECTION PROGRAM Task number Inspection/Reference Threshold (whichev- Repeated Interval (whichever er comes first) comes first) Flying Flying...
  • Page 108 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Table 5 Supplemental Structural Inspection Program (Continued from previous page) SUPPLEMENTAL STRUCTURAL INSPECTION PROGRAM Task number Inspection/Reference Threshold (whichev- Repeated Interval (whichever er comes first) comes first) Flying Flying...
  • Page 109 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Table 5 Supplemental Structural Inspection Program (Continued from previous page) SUPPLEMENTAL STRUCTURAL INSPECTION PROGRAM Task number Inspection/Reference Threshold (whichev- Repeated Interval (whichever er comes first) comes first) Flying Flying...
  • Page 110 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Table 5 Supplemental Structural Inspection Program (Continued from previous page) SUPPLEMENTAL STRUCTURAL INSPECTION PROGRAM Task number Inspection/Reference Threshold (whichev- Repeated Interval (whichever er comes first) comes first) Flying Flying...
  • Page 111 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Intentionally left blank Effectivity: All 12-B-04-00-00-00A-000A-A UNCLASSIFIED 2021-12-04 Page 18...
  • Page 112 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED OVERHAUL AND REPLACEMENT SCHEDULE SCHEDULED INSPECTIONS Table of Contents Page OVERHAUL AND REPLACEMENT SCHEDULE - SCHEDULED INSPECTIONS....Index of Tables Page References......................Required Conditions....................Support equipment....................Supplies........................

  • Page 113: 12-B-05-10-10-00A-281A-A

    PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Spares Table 5 Spares Name Identifications/References Reference Remark None Safety Conditions None Procedure Overhaul and Replacement Schedule Table 6 Overhaul and Replacement Schedule Task number Component Discard Interval Overhaul Interval...
  • Page 114 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Table 6 Overhaul and Replacement Schedule (Continued from previous page) Task number Component Discard Interval Overhaul Interval 72-00/308 Engine accessories P&WC SB 14603 latest re- vision 79-20/43 Oil cooler...
  • Page 115 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Intentionally left blank Effectivity: All 12-B-05-10-10-00A-281A-A UNCLASSIFIED 2021-12-04 Page 4...
  • Page 116 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED TIME LIMITED INSPECTION REQUIREMENTS SCHEDULED INSPECTIONS Table of Contents Page TIME LIMITED INSPECTION REQUIREMENTS - SCHEDULED INSPECTIONS....Index of Tables Page References......................Required Conditions....................Support equipment....................Supplies........................

  • Page 117: 12-B-05-10-20-00A-281A-A

    PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Data module/Technical publication Title 12-B-25-22-03-00A-920A-A STANDARD TRIM - REMOVAL INSTALLATION 12-B-25-63-04-00A-903A-A UNDERWATER LOCATOR BEACON - ADJUSTMENT/TEST 12-B-25-63-04-00A-920A-A UNDERWATER LOCATOR BEACON - REMOVAL/INSTALLA- TION 12-B-27-00-00-00A-313A-A FLIGHT CONTROLS - INSPECTION/CHECK 12-B-27-20-00-00A-903A-A RUDDER CONTROL SYSTEM - ADJUSTMENT/TEST 12-B-27-30-00-00A-903A-A...

  • Page 118: References

    PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Data module/Technical publication Title 12-B-53-30-01-00A-313A-A REAR FUSELAGE SKINS AND STRINGERS (RVSM) - IN- SPECTION/CHECK 12-B-56-11-02-00A-313A-A COCKPIT SIDE WINDOWS - INSPECTION/CHECK 12-B-57-00-00-00A-313A-A WING AND FUSELAGE FITTINGS - INSPECTION/CHECK 12-B-76-10-02-00A-903A-A PROPELLER FEATHER MICROSWITCHES - ADJUST- MENT/TEST...

  • Page 119: Time Limited Inspection Requirements

    PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Procedure Time Limited Inspection Requirements Table 6 Time Limited Inspection Requirements Task number Item Name Task Description Interval Data Module Refer- ence 00-00/45 Aircraft Do the corrosion and AMM 12- 12-B-20-40-00-00A- corrosion protection...
  • Page 120 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Table 6 Time Limited Inspection Requirements (Continued from previous page) Task number Item Name Task Description Interval Data Module Refer- ence 24-30/340 Lead acid batteries Remove and do a ca- Initially at 1000 FH or 12-B-24-30-07-00A-...
  • Page 121 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Table 6 Time Limited Inspection Requirements (Continued from previous page) Task number Item Name Task Description Interval Data Module Refer- ence 27-30/333 Elevator control ca- Check for new facto- Within the next 300 12-B-27-30-00-00A-...
  • Page 122 Moderate Corrosive 12-B-25-22-03-00A- lation mat for corro- Environment: 4000 920A-A sion. If corrosion is FH or 48 Months found, write to Pilatus Severe Corrosive En- 12-B-52-10-00-00A- for a specific repair. vironment: 2000 FH 313A-A Examine door hinge or 24 Months pin and hinges.
  • Page 123 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Table 6 Time Limited Inspection Requirements (Continued from previous page) Task number Item Name Task Description Interval Data Module Refer- ence 52-30/89 Cargo door Examine with trim re- Mild Corrosive Envi- 12-B-25-21-03-00A- moved...
  • Page 124 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Table 6 Time Limited Inspection Requirements (Continued from previous page) Task number Item Name Task Description Interval Data Module Refer- ence 53-00/91 Fuselage internal bot- Examine Frames 10, Mild Corrosive Envi- tom surface...
  • Page 125 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Table 6 Time Limited Inspection Requirements (Continued from previous page) Task number Item Name Task Description Interval Data Module Refer- ence 53-00/93 Structure around win- Examine Mild Corrosive Envi- dows...
  • Page 126 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Table 6 Time Limited Inspection Requirements (Continued from previous page) Task number Item Name Task Description Interval Data Module Refer- ence 55-10/95 Horizontal stabilizer Examine as far as Mild Corrosive Envi- internal surfaces possible with panels...
  • Page 127 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Table 6 Time Limited Inspection Requirements (Continued from previous page) Task number Item Name Task Description Interval Data Module Refer- ence 57-00/97 Wing internal surfa- Examine as far as Mild Corrosive Envi- ces and flap compart-...

  • Page 128: Time Limited Inspection Requirements - Rvsm Aircraft

    PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Table 6 Time Limited Inspection Requirements (Continued from previous page) Task number Item Name Task Description Interval Data Module Refer- ence 61-00/457 Five-bladed compo- Refer to the Hartzell Refer to Hartzell site propeller Owner’s Manual 147.
  • Page 129 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Intentionally left blank Effectivity: All 12-B-05-10-20-00A-281A-A UNCLASSIFIED 2021-12-04 Page 14...
  • Page 130 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED SUPPLEMENTAL STRUCTURAL INSPECTION DOCUMENT INSPECTIONS Table of Contents Page SUPPLEMENTAL STRUCTURAL INSPECTION DOCUMENT - INSPECTIONS...... Index of Tables Page References......................Required Conditions....................Support equipment....................Supplies........................Spares........................

  • Page 131: 12-B-05-10-30-00A-280A-A

    PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Required Conditions Table 2 Required Conditions Action / Condition Data module/Technical publication None Support equipment Table 3 Support equipment Name Identifications/References Reference Remark None Supplies Table 4 Supplies Name Identifications/References...

  • Page 132: Supplemental Inspections

    PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Procedure General This data module is referenced from the AMM Airworthiness Limitations data module 12-B-04-00-00- 00A-000A-A. Inspections Do these supplemental structural inspections to increase the life of the airframe above more than 25000 flying hours or 30000 landings: Table 6 Supplemental Inspections SUPPLEMENTAL INSPECTIONS...

  • Page 133: Required Conditions

    PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Table 6 Supplemental Inspections (Continued from previous page) SUPPLEMENTAL INSPECTIONS Task number Inspection/Reference Threshold (whichev- Repeated Interval (whichever er comes first) comes first) Flying Flying Landings Landings Years...
  • Page 134 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED JOB SET UP / CLOSE UP GENERAL MAINTENANCE PROCEDURE Table of Contents Page JOB SET UP / CLOSE UP - GENERAL MAINTENANCE PROCEDURE........Index of Tables Page References......................

  • Page 135: 12-B-05-20-00-00A-913A-A

    PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Support equipment Table 3 Support equipment Name Identifications/References Reference Remark None Supplies Table 4 Supplies Name Identifications/References Reference Remark None Spares Table 5 Spares Name Identifications/References Reference Remark...
  • Page 136 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Table 6 Job Set Up (Continued from previous page) Task number Item Name Task Description Data Module Signature/Stamp Inspection Reference 25-20/298 Passenger seats Remove as nec- 12-B-25-21-01- essary to do the 00A-920A-A...
  • Page 137 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Table 7 Job Close Up Task number Item Name Task Description Data Module Signature/Stamp Inspection Reference 00-00/121 Aircraft Airworthiness Di- rectives and Service Bulletins reviewed and complied with as required.
  • Page 138 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Requirements after job completion Required Conditions Table 8 Required Conditions Action / Condition Data module/Technical publication None Effectivity: All 12-B-05-20-00-00A-913A-A End of data module UNCLASSIFIED 2021-12-04 Page 5...
  • Page 139 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Intentionally left blank Effectivity: All 12-B-05-20-00-00A-913A-A UNCLASSIFIED 2021-12-04 Page 6...
  • Page 140 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED MASTER MAINTENANCE PLAN FUNCTION, DATA FOR PLANS AND DESCRIPTION Table of Contents Page MASTER MAINTENANCE PLAN - FUNCTION, DATA FOR PLANS AND DESCRIPTION..General........................Purpose........................Task List........................

  • Page 141: 12-B-05-40-00-00A-000B-A

    PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Data module/Technical publication Title 12-B-21-30-02-00A-250A-A SAFETY VALVE - CLEAN 12-B-21-30-05-00A-310A-A NEGATIVE PRESSURE RELIEF VALVE - EXAMINE 12-B-21-40-01-00A-903A-A UNDERFLOOR HEATER (MSN 1001 - 1080) - ADJUST- MENT/TEST 12-B-21-40-01-00A-903B-A UNDERFLOOR HEATER (MSN 1081 AND UP) - ADJUST-...
  • Page 142 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Data module/Technical publication Title 12-B-25-63-04-00A-903A-A UNDERWATER LOCATOR BEACON - ADJUSTMENT/TEST 12-B-25-63-04-00A-920A-A UNDERWATER LOCATOR BEACON - REMOVAL/INSTALLA- TION 12-B-27-00-00-00A-313A-A FLIGHT CONTROLS - INSPECTION/CHECK 12-B-27-00-01-00A-352A-A FLIGHT CONTROLS – CONTROL RODS - MAGNETIC PAR- TICLE INSPECTION 12-B-27-00-01-00A-353A-A FLIGHT CONTROLS –...
  • Page 143 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Data module/Technical publication Title 12-B-27-50-00-00A-903A-A FLAPS - ADJUSTMENT/TEST 12-B-27-50-03-00A-313A-A FLAP ACTUATOR - INSPECTION/CHECK 12-B-27-51-00-00A-310A-A FLAP DRIVE SYSTEM - EXAMINE 12-B-27-51-00-00A-313A-A FLAP DRIVE SYSTEM - IN SITU INSPECTION/CHECK 12-B-27-51-00-00A-353A-A FLAP DRIVE SYSTEM - IN SITU EDDY CURRENT INSPEC- TION...
  • Page 144 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Data module/Technical publication Title 12-B-30-60-00-00A-903D-A FIVE-BLADED PROPELLER DE–ICE SYSTEM (WITH PRO- PELLER DE-ICE TEST SET) - ADJUSTMENT/TEST 12-B-31-30-01-00A-903A-A RECORDERS - LDR - ADJUSTMENT/TEST 12-B-32-10-00-00A-310A-A MAIN LANDING GEAR ASSEMBLY - HYDRAULIC LANDING GEAR - ATTACHMENT BOLTS AND NUTS - EXAMINE 12-B-32-10-00-00A-310B-A MAIN LANDING GEAR ASSEMBLY - ELECTRO MECHANI-...
  • Page 145 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Data module/Technical publication Title 12-B-34-54-10-00A-903A-A SINGLE DIVERSITY AIR TRAFFIC CONTROL TRANSPOND- ER SYSTEM - ADJUSTMENT/TEST 12-B-34-54-10-00A-903B-A SINGLE NON–DIVERSITY AIR TRAFFIC CONTROL TRANS- PONDER SYSTEM - ADJUSTMENT/TEST 12-B-35-00-00-00A-903A-A OXYGEN (PLUG-IN MASK) SYSTEM - ADJUSTMENT/TEST 12-B-35-00-00-00A-903B-A...
  • Page 146 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Data module/Technical publication Title 12-B-53-20-02-00A-313A-A CENTER FUSELAGE – CARRY THROUGH FRAMES - IN- SPECTION/CHECK 12-B-53-20-02-00A-353A-A CENTER FUSELAGE FRAMES - CARRY THROUGH FRAMES - EDDY CURRENT INSPECTION 12-B-53-30-00-00A-310A-A REAR FUSELAGE - EXAMINE 12-B-53-30-01-00A-313A-A...
  • Page 147 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Data module/Technical publication Title 12-B-57-00-03-01A-353A-A WING AND FUSELAGE ATTACHMENT FITTINGS - HOLLOW BOLTS - EDDY CURRENT INSPECTION 12-B-57-20-01-00A-353A-A WING SKINS - EDDY CURRENT INSPECTION 12-B-57-20-05-00A-353A-A WING STRUCTURE - RIBS - EDDY CURRENT INSPECTION - RIB 6 STRAP 12-B-57-20-10-00A-353A-A...
  • Page 148 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Description General The Master Maintenance Plan (MMP) lists all the maintenance tasks from the Airworthiness Limitations (AL) DM, Time Limits DM and the Schedule Maintenance. The tasks have a task number and are listed in S1000D system, sub-system order.
  • Page 149 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Table 2 Master Maintenance Plan Task List Task number Item Name Task Description Interval Data Module Refer- ence 00-00/45 Aircraft Do the corrosion and AMM 12- 12-B-20-40-00-00A- corrosion protection B-20-40-00-00A-901...
  • Page 150 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Table 2 Master Maintenance Plan Task List (Continued from previous page) Task number Item Name Task Description Interval Data Module Refer- ence 06-00/592 Access panel, en- Remove and exam- 300 FH 12-B-06-20-00-00A-...
  • Page 151 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Table 2 Master Maintenance Plan Task List (Continued from previous page) Task number Item Name Task Description Interval Data Module Refer- ence 06-00/609 Access panels, fuse- Close or install 1,200 FH / 12 Months 12-B-06-20-00-00A- lage: 11AL, 11AR,...
  • Page 152 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Table 2 Master Maintenance Plan Task List (Continued from previous page) Task number Item Name Task Description Interval Data Module Refer- ence 06-00/618 Access panels, en- Remove and exam- 2,400 FH / 24 Months 12-B-06-20-00-00A- gine: 42AT, 42AB...
  • Page 153 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Table 2 Master Maintenance Plan Task List (Continued from previous page) Task number Item Name Task Description Interval Data Module Refer- ence *21-20/317 ECS emergency Attach a spring bal- 3,000 FH / 12 Months shut-off system...
  • Page 154 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Table 2 Master Maintenance Plan Task List (Continued from previous page) Task number Item Name Task Description Interval Data Module Refer- ence *21-30/469 MSN 1720-9999 - Functional test 4,800 FH / 48 Months 12-B-21-30-00-00A- Cabin pressurization...
  • Page 155 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Table 2 Master Maintenance Plan Task List (Continued from previous page) Task number Item Name Task Description Interval Data Module Refer- ence 21-50/462 Vapor cycle compres- Check for tension 600 Operating hours 12-B-21-50-01-00A-...
  • Page 156 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Table 2 Master Maintenance Plan Task List (Continued from previous page) Task number Item Name Task Description Interval Data Module Refer- ence 24-30/340 Lead acid batteries Remove and do a ca- Initially at 1000 FH or 12-B-24-30-07-00A-...
  • Page 157 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Table 2 Master Maintenance Plan Task List (Continued from previous page) Task number Item Name Task Description Interval Data Module Refer- ence 25-10/300 Crew seats Remove cushions, 1,200 FH / 12 Months The CMM document covers and shells...
  • Page 158 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Table 2 Master Maintenance Plan Task List (Continued from previous page) Task number Item Name Task Description Interval Data Module Refer- ence 25-20/302 Passenger seats Examine as far as 300 FH possible with seats...
  • Page 159 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Table 2 Master Maintenance Plan Task List (Continued from previous page) Task number Item Name Task Description Interval Data Module Refer- ence 26-20/24 Fire extinguisher Content check 12 Months (except Model...
  • Page 160 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Table 2 Master Maintenance Plan Task List (Continued from previous page) Task number Item Name Task Description Interval Data Module Refer- ence *27-10/394 Aileron control sys- Examine Threshold 12-B-27-10-00-00A-...
  • Page 161 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Table 2 Master Maintenance Plan Task List (Continued from previous page) Task number Item Name Task Description Interval Data Module Refer- ence 27-20/240 Rudder static dis- Examine 2,400 FH / 24 Months - chargers...
  • Page 162 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Table 2 Master Maintenance Plan Task List (Continued from previous page) Task number Item Name Task Description Interval Data Module Refer- ence 27-30/247 Elevator electrical Examine 1,200 FH / 12 Months - bonding straps...
  • Page 163 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Table 2 Master Maintenance Plan Task List (Continued from previous page) Task number Item Name Task Description Interval Data Module Refer- ence *27-30/449 Autopilot control ca- Life limit 20,000 FH / bles, elevator...
  • Page 164 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Table 2 Master Maintenance Plan Task List (Continued from previous page) Task number Item Name Task Description Interval Data Module Refer- ence 27-50/255 Flaps Functional test and 1,200 FH / 12 Months 12-B-27-50-00-00A- asymmetry monitor 903A-A...
  • Page 165 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Table 2 Master Maintenance Plan Task List (Continued from previous page) Task number Item Name Task Description Interval Data Module Refer- ence *27-50/390 Flap cove rib fittings Eddy current inspec- Threshold 12-B-27-51-01-00A-...
  • Page 166 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Table 2 Master Maintenance Plan Task List (Continued from previous page) Task number Item Name Task Description Interval Data Module Refer- ence 27-50/576 Flap actuators (black Lubricate 300 FH / 12 Months 12-B-27-50-00-00A-...
  • Page 167 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Table 2 Master Maintenance Plan Task List (Continued from previous page) Task number Item Name Task Description Interval Data Module Refer- ence 29-10/257 Power pack (If instal- Examine, specially 1,200 FH / 12 Months 12-B-29-00-00-00A- led)
  • Page 168 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Table 2 Master Maintenance Plan Task List (Continued from previous page) Task number Item Name Task Description Interval Data Module Refer- ence 30-10/260 Airfoil de-ice system Functional test 1,200 FH / 12 Months 12-B-30-10-00-00A- 903A-A...
  • Page 169 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Table 2 Master Maintenance Plan Task List (Continued from previous page) Task number Item Name Task Description Interval Data Module Refer- ence 32-10/263 Main landing gear Examine 1,200 FH / 12 Months - electrical bonding...
  • Page 170 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Table 2 Master Maintenance Plan Task List (Continued from previous page) Task number Item Name Task Description Interval Data Module Refer- ence 32-20/168 Nose landing gear Examine, in particular 600 FH / 12 Months leg and steering...
  • Page 171 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Table 2 Master Maintenance Plan Task List (Continued from previous page) Task number Item Name Task Description Interval Data Module Refer- ence *32-30/426 Time delay relays Functional test 2,000 FH / 12 Months 12-B-32-30-08-00A-...
  • Page 172 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Table 2 Master Maintenance Plan Task List (Continued from previous page) Task number Item Name Task Description Interval Data Module Refer- ence 32-50/404 NLG steering mecha- Examine Threshold 12-B-32-50-00-00A-...
  • Page 173 Oxygen bottle Hydrostatic test Refer to AVOX Refer to AVOX Service Information Service Information Letter SIL-35-114 Letter SIL-35-114 latest revision latest revision (www.avoxsys.com) (www.avoxsys.com) or (www.pilatus-air- or (www.pilatus-air- craft.com->Customer craft.com->Customer Support->Technical Support->Technical Publications->PC-12- Publications->PC-12- >Third-Party Docu- >Third-Party Docu- ments->Zodiac) ments->Zodiac)
  • Page 174 Moderate Corrosive 12-B-25-22-03-00A- lation mat for corro- Environment: 4000 920A-A sion. If corrosion is FH or 48 Months found, write to Pilatus Severe Corrosive En- 12-B-52-10-00-00A- for a specific repair. vironment: 2000 FH 313A-A Examine door hinge or 24 Months pin and hinges.
  • Page 175 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Table 2 Master Maintenance Plan Task List (Continued from previous page) Task number Item Name Task Description Interval Data Module Refer- ence 52-10/192 Passenger/crew door Examine and lubri- 600 FH / 12 Months hinges...
  • Page 176 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Table 2 Master Maintenance Plan Task List (Continued from previous page) Task number Item Name Task Description Interval Data Module Refer- ence 52-30/89 Cargo door Examine with trim re- Mild Corrosive Envi- 12-B-25-21-03-00A-...
  • Page 177 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Table 2 Master Maintenance Plan Task List (Continued from previous page) Task number Item Name Task Description Interval Data Module Refer- ence 52-30/408 Cargo door skin Eddy current inspec- Threshold 12-B-52-30-01-00A-...
  • Page 178 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Table 2 Master Maintenance Plan Task List (Continued from previous page) Task number Item Name Task Description Interval Data Module Refer- ence 53-00/91 Fuselage internal bot- Examine Frames 10, Mild Corrosive Envi- tom surface...
  • Page 179 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Table 2 Master Maintenance Plan Task List (Continued from previous page) Task number Item Name Task Description Interval Data Module Refer- ence 53-00/93 Structure around win- Examine Mild Corrosive Envi- dows...
  • Page 180 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Table 2 Master Maintenance Plan Task List (Continued from previous page) Task number Item Name Task Description Interval Data Module Refer- ence 53-00/277 Floor top and bottom Examine as far as 1,200 FH / 12 Months - surface and seat rails...
  • Page 181 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Table 2 Master Maintenance Plan Task List (Continued from previous page) Task number Item Name Task Description Interval Data Module Refer- ence *53-00/355 Antenna structure Examine Threshold 12-B-53-00-00-00A-...
  • Page 182 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Table 2 Master Maintenance Plan Task List (Continued from previous page) Task number Item Name Task Description Interval Data Module Refer- ence *55-00/325 Tail structure (Post Life limit 25,000 FH / SB 04-009)
  • Page 183 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Table 2 Master Maintenance Plan Task List (Continued from previous page) Task number Item Name Task Description Interval Data Module Refer- ence *55-20/362 Elevator Examine Threshold 12-B-55-20-00-00A- 32,500 FH /...
  • Page 184 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Table 2 Master Maintenance Plan Task List (Continued from previous page) Task number Item Name Task Description Interval Data Module Refer- ence *55-30/372 Vertical stabilizer Eddy current inspec- Threshold 12-B-55-30-02-00A-...
  • Page 185 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Table 2 Master Maintenance Plan Task List (Continued from previous page) Task number Item Name Task Description Interval Data Module Refer- ence 56-11/332 Cockpit side windows Inspection/check 11,000 FH / 12-B-56-11-02-00A- 120 Months...
  • Page 186 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Table 2 Master Maintenance Plan Task List (Continued from previous page) Task number Item Name Task Description Interval Data Module Refer- ence 57-00/98 Landing gear com- Examine, especially Mild Corrosive Envi- partments...
  • Page 187 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Table 2 Master Maintenance Plan Task List (Continued from previous page) Task number Item Name Task Description Interval Data Module Refer- ence *57-00/380 Wing main and rear Eddy current inspec- Threshold 12-B-57-00-03-00A-...
  • Page 188 No cracks are 22,500 wing landings. permitted. If you All wings with no find cracks, con- landing records must tact Pilatus Custom- apply a calculated er Support for ad- applicable landings vice, www.pilatus-air- equal to 2 x flying craft.com -> contact.
  • Page 189 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Table 2 Master Maintenance Plan Task List (Continued from previous page) Task number Item Name Task Description Interval Data Module Refer- ence *71-00/17 Engine mounting Life limit 11,000 FH frame, replace all...
  • Page 190 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Table 2 Master Maintenance Plan Task List (Continued from previous page) Task number Item Name Task Description Interval Data Module Refer- ence 71-00/301 Engine tubular Examine with firewall 1,200 FH / 12 Months SRM mounting frame fire-...
  • Page 191 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Table 2 Master Maintenance Plan Task List (Continued from previous page) Task number Item Name Task Description Interval Data Module Refer- ence 76-00/211 Beta slip ring carbon Make sure gap is not 300 FH / 12 Months block...
  • Page 192 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED 300 FH INSPECTION FUNCTION, DATA FOR PLANS AND DESCRIPTION Table of Contents Page 300 FH INSPECTION - FUNCTION, DATA FOR PLANS AND DESCRIPTION......General........................Inspections......................Index of Tables Page References......................

  • Page 193: 12-B-05-40-01-01A-000B-A

    PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Inspections Table 2 300 FH Inspection Task number Item Name Task Description Data Module Signature/Stamp Inspection Reference 06-00/590 Access panels, Remove and ex- 12-B-06-20-00- fuselage: 11BR , amine 00A-040A-A 21QZ...
  • Page 194 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Table 2 300 FH Inspection (Continued from previous page) Task number Item Name Task Description Data Module Signature/Stamp Inspection Reference 76-00/212 Cockpit control 12-B-76-10-00- CAUTION quadrant 00A-903A-A Do not move...
  • Page 195 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Intentionally left blank Effectivity: All 12-B-05-40-01-01A-000B-A UNCLASSIFIED 2021-12-04 Page 4...
  • Page 196 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED 300 FH OR 12 MONTHS INSPECTION FUNCTION, DATA FOR PLANS AND DESCRIPTION Table of Contents Page 300 FH OR 12 MONTHS INSPECTION - FUNCTION, DATA FOR PLANS AND DESCRIPTION...........................
  • Page 197 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Data module/Technical publication Title 12-B-46-30-06-00A-903A-A REVERSION CONTROL PANEL (3 SWITCH) - ADJUST- MENT/TEST 12-B-55-00-01-00A-664A-A VERTICAL STABILIZER SKIN CRACK - SPECIAL REPAIR PROCEDURES 12-B-55-40-00-00A-313A-A RUDDER - INSPECTION/CHECK 12-B-74-00-00-00A-903A-A IGNITION SYSTEM - ADJUSTMENT/TEST 12-B-79-30-01-00A-903A-A...
  • Page 198 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Table 2 300 FH or 12 Month Inspection (Continued from previous page) Task number Item Name Task Description Data Module Signature/Stamp Inspection Reference 10-10/428 External protec- Examine.
  • Page 199 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Table 2 300 FH or 12 Month Inspection (Continued from previous page) Task number Item Name Task Description Data Module Signature/Stamp Inspection Reference 28-20/147 Fuel tank vent Operational test 12-B-28-20-07- valve and flame...
  • Page 200 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Table 2 300 FH or 12 Month Inspection (Continued from previous page) Task number Item Name Task Description Data Module Signature/Stamp Inspection Reference 33-43/180 Navigation and Examine strobe lights 33-44/181...
  • Page 201 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Table 2 300 FH or 12 Month Inspection (Continued from previous page) Task number Item Name Task Description Data Module Signature/Stamp Inspection Reference 71-00/209 Engine drain Examine the mast and tank drain mast for...
  • Page 202 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED 600 FH INSPECTION FUNCTION, DATA FOR PLANS AND DESCRIPTION Table of Contents Page 600 FH INSPECTION - FUNCTION, DATA FOR PLANS AND DESCRIPTION......General........................Inspections......................Index of Tables Page References......................
  • Page 203 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Table 2 600 FH Inspection (Continued from previous page) Task number Item Name Task Description Data Module Signature/Stamp Inspection Reference 21-40/55 Cold air unit Add oil 12-B-21-40-02- 00A-902A-A 21-40/56...
  • Page 204 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED 600 FH OR 12 MONTHS INSPECTION FUNCTION, DATA FOR PLANS AND DESCRIPTION Table of Contents Page 600 FH OR 12 MONTHS INSPECTION - FUNCTION, DATA FOR PLANS AND DESCRIPTION...........................
  • Page 205 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Data module/Technical publication Title 12-B-52-30-00-00A-313A-A CARGO DOOR - INSPECTION/CHECK 12-B-71-00-00-00A-903G-A POWER PLANT TEST 6 – TORQUE LIMITER - ADJUST- MENT/TEST 12-B-71-00-00-00A-903H-A POWER PLANT TEST 7 – ENGINE PERFORMANCE - AD- JUSTMENT/TEST 12-B-71-00-03-00A-250A-A ELECTRICAL CONNECTORS - CLEAN...
  • Page 206 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Table 2 600 FH or 12 Month Inspection (Continued from previous page) Task number Item Name Task Description Data Module Signature/Stamp Inspection Reference 28-20/149 Firewall shutoff Operate FUEL valve EMERG SHUT-...
  • Page 207 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Table 2 600 FH or 12 Month Inspection (Continued from previous page) Task number Item Name Task Description Data Module Signature/Stamp Inspection Reference 32-20/166 Nose landing Check nitrogen 12-B-32-20-00- gear shock strut...
  • Page 208 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Table 2 600 FH or 12 Month Inspection (Continued from previous page) Task number Item Name Task Description Data Module Signature/Stamp Inspection Reference 52-10/191 Passenger/crew Make sure move- door handle lock ment is free.
  • Page 209 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Intentionally left blank Effectivity: All 12-B-05-40-01-04A-000B-A UNCLASSIFIED 2021-12-04 Page 6...
  • Page 210 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED 1200 FH OR 12 MONTHS INSPECTION FUNCTION, DATA FOR PLANS AND DESCRIPTION Table of Contents Page 1200 FH OR 12 MONTHS INSPECTION - FUNCTION, DATA FOR PLANS AND DESCRIPTION...........................
  • Page 211 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Data module/Technical publication Title 12-B-27-20-00-00A-903A-A RUDDER CONTROL SYSTEM - ADJUSTMENT/TEST 12-B-27-30-00-00A-313A-A ELEVATOR CONTROL SYSTEM - INSPECTION/CHECK 12-B-27-30-00-00A-903A-A ELEVATOR CONTROL SYSTEM - ADJUSTMENT/TEST 12-B-27-40-00-00A-903A-A HORIZONTAL STABILIZER TRIM - ADJUSTMENT/TEST 12-B-27-40-01-00A-313A-A PITCH TRIM ACTUATOR AND ATTACHMENTS - INSPEC- TION/CHECK...
  • Page 212 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Inspections Table 2 1200 FH or 12 Month Inspection Task number Item Name Task Description Data Module Signature/Stamp Inspection Reference 06-00/578 Access panels, Remove and ex- 12-B-06-20-00- wing: 51LB, amine...
  • Page 213 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Table 2 1200 FH or 12 Month Inspection (Continued from previous page) Task number Item Name Task Description Data Module Signature/Stamp Inspection Reference 06-00/609 Access panels, Close or install 12-B-06-20-00- fuselage: 11AL,...
  • Page 214 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Table 2 1200 FH or 12 Month Inspection (Continued from previous page) Task number Item Name Task Description Data Module Signature/Stamp Inspection Reference 21-40/50 Water separator Clean 12-B-21-40-03- condenser...
  • Page 215 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Table 2 1200 FH or 12 Month Inspection (Continued from previous page) Task number Item Name Task Description Data Module Signature/Stamp Inspection Reference 25-20/137 Passenger seats Examine If necessary, reference the...
  • Page 216 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Table 2 1200 FH or 12 Month Inspection (Continued from previous page) Task number Item Name Task Description Data Module Signature/Stamp Inspection Reference 27-30/249 Elevator control Inspection/check 12-B-27-30-00- system...
  • Page 217 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Table 2 1200 FH or 12 Month Inspection (Continued from previous page) Task number Item Name Task Description Data Module Signature/Stamp Inspection Reference 31-30/421 LDR (if installed) Operational test 12-B-31-30-01- 00A-903A-A...
  • Page 218 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Table 2 1200 FH or 12 Month Inspection (Continued from previous page) Task number Item Name Task Description Data Module Signature/Stamp Inspection Reference 53-00/277 Floor top and bot- Examine as far as tom surface and possible with car-...
  • Page 219 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Table 2 1200 FH or 12 Month Inspection (Continued from previous page) Task number Item Name Task Description Data Module Signature/Stamp Inspection Reference 71-00/301 Engine tubular Examine with fire- mounting frame wall insulation...
  • Page 220 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED 2400 FH OR 24 MONTHS INSPECTION FUNCTION, DATA FOR PLANS AND DESCRIPTION Table of Contents Page 2400 FH OR 24 MONTHS INSPECTION - FUNCTION, DATA FOR PLANS AND DESCRIPTION...........................
  • Page 221 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Inspections Table 2 2400 FH or 24 Month Inspection Task number Item Name Task Description Data Module Signature/Stamp Inspection Reference 06-00/614 Access panels, Open or remove. 12-B-06-20-00- fuselage: 11AL, Examine and...
  • Page 222 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Table 2 2400 FH or 24 Month Inspection (Continued from previous page) Task number Item Name Task Description Data Module Signature/Stamp Inspection Reference 21-30/314 Cabin pressuriza- Check for con- 12-B-21-30-02- tion positive pres-...
  • Page 223 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Table 2 2400 FH or 24 Month Inspection (Continued from previous page) Task number Item Name Task Description Data Module Signature/Stamp Inspection Reference 29-10/471 Nitrogen accu- Check nitrogen 12-B-29-10-02- mulator (P/N...
  • Page 224 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED UNSCHEDULED MAINTENANCE CHECKS INTRODUCTION Table of Contents Page UNSCHEDULED MAINTENANCE CHECKS - INTRODUCTION..........General........................Unscheduled Checks - Airframe................Refinement Charts....................Positive Load Factor....................Negative Load Factor..................... Unscheduled Checks - Engine................

  • Page 225: General

    PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Data module/Technical publication Title 12-B-05-50-07-00A-282A-A FUSELAGE CARRY THROUGH FRAMES - GEOMETRY IN- SPECTION 12-B-05-50-08-00A-282A-A MAXIMUM OPERATING SPEED (VMO/MMO) EXCEEDANCE - UNSCHEDULED INSPECTION 12-B-05-50-09-00A-282A-A MAXIMUM LANDING GEAR OPERATING SPEED (VLO) EX- CEEDANCE - UNSCHEDULED INSPECTION 12-B-05-50-10-00A-282A-A MAXIMUM LANDING GEAR EXTENDED SPEED (VLE) EX-...
  • Page 226 Abbreviation Unit Trigger Exceed- Maintenance Action ance range Max operating knots ≤245 None speed ≤252 12-B-05-50-08-00A-282A-A >252 Contact Pilatus¹ Max flap exten- Vfe ≤15° knots ≤170 None ded speed ≤180 12-B-05-50-03-00A-282A-A >180 Contact Pilatus¹ Max flap exten- Vfe >15° knots ≤135...

  • Page 227: Refinement Charts

    PRES- SURE Contact Pilatus Aircraft Ltd¹ - when you contact Pilatus give a detailed report of the aircraft exceedance. * - Read the allowable load factor from the refinement chart using the gross weight and fuel weight to determine the load factor ratio (R) = effective/allowable load factor.
  • Page 228 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Note The ADAHRS log files record g where 0g implies straight and level flight. Therefore you must use a correction of -1.0g for all recorded g values. Determine the allowable g using the chart, aircraft gross weight and fuel loading at the time of the exceedence.
  • Page 229 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED ALLOWABLE POSITIVE LOAD FACTOR GIVEN FUEL QUANTITY & GROSS WEIGHT 1200kg - 1222kg Fuel (total) 600kg - 1199kg Fuel (total) 400kg - 599kg Fuel (total) 0kg - 399kg Fuel (total) Notes: 1.
  • Page 230 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED ALLOWABLE NEGATIVE LOAD FACTOR GIVEN FUEL QUANTITY & GROSS WEIGHT -2.5 0kg - 1222kg Fuel (total) -2.6 -2.7 -2.8 Notes: -2.9 1. ADAHRS recorded "g" must be within this envelope. 2.

  • Page 231: Unscheduled Checks - Engine

    PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Unscheduled Checks - Engine Checks must be done after the following incidents occur, refer to P&WC EMM. Table 3 gives the inspections needed for engine exceedances: −...

  • Page 232: Index Of Tables Page

    PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED TAIL–DOWN DAMAGE INSPECTION UNSCHEDULED INSPECTION Table of Contents Page TAIL–DOWN DAMAGE INSPECTION - UNSCHEDULED INSPECTION........Index of Tables Page References......................Required Conditions....................Support equipment....................Supplies........................Spares........................
  • Page 233 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Data module/Technical publication Title 12-B-53-30-20-00A-664A-A REAR FUSELAGE STRAKES REPAIR RM09184 - SPECIAL REPAIR PROCEDURES 12-B-55-40-01-00A-920A-A RUDDER - REMOVAL/INSTALLATION Preliminary Requirements Required Conditions Table 2 Required Conditions Action / Condition Data module/Technical publication None...
  • Page 234 Even if there is no damage, do the functional test of the rudder control system, refer to AMM 12-B-27- 20-00-00A-903A-A. During the Inspection Procedure If you find damage during this procedure, you must contact Pilatus Aircraft Ltd. Preparation Lift the aircraft on jacks, refer to AMM 12-B-07-10-00-00A-901A-A.
  • Page 235 NDT inspection (eddy current or dye penetrant) is used to detect surface cracks in metals. No cracks are allowed. If cracks are found, replace the component or contact Pilatus. For information on the NDT inspection procedure, refer to SRM 12-B-51-00-00-00A-353A-A .
  • Page 236 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED 5.12 Examine the vertical stabilizer outer surface for cracks, deformation and skin distortion. 5.13 Examine the vertical stabilizer fairing 32CT for damage. 5.14 Examine the composite lower rudder fairing 32AB for damage. 5.15 Look at the rudder mechanism below the cockpit floor and examine the rudder stops for damage.
  • Page 237 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED 12-A-055011-A-S4080-00023-A-01-1 Figure 1 Rudder Control Cables – Adjustment Effectivity: All 12-B-05-50-11-00A-282A-A UNCLASSIFIED 2021-12-04 Page 6...
  • Page 238 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED 12-B-055011-A-S4080-00028-A-01-1 Figure 2 Cable Quadrant – Removal/Installation Effectivity: All 12-B-05-50-11-00A-282A-A UNCLASSIFIED 2021-12-04 Page 7...
  • Page 239 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED 12-B-055011-A-S4080-00027-A-01-1 Figure 3 Rudder Hinge Fittings – Removal/Installation Effectivity: All 12-B-05-50-11-00A-282A-A UNCLASSIFIED 2021-12-04 Page 8...
  • Page 240 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED 12-A-055011-A-S4080-00026-A-01-1 Figure 4 Vertical Stabilizer Attachment and Spars Effectivity: All 12-B-05-50-11-00A-282A-A UNCLASSIFIED 2021-12-04 Page 9...
  • Page 241 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Requirements after job completion Required Conditions Table 6 Required Conditions Action / Condition Data module/Technical publication None Effectivity: All 12-B-05-50-11-00A-282A-A End of data module UNCLASSIFIED 2021-12-04 Page 10...
  • Page 242 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED PARKING - AIRCRAFT WITH FOUR-BLADED PROPELLER MAINTENANCE PRACTICES Table of Contents Page PARKING - AIRCRAFT WITH FOUR-BLADED PROPELLER - MAINTENANCE PRACTICES Index of Tables Page References......................
  • Page 243 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Support equipment Table 3 Support equipment Name Identifications/References Reference Remark Wheel chocks Part T10-010 Wheel chock set Part T10-015 Alternative to T10-010 Sun screens (Optional) Part T10-005 Supplies Table 4 Supplies...
  • Page 244 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Name Identifications/References Reference Remark to P/N 510.10.12.046 Propeller restraint assembly Part 510.10.12.026 Cover assembly, propeller CSN 10-10-00-01-050 Also used as an alternative to P/N 510.10.12.026 Cover, protective, AOA sensor Part 110.88.07.001 Cover assembly, AOA sensor LH CSN 10-10-00-01-015...
  • Page 245 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Procedure General The aircraft can be temporarily parked in a hangar or outside in low wind speeds. If the aircraft is outside and the wind speeds are high, moor the aircraft, refer to AMM 12-B-10-20-00-00A-901A-A. If the aircraft is not to be used for a long time, do the storage of the aircraft, refer to AMM 12-B-10-10- 01-00A-901A-A.
  • Page 246 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED For aircraft with the superseded cover set, install them as follows: − Cover assembly, engine air-intake Figure 2 [1] − Cover assembly, air intakes (oil cooler, ECS and generator intakes) Figure 2 [7] −...
  • Page 247 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED IF INSTALLED 12-A-101000-A-S4080-00033-A-02-1 Figure 1 Parking (Original Cover Set) - Maintenance Practices Effectivity: All 12-B-10-10-00-00A-901A-A UNCLASSIFIED 2021-12-04 Page 6...
  • Page 248 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED INSIDE CABIN LOOKING OUTBOARD 12-A-101000-A-S4080-00034-A-02-1 Figure 1 Parking (Original Cover Set) - Maintenance Practices Effectivity: All 12-B-10-10-00-00A-901A-A UNCLASSIFIED 2021-12-04 Page 7...
  • Page 249 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED INSIDE CABIN LOOKING OUTBOARD 12-A-101000-A-S4080-30013-A-02-1 Figure 2 Parking (Alternative Cover Set) - Maintenance Practices Effectivity: All 12-B-10-10-00-00A-901A-A UNCLASSIFIED 2021-12-04 Page 8...
  • Page 250 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Requirements after job completion Required Conditions Table 6 Required Conditions Action / Condition Data module/Technical publication None Effectivity: All 12-B-10-10-00-00A-901A-A End of data module UNCLASSIFIED 2021-12-04 Page 9...
  • Page 251 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Intentionally left blank Effectivity: All 12-B-10-10-00-00A-901A-A UNCLASSIFIED 2021-12-04 Page 10...
  • Page 252 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED PARKING - AIRCRAFT WITH FIVE-BLADED PROPELLER MAINTENANCE PRACTICES Table of Contents Page PARKING - AIRCRAFT WITH FIVE-BLADED PROPELLER - MAINTENANCE PRACTICES... Index of Tables Page References......................
  • Page 253 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Support equipment Table 3 Support equipment Name Identifications/References Reference Remark Cockpit sun screen (optional) Part T10-005 Wheel chock set Part T10-015 Supplies Table 4 Supplies Name Identifications/References Reference...
  • Page 254 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Procedure General The aircraft can be temporarily parked in a hangar or outside in low wind speeds. If the aircraft is outside and the wind speeds are high, moor the aircraft, refer to AMM 12-B-10-20-00-00A-901A-A. If the aircraft is not to be used for a long time, do the storage of the aircraft, refer to AMM 12-B-10-10- 01-00A-901A-A.
  • Page 255 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED INSIDE CABIN LOOKING OUTBOARD 12-B-101000-A-S4080-79305-A-02-1 Figure 1 Parking - Aircraft With Five-Bladed Propeller - Maintenance Practices Effectivity: All 12-B-10-10-00-00A-901B-A UNCLASSIFIED 2021-12-04 Page 4...
  • Page 256 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Requirements after job completion Required Conditions Table 6 Required Conditions Action / Condition Data module/Technical publication None Effectivity: All 12-B-10-10-00-00A-901B-A End of data module UNCLASSIFIED 2021-12-04 Page 5...
  • Page 257 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Intentionally left blank Effectivity: All 12-B-10-10-00-00A-901B-A UNCLASSIFIED 2021-12-04 Page 6...
  • Page 258 It is the maintainers responsibility to make sure that the locally purchased consumable materials are acceptable to the regulatory authority. Table 1: Processing and Cleaning Material Product Name / Alternative Pilatus Material Name Notes Product / Specification Part No. P01 - Processing and Cleaning...
  • Page 259 Table 1: Processing and Cleaning (Continued) Material Product Name / Alternative Pilatus Material Name Notes Product / Specification Part No. P01-009 Solvent Methanol (pure) 908.44.52.003 AMS 3004 O-M-232K PWC011-010 P01-010 Solvent Methyl-Ethyl-Ketone (MEK) *910.21.61.015 No longer procurable ASTM D740 MIL-M-13999...
  • Page 260 Table 1: Processing and Cleaning (Continued) Material Product Name / Alternative Pilatus Material Name Notes Product / Specification Part No. P01-026 Disinfectant Virkon S, Antec International P01-027 Cleaner Extreme SIMPLE GREEN 910.21.21.121 P01-028 Cleaner Zip-Chem X-405, 12 oz. pump 908.64.22.216 spray bottle 5 gal.
  • Page 261 Table 2: Processing Sundries Material Product Name / Alternative Pilatus Material Name Notes Product / Specification Part No. P02 - Processing Sundries P02-001 Lockwire (standard) NASM20995 919.01.11.104 (diameter 0,8 mm (0.032 in)) MS20995C32 Safe-T-Cable 919.01.11.307 This alternative locking device is valid for the PC-12 only.
  • Page 262 Table 2: Processing Sundries (Continued) Material Product Name / Alternative Pilatus Material Name Notes Product / Specification Part No. P02-012 Abrasive cloth SIA1913 Siawat FC, grade 280 904.47.22.218 See note 1 P02-013 Abrasive cloth SIA1913 Siawat FC, grade 320 904.47.22.220...
  • Page 263 Table 2: Processing Sundries (Continued) Material Product Name / Alternative Pilatus Material Name Notes Product / Specification Part No. P02-036 Polishing hood Off polish hood, micro fiber, 904.49.76.361 See note 1 white P02-037 Micro fiber cloth *904.49.76.381 No longer procurable...
  • Page 264 Table 3: Welding and Metal Material Product Name / Alternative Pilatus Material Name Notes Product / Specification Part No. P03 - Welding and Metal P03-001 Welding rod Filler rod 347, AMS 5680, 907.83.32.501 (diameter 0,8 mm (0.032 in)) Filler rod 347, AMS 5680, 907.83.32.502...
  • Page 265 Table 4: Jointing Compounds and Greases Material Product Name / Alternative Pilatus Material Name Notes Product / Specification Part No. P04 - Jointing Compound and Greases P04-001 Grease AeroShell Grease 5 *908.21.52.003 No longer procurable P04-003 and P04-031 P04-002 Grease AeroShell Grease 7 908.20.02.063...
  • Page 266 Table 4: Jointing Compounds and Greases (Continued) Material Product Name / Alternative Pilatus Material Name Notes Product / Specification Part No. P04-024 Lubricant Molyslip liquid grease *908.10.09.013 No longer procurable P04-009 P04-025 Not used P04-026 Not used P04-027 Grease Mobilgrease Special *908.21.42.110 No longer procurable...
  • Page 267 Table 4: Jointing Compounds and Greases (Continued) Material Product Name / Alternative Pilatus Material Name Notes Product / Specification Part No. P04-047 Grease Nyebar Type P, 908.10.09.006 NYEBAR-TYPE-P-0-2PCT- 60ML P04-048 Grease, fluoro- Molykote FS-3451 908.20.02.095 silicone P04-049 Lubricant BOELUBE 70307 908.15.12.062...
  • Page 268 Table 5: Polishing Material Product Name / Alternative Pilatus Material Name Notes Product / Specification Part No. P05 - Polishing P05-001 The procedure that used the P05-001 has been deleted. P05-002 Plastic / Acrylic MGH No. 17 908.64.22.203 cleaner (paste)
  • Page 269 Table 6: Inspecting Material Product Name / Alternative Pilatus Material Name Notes Product / Specification Part No. P06 - Inspecting P06-001 Penetrant Ardrox 907PB, aerosol *908.68.12.105 No longer procurable. Used for dye AMS2644 Type 2 Method A and inspections in...
  • Page 270 Table 6: Inspecting (Continued) Material Product Name / Alternative Pilatus Material Name Notes Product / Specification Part No. P06-008 Remover Ardrox 9PR50, aerosol 908.68.12.108 Used for dye inspections in AMS2644 Class 2 accordance with P06-002 ASTM E1417, MIL- STD-2132 or ASTM...
  • Page 271 Table 7: Paints, Varnishes and Thinners Material Product Name / Alternative Pilatus Material Name Notes Product / Specification Part No. P07 - Paints, Varnishes and Thinners P07-001 CCC solution Bonderite M-CR 1200S Aero 908.40.32.251 (formerly Alodine 1200S) P07-002 Primer Zinc chromate primer...
  • Page 272 Table 7: Paints, Varnishes and Thinners (Continued) Material Product Name / Alternative Pilatus Material Name Notes Product / Specification Part No. P07-015 910.09.00.904 Deleted P07-010 P07-016 Primer 37045, white (barrier primer) 910.02.05.030 Hardener S 66/22 R (hardener) 910.04.04.316 Thinner C 25/90 S (thinner) 910.09.00.101...
  • Page 273 Table 7: Paints, Varnishes and Thinners (Continued) Material Product Name / Alternative Pilatus Material Name Notes Product / Specification Part No. Paint *910.04.04.319 No longer procurable Yellow, Aerodur finish, C21/ 100 UVR (LF), RAL 1023 P07-031 Paint *910.04.04.328 No longer procurable...
  • Page 274 Table 7: Paints, Varnishes and Thinners (Continued) Material Product Name / Alternative Pilatus Material Name Notes Product / Specification Part No. Paint White, ECL-G-10 BAC 7067, 910.04.04.534 Eclipse HS PUR topcoat paint FSB 17925 Paint Red 715045, ECL-G-3701, 910.04.04.535 Eclipse HS PUR topcoat paint...
  • Page 275 Table 7: Paints, Varnishes and Thinners (Continued) Material Product Name / Alternative Pilatus Material Name Notes Product / Specification Part No. Alumigrip 4200, RAL 9005 910.04.04.570 P07-020 and P07-022 Alumigrip 4200, RAL 5017 910.04.04.564 P07-020 and P07-022 Alumigrip 4200, RAL 9003 910.04.04.565...
  • Page 276 Table 7: Paints, Varnishes and Thinners (Continued) Material Product Name / Alternative Pilatus Material Name Notes Product / Specification Part No. P07-035 Topcoat, matt-black Aerodex 000744 910.04.04.321 Use until stocks polyurethane exhausted P07-040 Paint, hardener S66/22R 910.04.04.316 Paint, thinner C25/90S 910.09.00.101...
  • Page 277 Table 7: Paints, Varnishes and Thinners (Continued) Material Product Name / Alternative Pilatus Material Name Notes Product / Specification Part No. P07-043 Basecoat Alumigrip 4250 910.04.04.339 P07-044 Paint Locking varnish, marking, *910.33.82.160 No longer procurable orange Cross check, torque marker 910.33.82.161...
  • Page 278 Table 7: Paints, Varnishes and Thinners (Continued) Material Product Name / Alternative Pilatus Material Name Notes Product / Specification Part No. P07-053 Paint Topcoat, Alumigrip 4200, RAL 910.04.04.654 2004 P07-054 Paint Topcoat, Alumigrip 4200, RAL 910.04.04.665 5010 P07-055 Paint Topcoat, Aerowave 5001, grey, 910.04.54.005...
  • Page 279 Table 7: Paints, Varnishes and Thinners (Continued) Material Product Name / Alternative Pilatus Material Name Notes Product / Specification Part No. P07-068 Paint Desothane HS CA8000, 912.00.00.059 metallic Hardener CA8000B 910.04.04.611 Thinner CA8000C 910.04.04.621 Thinner CA8000C1 910.09.04.002 Thinner CA8000C2 910.09.04.003...
  • Page 280 Table 7: Paints, Varnishes and Thinners (Continued) Material Product Name / Alternative Pilatus Material Name Notes Product / Specification Part No. P07-075 Paint Aerowave 5001, semi gloss 912.00.00.032 Curing solution Curing solution 6002 910.04.54.001 P07-076 Paint Aerowave 5001, matt 912.00.00.020...
  • Page 281 Table 8: Bonding, Adhesives, Fillers and Sealers Material Product Name / Alternative Pilatus Material Name Notes Product / Specification Part No. P08 - Bonding, Adhesives, Fillers and Sealers P08-001 Caulking putty 3M body caulking *907.13.13.092 No longer procurable P08-069 P08-002 Silicon sealant Loctite 5368 910.42.12.126...
  • Page 282 Table 8: Bonding, Adhesives, Fillers and Sealers (Continued) Material Product Name / Alternative Pilatus Material Name Notes Product / Specification Part No. P08-021 Loctite, grade 542 910.42.12.121 P08-022 Sealant Permatex, Form-a-Gasket No. 1 907.12.11.203 MIL-S-45180D P08-023 Adhesive P08-059 P08-024 Coating PR 1005-L 907.10.02.001...
  • Page 283 Table 8: Bonding, Adhesives, Fillers and Sealers (Continued) Material Product Name / Alternative Pilatus Material Name Notes Product / Specification Part No. P08-043 Loctite Grade 243, blue, 50 cm3 910.42.12.128 P08-044 Resin Epoxy, Dexter Hysol AE 9395, 910.42.72.169 2 part...
  • Page 284 Table 8: Bonding, Adhesives, Fillers and Sealers (Continued) Material Product Name / Alternative Pilatus Material Name Notes Product / Specification Part No. P08-056 Sealant, fillet acrylic 551.32.99.004 Sealant group part black number PR1829B1/2N-FAP1001 907.10.11.262 With Adhesion Promoter. PR1829B1/2N-F1001 is without Adhesion...
  • Page 285 Table 8: Bonding, Adhesives, Fillers and Sealers (Continued) Material Product Name / Alternative Pilatus Material Name Notes Product / Specification Part No. P08-070 Sealant, interfay 551.32.99.005 Sealant group part electrically-conductive number PR-1764 MB2 907.10.11.274 P08-046 P08-071 Sealant, fillet MC-238 B-2 907.10.11.233...
  • Page 286 Table 8: Bonding, Adhesives, Fillers and Sealers (Continued) Material Product Name / Alternative Pilatus Material Name Notes Product / Specification Part No. P08-087 Filler Putty, Aerowave Filler 2501, 910.08.55.001 base Curing solution 6009 910.08.55.002 P08-088 Spray filler 20P20-3, base + curing solution 910.08.06.020 Thinner 910.09.00.103...
  • Page 287 Table 8: Bonding, Adhesives, Fillers and Sealers (Continued) Material Product Name / Alternative Pilatus Material Name Notes Product / Specification Part No. P08-105 Sealant, overcoat 551.32.99.002 Sealant group part number MC-780 C-1/3 907.10.11.234 MC-780 C-2 907.10.11.235 P08-073 P08-094 P08-106 Sealant, interfay 551.32.99.001...
  • Page 288 Table 9: General Stores Material Product Name / Alternative Pilatus Material Name Notes Product / Specification Part No. P09 - General Stores P09-001 Tape PTFE 01.1040.1212 *917.47.71.103 No longer procurable P09-059 P09-002 French chalk Talcum powder 908.44.12.203 P09-003 Fabric strip 50 mm (2.0 in) wide...
  • Page 289 Table 9: General Stores (Continued) Material Product Name / Alternative Pilatus Material Name Notes Product / Specification Part No. P09-020 Glass fiber tape 3M-361, FAR25.853(a), 19 mm 917.40.80.004 (0.75 in) wide P09-021 - P09-045 P09-022 Thread 917.54.16.203 P09-023 Lead seal 5,5 x 3,5 mm (0.22 x 0.14 in)
  • Page 290 Table 9: General Stores (Continued) Material Product Name / Alternative Pilatus Material Name Notes Product / Specification Part No. P09-043 Tape PPI 1022, blue 917.40.20.703 P09-044 Sleeve, heat shrink 9,53 mm (0.375 in) diameter 917.99.88.607 P09-045 Sleeve, heat shrink 6,35 mm (0.25 in) diameter 917.99.88.606...
  • Page 291 Table 9: General Stores (Continued) Material Product Name / Alternative Pilatus Material Name Notes Product / Specification Part No. P09-067 Tape Silicone (red), 19 mm (0.75 in) 917.40.60.310 wide P09-068 Tape, adhesive, 32 mm (1.26 in) wide 917.40.68.003 polyurethane P09-069 Tape, silicone Black, length 15 m x width 19 917.40.60.313...
  • Page 292 Table 9: General Stores (Continued) Material Product Name / Alternative Pilatus Material Name Notes Product / Specification Part No. P09-088 Tape, anti-chafe GORE tape, PTFE, 12,5 mm 917.73.17.063 (0.492 in) wide x 0,5 mm thick, GSC-21-99603-027 P09-089 Tape, anti-chafe GORE tape, PTFE, 25,4mm 917.73.17.064...
  • Page 293 Table 10: Oils and Fluids Material Product Name / Alternative Pilatus Material Name Notes Product / Specification Part No. P10 - Oils and Fluids P10-001 CPC Lear Chemical ACF-50 908.18.12.087 Lear Chemical ACF-50, aerosol 908.18.12.088 MIL-C-81309E type III P10-002 -...
  • Page 294 Table 10: Oils and Fluids (Continued) Material Product Name / Alternative Pilatus Material Name Notes Product / Specification Part No. P10-018 Ardrox / Dinitrol AV 15 908.18.12.090 Ardrox / Dinitrol AV 15, aerosol 908.18.12.093 MIL-PRF-16173, class 1, grade 1 & 4...
  • Page 295 Table 11: Fuels Material Product Name / Alternative Pilatus Material Name Notes Product / Specification Part No. P11 - Fuels P11-001 Fuel For PC-12 aircraft: For approved fuels, refer to AFM Section 2, Limitations. P11-001 Fuel For PC-12 NG aircraft:...
  • Page 296 Table 12: Packing Material Product Name / Alternative Pilatus Material Name Notes Product / Specification Part No. P12 - Packing There are no Pilatus Recommended Materials in this section. EFFECTIVITY: All Page 39 20-31-00 Oct 04/21...
  • Page 297 INTENTIONALLY BLANK EFFECTIVITY: All Page 40 20-31-00 Oct 04/21...
  • Page 298 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED PITCH ACTUATOR REMOVAL/INSTALLATION Table of Contents Page PITCH ACTUATOR - REMOVAL/INSTALLATION..............Index of Tables Page References......................Required Conditions....................Support equipment....................Supplies........................Spares........................Required Conditions....................Index of Figures Page Pitch Actuator - Removal/Installation..............
  • Page 299 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Support equipment Table 3 Support equipment Name Identifications/References Reference Remark Safety clip (circuit breaker hold Part T12-030 open) Supplies Table 4 Supplies Name Identifications/References Reference Remark Lockwire Part P02-007...
  • Page 300 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Put the pitch actuator Figure 1 [4] in position on the mount Figure 1 [5] and install the two washers Figure 1 [3] and bolts Figure 1 [2]. Torque the two bolts Figure 1 [2] to 4,5 to 5,6 Nm (40 to 50 lbf in).
  • Page 301 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED FRAME 39 FRAME 38 12-B-221002-A-S4080-01080-A-02-1 Figure 1 Pitch Actuator - Removal/Installation Effectivity: All 12-B-22-10-02-00A-920A-A UNCLASSIFIED 2021-12-04 Page 4...
  • Page 302 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED 12-B-221002-A-S4080-03782-A-01-1 Figure 1 Pitch Actuator - Removal/Installation Effectivity: All 12-B-22-10-02-00A-920A-A UNCLASSIFIED 2021-12-04 Page 5...
  • Page 303 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Requirements after job completion Required Conditions Table 6 Required Conditions Action / Condition Data module/Technical publication None Effectivity: All 12-B-22-10-02-00A-920A-A End of data module UNCLASSIFIED 2021-12-04 Page 6...
  • Page 304 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED ROLL ACTUATOR REMOVAL/INSTALLATION Table of Contents Page ROLL ACTUATOR - REMOVAL/INSTALLATION................ Index of Tables Page References......................Required Conditions....................Support equipment....................Supplies........................Spares........................Required Conditions....................Index of Figures Page Roll Actuator –...
  • Page 305 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Support equipment Table 3 Support equipment Name Identifications/References Reference Remark Safety clip (circuit breaker hold Part T12-030 open) Supplies Table 4 Supplies Name Identifications/References Reference Remark Lockwire Part P02-007...
  • Page 306 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Installation Make sure that the damping gasket is installed and is not damaged. If required, use the manufacturer's instructions to replace the damping gasket. Put the roll actuator Figure 1 [5] in position on the mount Figure 1 [3] and install the two washers Figure 1 [2] and bolts Figure 1 [1].
  • Page 307 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED FRAME 24 FRAME 23 12-B-221003-A-S4080-01081-A-02-1 Figure 1 Roll Actuator – Removal/Installation Effectivity: All 12-B-22-10-03-00A-920A-A UNCLASSIFIED 2021-12-04 Page 4...
  • Page 308 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED FRAME 23 12-B-221002-A-S4080-03782-A-01-1 Figure 1 Roll Actuator – Removal/Installation Effectivity: All 12-B-22-10-03-00A-920A-A UNCLASSIFIED 2021-12-04 Page 5...
  • Page 309 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Requirements after job completion Required Conditions Table 6 Required Conditions Action / Condition Data module/Technical publication None Effectivity: All 12-B-22-10-03-00A-920A-A End of data module UNCLASSIFIED 2021-12-04 Page 6...
  • Page 310 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED YAW ACTUATOR REMOVAL/INSTALLATION Table of Contents Page YAW ACTUATOR - REMOVAL/INSTALLATION................. Index of Tables Page References......................Required Conditions....................Support equipment....................Supplies........................Spares........................Required Conditions....................Index of Figures Page Yaw Actuator –...
  • Page 311 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Support equipment Table 3 Support equipment Name Identifications/References Reference Remark Safety clip (circuit breaker hold Part T12-030 open) Supplies Table 4 Supplies Name Identifications/References Reference Remark Lockwire Part P02-007...
  • Page 312 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Put the yaw actuator Figure 1 [2] in position on the mount Figure 1 [5] and install the two washers Figure 1 [3] and bolts Figure 1 [4]. Torque the bolts Figure 1 [4] to 4,5 to 5,6 Nm (40 to 50 lbf in).
  • Page 313 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED FRAME 39 FRAME 38 12-B-221004-A-S4080-01082-A-02-1 Figure 1 Yaw Actuator – Removal/Installation Effectivity: All 12-B-22-10-04-00A-920A-A UNCLASSIFIED 2021-12-04 Page 4...
  • Page 314 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED FRAME 38 12-B-221002-A-S4080-03782-A-01-1 Figure 1 Yaw Actuator – Removal/Installation Effectivity: All 12-B-22-10-04-00A-920A-A UNCLASSIFIED 2021-12-04 Page 5...
  • Page 315 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Requirements after job completion Required Conditions Table 6 Required Conditions Action / Condition Data module/Technical publication None Effectivity: All 12-B-22-10-04-00A-920A-A End of data module UNCLASSIFIED 2021-12-04 Page 6...
  • Page 316 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED SPEED AND ATTITUDE CORRECTION DESCRIPTION AND OPERATION Table of Contents Page SPEED AND ATTITUDE CORRECTION - DESCRIPTION AND OPERATION......General........................Component Description..................Stick Pusher Computer................... Stick Pusher Channels...................

  • Page 317: General

    PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Data module/Technical publication Title 12-B-23-50-00-00A-040A-A AUDIO INTEGRATING SYSTEM (KMA-29) - DESCRIPTION AND OPERATION 12-B-23-50-00-00A-040B-A AUDIO INTEGRATING SYSTEM (KMA-29A) - DESCRIPTION 12-B-23-50-10-00A-040A-A DUAL AUDIO INTEGRATING SYSTEM (KMA-29) - DESCRIP- TION AND OPERATION 12-B-23-50-10-00A-040B-A DUAL AUDIO INTEGRATING SYSTEM (KMA-29A) - DE-...

  • Page 318: Component Description

    PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED − A Power Control Lever (PCL) switch − A PUSHER test switch. The system gets signals from: − The flaps system, refer to AMM 12-B-27-50-00-00A-040A-A −...

  • Page 319: Stick Pusher Servo/Capstan

    PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED AOA data is used by the Fast/Slow (F/S) pointer (Primus APEX Build 7 or lower) or by the Dynamic Speed Bug (DSB) (Primus APEX Build 8 and higher) on the left of the Primary Flight Display (PFD). The data is also used to show the Low Speed Awareness Indication adjacent to the Air Speed tape on the PFD.

  • Page 320: Aoa Transmitter

    PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED The PUSHER INTR switch installed on the co-pilot’s control wheel stops the operation of the stick pusher servo. The electrical clutch remains engaged and makes movement of the control column heavy. AOA Transmitter The left and right AOA transmitters detect the angle of the aircraft pitch attitude in relation to the airflow and give aircraft pitch-angle signals to the stick pusher computer.

  • Page 321: Stick Shaker

    PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED When the PCL is set to IDLE a signal is given to the stick pusher computer to disable monitoring of the engine torque and engine running signals. This prevents the amber PUSHER message on the CAS display from coming on during a descent.

  • Page 322: Cas Captions

    PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED grounding circuit to the two channels of the stick pusher computer. This puts the system into ice mode operation. The AOA datums change by 8 degrees. CAS Captions 3.6.1 PUSHER...

  • Page 323: In-Flight Test

    PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED − Aircraft on ground − Engine torque more than 5 psi − PCL not set to IDLE − Flaps set to 15 degrees. When the PUSHER switch is pressed and held in, the system goes through this sequence: −...
  • Page 324 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED ENGINE POWER PCL IDLE ENGINE FLAP WEIGHT ON WEIGHT ON RUNNING WHEEL LH POSITION SWITCH WHEEL RH 60 PSI ESS BUS STALL WARN 1 LH STICK PUSHER RH STICK PUSHER COMPUTER COMPUTER...
  • Page 325 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Intentionally left blank Effectivity: All 12-B-22-20-00-00A-040A-A UNCLASSIFIED 2021-12-04 Page 10...
  • Page 326 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED RIGHT POWER JUNCTION BOX - HYDRAULIC LANDING GEAR ADJUSTMENT/TEST Table of Contents Page RIGHT POWER JUNCTION BOX - HYDRAULIC LANDING GEAR - ADJUSTMENT/TEST..Index of Tables Page References......................
  • Page 327 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Name Identifications/References Reference Remark Safety clip - Circuit breaker hold Part T12-030 open Supplies Table 4 Supplies Name Identifications/References Reference Remark None Spares Table 5 Spares Name Identifications/References Reference...
  • Page 328 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED − FOOT WARMER (NON ESSENTIAL BUS) (if installed). Open the access panels: − 21QZ − 43AL − 43AR − 11DZ. Disconnect wire P46A000 from Generator 2. Isolate the terminal lug and make sure that it does not touch the structure or other metal components.
  • Page 329 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED − U/FLOOR HTR (RHPJB). Use a Multimeter (Pt.No. Local supply) to measure the voltage between RHPJB terminal T7 and ground. The voltage reading is 28 VDC ±1 VDC. Make sure that the CAS caution message Main Bus is ON.
  • Page 330 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Remove the safety clip and close this circuit breaker: − GEN 2 (RHPJB). Make sure that: − the CAS Generator 2 Bus caution message is off −...
  • Page 331 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED − F/WARMER (RHPJB). 54.5 Measure the current in wire H92A8 (from RHPJB connector A122P1A pin 1). Make sure the current reading is 35A ±10A. 54.6 On the right crossbar panel set the FOOT WARMER switch to OFF.
  • Page 332 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED − RH FUEL PUMP (ESSENTIAL BUS). 72.2 Remove all the equipment, tools and materials from the work area. Make sure that the work area is clean.
  • Page 333 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Intentionally left blank Effectivity: All 12-B-24-52-20-00A-903A-A UNCLASSIFIED 2021-12-04 Page 8...
  • Page 334 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED FUEL MAINTENANCE PRACTICES Table of Contents Page FUEL - MAINTENANCE PRACTICES..................Index of Tables Page References......................Required Conditions....................Support equipment....................Supplies........................Spares........................Required Conditions....................References Table 1 References Data module/Technical publication Title...
  • Page 335 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Supplies Table 4 Supplies Name Identifications/References Reference Remark Grease Part P04-030 Spares Table 5 Spares Name Identifications/References Reference Remark None Safety Conditions None Procedure General General Safety Precautions Fuel and air mixtures are explosive.
  • Page 336 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Obey these safety precautions when work is done on fuel systems: 1.2.1 Use only clean clothing, tools and equipment. 1.2.2 Install clean blanking plugs on all openings. 1.2.3 Remove unwanted jointing compound and sealant while they are wet.
  • Page 337 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Requirements after job completion Required Conditions Table 6 Required Conditions Action / Condition Data module/Technical publication None Effectivity: All 12-B-28-00-00-00A-901A-A End of data module UNCLASSIFIED 2021-12-04 Page 4...
  • Page 338 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED DRAIN VALVE MAINTENANCE PRACTICES Table of Contents Page DRAIN VALVE - MAINTENANCE PRACTICES................Index of Tables Page References......................Required Conditions....................Support equipment....................Supplies........................Spares........................Required Conditions....................Index of Figures Page Fuel Drain Valve - Maintenance Practices..............
  • Page 339 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Supplies Table 4 Supplies Name Identifications/References Reference Remark O ring CSN 28-20-00-08-240 CSN 28-20-00-10-165 Spares Table 5 Spares Name Identifications/References Reference Remark None Safety Conditions WARNING BE CAREFUL WHEN YOU DO MAINTENANCE ON THE FUEL SYSTEM.
  • Page 340 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED For drain valves which do not have a replaceable O ring while the valve is installed, refer to AMM 12- B-28-10-02-00A-920A-A. Replace the O Ring Seal Refer to Fig.
  • Page 341 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED MAIN SPAR LEFT WING SHOWN, RIGHT WING SIMILAR VALVE IN OPEN POSITION VALVE IN CLOSED POSITION 12-A-281002-A-S4080-02123-A-01-1 Figure 1 Fuel Drain Valve - Maintenance Practices Effectivity: All 12-B-28-10-02-00A-901A-A UNCLASSIFIED...
  • Page 342 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Requirements after job completion Required Conditions Table 6 Required Conditions Action / Condition Data module/Technical publication None Effectivity: All 12-B-28-10-02-00A-901A-A End of data module UNCLASSIFIED 2021-12-04 Page 5...
  • Page 343 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Intentionally left blank Effectivity: All 12-B-28-10-02-00A-901A-A UNCLASSIFIED 2021-12-04 Page 6...
  • Page 344 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED DRAIN VALVE REMOVAL/INSTALLATION Table of Contents Page DRAIN VALVE - REMOVAL/INSTALLATION................Index of Tables Page References......................Required Conditions....................Support equipment....................Supplies........................Spares........................Required Conditions....................Index of Figures Page Drain Valve –...
  • Page 345 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Support equipment Table 3 Support equipment Name Identifications/References Reference Remark Defuel container Part Local supply Fuel drain tool Part T12-020 Supplies Table 4 Supplies Name Identifications/References Reference Remark...
  • Page 346 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Procedure General This data module gives the procedures for the LH and RH wing fuel tank drain valves. Two different types of drain valve can be installed: −...
  • Page 347 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED MAIN SPAR LEFT WING SHOWN, RIGHT WING SIMILAR 12-A-281002-A-S4080-01015-A-01-1 Figure 1 Drain Valve – Removal/Installation Effectivity: All 12-B-28-10-02-00A-920A-A UNCLASSIFIED 2021-12-04 Page 4...
  • Page 348 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Requirements after job completion Required Conditions Table 6 Required Conditions Action / Condition Data module/Technical publication None Effectivity: All 12-B-28-10-02-00A-920A-A End of data module UNCLASSIFIED 2021-12-04 Page 5...
  • Page 349 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Intentionally left blank Effectivity: All 12-B-28-10-02-00A-920A-A UNCLASSIFIED 2021-12-04 Page 6...
  • Page 350 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED AIRFOIL DE-ICE SYSTEM (TIMER WITHOUT INHIBIT FUNCTION) ADJUSTMENT/TEST Table of Contents Page AIRFOIL DE-ICE SYSTEM (TIMER WITHOUT INHIBIT FUNCTION) - ADJUSTMENT/TEST.. Index of Tables Page References......................
  • Page 351 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Support equipment Table 3 Support equipment Name Identifications/References Reference Remark Safety clip (circuit breaker hold Part T12-030 open) Ground air supply Part Local supply filtered, pres- sure 3,8 bar (55 psi) Air supply hose...
  • Page 352 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED − A leak test of the de-ice boots − A functional test of the de-ice system. It is recommended during the winter months to apply a layer of surface coating Icex (BF Goodrich) to the de-ice boots every 50 flight hours.
  • Page 353 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED 2.3.3 Install the access panels 12AR and 12ER. 2.3.4 Do the functional test of the de-ice system (Ref. Step 3). Functional Test Of The De-ice System Preparation 3.1.1 Open and install a Safety clip (circuit breaker hold open) (Pt.No.
  • Page 354 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED 3.2.8 Make sure that: 3.2.8.1 The BOOTS advisory caption on the lower MFD ICE PROTECTION window is ON. 3.2.8.2 The horizontal stabilizer de-ice boots pressurize for 8 seconds ±1 second then fully de-pressurize. 3.2.8.3 The lower part of the inboard de-ice boots on the wings pressurize for 8 seconds ±1 second then fully de-pressurize.
  • Page 355 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED 3.2.28 De-energize the aircraft electrical system, refer to AMM 12-B-24-00-00-00A-901A-A. 3.2.29 Disconnect the ground air supply hose Figure 1 [2] from the flexible hose Figure 1 [3]. 3.2.30 Connect the flexible hose Figure 1 [3] to the engine bleed-air pipe Figure 1 [1].
  • Page 356 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED 12-A-301000-A-S4080-00487-A-03-1 Figure 1 Airfoil De-ice System - Adjustment/Test Effectivity: All 12-B-30-10-00-00A-903A-A UNCLASSIFIED 2021-12-04 Page 7...
  • Page 357 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED TO HORIZONTAL STABILIZER TO WING OUTBOARD TOP LEFT/RIGHT TO WING OUTBOARD BOTTOM LEFT/RIGHT TO WING INBOARD BOTTOM LEFT/RIGHT TO WING INBOARD TOP LEFT/RIGHT 12-A-301000-A-S4080-00488-A-03-1 Figure 2 Leak Test Of The De-ice Boots Effectivity: All 12-B-30-10-00-00A-903A-A UNCLASSIFIED...
  • Page 358 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Requirements after job completion Required Conditions Table 6 Required Conditions Action / Condition Data module/Technical publication None Effectivity: All 12-B-30-10-00-00A-903A-A End of data module UNCLASSIFIED 2021-12-04 Page 9...
  • Page 359 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Intentionally left blank Effectivity: All 12-B-30-10-00-00A-903A-A UNCLASSIFIED 2021-12-04 Page 10...
  • Page 360 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED AIR INTAKE DE–ICE SYSTEM ADJUSTMENT/TEST Table of Contents Page AIR INTAKE DE–ICE SYSTEM - ADJUSTMENT/TEST............. Index of Tables Page References......................Required Conditions....................Support equipment....................Supplies........................Spares........................
  • Page 361 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Spares Table 5 Spares Name Identifications/References Reference Remark None Safety Conditions None Procedure General This data module gives the procedure to do an operational test of the inertial separator system. Procedure Energize the aircraft electrical system, refer to AMM 12-B-24-00-00-00A-901A-A.
  • Page 362 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED − The green INERT SEP caption is ON − The CAS INERTIAL SEPARATOR caution message is OFF. 2.17 On the left inner cross bar panel, set the ICE PROTECTION - INERT SEP switch to CLOSED. 2.18 Wait for the bypass door to fully close.
  • Page 363 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Intentionally left blank Effectivity: All 12-B-30-20-00-00A-903A-A UNCLASSIFIED 2021-12-04 Page 4...
  • Page 364 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED WINDSHIELD DE-ICE SYSTEM MAINTENANCE PRACTICES Table of Contents Page WINDSHIELD DE-ICE SYSTEM - MAINTENANCE PRACTICES..........Index of Tables Page References......................Required Conditions....................Support equipment....................Supplies........................Spares........................
  • Page 365 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Supplies Table 4 Supplies Name Identifications/References Reference Remark None Spares Table 5 Spares Name Identifications/References Reference Remark Splice Part 971.31.32.636 Safety Conditions None Procedure General This data module gives the procedure to check the operation of the windshield de-ice temperature sensor.
  • Page 366 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED 2.6.1 Cut the wire 1H77A22 at the splice SP 121 and the wire 1H78A22 at the splice SP 123. 2.6.2 Remove the caps from the ends of the wires from the spare sensor. 2.6.3 Connect the wires 1H77A22 and 1H78A22 to the spare sensor wires with the new Splice , SP 121 and SP 123.
  • Page 367 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Intentionally left blank Effectivity: All 12-B-30-40-00-00A-901A-A UNCLASSIFIED 2021-12-04 Page 4...
  • Page 368 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED FOUR-BLADED PROPELLER DE–ICE SYSTEM (WITH PROPELLER DE-ICE TEST SET) ADJUSTMENT/TEST Table of Contents Page FOUR-BLADED PROPELLER DE–ICE SYSTEM (WITH PROPELLER DE-ICE TEST SET) - ADJUSTMENT/TEST........................Index of Tables Page References......................
  • Page 369 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Name Identifications/References Reference Remark Stop watch Part Local supply Decade resistance box Part Local supply OAT simulator Part T30-005 Maintenance box Part T45-005 Jumper wire Part Local supply Propeller de-ice test set Part T30-010...
  • Page 370 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED − If these parts have been removed/installed: ● Propeller ● Brush block module ● Metal Oxide Varistor (MOV) module ● Outside Air Temperature (OAT) sensor ●...
  • Page 371 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED 2.2.5 Release the AIR/GND switch. 2.2.6 Set the ICE PROTECTION PROPELLER switch to OFF. 2.2.7 Remove jumper D from the propeller de-ice test set. 2.2.8 Set the ICE PROTECTION PROPELLER switch to ON.
  • Page 372 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED 2.2.27 Remove all the equipment, tools and materials from the work area. Make sure that the work area is clean. 2.2.28 Close the engine cowling 43AR. Functional Test Of The Propeller De-icing System Preparation 3.1.1...
  • Page 373 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Note The propeller heating is automatically disconnected when the aircraft is on the ground and the engine is not running. 3.2.4 Set the Maintenance box AIR/GND switch to AIR. 3.2.5 On the lower MFD make sure that: −...
  • Page 374 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED − The ICE PROTECTION window PROPELLER green caption is OFF. 3.2.21 Set the ICE PROTECTION - PROPELLER switch to OFF. 3.2.22 Disconnect the right decade resistance box or the OAT simulator from sockets G and H on the propeller de-ice test set.
  • Page 375 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED 3.2.43 Set the ICE PROTECTION - PROPELLER switch to OFF. 3.2.44 Wait 2 minutes. 3.2.45 Set the ICE PROTECTION - PROPELLER switch to ON. 3.2.46 On the lower MFD make sure that: −...
  • Page 376 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED FIVE-BLADED PROPELLER DE–ICE SYSTEM (WITH PROPELLER DE-ICE TEST SET) ADJUSTMENT/TEST Table of Contents Page FIVE-BLADED PROPELLER DE–ICE SYSTEM (WITH PROPELLER DE-ICE TEST SET) - ADJUSTMENT/TEST........................Index of Tables Page References......................
  • Page 377 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Support equipment Table 3 Support equipment Name Identifications/References Reference Remark Safety clip - Circuit breaker hold Part T12-030 open Stop watch Part Local supply OAT simulator Part T30-005 Decade resistance box Part Local supply...
  • Page 378 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Procedure General This data module gives the procedure to do an operational test of the propeller de-ice system. The operational test is necessary: − If required for scheduled maintenance −...
  • Page 379 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED 2.1.13 Set each decade resistance box to 91.7 Ohms (equivalent to -21 °C) or each OAT simulator to -21 °C. 2.1.14 Open the access panel 12QZ. 2.1.15 Connect the Maintenance box (Pt.No.
  • Page 380 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Make sure that all jumpers are installed on the propeller de-ice test set. Disconnect the propeller de-ice test set from the propeller de-ice timer and the aircraft wiring. Connect the plug A030P1 from the propeller de-ice timer A030 to the aircraft wiring.
  • Page 381 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Intentionally left blank Effectivity: All 12-B-30-60-00-00A-903D-A UNCLASSIFIED 2021-12-04 Page 6...
  • Page 382 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED RECORDERS - LDR DESCRIPTION AND OPERATION Table of Contents Page RECORDERS - LDR - DESCRIPTION AND OPERATION............General........................Description......................Operation........................ Audio Acquisition....................CSMU Data Recording................... ARINC 717 Flight Data...................
  • Page 383 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED The LDR simultaneously records: − One channel of audio from the pilots Audio Control Panel (ACP). The latest 120 minutes of recorded audio is retained. This data is stored in a crash-protected flash memory partition segregated from the flight data. −...

  • Page 384: Audio Acquisition

    PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Operation The steps that follow, describe the operation of the LDR: Audio Acquisition The audio signals received from the CAM and the pilots ACP are processed by a combination of hardware and software resident in the LDR.

  • Page 385: Cmos Battery

    PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED CMOS Battery This battery provides power for the system CMOS, which retains the system power-up and custom settings. However, should the LDR begin to show signs that the system clock resets on power-up or that the custom settings are lost, then it is possible that the battery may need replacement.
  • Page 386 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED LDR UNIT AUDIO PILOTS AUDIO INTERFACE CIRCUITS ARINC 717 FLIGHT DATA INFORMATION CSMU PROCESSING MODULE CVFDR TEST LED COPILOT AUXILIARY PANEL ERASE SWITCH POWER 28V DC SUPPLY SUPPLY LAPTOP 12-B-313001-A-S4080-00005-A-03-1...
  • Page 387 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED FRAME 37 FRAME 37 CVFDR/LDR POWER CIRCUIT BREAKER LDR UNIT FRAME 12 AV CONNECTORS DB50 CONNECTOR RJ-45 CONNECTOR FRAME 12 12-B-313001-A-S4080-00006-A-03-1 Figure 2 LDR - Equipment Location Effectivity: All 12-B-31-30-01-00A-040A-A UNCLASSIFIED...
  • Page 388 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED CVFDR TEST SELECT CV ERASE CVFDR TEST 12-B-313001-A-S4080-00016-A-01-1 Figure 3 CV ERASE/CVFDR TEST Switch and CVFDR LED Effectivity: All 12-B-31-30-01-00A-040A-A End of data module UNCLASSIFIED 2021-12-04 Page 7...
  • Page 389 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Intentionally left blank Effectivity: All 12-B-31-30-01-00A-040A-A UNCLASSIFIED 2021-12-04 Page 8...

  • Page 390: Table Of Contents

    PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED RECORDERS - LDR REMOVAL/INSTALLATION Table of Contents Page RECORDERS - LDR - REMOVAL/INSTALLATION..............Index of Tables Page References......................Required Conditions....................Support equipment....................Supplies........................Spares........................Required Conditions....................Index of Figures Page LDR - Removal/Installation..................
  • Page 391 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Support equipment Table 3 Support equipment Name Identifications/References Reference Remark ESD wrist strap Part Local supply Safety clip (circuit breaker hold Part T12-030 open) Supplies Table 4 Supplies Name Identifications/References...
  • Page 392 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Remove the bolt Figure 1 [9] and washer Figure 1 [8]. Remove the LDR Figure 1 [4] from the aircraft. Installation Make sure that the ESD wrist strap (Pt.No. Local supply) is securely connected to a good ground point on the LDR.
  • Page 393 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED FRAME 37 FRAME 37 12-B-313001-A-S4080-00010-A-02-1 Figure 1 LDR - Removal/Installation Effectivity: All 12-B-31-30-01-00A-920A-A UNCLASSIFIED 2021-12-04 Page 4...
  • Page 394 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Requirements after job completion Required Conditions Table 6 Required Conditions Action / Condition Data module/Technical publication None Effectivity: All 12-B-31-30-01-00A-920A-A End of data module UNCLASSIFIED 2021-12-04 Page 5...
  • Page 395 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Intentionally left blank Effectivity: All 12-B-31-30-01-00A-920A-A UNCLASSIFIED 2021-12-04 Page 6...
  • Page 396 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED RECORDERS - AREA MICROPHONE REMOVAL/INSTALLATION Table of Contents Page RECORDERS - AREA MICROPHONE - REMOVAL/INSTALLATION........Index of Tables Page References......................Required Conditions....................Support equipment....................Supplies........................Spares........................
  • Page 397 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Preliminary Requirements Required Conditions Table 2 Required Conditions Action / Condition Data module/Technical publication None Support equipment Table 3 Support equipment Name Identifications/References Reference Remark Safety clip (circuit breaker hold Part T12-030 open)
  • Page 398 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Remove and retain the right bulkhead, refer to AMM 12-B-25-10-03-00A-920A-A. Remove and retain the copilots seat, refer to AMM 12-B-25-10-01-00A-920A-A. In the cockpit, identify the Cockpit Area Microphone (CAM) Figure 1 [1] located on the trim panel 21MZ Figure 1 [3] at Frame 12, forward of the copilots cup holder Figure 1 [2].
  • Page 399 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED FRAME 12 FRAME 12 12-B-313002-A-S4080-00018-A-02-1 Figure 1 CAM Location Effectivity: All 12-B-31-30-02-00A-920A-A UNCLASSIFIED 2021-12-04 Page 4...
  • Page 400 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED FRAME 12 FRAME 12 12-B-313002-A-S4080-00015-A-02-1 Figure 2 CAM - Removal/Installation Effectivity: All 12-B-31-30-02-00A-920A-A UNCLASSIFIED 2021-12-04 Page 5...
  • Page 401 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Requirements after job completion Required Conditions Table 6 Required Conditions Action / Condition Data module/Technical publication None Effectivity: All 12-B-31-30-02-00A-920A-A End of data module UNCLASSIFIED 2021-12-04 Page 6...
  • Page 402 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED MODULAR AVIONICS UNIT MODULES REMOVAL/INSTALLATION Table of Contents Page MODULAR AVIONICS UNIT MODULES - REMOVAL/INSTALLATION........Index of Tables Page References......................Required Conditions....................Support equipment....................Supplies........................Spares........................
  • Page 403 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Support equipment Table 3 Support equipment Name Identifications/References Reference Remark None Supplies Table 4 Supplies Name Identifications/References Reference Remark None Spares Table 5 Spares Name Identifications/References Reference Remark...
  • Page 404 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Refer to AMM 12-B-00-00-00-00A-106A-A for the software part numbers and hardware compatability. Electrical Power The MAU Figure 1 [1] interfaces with most of the aircraft systems. It is necessary to remove all electrical power from the aircraft before you remove or install the MAU Figure 1 [1] or its module Figure 1 [2].
  • Page 405 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED − Put the module Figure 1 [2] in approved ESD-protective packing. Use ESDS procedures to remove the module Figure 1 [2] from the aircraft. Installation Make sure that all electrical power is removed from the aircraft: 3.1.1 De-energize the aircraft electrical system, refer to AMM 12-B-24-00-00-00A-901A-A.
  • Page 406 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED 3.5.2 Do the Operational Test of the MAU, refer to AMM 12-B-31-41-00-00A-903A-A. Do the MAU Installation procedure, refer to AMM 12-B-31-41-00-00A-920A-A . Effectivity: All 12-B-31-42-00-00A-920A-A UNCLASSIFIED 2021-12-04 Page 5...
  • Page 407 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED FR 21 FR 20 FR 19 FR 18 REFERENCE ARROW 12-B-314200-A-S4080-00001-A-01-1 Figure 1 MAU Module Removal/Installation – Example Effectivity: All 12-B-31-42-00-00A-920A-A UNCLASSIFIED 2021-12-04 Page 6...
  • Page 408 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Requirements after job completion Required Conditions Table 6 Required Conditions Action / Condition Data module/Technical publication None Effectivity: All 12-B-31-42-00-00A-920A-A End of data module UNCLASSIFIED 2021-12-04 Page 7...
  • Page 409 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Intentionally left blank Effectivity: All 12-B-31-42-00-00A-920A-A UNCLASSIFIED 2021-12-04 Page 8...
  • Page 410 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED MAIN LANDING GEAR AND DOORS – ELECTRO MECHANICAL LANDING GEAR ADJUSTMENT/TEST Table of Contents Page MAIN LANDING GEAR AND DOORS – ELECTRO MECHANICAL LANDING GEAR - ADJUSTMENT/TEST........................
  • Page 411 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Support equipment Table 3 Support equipment Name Identifications/References Reference Remark Safety clip (circuit breaker hold Part T12-030 open) Smooth file Part Local supply Supplies Table 4 Supplies Name Identifications/References Reference...
  • Page 412 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED − Adjust the left and right weight-on-wheels proximity switches. Rigging Of The MLG Doors Preparation 2.1.1 Lift the aircraft clear of the ground on jacks, refer to AMM 12-B-07-10-00-00A-901A-A. 2.1.2 Open and install a Safety clip (circuit breaker hold open) (Pt.No.
  • Page 413 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED 2.2.9.5 Remove the safety clip and close this circuit breaker: − LDG GEAR PWR (RH POWER JUNCTION BOX). 2.2.9.6 Retract the landing gear. 2.2.10 Do Step 2.2.8 and Step 2.2.9 until the MLG door Figure 1 [1] correctly aligns with the wing surface. 2.2.11 Remove the safety clip and close this circuit breaker: −...
  • Page 414 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED 3.2.7 Turn the proximity switch Figure 1 [13] clockwise or counter-clockwise until there is a gap of 0,5 mm (0.02 in) between the face of the proximity switch Figure 1 [13] and the MLG door Figure 1 [1]. 3.2.8 Tighten the two locknuts Figure 1 [12].
  • Page 415 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED 4.2.8 WARNING IF THE EMERGENCY GEAR EXTENSION HANDLE IS OPERATED, AN ABNORMAL LANDING GEAR SYSTEM CONFIGURATION CAN OCCUR . BEFORE YOU APPLY ELECTRICAL POWER TO THE AIRCRAFT, ALWAYS MAKE SURE THAT THE GEAR SELECTOR HANDLE AND GEAR POSITION AGREE.
  • Page 416 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED 0.1 mm (0.004 in) 0.5 mm (0.02 in) 2 mm (0.079 in) 12-C-321000-A-S4080-04120-A-01-1 Figure 1 Electro Mechanical Landing Gear - Adjustment/Test Effectivity: All 12-B-32-10-00-00A-903B-A UNCLASSIFIED 2021-12-04 Page 7...
  • Page 417 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Requirements after job completion Required Conditions Table 6 Required Conditions Action / Condition Data module/Technical publication None Effectivity: All 12-B-32-10-00-00A-903B-A End of data module UNCLASSIFIED 2021-12-04 Page 8...
  • Page 418 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED MAIN LANDING GEAR LEG – ELECTRO MECHANICAL LANDING GEAR REMOVAL/INSTALLATION Table of Contents Page MAIN LANDING GEAR LEG – ELECTRO MECHANICAL LANDING GEAR - REMOVAL/ INSTALLATION...........................
  • Page 419 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Data module/Technical publication Title 12-B-32-30-00-00A-903B-A EXTENSION AND RETRACTION – ELECTRO MECHANICAL LANDING GEAR - ADJUSTMENT/TEST 12-B-32-30-01-00A-920B-A MAIN LANDING GEAR ACTUATOR - ELECTRO MECHANI- CAL LANDING GEAR - REMOVAL/INSTALLATION 12-B-32-30-10-00A-903A-A EMERGENCY GEAR EXTENSION SYSTEM –...
  • Page 420 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Spares Table 5 Spares Name Identifications/References Reference Remark Spacer CSN 32-10-01-01E-085 Safety Conditions WARNING BEFORE YOU APPLY ELECTRICAL POWER TO THE AIRCRAFT, ALWAYS MAKE SURE THAT THE LANDING GEAR SELECTOR HANDLE AND THE LANDING GEAR POSITION AGREE.
  • Page 421 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Open and install a Safety clip (Circuit breaker hold open) (Pt.No. T12-030) on these circuit breakers: − FLAP (LEFT POWER JUNCTION BOX) − LDG GEAR PWR (RH POWER JUNCTION BOX). Remove the access panel 51 KB (61 KB).
  • Page 422 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED 1.20 Remove the nut Figure 3 [26] and the washer Figure 3 [25] from the bolt Figure 3 [23]. 1.21 Remove the bolt Figure 3 [23] and washer Figure 3 [24] and disconnect the bonding lead Figure 3 [20] from the MLG leg Figure 3 [16].
  • Page 423 2.2.4 Make sure that the bush Figure 3 [35] is installed in the front spar and that the hole in the bush aligns with the pin Figure 3 [36]. If the bush is not installed contact Pilatus Aircraft Ltd. 2.2.5 Move the MLG leg Figure 3 [16] forward until the bush Figure 3 [35] is fully engaged on the pin Figure 3 [36].
  • Page 424 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED − The washer Figure 3 [29]. Note Make sure the pins of the bush Figure 3 [35] align with the special washer Figure 3 [30] and the washer Figure 3 [29] .
  • Page 425 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED 2.2.32 Set the torque wrench to 2300 lb in. (260 Nm) plus the run-down torque measured in Step 2.2.30. Torque tighten the nut Figure 3 [18] as necessary within the torque limit to align with the next cotter pin hole.
  • Page 426 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED 3.15 Lower the aircraft to the ground and remove the jacks, refer to AMM 12-B-07-10-00-00A-901A-A. Effectivity: All 12-B-32-10-01-00A-920B-A UNCLASSIFIED 2021-12-04 Page 9...
  • Page 427 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED 12-B-326001-A-S4080-01066-A-01-1 Figure 1 Main Landing Gear Door Effectivity: All 12-B-32-10-01-00A-920B-A UNCLASSIFIED 2021-12-04 Page 10...
  • Page 428 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED LEFT SHOWN RIGHT SIMILAR 12-B-321001-A-S4080-01074-A-02-1 Figure 2 Main Landing Gear Leg - Removal/Installation (typical view) Effectivity: All 12-B-32-10-01-00A-920B-A UNCLASSIFIED 2021-12-04 Page 11...
  • Page 429 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED SECTION SECTION 12-B-321001-A-S4080-01075-A-02-1 Figure 3 Main Landing Gear Leg – Removal/Installation Effectivity: All 12-B-32-10-01-00A-920B-A UNCLASSIFIED 2021-12-04 Page 12...
  • Page 430 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Requirements after job completion Required Conditions Table 6 Required Conditions Action / Condition Data module/Technical publication None Effectivity: All 12-B-32-10-01-00A-920B-A End of data module UNCLASSIFIED 2021-12-04 Page 13...
  • Page 431 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Intentionally left blank Effectivity: All 12-B-32-10-01-00A-920B-A UNCLASSIFIED 2021-12-04 Page 14...
  • Page 432 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED MAIN LANDING GEAR DOOR – ELECTRO MECHANICAL LANDING GEAR REMOVAL/INSTALLATION Table of Contents Page MAIN LANDING GEAR DOOR – ELECTRO MECHANICAL LANDING GEAR - REMOVAL/ INSTALLATION...........................
  • Page 433 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Support equipment Table 3 Support equipment Name Identifications/References Reference Remark Safety clip (circuit breaker hold Part T12-030 As re- open) quired Supplies Table 4 Supplies Name Identifications/References Reference...
  • Page 434 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Installation Note Apply Grease (Pt.No. P04-028) to the bolts before you install them. If you removed the bushes, clean the bushes Figure 1 [2], Figure 1 [7], Figure 1 [15] and Figure 1 [20]. Install the bushes Figure 1 [7] and Figure 1 [15] in the fittings.
  • Page 435 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Figure 1 Main Landing Gear Door – Removal/Installation Effectivity: All 12-B-32-10-02-00A-920B-A UNCLASSIFIED 2021-12-04 Page 4...
  • Page 436 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Requirements after job completion Required Conditions Table 6 Required Conditions Action / Condition Data module/Technical publication None Effectivity: All 12-B-32-10-02-00A-920B-A End of data module UNCLASSIFIED 2021-12-04 Page 5...
  • Page 437 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Intentionally left blank Effectivity: All 12-B-32-10-02-00A-920B-A UNCLASSIFIED 2021-12-04 Page 6...
  • Page 438 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED MAIN WHEEL REMOVAL/INSTALLATION Table of Contents Page MAIN WHEEL - REMOVAL/INSTALLATION................Index of Tables Page References......................Required Conditions....................Support equipment....................Supplies........................Spares........................Required Conditions....................Index of Figures Page Main Wheel - Removal/Installation.................
  • Page 439 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Preliminary Requirements Required Conditions Table 2 Required Conditions Action / Condition Data module/Technical publication None Support equipment Table 3 Support equipment Name Identifications/References Reference Remark Safety clip (circuit breaker hold Part T12-030 open)
  • Page 440 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Note To identify the consumables used in this procedure refer to the Consumable Materials List, AMM 12-B-20-31-00- 00A-070A-A . Note To identify the AGE and tools used in this procedure refer to the List of AGE and Tools, TEM 12-B-00-00-00-00A- 060A-A .
  • Page 441 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED 2.12 Examine the bearings Figure 1 [15] and bearing cup Figure 1 [7] for corrosion and damage. Replace the bearings and bearing cup if necessary. 2.13 Remove all remaining grease from axle Figure 1 [16] with the White spirit (Pt.No.
  • Page 442 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED 3.12.3 For Parker wheels - apply Anti-seize compound (Pt.No. P04-010) to the threads of the screws Figure 1 [4]. 3.12.4 Install the wheel cover Figure 1 [3] onto the wheel Figure 1 [2] with the five screws Figure 1 [4], washers Figure 1 [5] and grommets Figure 1 [6] if previously removed.
  • Page 443 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED RIB 5 12-B-324001-A-S4080-00003-A-04-1 Figure 1 Main Wheel - Removal/Installation Effectivity: All 12-B-32-40-01-00A-920A-A UNCLASSIFIED 2021-12-04 Page 6...
  • Page 444 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Requirements after job completion Required Conditions Table 6 Required Conditions Action / Condition Data module/Technical publication None Effectivity: All 12-B-32-40-01-00A-920A-A End of data module UNCLASSIFIED 2021-12-04 Page 7...
  • Page 445 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Intentionally left blank Effectivity: All 12-B-32-40-01-00A-920A-A UNCLASSIFIED 2021-12-04 Page 8...
  • Page 446 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED BRAKE ASSEMBLY (MSN 1001 – 1230) REMOVAL/INSTALLATION Table of Contents Page BRAKE ASSEMBLY (MSN 1001 – 1230) - REMOVAL/INSTALLATION........Index of Tables Page References......................Required Conditions....................Support equipment....................
  • Page 447 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Preliminary Requirements Required Conditions Table 2 Required Conditions Action / Condition Data module/Technical publication None Support equipment Table 3 Support equipment Name Identifications/References Reference Remark Safety clip (circuit breaker hold Part T12-030 open)
  • Page 448 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Note To identify the consumables used in this procedure refer to the Consumable Materials List, AMM 12-B-20-31-00- 00A-070A-A . Note To identify the AGE and tools used in this procedure refer to the List of AGE and Tools, TEM 12-B-00-00-00-00A- 060A-A .
  • Page 449 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Apply Anti seize compound (Pt.No. P04-010) to the threads and bearing surfaces of the bolts Figure 1 [5] and nuts Figure 1 [1]. Note Use only inconel bolts with coated nuts. Note Each brake unit must have either all inconel bolts and coated nuts, or all current bolts and current nuts.
  • Page 450 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED − HYD CTL (ESSENTIAL BUS). Lower the aircraft to the ground and remove the jacks, refer to AMM 12-B-07-10-00-00A-901A-A. Effectivity: All 12-B-32-40-03-00A-920A-A UNCLASSIFIED 2021-12-04 Page 5...
  • Page 451 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED 12-A-324003-A-S4080-03589-A-01-1 Figure 1 Brake Assembly - Removal/Installation Effectivity: All 12-B-32-40-03-00A-920A-A UNCLASSIFIED 2021-12-04 Page 6...
  • Page 452 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Requirements after job completion Required Conditions Table 6 Required Conditions Action / Condition Data module/Technical publication None Effectivity: All 12-B-32-40-03-00A-920A-A End of data module UNCLASSIFIED 2021-12-04 Page 7...
  • Page 453 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Intentionally left blank Effectivity: All 12-B-32-40-03-00A-920A-A UNCLASSIFIED 2021-12-04 Page 8...
  • Page 454 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED RED FLASHING BEACONS REMOVAL/INSTALLATION Table of Contents Page RED FLASHING BEACONS - REMOVAL/INSTALLATION............Index of Tables Page References......................Required Conditions....................Support equipment....................Supplies........................Spares........................Required Conditions....................Index of Figures Page Top Red Flashing Beacon –...
  • Page 455 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Support equipment Table 3 Support equipment Name Identifications/References Reference Remark Safety clip (circuit breaker hold Part T12-030 open) Supplies Table 4 Supplies Name Identifications/References Reference Remark Cable tie Part P09-008...
  • Page 456 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Note The NAV LIGHTS circuit breaker is opened to prevent operation of the white navigation light on the tail, close to the upper red beacon. Remove the top or bottom filament: 2.2.1 Loosen the screw Figure 1 [2] or Figure 2 [7] and remove the lens Figure 1 [1] or Figure 2 [8].
  • Page 457 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED 3.2.3 Install the red flashing light Figure 1 [4] and gasket Figure 1 [5] on the access panel Figure 1 [6] with the five screws Figure 1 [9]. 3.2.4 Hold the access panel Figure 1 [6] in position and connect the electrical connectors A410J Figure 1 [8].
  • Page 458 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Figure 1 Top Red Flashing Beacon – Removal/Installation Effectivity: All 12-B-33-46-00-00A-920A-A UNCLASSIFIED 2021-12-04 Page 5...
  • Page 459 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED DRAIN HOLE Figure 2 Bottom Red Flashing Beacon – Removal/Installation Effectivity: All 12-B-33-46-00-00A-920A-A UNCLASSIFIED 2021-12-04 Page 6...
  • Page 460 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Requirements after job completion Required Conditions Table 6 Required Conditions Action / Condition Data module/Technical publication None Effectivity: All 12-B-33-46-00-00A-920A-A End of data module UNCLASSIFIED 2021-12-04 Page 7...
  • Page 461 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Intentionally left blank Effectivity: All 12-B-33-46-00-00A-920A-A UNCLASSIFIED 2021-12-04 Page 8...
  • Page 462 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED ALTITUDE AND VERTICAL SPEED INDICATION ADJUSTMENT/TEST Table of Contents Page ALTITUDE AND VERTICAL SPEED INDICATION - ADJUSTMENT/TEST....... Index of Tables Page References......................Required Conditions....................Support equipment....................Supplies........................
  • Page 463 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Name Identifications/References Reference Remark Static blank Part T34-020 Supplies Table 4 Supplies Name Identifications/References Reference Remark None Spares Table 5 Spares Name Identifications/References Reference Remark None Safety Conditions Note...
  • Page 464 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Baro Setting (InHg) Display Altitude (ft.) Display altitude (m) 30.98 976 ± 25 297 ± 7 29.92 11 ± 25 3 ± 7 28.86 -989 ± 25 -301 ±...
  • Page 465 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Reference altitude (m) PFD Altitude display (m) Thales ESIS altitude L3 ESIS altitude display display (m) 613 ± 9 613 ± 8 613 ± 9 1524 1528 ±...
  • Page 466 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED ALTITUDE AND VERTICAL SPEED INDICATION (RVSM) ADJUSTMENT/TEST Table of Contents Page ALTITUDE AND VERTICAL SPEED INDICATION (RVSM) - ADJUSTMENT/TEST....Index of Tables Page References......................Required Conditions....................Support equipment....................
  • Page 467 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Name Identifications/References Reference Remark Static blank Part T34-020 Supplies Table 4 Supplies Name Identifications/References Reference Remark None Spares Table 5 Spares Name Identifications/References Reference Remark None Safety Conditions Note...
  • Page 468 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Use the BARO controls on the PFD Controllers and the ESIS to set the BARO settings in the following table. Make sure that the PFD and ESIS altitude displays are within the limits. Baro Setting (InHg) Display Altitude (ft) Display altitude (m)
  • Page 469 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Reference altitude (m) PFD Altitude display (m) Thales ESIS altitude dis- L3 ESIS altitude display play (m) 461 ± 8 461 ± 8 461 ± 8 613 ±...
  • Page 470 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED 25.3 Remove the safety clip and close the circuit breakers: − XPNDR 1 (AVIONIC 1 BUS) − XPNDR 2 (AVIONIC 2 BUS). 25.4 Remove all the equipment, tools and materials from the work area. Make sure that the work area is clean.
  • Page 471 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Intentionally left blank Effectivity: All 12-B-34-14-00-00A-903B-A UNCLASSIFIED 2021-12-04 Page 6...
  • Page 472 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED AIRSPEED INDICATION ADJUSTMENT/TEST Table of Contents Page AIRSPEED INDICATION - ADJUSTMENT/TEST............... Index of Tables Page References......................Required Conditions....................Support equipment....................Supplies........................Spares........................Required Conditions....................References Table 1 References Data module/Technical publication Title...
  • Page 473 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Name Identifications/References Reference Remark Static adaptor kit Part T34-015 Static blank Part T34-020 Supplies Table 4 Supplies Name Identifications/References Reference Remark None Spares Table 5 Spares Name Identifications/References Reference...
  • Page 474 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED − Thales ESIS press the STD button to set 1013 hPa/29.92 InHg − L3 ESI-1000 ESIS press the S button to set 1013 hPa/29.92 InHg −...
  • Page 475 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Reference airspeed Airspeed indication CAS (kts) TAS (kts) Mach Display IAS (kts) TAS (kts) Mach PFD ADI 151 ±2 PFD HSI 151 ±8 PFD HSI Thales ESIS 151 ±2.5 L3 ESIS...
  • Page 476 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED AIR DATA, ATTITUDE AND HEADING REFERENCE SYSTEM KSG 7200 ADJUSTMENT/TEST Table of Contents Page AIR DATA, ATTITUDE AND HEADING REFERENCE SYSTEM KSG 7200 - ADJUSTMENT/ TEST............................
  • Page 477 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Preliminary Requirements Required Conditions Table 2 Required Conditions Action / Condition Data module/Technical publication None Support equipment Table 3 Support equipment Name Identifications/References Reference Remark Maintenance box Part T45-005 Sub-D cable...
  • Page 478 CAS message do the ACMF Download/Clear Logs, refer to AMM 12-B-45-45-00-00A-551A-A . Note A design change not authorised by Pilatus (for example an STC) requires a full functional test of the ADS-B system as per AMM 34-54 ATC TRANSPONDER ADS-B OUT, if that option is installed.
  • Page 479 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED 2.17 Make sure that the Certification File name agrees with the list given in AMM 12-B-00-00-00-00A-106A- 2.18 Set the appropriate COMM Port setting and click on the START button. An upload status bar will be shown.
  • Page 480 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Functional Check of the ADAHRS Note Do this procedure when an ADAHRS unit is replaced. Do a test of the altitude and vertical speed indication: −...
  • Page 481 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED ROM Boot CRC32 Test Passed ROM Application CRC32 Test Passed ROM On Side Channel ID Test Passed ROM Cross Side Channel ID Test Passed Timer Test Passed ARINC 429 Hi Speed Test Passed...
  • Page 482 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Note If one of the parameters is not the same as the value on the placard, enter the correct value and click on SET MAGNETOMETER PITCH/ROLL OFFSET button. With all fields completed, click on the STORE MAGNETOMETER OFFSETS button.
  • Page 483 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED ROM Cross Side Channel ID Test Passed Timer Test Passed ARINC 429 Hi Speed Test Passed ARINC 429 Lo Speed Test Passed Interprocessor Bus Not Operational Passed Configuration Module Test Passed...
  • Page 484 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Note If one of the parameters is not the same as the value on the placard, enter the correct value and click on SET MAGNETOMETER PITCH/ROLL OFFSET button. With all fields completed, click on the STORE MAGNETOMETER OFFSETS button.
  • Page 485 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED − When a change of the cargo is likely to affect the compass. Note A Landing Compass with an accuracy of ±2° is an alternative to the Compass Rose. Note When you do the ADAHRS check swing, do a check of the heading indications on the standby compass (if installed) and the ESIS.
  • Page 486 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED − HSI 1+2 is TRU TRK. 5.2.11.3 On the lower MFD Avionics Window on the PFD tab, make sure that the Heading selection is Magnetic. 5.2.12 Make sure that the HF radio system (if installed) is set to ON.
  • Page 487 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED 5.3.17 Use the compass base rose or the datum compass to put the aircraft on the magnetic heading of 000 (N) degrees. 5.3.18 Click on the AIRCRAFT INSTALLATION SETUP button. 5.3.19 On the computer Installation Setup screen, click on the COMPASS CALIBRATION button.
  • Page 488 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED − ADAHRS CH A (ESSENTIAL BUS) − ADAHRS CH B (MAIN BUS). 5.3.32 Wait for 5 seconds, then close these circuit breakers: − ADAHRS CH A (ESSENTIAL BUS) −...
  • Page 489 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Intentionally left blank Effectivity: All 12-B-34-25-00-00A-903A-A UNCLASSIFIED 2021-12-04 Page 14...
  • Page 490 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED RADAR ALTIMETER SYSTEM ADJUSTMENT/TEST Table of Contents Page RADAR ALTIMETER SYSTEM - ADJUSTMENT/TEST............. Index of Tables Page References......................Required Conditions....................Support equipment....................Supplies........................Spares........................Required Conditions....................Index of Figures Page Radar Altimeter Break-in Cable - Schematic............
  • Page 491 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Support equipment Table 3 Support equipment Name Identifications/References Reference Remark Break-in cable Part Local supply DC power supply (0 to 25 VDC) Part Local supply Insert/extract tool Part M15570-20 Maintenance box...
  • Page 492 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED − For standard interior, refer to AMM 12-B-25-22-04-00A-920A-A. Open the access panel 12HZ. Energize the aircraft electrical system, refer to AMM 12-B-24-00-00-00A-901A-A. Wait two minutes to allow the radar altimeter system to stabilize. Make sure the radar altitude is shown on the pilot Primary Flight Display (PFD) and the optional copilot PFD (if installed).
  • Page 493 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED 4.11 Energize the aircraft electrical system, refer to AMM 12-B-24-00-00-00A-901A-A. 4.12 On the pilot Audio Control Panel (ACP) push the SPKR/PA pushbutton to set the cockpit speaker to 4.13 Remove the safety clip and close this circuit breaker: −...
  • Page 494 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED − RAD ALT 1 (AVIONIC 1 BUS). 4.38 Wait for 30 seconds, then make sure that the PFD radar altitude digital display shows 0 feet. 4.39 De-energize the aircraft electrical system, refer to AMM 12-B-24-00-00-00A-901A-A.
  • Page 495 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED AIRCRAFT RAD ALT CONNECTOR CONNECTOR BLACK SHEATHED 300mm LONG ARINC A429 Tx 28Vdc I/P 28Vdc Rtn Pwr Gnd RAD ALT TEST ALT TEST ENABLE 1 CONNECTOR RECEPTICLE PIL 9717516031 ALT TEST ENABLE 2...
  • Page 496 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Requirements after job completion Required Conditions Table 6 Required Conditions Action / Condition Data module/Technical publication None Effectivity: All 12-B-34-42-00-00A-903A-A End of data module UNCLASSIFIED 2021-12-04 Page 7...
  • Page 497 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Intentionally left blank Effectivity: All 12-B-34-42-00-00A-903A-A UNCLASSIFIED 2021-12-04 Page 8...
  • Page 498 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED CENTRAL MAINTENANCE SYSTEM INTERFACE PREPARE TEST EQUIPMENT Table of Contents Page CENTRAL MAINTENANCE SYSTEM INTERFACE - PREPARE TEST EQUIPMENT....Index of Tables Page References......................Required Conditions....................Support equipment....................
  • Page 499 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Preliminary Requirements Required Conditions Table 2 Required Conditions Action / Condition Data module/Technical publication None Support equipment Table 3 Support equipment Name Identifications/References Reference Remark Laptop computer Part T45-010 Primus APEX®...
  • Page 500 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Procedure Computer Hardware and Software Standard For the minimum hardware and software standards for the laptop computer, refer to TEM 12-B-45-45- 00-00A-066A-A. Prepare the Laptop Computer Network Interface Option A: Wireless Data Loading System installed If the aircraft has the Wireless Data Loading System option installed (SB 46–004 or Factory Option), the aircraft Maintenance Panel has one RJ-45 connector marked High Speed LAN Bus.
  • Page 501 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Note If you do not see the categories as shown in Fig. 1 , make sure that the View by setting is set to Category. Figure 1 Control Panel - Network and Sharing 2.5.1.2 Click on Change adapter settings.
  • Page 502 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Figure 2 LAN Connection - Screen 2.5.1.3 Right click on the applicable LAN connection and open the Properties window. Effectivity: All 12-B-45-45-00-00A-330A-A UNCLASSIFIED 2021-12-04 Page 5...
  • Page 503 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Figure 3 LAN Properties - Screen 2.5.1.4 Select Internet Protocol Version 4 (TCP/IPv4) in the item list and click Properties. Effectivity: All 12-B-45-45-00-00A-330A-A UNCLASSIFIED 2021-12-04 Page 6...
  • Page 504 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Figure 4 LAN TCP/IPv4 Properties 2.5.1.5 Select the Alternative Configuration tab and change the IP address from Automatic private IP address to User configured and enter the following details: −...
  • Page 505 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Figure 5 IP Address and Subnet Mask 2.5.1.6 Close all windows by acknowledging with OK. 2.5.2 Set Windows XP SP2 Compatability Mode: Note If you use Windows 7 32 bit, set the CMC Remote Terminal software to a Windows XP SP2 compatability mode with the following procedure.
  • Page 506 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Figure 6 CMC RT Properties Figure 7 CMC Compatability Effectivity: All 12-B-45-45-00-00A-330A-A UNCLASSIFIED 2021-12-04 Page 9...
  • Page 507 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED 2.5.2.2 Activate Run this program in compatability mode for:, then select Windows XP SP2 from the drop- down list. Figure 8 Compatability Mode 2.5.2.3 Close all windows by acknowledging with OK. 2.5.3 Disable all Firewalls: 2.5.3.1...
  • Page 508 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Figure 9 System and Security Figure 10 Windows Firewall 2.5.3.2 Open Allow a program through Windows Firewall and press the Allow another program button. Effectivity: All 12-B-45-45-00-00A-330A-A UNCLASSIFIED 2021-12-04 Page 11...
  • Page 509 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Figure 11 Windows Firewall Setting 2.5.3.3 Add CMC Remote Terminal to the Firewall exemption list and make sure that all checkboxes are ticked. Effectivity: All 12-B-45-45-00-00A-330A-A UNCLASSIFIED 2021-12-04 Page 12...
  • Page 510 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Figure 12 Firewall Exemption 2.5.3.4 Close all windows by acknowledging with OK. 2.5.4 Disable any active anti-virus programs, active screensavers and power save options on the laptop computer.
  • Page 511 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Intentionally left blank Effectivity: All 12-B-45-45-00-00A-330A-A UNCLASSIFIED 2021-12-04 Page 14...
  • Page 512 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED CENTRAL MAINTENANCE SYSTEM INTERFACE CONNECT THE COMPUTER Table of Contents Page CENTRAL MAINTENANCE SYSTEM INTERFACE - CONNECT THE COMPUTER....Index of Tables Page References......................Required Conditions....................Support equipment....................
  • Page 513 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Support equipment Table 3 Support equipment Name Identifications/References Reference Remark Laptop computer Part T45-005 LAN Kit LANTAP-10 Part T45-020 LAN Kit LTEPIC-25 Part T45-020 Alterna- No longer avail- tive able...
  • Page 514 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Note Do not energize the aircraft electrical system at this step. Remove access panel 21QZ to get access to the aircraft Maintenance Panel aft of the copilot seat. Prepare the Laptop Computer Make sure that the laptop computer is correctly configured and the appropriate LAN Kit or Ethernet cable is used, refer to AMM 12-B-45-45-00-00A-330A-A.
  • Page 515 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED 3.3.1 Remove the 50 Ohm BNC termination resistor from the aircraft Maintenance Panel LAN Bus connector. 3.3.2 Connect one end of the BNC coaxial cable (included in the LAN kit) to the aircraft Maintenance Panel LAN Bus connector.
  • Page 516 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED 12-B-454500-A-S4080-00002-A-01-1 Figure 1 CMC Connection Failed Effectivity: All 12-B-45-45-00-00A-331A-A UNCLASSIFIED 2021-12-04 Page 5...
  • Page 517 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED If you see the screen shown in Fig. 2 , the Remote Terminal (RT) software installed on the computer does not match the CMC software version. Install the correct software on the computer, refer to AMM 12-B-00-00-00-00A-106A-A .
  • Page 518 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED 12-B-454500-A-S4080-00003-A-01-1 Figure 2 Incompatible Software Effectivity: All 12-B-45-45-00-00A-331A-A UNCLASSIFIED 2021-12-04 Page 7...
  • Page 519 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED 12-B-454500-A-S4080-00004-A-01-1 Figure 3 Cyclic Redundancy Check Effectivity: All 12-B-45-45-00-00A-331A-A UNCLASSIFIED 2021-12-04 Page 8...
  • Page 520 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED LAN Operation To make sure that the LAN is operating correctly, use the "ping" command in the Windows "cmd prompt" (black and white DOS window) to ping the IP address of the AGM1 module. 5.1.1 On the laptop computer, go to "Start"...
  • Page 521 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Intentionally left blank Effectivity: All 12-B-45-45-00-00A-331A-A UNCLASSIFIED 2021-12-04 Page 10...
  • Page 522 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED PASSENGER/CREW DOOR (MSN 1001 - 1575) ADJUSTMENT/TEST Table of Contents Page PASSENGER/CREW DOOR (MSN 1001 - 1575) - ADJUSTMENT/TEST......... Index of Tables Page References......................Required Conditions....................Support equipment....................
  • Page 523 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Support equipment Table 3 Support equipment Name Identifications/References Reference Remark Spring balance Part T23-010 Ruler Part Local supply Supplies Table 4 Supplies Name Identifications/References Reference Remark Lubricating paste Part P04-029...
  • Page 524 Examine the door frame Figure 1 [1] and the structure around the door entrance Figure 1 [3], if damage is found write to Pilatus. With the passenger/crew door Figure 1 [1] in the open position turn the inner door handle Figure 1 [4] to the closed position.
  • Page 525 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Table 6 Shoot Bolt Measurements Shoot Bolt Measurements Lower Shoot Bolt (nearest to the door Between 35,5 and 36,5 mm (1.40 and 1.44 in) hinge) Center Shoot Bolt Between 30,5 and 31,5 mm (1.20 and 1.24 in) Upper Shoot Bolt...
  • Page 526 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED 3.10.2 If the wear marks are not equal, replace the striker plates, refer to 12-B-52-10-07-00A-920A-A. 3.11 If none of the ramps Figure 1 [6] on the striker plates Figure 1 [5] show wear marks, do the procedure that follows: 3.11.1 Use a color waterproof pen to apply a layer to all the ramps Figure 1 [6] on the six striker plates...
  • Page 527 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED 4.18 Position the indicator Figure 1 [15] in the cover Figure 1 [16] and on the fork end Figure 1 [11]. Install the bolts Figure 1 [13], washers Figure 1 [14] and nuts Figure 1 [10]. 4.19 Close the door Figure 1 [1] and turn the door handle Figure 1 [2] to the closed position.
  • Page 528 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED TYPICAL STRIKER PLATE OUTBOARD SIDE STRIKER PLATE INBOARD SIDE 12-A-521000-A-S4080-00810-A-02-1 Figure 1 Passenger/Crew Door – Adjustment/Test Effectivity: All 12-B-52-10-00-00A-903A-A UNCLASSIFIED 2021-12-04 Page 7...
  • Page 529 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED = 3.4 Ø10.4 12-A-521000-A-S4080-00811-A-02-1 Figure 1 Passenger/Crew Door – Adjustment/Test Effectivity: All 12-B-52-10-00-00A-903A-A UNCLASSIFIED 2021-12-04 Page 8...
  • Page 530 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Requirements after job completion Required Conditions Table 7 Required Conditions Action / Condition Data module/Technical publication None Effectivity: All 12-B-52-10-00-00A-903A-A End of data module UNCLASSIFIED 2021-12-04 Page 9...
  • Page 531 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Intentionally left blank Effectivity: All 12-B-52-10-00-00A-903A-A UNCLASSIFIED 2021-12-04 Page 10...
  • Page 532 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED PASSENGER/CREW DOOR (MSN 1576 AND UP) ADJUSTMENT/TEST Table of Contents Page PASSENGER/CREW DOOR (MSN 1576 AND UP) - ADJUSTMENT/TEST......Index of Tables Page References......................Required Conditions....................Support equipment....................
  • Page 533 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Preliminary Requirements Required Conditions Table 2 Required Conditions Action / Condition Data module/Technical publication None Support equipment Table 3 Support equipment Name Identifications/References Reference Remark Spring balance Part T23-010 Ruler...
  • Page 534 − The loads on the shoot bolts, specially the lower, are not equal. Examine the door frame Figure 1 [1] and the structure around the door entrance Figure 1 [3] if damage is found contact Pilatus. Effectivity: All 12-B-52-10-00-00A-903B-A UNCLASSIFIED...
  • Page 535 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED With the passenger/crew door Figure 1 [1] in the open position turn the inner door handle Figure 1 [4] to the closed position. Identify the type of shoot bolt Figure 1 [7] installed, measure the distance from the center of the shoot bolt to the start of the chamfer.
  • Page 536 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Examine the outboard side of the striker plates Figure 1 [5] for signs of touch marks. If touch marks are found, it could be necessary to replace the shoot bolts (refer to Step 4) and the striker plates Figure 1 [5], refer to 12-B-52-10-07-00A-920B-A.
  • Page 537 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED 4.16 Position the indicator Figure 1 [15] in the cover Figure 1 [16] and on the fork end Figure 1 [11]. Install the bolts Figure 1 [13], washers Figure 1 [14] and nuts Figure 1 [10]. 4.17 Close the door Figure 1 [1] and push the door handle Figure 1 [2] inwards to the closed position.
  • Page 538 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED TYPICAL STRIKER PLATE OUTBOARD SIDE STRIKER PLATE INBOARD SIDE 12-B-521000-A-S4080-79155-A-03-1 Figure 1 MSN 1576 - 9999 Passenger/Crew Door - Adjustment/Test Effectivity: All 12-B-52-10-00-00A-903B-A UNCLASSIFIED 2021-12-04 Page 7...
  • Page 539 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED = 3.4 Ø10.4 12-B-521000-A-S4080-79156-A-02-1 Figure 1 MSN 1576 - 9999 Passenger/Crew Door - Adjustment/Test Effectivity: All 12-B-52-10-00-00A-903B-A UNCLASSIFIED 2021-12-04 Page 8...
  • Page 540 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Requirements after job completion Required Conditions Table 7 Required Conditions Action / Condition Data module/Technical publication None Effectivity: All 12-B-52-10-00-00A-903B-A End of data module UNCLASSIFIED 2021-12-04 Page 9...
  • Page 541 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Intentionally left blank Effectivity: All 12-B-52-10-00-00A-903B-A UNCLASSIFIED 2021-12-04 Page 10...
  • Page 542 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED PASSENGER DOOR STRIKER PLATES (MSN 1001 - 1575) REMOVAL/INSTALLATION Table of Contents Page PASSENGER DOOR STRIKER PLATES (MSN 1001 - 1575) - REMOVAL/INSTALLATION..Index of Tables Page References......................
  • Page 543 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Support equipment Table 3 Support equipment Name Identifications/References Reference Remark Depth gage Part Local supply Supplies Table 4 Supplies Name Identifications/References Reference Remark Lockwire (0,6 mm diameter) Part P02-007 Spares Table 5 Spares...
  • Page 544 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Procedure General This document gives the procedure to replace the striker plates. The new striker plates have a different contour that makes the last part of the shoot bolt motion easier. There is also a selection of three striker plates with different bolt hole positions available for each location.
  • Page 545 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Close the passenger/crew door Figure 1 [6] and turn the door handle Figure 1 [7] to the closed position. Check for play between each shoot bolts and the striker plates Figure 1 [2]. On the shoot bolts with play, the play must be measured as follows: 3.6.1 Refer to Fig.
  • Page 546 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED 12-A-521007-A-S4080-04105-A-01-1 Figure 1 Passenger Door Striker Plate - Removal/Installation Effectivity: All 12-B-52-10-07-00A-920A-A UNCLASSIFIED 2021-12-04 Page 5...
  • Page 547 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Requirements after job completion Required Conditions Table 6 Required Conditions Action / Condition Data module/Technical publication None Effectivity: All 12-B-52-10-07-00A-920A-A End of data module UNCLASSIFIED 2021-12-04 Page 6...
  • Page 548 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED PASSENGER DOOR STRIKER PLATES (MSN 1576 - 1942) REMOVAL INSTALLATION Table of Contents Page PASSENGER DOOR STRIKER PLATES (MSN 1576 - 1942) - REMOVAL INSTALLATION..Index of Tables Page References......................
  • Page 549 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Preliminary Requirements Required Conditions Table 2 Required Conditions Action / Condition Data module/Technical publication None Support equipment Table 3 Support equipment Name Identifications/References Reference Remark Depth gage Part Local supply Supplies...
  • Page 550 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Safety Conditions WARNING BE CAREFUL WHEN YOU USE THE CONSUMABLE MATERIALS. OBEY THE MANUFACTURERS' HEALTH AND SAFETY INSTRUCTIONS AND ALL THE APPLICABLE LOCAL INSTRUCTIONS. CONSUMABLE MATERIALS CAN BE DANGEROUS AND CAN CAUSE DEATH OR INJURY TO PERSONNEL AND/OR DAMAGE TO EQUIPMENT.
  • Page 551 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Put the new applicable Striker plate Figure 1 [2] and Striker plate Figure 1 [9] in the forward position of the passenger/crew door structure. If necessary use a knife to make the cut out in the door seal compressor larger.
  • Page 552 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED 12-A-521007-A-S4080-04112-A-01-1 Figure 1 Passenger Door Striker Plates - Removal/Installation Effectivity: All 12-B-52-10-07-00A-920B-A UNCLASSIFIED 2021-12-04 Page 5...
  • Page 553 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Requirements after job completion Required Conditions Table 6 Required Conditions Action / Condition Data module/Technical publication None Effectivity: All 12-B-52-10-07-00A-920B-A End of data module UNCLASSIFIED 2021-12-04 Page 6...
  • Page 554 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED HORIZONTAL STABILIZER REMOVAL/INSTALLATION Table of Contents Page HORIZONTAL STABILIZER - REMOVAL/INSTALLATION............Index of Tables Page References......................Required Conditions....................Support equipment....................Supplies........................Spares........................Required Conditions....................Index of Figures Page Horizontal Stabilizer - Removal/Installation............
  • Page 555 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Preliminary Requirements Required Conditions Table 2 Required Conditions Action / Condition Data module/Technical publication None Support equipment Table 3 Support equipment Name Identifications/References Reference Remark Safety clip (Circuit breaker hold Part T12-030 open)
  • Page 556 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED WARNING BE CAREFUL WHEN YOU USE THE CONSUMABLE MATERIALS. OBEY THE MANUFACTURERS' HEALTH AND SAFETY INSTRUCTIONS AND ALL THE APPLICABLE LOCAL INSTRUCTIONS. CONSUMABLE MATERIALS CAN BE DANGEROUS AND CAN CAUSE DEATH OR INJURY TO PERSONNEL AND/OR DAMAGE TO EQUIPMENT.
  • Page 557 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED 1.12 Remove the nuts Figure 1 [16] and Figure 1 [17] and bolts Figure 1 [19] and Figure 1 [20] and disconnect the stabilizer Figure 1 [1] from the stabilizer trim actuator Figure 1 [18]. 1.13 Remove the cotter pins Figure 1 [5], nuts Figure 1 [4], washers Figure 1 [6], bolts Figure 1 [2] and washers Figure 1 [3] from the stabilizer Figure 1 [1].
  • Page 558 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED 2.8.7 CAUTION DO NOT APPLY CORROSION PREVENTIVE TO THE BEARING AND RAM. Use CPC (Pt.No. P10-013) to protect the stabilizer trim actuator upper attachment and fasteners. Remove the sling from the stabilizer Figure 1 [1].
  • Page 559 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED 12-B-551000-A-S4080-01557-A-01-1 Figure 1 Horizontal Stabilizer - Removal/Installation Effectivity: All 12-B-55-10-01-00A-920A-A UNCLASSIFIED 2021-12-04 Page 6...
  • Page 560 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Requirements after job completion Required Conditions Table 6 Required Conditions Action / Condition Data module/Technical publication None Effectivity: All 12-B-55-10-01-00A-920A-A End of data module UNCLASSIFIED 2021-12-04 Page 7...
  • Page 561 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Intentionally left blank Effectivity: All 12-B-55-10-01-00A-920A-A UNCLASSIFIED 2021-12-04 Page 8...
  • Page 562 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED WINDSHIELD REMOVAL/INSTALLATION Table of Contents Page WINDSHIELD - REMOVAL/INSTALLATION................Index of Tables Page References......................Required Conditions....................Support equipment....................Supplies........................Spares........................Required Conditions....................Index of Figures Page Windshield - Removal/Installation................
  • Page 563 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Preliminary Requirements Required Conditions Table 2 Required Conditions Action / Condition Data module/Technical publication None Support equipment Table 3 Support equipment Name Identifications/References Reference Remark Safety clip - Circuit breaker hold Part T12-030 open...
  • Page 564 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Safety Conditions WARNING BE CAREFUL WHEN YOU USE THE CONSUMABLE MATERIALS. OBEY THE MANUFACTURERS' HEALTH AND SAFETY INSTRUCTIONS AND ALL THE APPLICABLE LOCAL INSTRUCTIONS. CONSUMABLE MATERIALS CAN BE DANGEROUS AND CAN CAUSE DEATH OR INJURY TO PERSONNEL AND/OR DAMAGE TO EQUIPMENT.
  • Page 565 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Remove the screws Figure 1 [10] from around the left or right windshield Figure 1 [5] or Figure 1 [7]. Remove sufficient screws Figure 1 [10] from around the adjacent windshield Figure 1 [5] or Figure 1 [7] to make it possible to move the doubler Figure 1 [6] away from the windshield Figure 1 [5] or Figure 1 [7] that is to be removed.
  • Page 566 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Left Windshield Right Windshield Max. Cable Length to Splice M to 1H81B10 M to 2H81B10 Maximum 300 mm J to 1H83B10 J to 2H83B10 Maximum 150 mm K to 1H87A10N K to 2H87A10N Maximum 150 mm...
  • Page 567 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED 4.14 Apply Sealant (Pt.No. P08-040) around the edges of the doubler Figure 1 [6], the windshields Figure 1 [5] and Figure 1 [7], and the side windows Figure 1 [4] and Figure 1 [1]. Close Up Remove all the equipment, tools and materials from the work area.
  • Page 568 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED SECTION Figure 1 Windshield - Removal/Installation Effectivity: All 12-B-56-11-01-00A-920A-A UNCLASSIFIED 2021-12-04 Page 7...
  • Page 569 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED SENSOR WIRE 50 mm INLINE WINDSHIELD SPLICE EXISTING SLEEVE NEW SLEEVE 917.99.88.603 OVERLAPPING SLEEVE POWER WIRE FOR CORRECT LENGTH REFER TO TABLE MAX 50 mm INLINE WINDSHIELD SPLICE...
  • Page 570 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Requirements after job completion Required Conditions Table 6 Required Conditions Action / Condition Data module/Technical publication None Effectivity: All 12-B-56-11-01-00A-920A-A End of data module UNCLASSIFIED 2021-12-04 Page 9...
  • Page 571 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Intentionally left blank Effectivity: All 12-B-56-11-01-00A-920A-A UNCLASSIFIED 2021-12-04 Page 10...
  • Page 572 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED LEFT WING - HYDRAULIC LANDING GEAR INSTALLATION Table of Contents Page LEFT WING - HYDRAULIC LANDING GEAR - INSTALLATION..........Index of Tables Page References......................Required Conditions....................Support equipment....................
  • Page 573 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Data module/Technical publication Title 12-B-27-50-00-00A-903A-A FLAPS - ADJUSTMENT/TEST 12-B-27-50-02-00A-920A-A FLAP DRIVE SHAFTS - REMOVAL/INSTALLATION 12-B-28-21-00-00A-903A-A BALANCING SYSTEM - ADJUSTMENT/TEST 12-B-29-00-00-00A-902A-A HYDRAULIC SYSTEM - SERVICING 12-B-29-10-01-00A-920A-A HYDRAULIC POWER PACK - REMOVAL/INSTALLATION 12-B-30-10-00-00A-903A-A AIRFOIL DE-ICE SYSTEM (TIMER WITHOUT INHIBIT FUNC-...
  • Page 574 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Name Identifications/References Reference Remark Cable tie Part P09-008 Grease Part P04-029 Spares Table 5 Spares Name Identifications/References Reference Remark Bolt, tension CSN 57-10-00-01-090 Bolt, tension CSN 57-10-00-01-045 CSN 57-10-00-01-100 Shim...
  • Page 575 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Installation of the Wing and Fittings Note The Corrosion preventive (Pt.No. P04-039) may be diluted with the Thinner (Pt.No. P04-039) to ease the bolt Figure 1 [5] , Figure 1 [11] and Figure 1 [18] installation in the fuselage and wing fitting holes. The maximum mixing ratio is 10 parts by weight of Corrosion preventive (Pt.No.
  • Page 576 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED preventative. Put the installation tools Figure 1 [30] and Figure 1 [31] in the ends of the long bolt Figure 1 [11]. 2.1.16 Install the forward bottom long bolt Figure 1 [11] and the torlon plates Figure 1 [13] and Figure 1 [14] through the wing and fuselage fittings Figure 1 [10].
  • Page 577 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED LEFT SHOWN RIGHT SIMILAR 12-A-570000-A-S4080-30109-A-03-1 Figure 1 Wing Installation - Attachment Fittings Effectivity: All 12-B-57-00-00-00A-720A-A UNCLASSIFIED 2021-12-04 Page 6...
  • Page 578 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED LEFT SHOWN RIGHT SIMILAR SECTION SECTION 12-B-570000-A-S4080-79011-A-02-1 Figure 1 Wing Installation - Attachment Fittings Effectivity: All 12-B-57-00-00-00A-720A-A UNCLASSIFIED 2021-12-04 Page 7...
  • Page 579 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Removal of the Sling Equipment 2.2.1 Release the lift force from the wing sling Figure 2 [1], if needed. 2.2.2 Disconnect the wing sling Figure 2 [1] from the lift straps Figure 2 [5], Figure 2 [6] and Figure 2 [7]. 2.2.3 Remove the lift straps Figure 2 [5] and Figure 2 [6] from around the forward and aft main spars.
  • Page 580 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED LEFT WING SHOWN RIGHT WING SIMILAR Figure 2 Wing Removal/Installation - Sling Attachment/Removal Effectivity: All 12-B-57-00-00-00A-720A-A UNCLASSIFIED 2021-12-04 Page 9...
  • Page 581 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Equipment Connection at the Wing Top and Rear 2.3.1 Remove the padding from the aileron rod Figure 3 [12]. Connect the aileron rod Figure 3 [12] to the bellcrank Figure 3 [13] and install the bolt Figure 3 [11], washer Figure 3 [14] and nut Figure 3 [15].
  • Page 582 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED WING NOT SHOWN FOR CLARITY 12-B-570000-A-S4080-00012-A-02-1 Figure 3 Left Wing Removal - Top and Rear Equipment Effectivity: All 12-B-57-00-00-00A-720A-A UNCLASSIFIED 2021-12-04 Page 11...
  • Page 583 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Equipment Connection at the Wing Bottom Center 2.4.1 Put the ends of the bonding straps Figure 4 [9] and the flap drive shaft support angle Figure 3 [10] in position and install the bolt Figure 4 [10] and nut Figure 4 [11].
  • Page 584 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED LEFT SHOWN RIGHT SIMILAR 12-A-570000-A-S4080-00869-A-02-1 Figure 4 Left Wing Removal/Installation - Bottom Center Equipment Effectivity: All 12-B-57-00-00-00A-720A-A UNCLASSIFIED 2021-12-04 Page 13...
  • Page 585 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Hydraulic Pipeline Connection 2.5.1 Put the service tray assembly Figure 5 [16] in position in the aircraft. 2.5.2 Install the four bolts Figure 5 [15] and washers Figure 5 [14] that attach the service tray assembly Figure 5 [16].
  • Page 586 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Figure 5 Left Wing Removal/Installation - Hydraulic Pipelines Effectivity: All 12-B-57-00-00-00A-720A-A UNCLASSIFIED 2021-12-04 Page 15...
  • Page 587 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Wiring Harness Loop Clamp Check 2.6.1 Do a check of the seven loop clamps that hold the wiring harness for the red beacon light, refer to Fig.
  • Page 588 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED DE-ICING PIPES BEACON LIGHT HYDRAULIC PIPE MAIN SPAR HYDRAULIC SYSTEM TYPICAL 12-B-570000-A-S4080-04088-A-01-1 Figure 6 Wiring Harness Loop Clamp - Check Effectivity: All 12-B-57-00-00-00A-720A-A UNCLASSIFIED 2021-12-04 Page 17...
  • Page 589 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Close Up Note If a new wing is installed, do a check of the alignment and symmetry, refer to AMM 12-B-05-50-06-00A- 282A-A . Install the Cable tie (Pt.No. P09-008) Figure 7 [3] on the hydraulic pipe Figure 7 [4] between the hydraulic power pack and the nitrogen tank.
  • Page 590 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED 3.25 Remove all the equipment, tools and materials from the work area. Make sure that the work area is clean. 3.26 Install the access panels 12AL, 12BL, 12DL, 12EL and 12FL. 3.27 Close the access panel 11AL.
  • Page 591 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED 12 BL 12 DL 12 FL 12 EL 12 AL 12 ER 12 FR Figure 7 Left Wing Removal/Installation - Preparation Effectivity: All 12-B-57-00-00-00A-720A-A UNCLASSIFIED 2021-12-04 Page 20...
  • Page 592 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED 150Kg 25° MAX. Figure 8 Wing Removal/Installation - Preparation and Close Up Effectivity: All 12-B-57-00-00-00A-720A-A UNCLASSIFIED 2021-12-04 Page 21...
  • Page 593 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Requirements after job completion Required Conditions Table 6 Required Conditions Action / Condition Data module/Technical publication None Effectivity: All 12-B-57-00-00-00A-720A-A End of data module UNCLASSIFIED 2021-12-04 Page 22...
  • Page 594 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED LEFT WING – ELECTRO MECHANICAL LANDING GEAR INSTALLATION Table of Contents Page LEFT WING – ELECTRO MECHANICAL LANDING GEAR - INSTALLATION......Index of Tables Page References......................
  • Page 595 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Data module/Technical publication Title 12-B-24-30-07-00A-920C-A HEATED NI-CAD BATTERY - REMOVAL/INSTALLATION 12-B-27-10-00-00A-903A-A AILERON CONTROL SYSTEM - ADJUSTMENT/TEST 12-B-27-50-00-00A-903A-A FLAPS - ADJUSTMENT/TEST 12-B-27-50-02-00A-920A-A FLAP DRIVE SHAFTS - REMOVAL/INSTALLATION 12-B-28-21-00-00A-903A-A BALANCING SYSTEM - ADJUSTMENT/TEST 12-B-30-10-00-00A-903A-A...
  • Page 596 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Supplies Table 4 Supplies Name Identifications/References Reference Remark Solvent Part P01-010 Corrosion preventive Part P04-039 Chromate free Thinner Part P04-039 for corrosion preventive Cable tie Part P09-008 Grease Part P04-029...
  • Page 597 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Installation CAUTION DAMAGE TO THE FUSELAGE AND WING BUSHINGS WILL OCCUR IF TOO MUCH FORCE IS ON THE WING BOLTS. ONLY USE HAND FORCE TO INSTALL THE BOLTS. IF MORE FORCE IS NECESSARY, STOP AND ADJUST THE FORCE ON THE SLING UNTIL THE BOLT CAN BE EASILY INSTALLED.
  • Page 598 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED preventative. Put the installation tools Figure 1 [30] and Figure 1 [31] in the ends of the short bolt Figure 1 [18]. 2.1.13 Install the rear bottom short bolt Figure 1 [18] and the torlon plates Figure 1 [19] through the wing and fuselage fittings Figure 1 [20].
  • Page 599 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED 2.1.24.1 If the gap is less than 0,5 mm (0.02 in) go to Step 2.1.25. 2.1.24.2 If the gap is 0,5 mm (0.02 in) or more, install a shim Figure 1 [26] between the fuselage frame 24 and the wing rear spar.
  • Page 600 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED LEFT SHOWN RIGHT SIMILAR 12-A-570000-A-S4080-30109-A-03-1 Figure 1 Wing Installation - Attachment Fittings Effectivity: All 12-B-57-00-00-00A-720B-A UNCLASSIFIED 2021-12-04 Page 7...
  • Page 601 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED LEFT SHOWN RIGHT SIMILAR SECTION SECTION 12-B-570000-A-S4080-79011-A-02-1 Figure 1 Wing Installation - Attachment Fittings Effectivity: All 12-B-57-00-00-00A-720B-A UNCLASSIFIED 2021-12-04 Page 8...
  • Page 602 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Removal of the Sling Equipment 2.2.1 Release the lift force from the wing sling Figure 2 [1], if necessary. 2.2.2 Disconnect the wing sling Figure 2 [1] from the lift straps Figure 2 [5], Figure 2 [6] and Figure 2 [7]. 2.2.3 Remove the lift straps Figure 2 [5] and Figure 2 [6] from around the forward and aft main spars.
  • Page 603 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED LEFT WING SHOWN RIGHT WING SIMILAR Figure 2 Wing Installation - Sling Attachment/Removal Effectivity: All 12-B-57-00-00-00A-720B-A UNCLASSIFIED 2021-12-04 Page 10...
  • Page 604 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Equipment Connection at the Wing Top and Rear 2.3.1 Connect the bonding cable Figure 4 [18] to the earth stud GS500 Figure 4 [17] and install the washer Figure 4 [19] and the nut Figure 4 [20].
  • Page 605 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED LEFT SHOWN RIGHT SIMILAR 12-A-570000-A-S4080-00869-A-02-1 Figure 3 Left Wing Installation - Bottom Center Equipment Effectivity: All 12-B-57-00-00-00A-720B-A UNCLASSIFIED 2021-12-04 Page 12...
  • Page 606 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED WING NOT SHOWN FOR CLARITY 12-B-570000-A-S4080-00012-A-02-1 Figure 4 Left Wing Installation - Top and Rear Equipment Effectivity: All 12-B-57-00-00-00A-720B-A UNCLASSIFIED 2021-12-04 Page 13...
  • Page 607 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Wiring Harness Loop Clamp Check 2.5.1 Do a check of the six loop clamps that hold the wiring harness for the red beacon light, refer to Fig. 5 . Make sure that: −...
  • Page 608 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED DE-ICING PIPES BEACON LIGHT MAIN SPAR TYPICAL 12-B-570000-A-S4080-04091-A-01-1 Figure 5 Wiring Harness Loop Clamp - Check Effectivity: All 12-B-57-00-00-00A-720B-A UNCLASSIFIED 2021-12-04 Page 15...
  • Page 609 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Close Up If a new wing is installed, do a check of the alignment and symmetry, refer to AMM 12-B-05-50-06- 00A-282A-A. Remove the caps and install the two forward de-ice pipes Figure 8 [1] and Figure 8 [2] between the wing and the fuselage.
  • Page 610 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED 3.22 Connect the electrical connector P148. 3.23 Install the panel 12AB with the screws. 3.24 Do the exterior lights operational test for the landing, navigation, strobe, recognition and red beacon (if installed), refer to AMM 12-B-33-40-00-00A-903A-A.
  • Page 611 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED 150Kg 25° MAX. Figure 6 Wing Installation MSN 1300, 1451 - 9999 - Close Up Effectivity: All 12-B-57-00-00-00A-720B-A UNCLASSIFIED 2021-12-04 Page 18...
  • Page 612 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED 150Kg 25° MAX. 12-B-570000-A-S4080-79090-A-01-1 Figure 7 Wing Installation MSN 1576 - 9999 - Close Up Effectivity: All 12-B-57-00-00-00A-720B-A UNCLASSIFIED 2021-12-04 Page 19...
  • Page 613 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED 12BL 11AL 11BL 12AL 12DL 12FL 12EL 12AB 12ER 12FR 12-B-570000-A-S4080-00014-A-02-1 Figure 8 Left Wing Installation - Close Up Effectivity: All 12-B-57-00-00-00A-720B-A UNCLASSIFIED 2021-12-04 Page 20...
  • Page 614 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Requirements after job completion Required Conditions Table 6 Required Conditions Action / Condition Data module/Technical publication None Effectivity: All 12-B-57-00-00-00A-720B-A End of data module UNCLASSIFIED 2021-12-04 Page 21...
  • Page 615 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Intentionally left blank Effectivity: All 12-B-57-00-00-00A-720B-A UNCLASSIFIED 2021-12-04 Page 22...
  • Page 616 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED RIGHT WING – HYDRAULIC LANDING GEAR INSTALLATION Table of Contents Page RIGHT WING – HYDRAULIC LANDING GEAR - INSTALLATION..........Index of Tables Page References......................Required Conditions....................Support equipment....................
  • Page 617 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Data module/Technical publication Title 12-B-27-50-02-00A-920A-A FLAP DRIVE SHAFTS - REMOVAL/INSTALLATION 12-B-28-21-00-00A-903A-A BALANCING SYSTEM - ADJUSTMENT/TEST 12-B-29-00-00-00A-902A-A HYDRAULIC SYSTEM - SERVICING 12-B-30-10-00-00A-903A-A AIRFOIL DE-ICE SYSTEM (TIMER WITHOUT INHIBIT FUNC- TION) - ADJUSTMENT/TEST 12-B-30-10-00-00A-903B-A AIRFOIL DE-ICE SYSTEM (TIMER WITH INHIBIT FUNC-...
  • Page 618 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Name Identifications/References Reference Remark Grease Part P04-029 Spares Table 5 Spares Name Identifications/References Reference Remark Bolt, tension CSN 57-10-00-01-090 Bolt, tension CSN 57-10-00-01-045 CSN 57-10-00-01-100 Shim Part 557.12.12.146 Safety Conditions...
  • Page 619 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Installation of the Wing and Fittings Note The Corrosion preventive (Pt.No. P04-039) may be diluted with the Thinner (Pt.No. P04-039) to ease the bolt Figure 1 [5] , Figure 1 [11] and Figure 1 [18] installation in the fuselage and wing fitting holes. The maximum mixing ratio is 10 parts by weight of Corrosion preventive (Pt.No.
  • Page 620 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED preventative. Put the installation tools Figure 1 [30] and Figure 1 [31] in the ends of the long bolt Figure 1 [11]. 2.1.15 Install the forward bottom long bolt Figure 1 [11] and the torlon plates Figure 1 [13] and Figure 1 [14] through the wing and fuselage fittings Figure 1 [10].
  • Page 621 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED LEFT SHOWN RIGHT SIMILAR 12-A-570000-A-S4080-30109-A-03-1 Figure 1 Wing Installation - Attachment Fittings Effectivity: All 12-B-57-00-00-00B-720A-A UNCLASSIFIED 2021-12-04 Page 6...
  • Page 622 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED LEFT SHOWN RIGHT SIMILAR SECTION SECTION 12-B-570000-A-S4080-79011-A-02-1 Figure 1 Wing Installation - Attachment Fittings Effectivity: All 12-B-57-00-00-00B-720A-A UNCLASSIFIED 2021-12-04 Page 7...
  • Page 623 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Removal of the Sling Equipment 2.2.1 Release the lift force from the wing sling Figure 2 [1], if needed. 2.2.2 Disconnect the wing sling Figure 2 [1] from the lift straps Figure 2 [5], Figure 2 [6] and Figure 2 [7]. 2.2.3 Remove the lift straps Figure 2 [5] and Figure 2 [6] from around the forward and aft main spar.
  • Page 624 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED LEFT WING SHOWN RIGHT WING SIMILAR Figure 2 Wing Removal/Installation - Sling Attachment/Removal Effectivity: All 12-B-57-00-00-00B-720A-A UNCLASSIFIED 2021-12-04 Page 9...
  • Page 625 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Equipment Connection at the Wing Top and Rear 2.3.1 Remove the padding from the aileron control rod Figure 3 [11]. Connect the aileron control rod Figure 3 [11] to the bellcrank Figure 3 [14] and install the bolt Figure 3 [10], washer Figure 3 [13] and nut Figure 3 [12].
  • Page 626 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED WING NOT SHOWN FOR CLARITY Figure 3 Right Wing Removal/Installation - Top and Rear Equipment Effectivity: All 12-B-57-00-00-00B-720A-A UNCLASSIFIED 2021-12-04 Page 11...
  • Page 627 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Equipment Connection at the Wing Bottom Center 2.4.1 Remove the caps and install the brake pipe Figure 4 [10] between the fuselage and wing. 2.4.2 Remove the caps and install the grommet Figure 4 [9] and the three fuel pipes Figure 4 [3], Figure 4 [4] and Figure 4 [5] between the fuselage and the connections in the landing gear compartment.
  • Page 628 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED 12-A-570000-A-S4080-00876-A-02-1 Figure 4 Right Wing Removal/Installation - Bottom Center Equipment Effectivity: All 12-B-57-00-00-00B-720A-A UNCLASSIFIED 2021-12-04 Page 13...
  • Page 629 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Rear De-ice Pipeline Connection 2.5.1 Put the outboard end of the bonding strap Figure 5 [12] and the flap drive support angle Figure 3 [4] in position and install the bolt Figure 5 [11] and nut Figure 5 [13].
  • Page 630 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Figure 5 Right Wing Removal/Installation - Rear De-ice Pipelines Effectivity: All 12-B-57-00-00-00B-720A-A UNCLASSIFIED 2021-12-04 Page 15...
  • Page 631 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Forward De-ice Pipeline Connection 2.6.1 Remove the caps. Put the forward cross connector Figure 6 [19] in position and connect the de-ice pipe Figure 6 [7] to the ejector flow control valve Figure 6 [8]. 2.6.2 Remove the caps and connect the de-ice pipe Figure 6 [15] to the pressure switch Figure 6 [12].
  • Page 632 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED 12 BR 12 AR 12 AB 12 DR 12 FR 12 ER Figure 6 Right Wing Removal/Installation - Panels and Forward De-ice Pipelines Effectivity: All 12-B-57-00-00-00B-720A-A UNCLASSIFIED 2021-12-04 Page 17...
  • Page 633 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Close-Up Note If a new wing is installed, do a check of the alignment and symmetry, refer to AMM 12-B-05-50-06-00A- 282A-A . Connect the aircraft batteries: −...
  • Page 634 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED 150Kg 25° MAX. Figure 7 Wing Removal/Installation - Preparation and Close Up Effectivity: All 12-B-57-00-00-00B-720A-A UNCLASSIFIED 2021-12-04 Page 19...
  • Page 635 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Requirements after job completion Required Conditions Table 6 Required Conditions Action / Condition Data module/Technical publication None Effectivity: All 12-B-57-00-00-00B-720A-A End of data module UNCLASSIFIED 2021-12-04 Page 20...
  • Page 636 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED RIGHT WING – ELECTRO MECHANICAL LANDING GEAR INSTALLATION Table of Contents Page RIGHT WING – ELECTRO MECHANICAL LANDING GEAR - INSTALLATION......Index of Tables Page References......................
  • Page 637 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Data module/Technical publication Title 12-B-24-30-07-00A-920C-A HEATED NI-CAD BATTERY - REMOVAL/INSTALLATION 12-B-27-10-00-00A-903A-A AILERON CONTROL SYSTEM - ADJUSTMENT/TEST 12-B-27-50-00-00A-903A-A FLAPS - ADJUSTMENT/TEST 12-B-27-50-02-00A-920A-A FLAP DRIVE SHAFTS - REMOVAL/INSTALLATION 12-B-28-21-00-00A-903A-A BALANCING SYSTEM - ADJUSTMENT/TEST 12-B-30-10-00-00A-903A-A...
  • Page 638 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Supplies Table 4 Supplies Name Identifications/References Reference Remark Solvent Part P01-010 Corrosion preventive Part P04-039 Chromate free Thinner Part P04-039 for corrosion preventive Cable tie Part P09-008 Paste Part P04-029...
  • Page 639 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Procedure General This procedure assumes that the right wing is removed as given in AMM 12-B-57-00-00-00B-520B-A. Installation of the Wing and Fittings CAUTION DAMAGE TO THE FUSELAGE AND WING BUSHINGS WILL OCCUR IF TOO MUCH FORCE IS ON THE WING BOLTS.
  • Page 640 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED 2.1.11 Use the hoist as necessary to carefully align the rear bottom bushes in the wing fittings and the fuselage fittings. 2.1.12 Apply a layer of Corrosion preventive (Pt.No. P04-039) to the outer surface of the short bolt Figure 1 [18].
  • Page 641 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED 2.1.23 If a new wing is installed, release the lift force from the sling and carefully lower the jack that supports the wing until the wing is not supported on the jack. If you install the wing that was removed, go to Step 2.1.25.
  • Page 642 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED LEFT SHOWN RIGHT SIMILAR 12-A-570000-A-S4080-30109-A-03-1 Figure 1 Wing Installation - Attachment Fittings Effectivity: All 12-B-57-00-00-00B-720B-A UNCLASSIFIED 2021-12-04 Page 7...
  • Page 643 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED LEFT SHOWN RIGHT SIMILAR SECTION SECTION 12-B-570000-A-S4080-79011-A-02-1 Figure 1 Wing Installation - Attachment Fittings Effectivity: All 12-B-57-00-00-00B-720B-A UNCLASSIFIED 2021-12-04 Page 8...
  • Page 644 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Removal of the Sling Equipment 2.2.1 Release the lift force from the wing sling Figure 2 [1], if needed. 2.2.2 Disconnect the wing sling Figure 2 [1] from the lift straps Figure 2 [5], Figure 2 [6] and Figure 2 [7]. 2.2.3 Remove the lift straps Figure 2 [5] and Figure 2 [6] from around the forward and aft main spars.
  • Page 645 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED LEFT WING SHOWN RIGHT WING SIMILAR Figure 2 Wing Installation - Sling Attachment/Removal Effectivity: All 12-B-57-00-00-00B-720B-A UNCLASSIFIED 2021-12-04 Page 10...
  • Page 646 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Equipment Connection at the Wing Top and Rear 2.3.1 Remove the padding from the aileron control rod Figure 3 [12]. Connect the aileron control rod Figure 3 [12] to the bell crank Figure 3 [15] and install the bolt Figure 3 [11], washer Figure 3 [14] and nut Figure 3 [13].
  • Page 647 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED WING NOT SHOWN FOR CLARITY 12-B-570000-A-S4080-00013-A-03-1 Figure 3 Right Wing Installation - Top and Rear Equipment Effectivity: All 12-B-57-00-00-00B-720B-A UNCLASSIFIED 2021-12-04 Page 12...
  • Page 648 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Equipment Connection at the Wing Bottom Center 2.4.1 Remove the caps and install the brake pipe Figure 4 [8] between the fuselage and wing. 2.4.2 Remove the caps and install the grommet Figure 4 [7] and the three fuel pipes Figure 4 [1], Figure 4 [2] and Figure 4 [3] between the fuselage and the connections in the landing gear compartment.
  • Page 649 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED 12-B-570000-A-S4080-00008-A-02-1 Figure 4 Right Wing Installation - Bottom Center Equipment Effectivity: All 12-B-57-00-00-00B-720B-A UNCLASSIFIED 2021-12-04 Page 14...
  • Page 650 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Rear De-ice Pipeline Connection 2.5.1 Put the outboard end of the bonding strap Figure 5 [12] and the flap drive support angle in position and install the bolt Figure 5 [11] nut Figure 5 [13]. 2.5.2 Remove the caps and connect the two rear de-ice pipes Figure 5 [2].
  • Page 651 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Figure 5 Right Wing Installation - Rear De-ice Pipelines Effectivity: All 12-B-57-00-00-00B-720B-A UNCLASSIFIED 2021-12-04 Page 16...
  • Page 652 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Forward De-ice Pipeline Connection 2.6.1 Remove the caps. Put the forward cross connector Figure 6 [19] in position and connect the de-ice pipe Figure 6 [7] to the ejector flow control valve Figure 6 [8]. 2.6.2 Remove the caps and connect the de-ice pipe Figure 6 [15] to the pressure switch Figure 6 [12].
  • Page 653 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED 12 BR 12 AR 12 AB 12 DR 12 FR 12 ER Figure 6 Right Wing Installation - Panels and Forward De-ice Pipelines Effectivity: All 12-B-57-00-00-00B-720B-A UNCLASSIFIED 2021-12-04 Page 18...
  • Page 654 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Close-up If a new wing is installed, do a check of the alignment and symmetry, refer to AMM 12-B-05-50-06- 00A-282A-A. Connect the aircraft batteries: − Lead acid batteries, refer to AMM 12-B-24-30-07-00A-920A-A −...
  • Page 655 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED 3.23 Close the access panel 11AL. Effectivity: All 12-B-57-00-00-00B-720B-A UNCLASSIFIED 2021-12-04 Page 20...
  • Page 656 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED 150Kg 25° MAX. Figure 7 Wing Installation MSN 1300, 1451 - 1575 - Close Up Effectivity: All 12-B-57-00-00-00B-720B-A UNCLASSIFIED 2021-12-04 Page 21...
  • Page 657 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED 150Kg 25° MAX. 12-B-570000-A-S4080-79090-A-01-1 Figure 8 Wing Installation MSN 1576 - 9999 - Close Up Effectivity: All 12-B-57-00-00-00B-720B-A UNCLASSIFIED 2021-12-04 Page 22...
  • Page 658 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Requirements after job completion Required Conditions Table 6 Required Conditions Action / Condition Data module/Technical publication None Effectivity: All 12-B-57-00-00-00B-720B-A End of data module UNCLASSIFIED 2021-12-04 Page 23...
  • Page 659 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Intentionally left blank Effectivity: All 12-B-57-00-00-00B-720B-A UNCLASSIFIED 2021-12-04 Page 24...
  • Page 660 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED FIVE-BLADED PROPELLER ADJUSTMENT/TEST Table of Contents Page FIVE-BLADED PROPELLER - ADJUSTMENT/TEST..............Index of Tables Page References......................Required Conditions....................Support equipment....................Supplies........................Spares........................Required Conditions....................Index of Figures Page Five- Bladed Propeller - Adjustment/Test Preparation..........
  • Page 661 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Preliminary Requirements Required Conditions Table 2 Required Conditions Action / Condition Data module/Technical publication None Support equipment Table 3 Support equipment Name Identifications/References Reference Remark Safety clip (Circuit breaker hold Part T12-030 open)
  • Page 662 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Name Identifications/References Reference Remark Bolt AN3-3A (Propeller balance CSN 61-10-00-01-060 weights) Washer NAS1149F0363P (Pro- CSN 61-10-00-01-065 peller balance weights) Washer NAS1149F0332P (Pro- CSN 61-10-00-01-070 peller balance weights) Washer AN970-3 (Propeller bal- CSN 61-10-00-01-075 ance weights)
  • Page 663 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Dynamic balancing must be done when propeller vibration is reported. Preparation Propeller Inspection Note Only qualified persons can do a dynamic balance of the propeller. 2.1.1 Examine the record of balance tests in the aircraft and propeller log books.
  • Page 664 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Note The velometer must be correctly aligned with the horizontal axis to give the correct indications to the balancer unit. 2.2.2.5 Install the magnetic pick-up Figure 1 [18]: 2.2.2.5.1 Remove the nuts Figure 1 [14] and washers Figure 1 [15] from the blanking plate Figure 1 [16].
  • Page 665 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED SWITCH POSITION FUNCTION selector MAGNETIC PICKUP COMMON RPM RANGE selector INTERRUPTER LOGIC SINGLE 3.1.7 Energize the aircraft electrical system, refer to AMM 12-B-24-00-00-00A-901A-A. Test Of The Propeller Balance 3.2.1 Start the engine, refer to AMM 12-B-71-00-00-00A-901A-A.
  • Page 666 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Note There can be a large error in the track of the propeller blades with a very small error in the angle that they are set to. 3.2.24 If the IPS shown in Step 3.2.19 is not more than 0.2 IPS, the dynamic balance of the propeller is satisfactory.
  • Page 667 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Test Of The Propeller Balance Refer to Fig. 3 and Fig. 4 4.2.1 Start the engine, refer to AMM 12-B-71-00-00-00A-901A-A. 4.2.2 Set the PCL to GROUND IDLE. 4.2.3 Make sure the propeller input cables are connected to the VELO 1 and MAG PU A connections on the Vibrex 2000 unit.
  • Page 668 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED 4.2.22.1 Plot the IPS and clock position on the balance chart (Fig. 4 Chart A). 4.2.22.2 Calculate the quantity of weights required and make a record on the chart (Fig. 4 Chart B). Note For each 0.1 IPS out of balance approximately 12 g (0.42 oz) is required.
  • Page 669 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED 5.13 Torque the nut Figure 1 [10] to between 19,2 and 21,5 Nm (170 and 190 lbf in). 5.14 Remove the lockwire from the velometer Figure 1 [8]. 5.15 Remove the velometer Figure 1 [8] from the velometer bracket Figure 1 [9].
  • Page 670 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED 12-B-611000-A-S4080-79148-A-02-1 Figure 1 Five- Bladed Propeller - Adjustment/Test Preparation Effectivity: All 12-B-61-00-00-00A-903B-A UNCLASSIFIED 2021-12-04 Page 11...
  • Page 671 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED ACCELEROMETER CONNECTION FUNCTION SELECTOR CHANNEL A A CHANNEL B INDEPENDENT TRACK MAGNETIC MAG P/U PICKUP SWITCH PHOTOCELL FUNCTION COMMON -IMPORTANT- BALANCER Use"COMMON"unless R.P.M. TUNE two magnetic pickups MODEL 8350 are in use Do not...
  • Page 672 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED CONNECTION INTERFACES DISPLAY SCREEN CHADWICK HELMUTH CONTEXT CONTRAST KEYS KEYS GO BACK START PRINT REVIEW KEYPAD YZ : + / - SPACE BATTERY END PLATE Figure 3 Vibrex 2000 Dynamic Balancer Effectivity: All 12-B-61-00-00-00A-903B-A...
  • Page 673 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED PROPELLER DYNAMIC BALANCE CHART/DATA SHEET AIRCRAFT SERIAL No..........ENGINE SERIAL No............ PROPELLER SERIAL No........... DATE ................NAME ................SIGNATURE ..............BALANCE IS ACCEPTABLE WHEN IPS INDICATION IS 0.2 OR LESS AND CLOCK POSITION INDICATION IS ERRATIC. CONDITION IDLE MAXIMUM PROPELLER RPM...
  • Page 674 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Requirements after job completion Required Conditions Table 6 Required Conditions Action / Condition Data module/Technical publication None Effectivity: All 12-B-61-00-00-00A-903B-A End of data module UNCLASSIFIED 2021-12-04 Page 15...
  • Page 675 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Intentionally left blank Effectivity: All 12-B-61-00-00-00A-903B-A UNCLASSIFIED 2021-12-04 Page 16...
  • Page 676 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED POWERPLANT CLEAN Table of Contents Page POWERPLANT - CLEAN......................Index of Tables Page References......................Required Conditions....................Support equipment....................Supplies........................Spares........................Rinse Solution - Quantities Necessary..............Rinse Solution - Water/Methyl Alcohol Ratios............
  • Page 677 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Preliminary Requirements Required Conditions Table 2 Required Conditions Action / Condition Data module/Technical publication None Support equipment Table 3 Support equipment Name Identifications/References Reference Remark Blanking cap Part Local supply P3 pipe...
  • Page 678 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Spares Table 5 Spares Name Identifications/References Reference Remark Gasket CSN 21-40-00-01-090 Safety Conditions WARNING BE CAREFUL WHEN YOU USE THE CONSUMABLE MATERIALS. OBEY THE MANUFACTURERS' HEALTH AND SAFETY INSTRUCTIONS AND ALL THE APPLICABLE LOCAL INSTRUCTIONS.
  • Page 679 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED 2.1.6 Remove and discard the lockwire from the exhaust duct cap Figure 1 [20]. 2.1.7 Remove the exhaust duct cap Figure 1 [20] from the union Figure 1 [21]. 2.1.8 Aircraft pre SB 71-012: 2.1.8.1...
  • Page 680 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED 2.3.6 Safety the exhaust duct cap Figure 1 [20] with Lockwire (standard) (Pt.No. P02-007). 2.3.7 Remove all the equipment, tools and materials from the work area. Make sure that the work area is clean.
  • Page 681 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED 3.1.13 Remove the exhaust duct cap Figure 1 [20] from the union Figure 1 [21]. 3.1.14 Aircraft pre SB 71-012: 3.1.14.1 Remove and discard the lockwire from the blanking cap Figure 1 [19]. 3.1.14.2 Remove the blanking cap Figure 1 [19] from the wash ring Figure 1 [18].
  • Page 682 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED 3.3.2.4 Safety the blanking cap Figure 1 [19] with Lockwire (standard) (Pt.No. P02-007). 3.3.3 Aircraft post SB 71-012: 3.3.3.1 Disconnect the engine wash rig from the compressor wash coupling Figure 2 [2]. 3.3.3.2 Install the protective cap Figure 2 [1] on the compressor wash coupling Figure 2 [2].
  • Page 683 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED 4.1.3 Open and install a Safety clip - Circuit breaker hold open (Pt.No. T12-030) on this circuit breaker: − IGNITION (ESSENTIAL BUS) − STARTER (ESSENTIAL BUS). 4.1.4 Remove the engine cowlings 42AT and 42AB.
  • Page 684 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED 4.3.10 Remove all the equipment, tools and materials from the work area. Make sure that the work area is clean. 4.3.11 Install the engine cowlings 42AB and 42AT. 4.3.12 Remove the safety clip and close the circuit breaker: −...
  • Page 685 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED DIRECTION OF AIRFLOW 12-A-710000-A-S4080-71127-A-02-1 Figure 1 Powerplant - Clean and Apply Surface Protection Effectivity: All 12-B-71-00-00-00A-250A-A UNCLASSIFIED 2021-12-04 Page 10...
  • Page 686 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED 12-A-710000-A-S4080-00925-A-03-1 Figure 1 Powerplant - Clean and Apply Surface Protection Effectivity: All 12-B-71-00-00-00A-250A-A UNCLASSIFIED 2021-12-04 Page 11...
  • Page 687 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED 12-B-710000-A-S4080-03745-A-01-1 Figure 2 Powerplant - Compressor Wash Post SB 71-012 Effectivity: All 12-B-71-00-00-00A-250A-A UNCLASSIFIED 2021-12-04 Page 12...
  • Page 688 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Requirements after job completion Required Conditions Table 10 Required Conditions Action / Condition Data module/Technical publication None Effectivity: All 12-B-71-00-00-00A-250A-A End of data module UNCLASSIFIED 2021-12-04 Page 13...
  • Page 689 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Intentionally left blank Effectivity: All 12-B-71-00-00-00A-250A-A UNCLASSIFIED 2021-12-04 Page 14...
  • Page 690 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED POWERPLANT TEST 20 – AFTER ENGINE STOP ADJUSTMENT/TEST Table of Contents Page POWERPLANT TEST 20 – AFTER ENGINE STOP - ADJUSTMENT/TEST......Index of Tables Page References......................
  • Page 691 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Spares Table 5 Spares Name Identifications/References Reference Remark None Safety Conditions None Procedure TEST 20 - AFTER ENGINE STOP Open the engine cowlings 43AL and 43AR. Remove the engine cowlings 42AT and 42AB.

  • Page 692: References

    PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED POWERPLANT STRIP/BUILD Table of Contents Page POWERPLANT - STRIP/BUILD....................Index of Tables Page References......................Required Conditions....................Support equipment....................Supplies........................Spares........................Required Conditions....................Index of Figures Page Engine - Accessory Gearbox - Strip/Build..............
  • Page 693 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Preliminary Requirements Required Conditions Table 2 Required Conditions Action / Condition Data module/Technical publication None Support equipment Table 3 Support equipment Name Identifications/References Reference Remark Spillage container Part Local supply Plug...

  • Page 694: General

    PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Name Identifications/References Reference Remark Washer CSN 71-20-00-01-035 Shockmount Assy CSN 71-20-00-01-045 Retainer CSN 71-70-00-01-110 O-ring CSN 71-70-00-01-112 O-ring CSN 73-10-00-01-030 O-ring CSN 73-10-00-01-060 Cotter pin CSN 76-10-00-01-090 O-ring CSN 79-10-00-01-015...
  • Page 695 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED 2.1.2 Remove the fuel flow transmitter, refer to AMM 12-B-73-30-01-00A-920A-A. 2.1.3 Remove the cotter pin Figure 1 [4], nut Figure 1 [3], the two washers Figure 1 [5] and the bolt Figure 1 [6] and remove the input lever Figure 1 [2] from the cam linkage Figure 1 [1].
  • Page 696 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED 2.3.6 Remove the nut Figure 5 [13], washer Figure 5 [12], screw Figure 5 [8] and clamps Figure 5 [9] and Figure 5 [10] from the Py pipe Figure 5 [11]. 2.3.7 Remove the nut Figure 5 [15], bolt Figure 5 [16] and bracket Figure 5 [14] from the engine.
  • Page 697 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED 2.5.6 Remove the screws Figure 7 [19], washers Figure 7 [20], plate halves Figure 7 [21] and seal halves Figure 7 [22]. 2.5.7 Remove the lockwire from the bolts Figure 7 [18]. 2.5.8 Remove the bolts Figure 7 [18] and the washers Figure 7 [17].
  • Page 698 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED 3.1.4 Install the union Figure 8 [23] and new O-ring Figure 8 [22] in the HP pump Figure 8 [21]. 3.1.5 Install the fitting Figure 8 [14], nut Figure 8 [13], new O-ring Figure 8 [12] and the new Retainer Figure 8 [11] in the reduction gearbox Figure 8 [10].
  • Page 699 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Install Components On The Engine Note If the engine stand does not give sufficient access to install the shockmount assemblies on the engine, install the shockmount assemblies on the engine when it is on the hoist before it is installed in the airframe.
  • Page 700 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED 3.4.4 Install the brackets Figure 5 [50] and the bonding lead Figure 5 [51] on the engine with the nuts Figure 5 [52]. 3.4.5 Torque the nuts Figure 5 [52] to between 3,6 and 4,0 Nm (32 and 36 lbf in). 3.4.6 Install the clamps Figure 5 [47] and Figure 5 [48] on the engine with the screw Figure 5 [49], washer Figure 5 [46] and nut Figure 5 [45].
  • Page 701 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Note If necessary, carefully bend the firewire to suit the new clamp position. 3.5.5 Close the firewire clamp Figure 4 [2] and tighten the fastener Figure 4 [3]. 3.5.6 Remove and discard the lockwire from the compressor wash ring cap Figure 3 [1].
  • Page 702 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED 3.6.11 Install the rigging pin through the rigging holes Figure 1 [22]. 3.6.12 Install the input lever Figure 1 [2] in a 20° up position on the cam shaft Figure 1 [1] with the bolt Figure 1 [6], two washers Figure 1 [5], the nut Figure 1 [3] and new Cotter pin Figure 1 [4].
  • Page 703 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Figure 1 Engine - Accessory Gearbox - Strip/Build Effectivity: All 12-B-71-00-00-00A-920A-B UNCLASSIFIED 2021-12-04 Page 12...
  • Page 704 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Figure 1 Engine - Accessory Gearbox - Strip/Build Effectivity: All 12-B-71-00-00-00A-920A-B UNCLASSIFIED 2021-12-04 Page 13...
  • Page 705 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED 12-B-710000-A-S4080-03738-A-02-1 Figure 2 Compressor Wash Kit (If Installed) - Removal/Installation Effectivity: All 12-B-71-00-00-00A-920A-B UNCLASSIFIED 2021-12-04 Page 14...
  • Page 706 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED 12-B-710000-A-S4080-03755-A-02-1 Figure 3 Compressor Wash Kit (If Installed) - Removal/Installation Effectivity: All 12-B-71-00-00-00A-920A-B UNCLASSIFIED 2021-12-04 Page 15...
  • Page 707 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED PRE SB 71-012 POST SB 71-012 12-B-710000-A-S4080-04014-A-01-1 Figure 4 Firewire Clamp - Compressor Wash Kit (if installed) Effectivity: All 12-B-71-00-00-00A-920A-B UNCLASSIFIED 2021-12-04 Page 16...
  • Page 708 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED 12-B-710001-A-S4080-00040-A-01-1 Figure 5 Engine - Firewire - Strip/Build Effectivity: All 12-B-71-00-00-00A-920A-B UNCLASSIFIED 2021-12-04 Page 17...
  • Page 709 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Figure 5 Engine - Firewire - Strip/Build Effectivity: All 12-B-71-00-00-00A-920A-B UNCLASSIFIED 2021-12-04 Page 18...
  • Page 710 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED 35 mm (1.38 in) 45 mm (1.77 in) 12 13 12-B-710000-A-S4080-00046-A-02-1 Figure 6 Engine - Components - Strip/Build Effectivity: All 12-B-71-00-00-00A-920A-B UNCLASSIFIED 2021-12-04 Page 19...
  • Page 711 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED 12-A-710002-A-S4080-00943-A-03-1 Figure 6 Engine - Components - Strip/Build Effectivity: All 12-B-71-00-00-00A-920A-B UNCLASSIFIED 2021-12-04 Page 20...
  • Page 712 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Figure 7 Engine - Plenum - Strip/Build Effectivity: All 12-B-71-00-00-00A-920A-B UNCLASSIFIED 2021-12-04 Page 21...
  • Page 713 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Figure 7 Engine - Plenum - Strip/Build Effectivity: All 12-B-71-00-00-00A-920A-B UNCLASSIFIED 2021-12-04 Page 22...
  • Page 714 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED 12-A-710002-A-S4080-00946-A-02-1 Figure 8 Engine - Stripdown/Build-up - Pipes and Unions Effectivity: All 12-B-71-00-00-00A-920A-B UNCLASSIFIED 2021-12-04 Page 23...
  • Page 715 PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719, 12-B-AM-00-00-00-I 1721-1999 UNCLASSIFIED Requirements after job completion Required Conditions Table 6 Required Conditions Action / Condition Data module/Technical publication None Effectivity: All 12-B-71-00-00-00A-920A-B End of data module UNCLASSIFIED 2021-12-04 Page 24...

Table of Contents

Save PDF