Aquila AT01-100B Maintenance Manual
  1. Manuals
  2. Brands
  3. Aquila Manuals
  4. Aircrafts
  5. AT01-100B
  6. Maintenance manual

Aquila AT01-100B Maintenance Manual

Hide thumbs Also See for AT01-100B:
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
716
717
718
719
720
Table of Contents

Advertisement

Quick Links

Download this manual See also: Handbook
A

MAINTENANCE MANUAL

AQUILA AT01-100C (A211GX)
This document is protected by copyright. All associated rights, in particular those of translation, reprinting, reproduction
by photo mechanical or similar means and storing in data processing facilities in whole or part are reserved.
The technical content of this document is approved under the authority of DOA ref. EASA.21J.025.
AQUILA Aviation GmbH
Flugplatz
14959 Schönhagen
AQUILA AT01-100
MAINTENANCE MANUAL
AQUILA AT01-100A (A211)
AQUILA AT01-100B (A211G)
Doc.-No. MM-AT01-1020-110
Issued: April, 2013
AQUILA Aviation GmbH
Phone:++49 33 731 707 - 0
Fax:
++49 33 731 707 - 11
e-mail: kontakt@aquila-aviation.de

Advertisement

Table of Contents
loading
Need help?

Need help?

Do you have a question about the AT01-100B and is the answer not in the manual?

Questions and answers

Subscribe to Our Youtube Channel

Related Manuals for Aquila AT01-100B

Summary of Contents for Aquila AT01-100B

  • Page 1: Maintenance Manual

    AQUILA AT01-100 AQUILA Aviation GmbH MAINTENANCE MANUAL MAINTENANCE MANUAL AQUILA AT01-100A (A211) AQUILA AT01-100B (A211G) AQUILA AT01-100C (A211GX) Doc.-No. MM-AT01-1020-110 Issued: April, 2013 This document is protected by copyright. All associated rights, in particular those of translation, reprinting, reproduction by photo mechanical or similar means and storing in data processing facilities in whole or part are reserved.
  • Page 2 AQUILA AT01-100 MAINTENANCE MANUAL...
  • Page 3 This Temporary Revision 2 contains an update to the Aquila AT01-100 Maintenance Manual to add an additional inspection of the throttle lever Bowden cable. It is valid in conjunction with the latest revision of the Aquila AT01-100 Maintenance Manual until the next revision of the affected chapters.
  • Page 5 This Temporary Revision 1 contains an update to the Aquila AT01-100 Maintenance Manual as a result of changed replacement times for the teflon hoses of the brake, fuel and oil systems. It is valid in conjunction with the latest revision of the Aquila AT01-100 Maintenance Manual until the next revision of the affected chapters.

  • Page 7: Table Of Contents

    AQUILA AT01-100 Table of Contents MAINTENANCE MANUAL TABLE OF CONTENTS Cha/Sec/Sub Title Pages TABLE OF CONTENTS INTRODUCTION LIST OF EFFECTIVE CHAPTERS AIRWORTHINESS LIMITATIONS 04-00-00 Airworthiness Limitations - General TIME LIMITS / MAINTENANCE CHECKS 05-00-00 Time Limits / Maintenance Checks - General...
  • Page 8 AQUILA AT01-100 Table of Contents MAINTENANCE MANUAL TABLE OF CONTENTS (Cont.) Cha/Sec/Sub Title Pages PLACARDS AND MARKINGS 11-00-00 Placards and Markings - General 11-20-00 Exterior Placards and Markings 201-206 11-30-00 Interior Placards and Markings 201-208 SERVICING 12-00-00 Servicing - General...
  • Page 9 AQUILA AT01-100 Table of Contents MAINTENANCE MANUAL TABLE OF CONTENTS (Cont.) Cha/Sec/Sub Title Pages 24-30-00 Battery - Maintenance 24-40-00 External Power - Maintenance 201-203 24-60-00 Electrical Load Distribution - Description 24-61-00 Circuit Breaker - Maintenance 201-202 24-97-00 Electrical System Wiring - Maintenance...
  • Page 10 AQUILA AT01-100 Table of Contents MAINTENANCE MANUAL TABLE OF CONTENTS (Cont.) Cha/Sec/Sub Title Pages 32-20-00 Nose Landing Gear - Description 32-20-00 Nose Landing Gear - Maintenance 201-203 32-40-00 Wheels and Brakes - Description 32-40-00 Wheels and Brakes - Maintenance 201-221/208...
  • Page 11 AQUILA AT01-100 Table of Contents MAINTENANCE MANUAL TABLE OF CONTENTS (Cont.) Cha/Sec/Sub Title Pages WINDOWS 56-00-00 Windows - General 56-10-00 Flight Compartment Windows - Maintenance 201-203 WINGS 57-00-00 Wings - General 57-00-00 Wings - Maintenance 201-205 57-50-00 Control Surfaces - Maintenance...
  • Page 12 AQUILA AT01-100 Table of Contents MAINTENANCE MANUAL TABLE OF CONTENTS (Cont.) Cha/Sec/Sub Title Pages 79-00-00 Oil - General 79-10-00 Oil Tank - Maintenance 201-202 79-20-00 Oil Cooler - Maintenance 201-202 79-31-00 Oil Pressure Indication - Maintenance 201/201 79-33-00 Oil Temperature Indication - Maintenance...
  • Page 13 AQUILA AT01-100 Record of Revisions MAINTENANCE MANUAL RECORD OF REVISIONS Date Revision Date of Date Revision Date of Number Inserted Revision Inserted Number Revision A.01 30.04.13 A.02 26.08.13 A.03 24.10.13 A.04 02.03.15...
  • Page 14 AQUILA AT01-100 MAINTENANCE MANUAL...
  • Page 15 AQUILA AT01-100 Record of Temp. Revisions MAINTENANCE MANUAL RECORD OF TEMPORARY REVISIONS Temp. Revision Date of Date Page Number Revision Removed 05-10-00 p.1 & 3 11.06.14 05-20-00 p.7 14.08.14 76-00-00 p.203 & 204...
  • Page 16 AQUILA AT01-100 MAINTENANCE MANUAL...

  • Page 17: Airworthiness Limitations

    AQUILA AT01-100 Highlights of Revisions MAINTENANCE MANUAL HIGHLIGHTS OF REVISIONS Revision Date of Revision Date of Reason for Revision Reason for Revision Number Revision Number Revision A.01 30.04.13 Initial issue. A.02 26.08.13 SB-AT01-027 A.03 24.10.13 FAA validation (airworthiness limitations, wire routing diagrams);...
  • Page 18 AQUILA AT01-100 MAINTENANCE MANUAL...
  • Page 19 Table 1 - List of Technical Publications Title Manual No. / Part No. Supplier Airplane Flight Manual FM-AT01-1010-101/102/103 AQUILA Aviation GmbH AQUILA AT01-100A/B/C Maintenance Manual (Line Maintenance) MML-912 BRP-Powertrain GmbH & Co KG ROTAX Engine Type 912 Series 899191...
  • Page 20 AQUILA AT01-100 Introduction MAINTENANCE MANUAL Table 1 - List of Technical Publications (Cont.) Title Manual No. / Part No. Supplier Maintenance Manual AWBCMM0001 Parker Hannifin Corp. Cleveland Wheels and Brakes G500 AML STC Installation Manual 190-01102-06 Garmin International Inc. Instructions for Continued Airworthiness 190-01102-00 Garmin International Inc.
  • Page 21 AQUILA AT01-100 Introduction MAINTENANCE MANUAL Intentionally left blank! Page 3 INTRODUCTION 30.04.13...
  • Page 22 AQUILA AT01-100 Introduction MAINTENANCE MANUAL Structure of the Maintenance Manual The MM has been prepared in accordance with the Air Transport Association (ATA) specification number 100 for manufacturer’s technical data. Classification of Subject Matter The MM is divided into 5 major sections. Each of these sections is sub-divided into chapters.
  • Page 23 AQUILA AT01-100 Introduction MAINTENANCE MANUAL (2) When the chapter/system element number is followed by zeros in the section/subsystem and subject/unit element number (28-00-00), the information is applicable to the entire system. (3) When the section/subsystem element number is followed by zeros in the subject/unit element number (28-20-00), the information is applicable to subsystem within the system.
  • Page 24 AQUILA AT01-100 Introduction MAINTENANCE MANUAL Record of Temporary Revisions Highlights of Revisions Introduction List of Effective Chapters (2) Each chapter begins with: Title Table of Contents Figures The figures within the sections of a chapter are numbered in accordance with the appropriate page number block.
  • Page 25 AQUILA AT01-100 Introduction MAINTENANCE MANUAL Effectivity This maintenance manual is "customized". It includes the following effectivity identification system to show modification and/or configuration differences. (1) The MM starts with a list of effective chapters. Each chapter is listed with date of issue or revision.
  • Page 26 AQUILA AT01-100 Introduction MAINTENANCE MANUAL (4) Incorporating revisions into the manual (a) In order to keep track of revisions and to facilitate the use of the manual, a revision always affects the entire chapter, i.e. all pages of a chapter have the same date of issue or revision and the entire chapter is replaced during a revision.

  • Page 27: Time Limits / Maintenance Checks

    AQUILA AT01-100 List of Chapters MAINTENANCE MANUAL LIST OF EFFECTIVE CHAPTERS Chapter Title Date* GENERAL Table of Contents 24.10.13 Introduction 30.04.13 Airworthiness Limitations .03.15 Time Limits / Maintenance Checks 26.08.13 Dimensions and Areas 30.04.13 Lifting & Shoring 30.04.13 Leveling and Weighing 30.04.13...
  • Page 28 AQUILA AT01-100 List of Chapters MAINTENANCE MANUAL LIST OF EFFECTIVE CHAPTERS Chapter Title Date* POWER PLANT Power Plant 30.04.13 Ignition 30.04.13 Cooling System 30.04.13 Engine Controls 30.04.13 Engine Indicating 30.04.13 Exhaust 30.04.13 30.04.13 Starting 30.04.13 Charts and Wiring Diagrams 24.10.13 * The date refers to the issue / revision date of the respective chapter.
  • Page 29 AQUILA AT01-100 MAINTENANCE MANUAL CHAPTER 4 AIRWORTHINESS LIMITATIONS...
  • Page 30 AQUILA AT01-100 MAINTENANCE MANUAL...
  • Page 31 AQUILA AT01-100 Airworthiness Limitations MAINTENANCE MANUAL RECORD OF REVISIONS - CHAPTER 4 Revision Date of Number Revision Reason for Revision Approval Reference A.01 30.04.13 Initial issue EASA Major Change Approval 10045112 A.02 24.10.13 FAA validation A.03 02.03.15 Life time limit /...
  • Page 32 AQUILA AT01-100 MAINTENANCE MANUAL...
  • Page 33 AQUILA AT01-100 Airworthiness Limitations MAINTENANCE MANUAL TABLE OF CONTENTS Chapter Section Title Subject Page AIRWORTHINESS LIMITATIONS - GENERAL ..........04-00-00 Introduction 04-00-00 Airworthiness Limitations 04-00-00 Page 1 04 - TOC 02.03.15...
  • Page 34 AQUILA AT01-100 MAINTENANCE MANUAL...
  • Page 35 6000 h airframe of the AQUILA AT01-100 is limited to of flight time. An inspection program to reach an extension of replacement time can be obtained from AQUILA Aviation GmbH. NOTE: The life time limit of 6000 h of flight time will be kept for all models listed in the data sheet.
  • Page 36 / shade is Du Pont PUR EV310 Performance Coating / RAL 9016. Before painting the aircraft with a different coating AQUILA Aviation GmbH must be contacted. For airplanes registered in Europe or countries where the EASA-TC has been accepted, the approved shade is RAL 9016.
  • Page 37 AQUILA AT01-100 MAINTENANCE MANUAL CHAPTER 5 TIME LIMITS / MAINTENANCE CHECKS...
  • Page 38 AQUILA AT01-100 MAINTENANCE MANUAL...
  • Page 39 AQUILA AT01-100 Maintenance Checks MAINTENANCE MANUAL TABLE OF CONTENTS Chapter Section Title Subject Page TIME LIMITS / MAINTENANCE CHECKS - GENERAL ......05-00-00 Introduction 05-00-00 General Description 05-00-00 COMPONENT TIME LIMITS .................05-10-00 General 05-10-00 Component Time Limits 05-10-00 SCHEDULED MAINTENANCE CHECKS............05-20-00...
  • Page 40 AQUILA AT01-100 MAINTENANCE MANUAL...
  • Page 41 TIME LIMITS / MAINTENANCE CHECKS - GENERAL Introduction This chapter provides scheduled and unscheduled maintenance checks and inspections, recommended by the type certificate holder AQUILA Aviation GmbH as well as the time limits for service life limited components and parts. General Description In the following, a brief description and intended purpose of each section of this chapter is given.
  • Page 42 AQUILA AT01-100 MAINTENANCE MANUAL...
  • Page 43 Component Time Limits Under certain circumstances the replacement or overhaul of components may be required before the time limits listed below are reached. Replacement time limits, recommended by the type certificate holder AQUILA Aviation GmbH Chapter Component / Part Replacement Time...
  • Page 44 AQUILA AT01-100 Maintenance Checks MAINTENANCE MANUAL Vendor Established Component Time Limits Chapter Component / Part Replacement Time Overhaul ELT battery Note 1 Fire extinguisher 10 years Note 4 Air Total Fire extinguisher 12 years ASPEN internal battery 800 h or 3 years...
  • Page 45 AQUILA AT01-100 Maintenance Checks MAINTENANCE MANUAL Engine ROTAX 912S 2000 h or 15 years Note 3 ROTAX mechanical 5 years fuel pump Note 3 ROTAX flexible teflon with engine overhaul hoses of the fuel system Note 3 ROTAX rubber parts...
  • Page 46 AQUILA AT01-100 Maintenance Checks MAINTENANCE MANUAL...
  • Page 47 The inspection time intervals chart contained in this chapter shows the recommended intervals at which maintenance and maintenance checks should be carried out on the aircraft. Annual inspections and 100 hour inspections on the AQUILA AT01-100 must include all inspection items as required by FAR 43, Appendix D, “Scope and detail of annual/100h inspections”.
  • Page 48 Airworthiness directives - Verify all airworthiness directives have been complied with. Service letters, service bulletins, and service information - Verify all AQUILA GmbH and suppliers service letters, service bulletins and service information have been complied with. Service time records, equipment list and weight and balance records - Check.
  • Page 49 AQUILA AT01-100 Maintenance Checks MAINTENANCE MANUAL Pre-Inspection / Engine Ground Test (Cont.) Reference Interval Initials 100h other RPM drop: _______RPM / Man. Press :_______in. Hg Engine instruments - Check engine parameters. Magneto RPM drop - Set 1700 RPM. Check that RPM drop...
  • Page 50 AQUILA AT01-100 Maintenance Checks MAINTENANCE MANUAL Engine (Cont.) Reference Interval Initials 100h other CAUTION: SI-912-016 DO NOT USE AIRCRAFT ENGINE OIL. latest Rev. Due to the friction clutch and the high stresses SB-912-033 in the reduction gear 4-stroke motor cycle oils are latest Rev.
  • Page 51 AQUILA AT01-100 Maintenance Checks MAINTENANCE MANUAL Engine (Cont.) Reference Interval Initials 100h other Coolant expansion tank - Check for damage and R* 12-20-00 1 year abnormalities. Inspect rubber protection plate on tank base Sec. 9.1 for secure fit. Check coolant level, replenish as necessary.
  • Page 52 AQUILA AT01-100 Maintenance Checks MAINTENANCE MANUAL Engine (Cont.) Reference Interval Initials 100h other Spark plug connectors - Check that resistance spark plug 200h connectors fit tightly on the spark plugs. Minimum pull-off force is 30 N (7 lb). Replace spark plugs...
  • Page 53 Other external engine accessories - Inspect screws and nuts 1 year of all other external engine parts and accessories for tight fit. Inspect safety wiring if applicable, replace as necessary. Engine mounts (manufactured by ROTAX and AQUILA) - R* 12-20-00 1 year Check mounts for deformation, cracks, corrosion, sec.
  • Page 54 AQUILA AT01-100 Maintenance Checks MAINTENANCE MANUAL Propeller (Cont.) Reference Interval Initials 100h other Propeller blades - Check blade angle play. (max. 2°) Hub - Inspect outside condition of the hub and parts for cracks, corrosion and deterioration. Check nuts for low pitch - Inspect for tightness and safety wire.
  • Page 55 AQUILA AT01-100 Maintenance Checks MAINTENANCE MANUAL Fuselage / Cabin (Cont.) Reference Interval Initials 100h other Baggage door - Check door seal, door latching mechanism, and door hinge for defects and condition. Inspect door structure for cracks or other damage. ELT - Perform ELT inspection. Check ELT mount and Velcro...
  • Page 56 AQUILA AT01-100 Maintenance Checks MAINTENANCE MANUAL Fuselage / Cabin (Cont.) Reference Interval Initials 100h other Rudder control - Check rudder control weldment and rudder bellcrank for cracks, distortion, chafing and security. Examine rudder control support brackets, rudder pedal pivot brackets and connection of the rudder controls with the nose gear steering tubes for security, condition and correct splintering.
  • Page 57 AQUILA AT01-100 Maintenance Checks MAINTENANCE MANUAL Wings, Ailerons, Flaps (Cont.) Reference Interval Initials 100h other Drain and vent holes - Check for blockage and suspect appearance of any liquid. Ailerons - Check aileron hinges, bearings, and hinge brackets for security and excessive play. Check bolts and nuts for proper safetying.
  • Page 58 AQUILA AT01-100 Maintenance Checks MAINTENANCE MANUAL Wings, Ailerons, Flaps (Cont.) Reference Interval Initials 100h other Tie-down points - Check thread and structure around the tie- 10-20-00 down attach points for any damage. Empennage, Elevator, Rudder Reference Interval Initials 100h other...
  • Page 59 AQUILA AT01-100 Maintenance Checks MAINTENANCE MANUAL Nose and Main Landing Gear Reference Interval Initials 100h other Wheel fairings - Check condition and correct fit. Remove and clean. Check for paint coat damage, cracks, dents and delamination. Fairing mounts - Inspect for cracks, distortion or other damage.
  • Page 60 AQUILA AT01-100 Maintenance Checks MAINTENANCE MANUAL Nose and Main Landing Gear (Cont.) Reference Interval Initials 100h other Wheel brakes - Remove caliper assembly from axle, disconnect 32-40-00 3000h, from brake hose. Disassemble brake caliper. Clean all metal 5 years parts. Visually inspect caliper casing and back plate for cracks, nicks, corrosion or other damage.
  • Page 61 AQUILA AT01-100 Maintenance Checks MAINTENANCE MANUAL Return to Service Reference Interval Initials 100h other Install wheel fairings. Install seats (if removed). Install cabin floor boards. Install baggage compartment floorboard. Install access panel of the baggage compartment bulkhead. Install access panel 210AB.
  • Page 62 AQUILA AT01-100 MAINTENANCE MANUAL...
  • Page 63 The scope of the pre-flight check is listed in the AQUILA AT01-100 flight manual, section 4. Pre-flight checks are essential for flight safety as numerous accidents can be traced back to inadequate pre-flight checks.
  • Page 64 AQUILA AT01-100 MAINTENANCE MANUAL...
  • Page 65 AQUILA AT01-100 Maintenance Checks MAINTENANCE MANUAL UNSCHEDULED MAINTENANCE CHECKS General Special checks are to be carried out when an incident has occurred that may have caused damage to the aircraft or impaired airworthiness. In addition, a 25-hour inspection must be carried out on new aircraft and its engine, on overhauled engines and after extensive airframe repairs.
  • Page 66 AQUILA AT01-100 Maintenance Checks MAINTENANCE MANUAL (3) Inspect nose landing gear. (a) Check wheel fairing for cracks, dents and delamination. (b) Inspect fairing mounts for cracks, distortion and other damage. (c) Check nose gear strut mount for deformation and cracks. Check nose gear strut journal bearing for proper operation and play.
  • Page 67 AQUILA AT01-100 MAINTENANCE MANUAL CHAPTER 06 DIMENSIONS AND AREAS...
  • Page 68 AQUILA AT01-100 MAINTENANCE MANUAL...
  • Page 69 AQUILA AT01-100 Dimensions and Areas MAINTENANCE MANUAL TABLE OF CONTENTS Chapter Section Title Subject Page DIMENSIONS AND AREAS - GENERAL .............06-00-00 Introduction 06-00-00 General Description 06-00-00 AIRCRAFT DIMENSIONS AND AREAS............06-10-00 General 06-10-00 Dimensions and Areas 06-10-00 Weight and Static Moments of Control Surfaces 06-10-00 AIRCRAFT ZONING ..................06-20-00...
  • Page 70 AQUILA AT01-100 MAINTENANCE MANUAL...
  • Page 71 AQUILA AT01-100 Dimensions and Areas MAINTENANCE MANUAL DIMENSIONS AND AREAS - GENERAL Introduction This chapter provides information about dimensions and control surface travel and tolerances. Furthermore, this chapter contains information about aircraft zoning and access and inspection plates. Dimensions are presented to aid the operator and/or maintenance personnel in the ground handling of the aircraft, e.g.
  • Page 72 AQUILA AT01-100 MAINTENANCE MANUAL...
  • Page 73 AQUILA AT01-100 Dimensions and Areas MAINTENANCE MANUAL AIRCRAFT DIMENSIONS AND AREAS General The wing and tail spans are measured parallel to the relevant reference level. Refer to figure 1 for an illustration of aircraft dimensions. Dimensions and Areas Aircraft overall:...
  • Page 74 AQUILA AT01-100 Dimensions and Areas MAINTENANCE MANUAL Horizontal Stabilizer and Elevator: Profile FX 71/L150-30 Area (entire) 2,0 m² 21.64 ft² 0,68 m 2.24 ft Elevator area 0,58 m² 6.28 ft² Up travel 23 ° ±1,5 ° Down travel 24 ° ±1,5 °...
  • Page 75 AQUILA AT01-100 Dimensions and Areas MAINTENANCE MANUAL 2,3 (7.55) 1,68 (5.51) 7,4 (24.2) 10,3 (33.8) 2,0 (6.58) MAC 1,07 (3.52) MAC 0,68 (2.24) 3,0 (9.87) Aircraft Dimensions [m (ft.)] Figure 1 Page 3 06-10-00 30.04.13...
  • Page 76 AQUILA AT01-100 MAINTENANCE MANUAL...
  • Page 77 AQUILA AT01-100 Dimensions and Areas MAINTENANCE MANUAL AIRCRAFT ZONING General The aircraft is divided into numbered zones to facilitate the location of aircraft components and parts. The zoning used here is standard. The zones are identified by a three-digit number. The first digit in the sequence denotes the major...
  • Page 78 AQUILA AT01-100 Dimensions and Areas MAINTENANCE MANUAL (Interior) Instrument Panel Firewall Aircraft Zones Figure 1 Page 2 06-20-00 30.04.13...
  • Page 79 AQUILA AT01-100 Dimensions and Areas MAINTENANCE MANUAL ACCESS & INSPECTION PLATES General Access / inspection plates are used to gain access to various systems, components and parts of structure during maintenance and for inspection. The access and inspection plates are designated logically.
  • Page 80 AQUILA AT01-100 Dimensions and Areas MAINTENANCE MANUAL 610AB 510AB 210AB 520AB 620AB 610BB 510BB Access / Inspection Plates Figure 1 Page 2 06-30-00 30.04.13...

  • Page 81: Lifting And Shoring

    AQUILA AT01-100 MAINTENANCE MANUAL CHAPTER 07 LIFTING AND SHORING...
  • Page 82 AQUILA AT01-100 MAINTENANCE MANUAL...
  • Page 83 AQUILA AT01-100 Lifting and Shoring MAINTENANCE MANUAL TABLE OF CONTENTS Chapter Section Title Subject Page LIFTING AND SHORING - GENERAL............07-00-00 Introduction 07-00-00 General Description 07-00-00 JACKING......................07-10-00 General 07-10-00 Tools, Equipment and Material 07-10-00 Jacking 07-10-00 Hoisting 07-10-00 Page 1 07 - TOC...
  • Page 84 AQUILA AT01-100 MAINTENANCE MANUAL...
  • Page 85 AQUILA AT01-100 Lifting and Shoring MAINTENANCE MANUAL LIFTING AND SHORING - GENERAL Introduction This chapter describes procedures used to jack the aircraft. The equipment required to jack the aircraft and the procedures to be followed are described. General Description In the following, a brief description and intended purpose of each section of this chapter is given.
  • Page 86 AQUILA AT01-100 MAINTENANCE MANUAL...
  • Page 87 Tools, Equipment and Material Quantity Equipment Parts No. Manufacturer Jack commercially available Adapter AQUILA Aviation GmbH Tail stand commercially available Wing trestles commercially available Jacking Jacking the Aircraft CAUTION: DO NOT JACK THE AIRCRAFT IN THE OPEN IF WIND VELOCITY EXCEEDS 6 KNOTS.
  • Page 88 AQUILA AT01-100 Lifting and Shoring MAINTENANCE MANUAL (5) Remove tail stand. (6) Remove adapters from jack points. Hoisting Hoisting Procedure (1) The airplane may be lifted with a one metric ton (2205 lbs) hoist for maintenance purposes. The front sling is hooked to the two upper engine mount bars. The aft sling is positioned around the aft fuselage forward the vertical stabilizer.

  • Page 89: Leveling And Weighing

    AQUILA AT01-100 MAINTENANCE MANUAL CHAPTER 08 LEVELING AND WEIGHING...
  • Page 90 AQUILA AT01-100 MAINTENANCE MANUAL...
  • Page 91 AQUILA AT01-100 Leveling and Weighing MAINTENANCE MANUAL TABLE OF CONTENTS Chapter Section Title Subject Page LEVELING AND WEIGHING - GENERAL..........08-00-00 Introduction 08-00-00 General Description 08-00-00 WEIGHING ......................08-10-00 General 08-10-00 Tools, Equipment and Material 08-10-00 Weighing Procedure 08-10-00 LEVELING......................08-20-00 General 08-20-00...
  • Page 92 AQUILA AT01-100 MAINTENANCE MANUAL...
  • Page 93 AQUILA AT01-100 Leveling and Weighing MAINTENANCE MANUAL LEVELING AND WEIGHING - GENERAL Introduction This chapter provides all the necessary information to properly level the aircraft and prepare it for weighing. General Description In the following, a brief description and intended purpose of each section of this chapter is given.
  • Page 94 AQUILA AT01-100 MAINTENANCE MANUAL...
  • Page 95 C.G. position in flight. Essential condition for a correct function is the input of the latest weighing data. Refer to Electronics International MVP-50 operating instructions for the appropriate procedures. The necessary password can be obtained from AQUILA on request. Tools, Equipment and Material...
  • Page 96 AQUILA AT01-100 Leveling and Weighing MAINTENANCE MANUAL AIRCRAFT WEIGHING REPORT MODEL: SERIAL NUMBER: REGISTRATION NUMBER: DATE: Data in accordance with Airplane Flight Manual Reference datum: Leading edge of wing root rib. Horizontal reference line: Refer to 08-20-00 for information on longitudinal leveling.
  • Page 97 (floor). NOTE: The distances „D “ and „D / D “ must be measured during every weighing! Further information on how to calculate the C.G. are contained in the AQUILA AT01-100 airplane flight manual, section 6. Page 203 08-10-00 30.04.13...
  • Page 98 AQUILA AT01-100 MAINTENANCE MANUAL...
  • Page 99 AQUILA AT01-100 Leveling and Weighing MAINTENANCE MANUAL LEVELING General Before every weighing process, the aircraft has to be leveled. Tools, Equipment and Material Quantity Equipment Parts No. Manufacturer Spirit level commercially at least 1 m available (3.28 ft) length Straight edge...
  • Page 100 AQUILA AT01-100 Leveling and Weighing MAINTENANCE MANUAL Longitudinal Leveling Wedge Positioning Figure 201 Page 202 08-20-00 30.04.13...

  • Page 101: Towing And Taxiing

    AQUILA AT01-100 MAINTENANCE MANUAL CHAPTER 09 TOWING AND TAXIING...
  • Page 102 AQUILA AT01-100 MAINTENANCE MANUAL...
  • Page 103 AQUILA AT01-100 Towing and Taxiing MAINTENANCE MANUAL TABLE OF CONTENTS Chapter Section Title Subject Page TOWING AND TAXIING - GENERAL ............09-00-00 Introduction 09-00-00 General Description 09-00-00 TOWING......................09-10-00 General 09-10-00 Tools, Equipment and Material 09-10-00 Towing Procedure 09-10-00 TAXIING ......................09-20-00 General...
  • Page 104 AQUILA AT01-100 MAINTENANCE MANUAL...
  • Page 105 AQUILA AT01-100 Towing and Taxiing MAINTENANCE MANUAL TOWING AND TAXIING - GENERAL Introduction This chapter describes towing and taxiing procedures. It contains instructions as to how the aircraft can be moved without a tow bar. General Description In the following, a brief description and intended purpose of each section of this chapter is given.
  • Page 106 AQUILA AT01-100 MAINTENANCE MANUAL...
  • Page 107 Tools, Equipment and Materials Quantity Equipment Parts No. Manufacturer 3.A. Tow bar AQUILA Aviation GmbH 3.B. Tow bar AQUILA Aviation GmbH (vehicle) Towing Procedure Towing by Tow Bar The aircraft is usually moved manually by means of a tow bar.
  • Page 108 AQUILA AT01-100 Towing and Taxiing MAINTENANCE MANUAL (8) If necessary install any rudder lock. (9) Remove tow bar from tow vehicle and aircraft. Moving Aircraft Without Tow Bar CAUTION: DO NOT PUSH OR PULL AT THE CONTROL SURFACES, THE PROPELLER TIPS OR PROPELLER SPINNER.
  • Page 109 PREVENT ABRASION AND STONE DAMAGE TO THE PROPELLER BLADES. (7) Taxi aircraft to the desired parking area. (8) Shut down the engine (refer to AQUILA AT01-100 airplane flight manual, section 4). (9) Park and secure the aircraft (refer to 10-00-00).
  • Page 110 AQUILA AT01-100 MAINTENANCE MANUAL...

  • Page 111: Parking, Mooring, Storage And Return To Service

    AQUILA AT01-100 MAINTENANCE MANUAL CHAPTER 10 PARKING, MOORING, STORAGE AND RETURN TO SERVICE...
  • Page 112 AQUILA AT01-100 MAINTENANCE MANUAL...
  • Page 113 AQUILA AT01-100 Parking, Mooring . . MAINTENANCE MANUAL TABLE OF CONTENTS Chapter Section Title Subject Page PARKING, MOORING, STORAGE AND RETURN TO SERVICE - GENERAL ..............10-00-00 Introduction 10-00-00 General Description 10-00-00 PARKING ......................10-10-00 General 10-10-00 Parking 10-10-00 STORAGE ......................10-11-00 Storage with a Duration up to 30 Days...
  • Page 114 AQUILA AT01-100 MAINTENANCE MANUAL...
  • Page 115 AQUILA AT01-100 Parking, Mooring . . MAINTENANCE MANUAL PARKING, MOORING, STORAGE AND RETURN TO SERVICE - GENERAL Introduction This chapter provides instructions on how to park, moor, store and transport the aircraft. General description The chapter is divided into different sections to help maintenance personnel to find any information required more easily.
  • Page 116 AQUILA AT01-100 MAINTENANCE MANUAL...
  • Page 117 AQUILA AT01-100 Parking, Mooring . . MAINTENANCE MANUAL PARKING General In order to protect the aircraft when it is parked in the open, the following parking instructions should be followed. The extent of the measures depends on park duration and weather conditions.
  • Page 118 AQUILA AT01-100 MAINTENANCE MANUAL...
  • Page 119 AQUILA AT01-100 Parking, Mooring . . MAINTENANCE MANUAL STORAGE Storage with a Duration up to 30 Days The following procedures should be followed if the aircraft is be stored for 7 to 30 days to prevent deterioration during periods of non-use.
  • Page 120 AQUILA AT01-100 Parking, Mooring . . MAINTENANCE MANUAL (5) Brakes (a) Apply brakes at least once a week. (6) Pitot tube (a) Put on a pitot tube cover. (7) Ventilation of the aircraft (a) Ventilate aircraft well before storage. (b) In the open, depending on external conditions (high humidity, high temperatures etc.) ventilate the aircraft several times during storage.
  • Page 121 Tools, Equipment and Material Quantity Equipment Parts No. Manufacturer 3.B. Ropes AQUILA Aviation GmbH 3.B. Tie-down AQUILA Aviation GmbH rings Mooring The aircraft has three tie-down points; two are located on the underside of the wings and the third is located on the lower fin.
  • Page 122 AQUILA AT01-100 MAINTENANCE MANUAL...
  • Page 123 AQUILA AT01-100 Parking, Mooring . . MAINTENANCE MANUAL RETURN TO SERVICE Storage between 5 and 30 Days After storage lasting between 5 and 30 days, the following should be carried out before returning to service: (1) Perform a thorough pre-flight check...
  • Page 124 AQUILA AT01-100 MAINTENANCE MANUAL...
  • Page 125 AQUILA AT01-100 Parking, Mooring . . MAINTENANCE MANUAL TRANSPORT General The aircraft may be transported in open or closed trailers. It is recommended to use a standard semi-trailer container or an ISO container for transportation over greater distances. Container dimensions have to be at least: length = 12 000 mm, width = 2300 mm, height = 2350 mm.
  • Page 126 AQUILA AT01-100 Parking, Mooring . . MAINTENANCE MANUAL NOTE: Stow wing close to the container sidewall in order to have the entire diagonal of the container cross-section available to store the fuselage. NOTE: If sufficient space is available, the wing may also be transported lying on pads and a pallet-like support to match or compensate wing dihedral.
  • Page 127 AQUILA AT01-100 MAINTENANCE MANUAL CHAPTER 11 PLACARDS AND MARKINGS...
  • Page 128 AQUILA AT01-100 MAINTENANCE MANUAL...

  • Page 129: Placards And Markings - General

    AQUILA AT01-100 Placards and Markings MAINTENANCE MANUAL TABLE OF CONTENTS Chapter Section Title Subject Page PLACARDS AND MARKINGS - GENERAL ..........11-00-00 Introduction 11-00-00 General Description 11-00-00 EXTERIOR PLACARDS AND MARKINGS...........11-20-00 General 11-20-00 Tools, Equipment and Material 11-20-00 Removal/Installation 11-20-00 Maintenance/Care 11-20-00 INTERIOR PLACARDS AND MARKINGS ...........11-30-00...
  • Page 130 AQUILA AT01-100 MAINTENANCE MANUAL...
  • Page 131 AQUILA AT01-100 Placards and Markings MAINTENANCE MANUAL PLACARDS AND MARKINGS - GENERAL Introduction This chapter provides information about interior and exterior graphics, placards, labels and interior markings, their maintenance and repair. General Description Below a brief description and intended purpose of each section of this chapter is given.
  • Page 132 AQUILA AT01-100 MAINTENANCE MANUAL...
  • Page 133 AQUILA AT01-100 Placards and Markings MAINTENANCE MANUAL EXTERIOR PLACARDS AND MARKINGS General This section gives maintenance and care instructions for exterior graphics, markings, etc.. Figure 201 shows the locations of the exterior placards and markings. Tools, Equipment and Material Quantity Equipment Parts No.
  • Page 134 AQUILA AT01-100 Placards and Markings MAINTENANCE MANUAL (4) Do not allow fuel to spill on to graphics. If fuel spills on to graphics, wipe off with a cloth and rinse with water thoroughly. (5) Do not remove snow and ice from surfaces using sharp-edged instruments.
  • Page 135 AQUILA AT01-100 Placards and Markings MAINTENANCE MANUAL Note: Placards illustrated are not to scale. Detail- Exterior Placards and Markings Figure 201 (1) Page 203 11-20-00 30.04.13...
  • Page 136 AQUILA AT01-100 Placards and Markings MAINTENANCE MANUAL Note: Placards illustrated are not to scale. KRAFTSTOFF FUEL DRAIN ABLASS Detail- TIE DOWN VERZURRPUNKT Detail- 2,5 bar 36 psi Detail- 2,5 bar 36 psi Detail- 2,0 bar 29 psi Detail- (rote Markierung...
  • Page 137 AQUILA AT01-100 Placards and Markings MAINTENANCE MANUAL Note: Placards illustrated are not to scale. Green Grün Yellow Gelb Detail- (Farbmarkierungen für die Position (colored flap position markings ) der Landeklappe) Detail- HIER EINGEBAUT INSTALLED HERE Detail- NICHT SCHIEBEN Detail- NO PUSH...
  • Page 138 AQUILA AT01-100 Placards and Markings MAINTENANCE MANUAL Note: Placards illustrated are not to scale. Externe GROUND Stromversorgung POWER 12 V DC 12 VDC Detail- Exterior Placards and Markings Figure 201 (4) EFFECTIVITY Aircraft equipped with an external power system Page 206 11-20-00 30.04.13...
  • Page 139 AQUILA AT01-100 Placards and Markings MAINTENANCE MANUAL INTERIOR PLACARDS AND MARKINGS General This section gives information about removal and installation of interior placards, markings etc.. Figure 201 shows the aircraft interior placards and markings. If the information on the placard is no longer legible or the placard is partially destroyed or is no longer in place, it must be replaced.
  • Page 140 AQUILA AT01-100 Placards and Markings MAINTENANCE MANUAL * Position of this placard can On the right side wall of the vary on the instrument panel. center pedestal adjacent to the adjusting knob. Interior Placards and Markings Figure 201 (1) Page 202 11-30-00 30.04.13...
  • Page 141 AQUILA AT01-100 Placards and Markings MAINTENANCE MANUAL Note: Placards illustrated are not to scale. Warning Stall Kontr Überzieh Attitude Künstl Lights Warning Indicator Leuchten Warnung Horizont Trimm Wende Trim Turn (OAT) Strg (OAT) Zeiger Control Coordin. Fuel Trimm Kurs NAV/GPS...
  • Page 142 AQUILA AT01-100 Placards and Markings MAINTENANCE MANUAL Note: Placards illustrated are not to scale. Detail- OIL TEMP. ÖLTEMPERATUR CYL. HEAD TEMP ZYL. KOPF TEMP Detail- CABIN HEAT HEIZUNG PULL ON ZIEHEN EIN Detail- CARB. HEAT VERGASERVORW. PULL ON ZIEHEN EIN...
  • Page 143 AQUILA AT01-100 Placards and Markings MAINTENANCE MANUAL Note: Placards illustrated are not to scale. ÖLDRUCK OIL PRESS. Detail- PARKBREMSE PARKING BRAKE ZIEHEN EIN PULL SET Detail- KRAFTSTOFF FUEL AUSFLIEGBAR USABLE 109.6 LTR 109,6 LITER 28.9 GAL TANKWECHSEL SWITCH TANKS ALLE 60 MIN...
  • Page 144 AQUILA AT01-100 Placards and Markings MAINTENANCE MANUAL Note: Placards illustrated are not to scale. HYDRAULIKÖL HYD. BRAKE Detail- Detail- FLUID 4 FLUID 4) FLUID ( ! ACHTUNG ! ! CAUTION ! Kein Flugmotorenöl einfüllen. DO NOT use aviation grade oil...
  • Page 145 AQUILA AT01-100 Placards and Markings MAINTENANCE MANUAL Note: Placards illustrated are not to scale. Maneuvering Speed Manövergeschwindigkeit VA = 112 kts VA = 112 kts Detail- Lande- Landing ALT1 / BAT ALT1 / BAT licht Light Instrumenten- Fuel Kraftstoff- Instrument...
  • Page 146 AQUILA AT01-100 Placards and Markings MAINTENANCE MANUAL Note: Placards illustrated are not to scale. ELT und Feuerlöscher ELT and Fire-Extinguisher hinter dem Copilotensitz behind Copilot seat Detail- COM/NAV 1 Detail- COM/NAV 2 Detail- POSTLIGHTS POSTLIGHTS I-BRETT- PANEL BELEUCHTUNG INSTRUMENTE LIGHT...
  • Page 147 AQUILA AT01-100 MAINTENANCE MANUAL CHAPTER 12 SERVICING...
  • Page 148 AQUILA AT01-100 MAINTENANCE MANUAL...

  • Page 149: Replenishing - Description

    AQUILA AT01-100 Servicing MAINTENANCE MANUAL TABLE OF CONTENTS Chapter Section Title Subject Page SERVICING - GENERAL..................12-00-00 Introduction 12-00-00 General Description 12-00-00 REPLENISHING - DESCRIPTION..............12-10-00 General 12-10-00 Fuel 12-10-00 Engine Oil 12-10-00 Hydraulic Fluid 12-10-00 FUEL - SERVICING...................12-11-00 General 12-11-00 Safety and Maintenance Precautions...

  • Page 150: Battery - Servicing

    AQUILA AT01-100 Servicing MAINTENANCE MANUAL TABLE OF CONTENTS (Cont.) Chapter Section Title Subject Page BATTERY - SERVICING ...................12-17-00 General 12-17-00 Battery Servicing 12-17-00 SCHEDULED SERVICING - DESCRIPTION ..........12-20-00 General 12-20-00 LUBRICANTS - DESCRIPTION..............12-21-00 General 12-21-00 Service Notes 12-21-00 Definition of „As Needed“...
  • Page 151 AQUILA AT01-100 Servicing MAINTENANCE MANUAL SERVICING - GENERAL Introduction This chapter gives information on the replenishment of fluids and the lubrication of components. The chapter also contains instructions required to carry out scheduled servicing. General Description The chapter is designed to help authorized personnel to correctly service the aircraft.
  • Page 152 AQUILA AT01-100 MAINTENANCE MANUAL...
  • Page 153 29.0 Unusable Fuel 10,4 Fuel Specification The following fuel is approved for use in the AQUILA AT01-100. The minimum RON should be 95. EN 228 Super (Premium) EN 228 Super plus (Premium plus) AVGAS 100 LL (Grade ASTM-D910, blue color)
  • Page 154 AQUILA AT01-100 Servicing MAINTENANCE MANUAL Engine Oil Engine Oil Capacity Liters U.S. Quarts Engine oil capacity 3.17 Initial filling 3.70 Minimum 2.11 Oil Specification CAUTION: DO NOT USE AVIATION GRADE ENGINE OIL. IF MORE THAN 30% OF OPERATION HOURS HAVE BEEN FLOWN WITH LEADED FUEL (E.G.
  • Page 155 AQUILA AT01-100 Servicing MAINTENANCE MANUAL FUEL - SERVICING General Fuel Tanks (1) The aircraft is equipped with two integral wing fuel tanks. The fuel tanks are located inside each wing between the front and rear spars. Each fuel tank has a filler cap on the top wing surface.
  • Page 156 AQUILA AT01-100 Servicing MAINTENANCE MANUAL Maintenance Precautions (1) Use designated equipment for fuel loading / unloading to prevent contamination. (2) Only use approved anti-icing additive. (3) Blend fuel in accordance with prescribed procedures. (4) Document all fuel blending. Fueling and Defueling Fueling (1) Move aircraft to a designated fuel loading / fuel unloading area.
  • Page 157 AQUILA AT01-100 Servicing MAINTENANCE MANUAL ENGINE OIL - SERVICING General This chapter provides information for checking and changing engine oil. The oil filler cap of the oil tank is located on the right (starboard) side of the engine behind cylinder no. 3. It is accessible by opening the oil access plate on the upper cowling. The oil filler cap has a dipstick with min - max markings to check oil level.
  • Page 158 AQUILA AT01-100 Servicing MAINTENANCE MANUAL CAUTION: UNDER SEVERE OPERATING CONDITIONS, THE FREQUENCY OF OIL CHANGES MUST BE INCREASED REGARDLESS OF THE TYPE OF FUEL USED (MOGAS OR AVGAS). Oil Change Intervals (1) Under normal operating conditions, oil must be changed every 100 hours.
  • Page 159 AQUILA AT01-100 Servicing MAINTENANCE MANUAL INDUCTION AIR FILTER - SERVICING General The air filter in the air induction system keeps dust and dirt particles from entering the system. It is located in the air filter box on the left inside of lower cowling.
  • Page 160 AQUILA AT01-100 MAINTENANCE MANUAL Page 302 12-13-00 12.04.00...
  • Page 161 AQUILA AT01-100 Servicing MAINTENANCE MANUAL COOLING SYSTEM - SERVICING General The cooling system of the ROTAX 912 is designed for liquid cooling of the cylinder heads and ram air cooling of the cylinders. The cooling system of the cylinder heads is a closed circuit with an expansion tank.
  • Page 162 AQUILA AT01-100 Servicing MAINTENANCE MANUAL (2) Install attachment screw (stainless steel) along with a new sealing ring. Tighten to 10 Nm (90 in.lbs). (3) Refill freshly mixed coolant into expansion tank (highest point of the cooling system). Install radiator cap.
  • Page 163 AQUILA AT01-100 Servicing MAINTENANCE MANUAL BRAKE SYSTEM - SERVICING General Ground service for the brake system is limited to the replenishment of brake fluid. The brake fluid reservoir is located at the upper left firewall in the engine compartment. Replenishing...
  • Page 164 AQUILA AT01-100 MAINTENANCE MANUAL...
  • Page 165 AQUILA AT01-100 Servicing MAINTENANCE MANUAL TIRES - SERVICING General The landing gear is equipped with 5.00-5 tires. Depending on the wheel/brake system installed, either 10 PLY rated tubeless tires (Beringer wheels) or 6 PLY rated tube-type tires (Cleveland / Grove wheels) are mounted. Required tire pressure is:...
  • Page 166 AQUILA AT01-100 MAINTENANCE MANUAL...
  • Page 167 AQUILA AT01-100 Servicing MAINTENANCE MANUAL BATTERY - SERVICING General The battery should be serviced every 100 hours. In the case of heavy-duty operation or operation in cold regions, service intervals should be shorter. For procedures on how to remove and install the battery, refer to 24-30-00.
  • Page 168 AQUILA AT01-100 MAINTENANCE MANUAL...
  • Page 169 AQUILA AT01-100 Servicing MAINTENANCE MANUAL SCHEDULED SERVICING - DESCRIPTION General This section provides instructions necessary to carry out scheduled servicing, such as the periodic lubrication of aircraft components; external and internal cleaning. Service intervals are also provided. This section does not include lubrication procedures required to complete maintenance measures.
  • Page 170 AQUILA AT01-100 MAINTENANCE MANUAL...
  • Page 171 AQUILA AT01-100 Servicing MAINTENANCE MANUAL LUBRICANTS - DESCRIPTION General This section assists with the selection of proper lubricants used to maintain the aircraft. To ensure a long service life of the lubricated components, it is recommended to always pure and authorized lubricants.
  • Page 172 AQUILA AT01-100 Servicing MAINTENANCE MANUAL MIL-L-7870 Oil, general purpose VV-P-236 Technical petrolatum SS-G-659 Powdered graphite MIL-G-21164 Grease, molybdenum disulfide, for high and low temperatures VV-L-800 Light oil FDA CFR 178.3570 Thick silicone grease (-50°C to 200°C), (liquid grease in spray is not allowed)
  • Page 173 AQUILA AT01-100 Servicing MAINTENANCE MANUAL LUBRICATION - SERVICING General This section contains information on lubrication intervals for components or parts. Lubrication Chart Figure 201 shows the location of components or parts to be regularly lubricated. The following chart contains detailed information about the lubrication interval, the recommended lubricant and the dispensing equipment.
  • Page 174 AQUILA AT01-100 Servicing MAINTENANCE MANUAL Lubrication Chart Figure 301 (1) Page 302 12-22-00 24.10.13...
  • Page 175 AQUILA AT01-100 Servicing MAINTENANCE MANUAL ACCESS ZONE INDEX ITEM LUBE TYPE (APPL.) INTERVAL PLATE Cleveland / Grove: 721, Main wheel bearings GR (Hand) 500 h or GR (Hand) Nose wheel bearings annual Battery terminals PL (Hand) 100 h annual or...
  • Page 176 AQUILA AT01-100 MAINTENANCE MANUAL Page 304 12-22-00 12.04.00...
  • Page 177 AQUILA AT01-100 Servicing MAINTENANCE MANUAL AIRCRAFT EXTERIOR - CLEANING AND CARE General The good flight performance of the aircraft is achieved due to the modern construction and the use of specific materials. For efficient laminar flow, a clean surface is very important. Therefore, one should always keep the entire aircraft clean, but especially the leading edges of the wing.
  • Page 178 AQUILA AT01-100 Servicing MAINTENANCE MANUAL Cleaning and Care of the Aircraft Exterior Surfaces Procedure for cleaning the exterior surface of the aircraft (1) Park the aircraft in a hangar or in the shadows, avoid places with a lot of dust caused by wind or vehicles.
  • Page 179 AQUILA AT01-100 Servicing MAINTENANCE MANUAL Cleaning the Engine Safety and Maintenance Precautions (1) The engine should be cleaned during every 100-hour inspection. (2) Handle chemical cleaners and solvents with caution. Always read the manufacturer ’s instruction and follow them carefully (3) Cleaning should be performed in the open air or in a well ventilated hangar.
  • Page 180 AQUILA AT01-100 Servicing MAINTENANCE MANUAL CAUTION: DO NOT ROTATE THE PROPELLER CLOCKWISE. (11) Before starting the engine, rotate the propeller by hand no less than five complete revolutions. Cleaning and Care of the Propeller Clean propeller if necessary with any car wash solution or equivalent. This should be done at least every 50 hours.
  • Page 181 AQUILA AT01-100 Servicing MAINTENANCE MANUAL AIRCRAFT INTERIOR - CLEANING AND CARE General This section provides the information required to clean the aircraft interior properly. Several recommended types of cleaning agents for different materials and the relevant cleaning and care procedures are also described below.
  • Page 182 AQUILA AT01-100 Servicing MAINTENANCE MANUAL Blot up any liquid spilled promptly with an absorbent tissue or cloth. Press the blotting material firmly against the upholstery and hold for several seconds. Continue blotting until no more liquid is absorbed. Scrape off sticky materials cautiously with a dull knife, then clean area as required.
  • Page 183 AQUILA AT01-100 Servicing MAINTENANCE MANUAL UNSCHEDULED SERVICING General This section contains those instructions necessary to carry out unscheduled servicing for example: removing ice and snow from a parked aircraft. Removing Snow and Ice CAUTION: DO NOT REMOVE SNOW AND ICE FROM SURFACES USING SHARP-EDGED INSTRUMENTS.
  • Page 184 AQUILA AT01-100 MAINTENANCE MANUAL...
  • Page 185 AQUILA AT01-100 MAINTENANCE MANUAL CHAPTER 20 STANDARD PRACTICES - AIRFRAME...
  • Page 186 AQUILA AT01-100 MAINTENANCE MANUAL...

  • Page 187: Fastener Identification And Torque Data

    AQUILA AT01-100 Standard Practices MAINTENANCE MANUAL TABLE OF CONTENTS Chapter Section Title Subject Page STANDARD PRACTICES AIRFRAME - GENERAL........20-00-00 Introduction 20-00-00 General Description 20-00-00 FASTENER IDENTIFICATION AND TORQUE DATA .......20-10-00 General 20-10-00 Bolt Types 20-10-00 Torques 20-10-00 CONVERSION DATA..................20-11-00 General...
  • Page 188 AQUILA AT01-100 MAINTENANCE MANUAL...
  • Page 189 Maintenance procedures which are unique to a specific system / component / part are described in the corresponding chapter. As far as the maintenance of the AQUILA AT01-100 is concerned, there are no standard practices or relevant safety regulations, which require special knowledge other than that which is commonly expected for the maintenance of small aircraft.
  • Page 190 AQUILA AT01-100 MAINTENANCE MANUAL...
  • Page 191 AQUILA AT01-100 Standard Practices MAINTENANCE MANUAL FASTENER IDENTIFICATION AND TORQUE DATA General This section contains information concerning the identification of bolts, the correct usage of bolts and nuts and torque data. CAUTION: OBSERVE STANDARD OR TORQUE VALUES RECOMMENDED BY THE MANUFACTURER AND MAKE SURE THE RECOMMENDED SAFETYING DEVICE FOR EVERY FASTENER IS APPLIED.
  • Page 192 AQUILA AT01-100 Standard Practices MAINTENANCE MANUAL Torques NOTE: When a specific torque is not provided in the maintenance instructions contained in this maintenance manual, use the standard torque patterns shown in table 201 respectively the special torques in table 202.
  • Page 193 AQUILA AT01-100 Standard Practices MAINTENANCE MANUAL Table 201: Standard Torques DIN and LN specifications Torque values Torque values Thread size in.lbs 15.9 31.9 56.6 141.6 283.2 NOTE: Castellated nuts (DIN 935, 937) 531.1 should be finger tightened. Table 202: Special Torques Remarks Torque (Nm / in.lbs)
  • Page 194 AQUILA AT01-100 Standard Practices MAINTENANCE MANUAL 1. Variant - The adapter increases the effective length of the torque wrench. adapter drive centerline handgrip centerline wrench drive centerline T x L Y = apparent (indicated) torque formula: L + E T = actual (desired) torque...
  • Page 195 AQUILA AT01-100 Standard Practices MAINTENANCE MANUAL CONVERSION DATA General This chapter is designed to assist the operator with the conversion of commonly used measuring units found in this manual from Imperial, US and metric measuring systems. Conversion Factors Subsequent conversion factors of units of measurement are given from the metric system to the US / Imperial systems and vice versa.
  • Page 196 AQUILA AT01-100 Standard Practices MAINTENANCE MANUAL (3) Cubic measures Table 3 - Conversion of Cubic Measures Unit m³ Cu. in. Cu. ft. Imp.-Gallons U.S.-Gallons 1 Liter 0,001 61,03 0,05332 0,22 0,2642 1 m³ 1000 61023 35,315 219,97 264,175 1 cu. in.
  • Page 197 AQUILA AT01-100 Standard Practices MAINTENANCE MANUAL Equivalents for Standard Values For conversion data to convert standard drill sizes to inch and millimeter equivalents refer to figure 1. Drill Drill Drill 0,34 0,0135 1,85 0,0730 4,09 0,1610 0,37 0,0145 1,93 0,0760...
  • Page 198 AQUILA AT01-100 MAINTENANCE MANUAL...
  • Page 199 AQUILA AT01-100 MAINTENANCE MANUAL CHAPTER 21 VENTILATION AND HEATING...
  • Page 200 AQUILA AT01-100 MAINTENANCE MANUAL...

  • Page 201: Heating - Maintenance

    AQUILA AT01-100 Ventilation and Heating MAINTENANCE MANUAL TABLE OF CONTENTS Chapter Section Title Subject Page VENTILATION AND HEATING - GENERAL..........21-00-00 Introduction 21-00-00 General Description 21-00-00 FRESH AIR DISTRIBUTION - MAINTENANCE .........21-20-00 General 21-20-00 Eyeball Ventilator Removal/Installation 21-20-00 Heat Relief Valve Removal/Installation 21-20-00 HEATING - MAINTENANCE .................21-40-00...
  • Page 202 AQUILA AT01-100 MAINTENANCE MANUAL...
  • Page 203 AQUILA AT01-100 Ventilation and Heating MAINTENANCE MANUAL VENTILATION AND HEATING - GENERAL Introduction This chapter describes those systems and components used to heat and ventilate the cabin. Fresh air for ventilation (outside air temperature) and heated fresh air for heating and windshield defrosting is supplied to the cabin.
  • Page 204 AQUILA AT01-100 MAINTENANCE MANUAL...
  • Page 205 AQUILA AT01-100 Ventilation and Heating MAINTENANCE MANUAL FRESH AIR DISTRIBUTION - MAINTENANCE General Maintenance is limited to the removal and installation of the components. Eyeball Ventilator Removal/Installation (Ref. Fig. 201) NOTE: Removal/installation of the left and right eyeball ventilator is analogous.
  • Page 206 AQUILA AT01-100 Ventilation and Heating MAINTENANCE MANUAL flexible air duct to air inlet hose clamp eyeball ventilator Detail- Eyeball Ventilator Installation Figure 201 Page 202 21-20-00 30.04.13...
  • Page 207 AQUILA AT01-100 Ventilation and Heating MAINTENANCE MANUAL cabin heat control knob flexible air duct to windscreen heating manifold Detail- heated air distributor actuating lever control cable to relief valve flexible air duct to heat exchanger Detail- heat relief valve flexible air duct...
  • Page 208 AQUILA AT01-100 MAINTENANCE MANUAL...
  • Page 209 AQUILA AT01-100 Ventilation and Heating MAINTENANCE MANUAL HEATING - MAINTENANCE General Fresh air is heated when it passes through the heat exchanger at the engine. The heat exchanger consists of a shroud, which is set around the exhaust muffler. Flexible ducts are connected to the heat exchanger through which the air enters and exits.
  • Page 210 AQUILA AT01-100 MAINTENANCE MANUAL...
  • Page 211 AQUILA AT01-100 MAINTENANCE MANUAL CHAPTER 23 COMMUNICATIONS...
  • Page 212 AQUILA AT01-100 MAINTENANCE MANUAL...
  • Page 213 AQUILA AT01-100 Communications MAINTENANCE MANUAL TABLE OF CONTENTS Chapter Section Title Subject Page Effectivity COMMUNICATIONS - GENERAL ............23-00-00 Introduction 23-00-00 General Description 23-00-00 SPEECH COMMUNICATION - DESCRIPTION ......23-10-00 GNS 430W / GTN 650 Introduction 23-10-00 GNS 430W / GTN 650...
  • Page 214 AQUILA AT01-100 MAINTENANCE MANUAL...
  • Page 215 AQUILA AT01-100 Communications MAINTENANCE MANUAL COMMUNICATIONS - GENERAL Introduction This chapter describes and provides maintenance instructions for components and systems used to communicate between occupants of the aircraft and between the aircraft and other aircraft or ground stations. Technical publications available from the manufacturer or vendor of the various components and systems, which are not covered in this manual, must be utilized as necessary for the maintenance of those components and systems.
  • Page 216 AQUILA AT01-100 MAINTENANCE MANUAL...
  • Page 217 AQUILA AT01-100 Communications MAINTENANCE MANUAL SPEECH COMMUNICATION – DESCRIPTION Introduction This section covers the portion of the system which utilizes voice communication from air-to-air or air-to-ground installations. It includes the VHF speech communications portion of the NAV/COM radio Garmin GNS 430W or GTN 650.
  • Page 218 AQUILA AT01-100 Communications MAINTENANCE MANUAL GNS 430 unit jackscrew access hole GTN 650 unit jackscrew access hole GNS 430, GTN 650 Front View Figure 1 EFFECTIVITY Page 2 Aircraft equipped with Garmin 23-10-00 GNS 430W / GTN 650 30.04.13...
  • Page 219 AQUILA AT01-100 Communications MAINTENANCE MANUAL SPEECH COMMUNICATION – MAINTENANCE General The scope of maintenance is limited to the removal and installation of the components. For removal and installation procedures for the GNS 430W / GTN 650 GPS antenna, refer to 34-40-00.
  • Page 220 AQUILA AT01-100 Communications MAINTENANCE MANUAL Install Antenna CAUTION: WIRING MUST NOT INTERFERE WITH THE OPERATION OF MOVEABLE AIRCRAFT COMPONENTS. (1) Position antenna with gasket to fuselage. (2) Install mounting plate from inside the fuselage. (3) Secure antenna base to fuselage using screws, nuts and washers. Reinstall ground wire.
  • Page 221 AQUILA AT01-100 Communications MAINTENANCE MANUAL SPEECH COMMUNICATION - DESCRIPTION Introduction This section covers the portion of the system which utilizes voice communication from air-to-air or air-to-ground installations. It includes the VHF speech communications portion of the NAV/COM radio Garmin SL30 or SL40.
  • Page 222 AQUILA AT01-100 Communications MAINTENANCE MANUAL transmit function to/from annunciator annunciators indication active standby standby Graphic large outer frequency symbol frequency Bearing photocell knob SL30 118.00 s136.00 PULL SQUELCH COM NAV power / frequency ident enter small inner volume / flip/flop...
  • Page 223 AQUILA AT01-100 Communications MAINTENANCE MANUAL SPEECH COMMUNICATION – MAINTENANCE General The scope of maintenance is limited to the removal and installation of system components. For further information, refer to Garmin SL30 NAV/COM installation manual, P/N 560-0404-XX, latest revision, or Garmin SL40 NAV/COM installation manual, P/N 560-0956-XX, latest revision, as well as any other appropriate manufacturer publications.
  • Page 224 AQUILA AT01-100 Communications MAINTENANCE MANUAL Install Antenna CAUTION: WIRING MUST NOT INTERFERE WITH THE OPERATION OF MOVEABLE AIRCRAFT COMPONENTS. (1) Position antenna with gasket to fuselage. (2) Install mounting plate from inside the fuselage. (3) Secure antenna base to fuselage using screws, nuts and washers. Reinstall ground wire.
  • Page 225 AQUILA AT01-100 Communications MAINTENANCE MANUAL AUDIO INTEGRATING - MAINTENANCE General This section covers that portion of the system which controls the output of the communication and navigation receivers to crew member headphones and speakers, and the output of the crew member microphones to the communication transmitters.
  • Page 226 AQUILA AT01-100 Communications MAINTENANCE MANUAL Audio Control Unit Removal/Installation Remove Audio Control Unit (1) Ensure electrical power to aircraft is OFF. (2) Disconnect the plug at the back of the audio control unit. (3) Remove control knob caps o n the front panel of the audio control unit (4) Loosen and remove nuts attaching audio control unit on the left side to mounting bracket.
  • Page 227 AQUILA AT01-100 Communications MAINTENANCE MANUAL AUDIO INTEGRATING - MAINTENANCE General This section covers that portion of the system which controls the output of the communication and navigation receivers to crew member headphones and speakers, and the output of the crew member microphones to the communication transmitters.
  • Page 228 AQUILA AT01-100 Communications MAINTENANCE MANUAL (3) Turn the wrench clockwise until the unit is secured in the rack. Continue turning until tight, but do not over-tighten. (4) Conduct a functional test of the unit. MKR/BCN A O M NAV1 NAV2...
  • Page 229 AQUILA AT01-100 MAINTENANCE MANUAL CHAPTER 24 ELECTRICAL POWER...
  • Page 230 AQUILA AT01-100 MAINTENANCE MANUAL...

  • Page 231: Alternator System - Description

    AQUILA AT01-100 Electrical Power MAINTENANCE MANUAL TABLE OF CONTENTS Chapter Section Title Subject Page Effectivity ELECTRICAL POWER - GENERAL ...............24-00-00 Introduction 24-00-00 General Description 24-00-00 ELECTRICAL POWER - TROUBLESHOOTING.........24-00-00 Troubleshooting 24-00-00 ALTERNATOR SYSTEM - DESCRIPTION ............24-20-00 Introduction 24-20-00 Description and Operation 24-20-00 ALTERNATOR SYSTEM - MAINTENANCE ..........24-20-00...

  • Page 232: Electrical System Wiring - Maintenance

    AQUILA AT01-100 Electrical Power MAINTENANCE MANUAL TABLE OF CONTENTS (Cont.) Chapter Section Title Subject Page Effectivity ELECTRICAL SYSTEM WIRING - MAINTENANCE........24-97-00 General 24-97-00 Splicing 24-97-00 Wire Replacement 24-97-00 Page 2 24 - TOC 30.04.13...
  • Page 233 AQUILA AT01-100 Electrical Power MAINTENANCE MANUAL ELECTRICAL POWER - GENERAL Introduction This chapter describes the units and components, which generate, control and supply AC and DC electrical power for other systems. General Description The aircraft is equipped with a 12V DC electrical system. It is powered by a belt driven 600W alternator and a 12V battery which is installed on the front-right side of the firewall.
  • Page 234 AQUILA AT01-100 MAINTENANCE MANUAL...
  • Page 235 AQUILA AT01-100 Electrical Power MAINTENANCE MANUAL ELECTRICAL POWER - TROUBLESHOOTING Troubleshooting If a power problem or a complete blackout occurs, first check all connections to the components and the circuit breakers. Troubleshooting Chart: TROUBLE POSSIBLE CAUSE REMEDY No alternator ALT 1 switch OFF Turn switch ON.
  • Page 236 AQUILA AT01-100 Electrical Power MAINTENANCE MANUAL If a voltage reading is obtained, replace battery relay. Defective wiring or electrical Step 5: connection between battery With switch BAT in ON position, relay and starter relay. measure voltage between starter side relay terminal, and starter relay.
  • Page 237 AQUILA AT01-100 Electrical Power MAINTENANCE MANUAL ALTERNATOR SYSTEM - DESCRIPTION Introduction The alternator system supplies the electrical equipment with electrical power when the engine is running and is the main current source in the power supply design. The alternator system consists of the following components:...
  • Page 238 AQUILA AT01-100 Electrical Power MAINTENANCE MANUAL warning light “ALT 1” circuit breaker “Warning Lights” external alternator circuit breaker “ALT 1” circuit breaker “ALT 1 Excitation” ALT 1 External Alternator System (Schematic) Figure 1 warning light “ALT 2” ROTAX circuit breaker internal alternator “Warning Lights”...
  • Page 239 AQUILA AT01-100 Electrical Power MAINTENANCE MANUAL ALTERNATOR SYSTEM - MAINTENANCE General Maintenance is limited to the removal and installation of the (external) alternator, drive belt and rectifier-regulator unit (only Night-VFR equipped aircraft). Refer to the appropriate ROTAX publications for maintenance procedures on the internal alternator.
  • Page 240 AQUILA AT01-100 Electrical Power MAINTENANCE MANUAL Detail- External Alternator Installation Figure 201 Page 202 24-20-00 30.04.13...
  • Page 241 AQUILA AT01-100 Electrical Power MAINTENANCE MANUAL (5) Slip drive belt off alternator pulley. (6) Remove propeller (refer to 61-10-00). (7) Remove alternator drive belt. Install Alternator Drive Belt (1) Install alternator drive belt around drive pulley. (2) Install propeller (refer to 61-10-00).
  • Page 242 AQUILA AT01-100 Electrical Power MAINTENANCE MANUAL nut M8 (2ea) rectifier-regulator unit Detail- “Nordlock” washer (4ea) bolt M8x20 (2ea) Rectifier-Regulator Unit Installation ( Night-VFR equipped aircraft only) Figure 202 Page 204 24-20-00 30.04.13...
  • Page 243 AQUILA AT01-100 Electrical Power MAINTENANCE MANUAL BATTERY SYSTEM - DESCRIPTION Introduction The battery system supplies power to the electrical equipment if the alternator fails. It represents the auxiliary power source in supply design. The battery system consists of the following components:...
  • Page 244 AQUILA AT01-100 Electrical Power MAINTENANCE MANUAL BATTERY SYSTEM (SCHEMATIC) to aircraft bus bar battery AMPS ALT 1 ammeter DC VOLTS voltmeter to clock (optional) firewall battery- relay battery Battery System (Schematic) Figure 1 Page 2 24-30-00 30.04.13...
  • Page 245 AQUILA AT01-100 Electrical Power MAINTENANCE MANUAL BATTERY SYSTEM - MAINTENANCE General CAUTION: ALWAYS DISCONNECT THE BATTERY BEFORE DOING ANY MAINTENANCE ON THE ELECTRICAL SYSTEM. DISCONNECT THE NEGATIVE LEAD FIRST. RECONNECT THE NEGATIVE LEAD LAST. SECURE THE BATTERY LEADS FROM ACCIDENTAL CONNECTION DURING MAINTENANCE WORKS.
  • Page 246 AQUILA AT01-100 MAINTENANCE MANUAL...
  • Page 247 AQUILA AT01-100 Electrical Power MAINTENANCE MANUAL EXTERNAL POWER - MAINTENANCE General This section covers that portion of the system in the aircraft which connects external electrical power to the aircraft's electrical systems. It includes items such as external power receptacle and relays.
  • Page 248 AQUILA AT01-100 Electrical Power MAINTENANCE MANUAL 1,4-2 Nm 12-18 in.lbs external power relay 5-6 Nm 44-55 in.lbs Detail- ground 4 Pl. power 8212A04N 8212B04 Signal Detail- External Power Receptacle Installation 8212A20 Figure 201 EFFECTIVITY Page 202 24-40-00 Aircraft equipped with an external power receptacle...
  • Page 249 AQUILA AT01-100 Electrical Power MAINTENANCE MANUAL Install External Power Relay (1) Position and secure external power relay to engine mount using bolts, washers and nuts. (2) Identify and reconnect wires to external power relay. CAUTION: DO NOT REMOVE INNER NUT WHEN ASSEMBLING. USE WRENCH TO HOLD INNER NUT IN PLACE WHEN APPLYING OUTER NUT.
  • Page 250 AQUILA AT01-100 MAINTENANCE MANUAL...
  • Page 251 AQUILA AT01-100 Electrical Power MAINTENANCE MANUAL ELECTRICAL LOAD DISTRIBUTION - DESCRIPTION Introduction Distribution of electrical power supplied by the external and optional the internal alternator and the battery is accomplished by bus bars. The bus architecture allows power to be routed to the essential circuitry if any one of the main power sources fails.
  • Page 252 AQUILA AT01-100 MAINTENANCE MANUAL...
  • Page 253 AQUILA AT01-100 Electrical Power MAINTENANCE MANUAL CIRCUIT BREAKER - MAINTENANCE General The circuit breaker panel is equipped with circuit breakers of the push to reset type. " " One terminal of each switch/breaker is directly connected to the appropriate bus bar, the other is wired to the component/system it protects.
  • Page 254 AQUILA AT01-100 Electrical Power MAINTENANCE MANUAL Table 201: Circuit Breaker Current Ratings (Cont.) Current Rating Circuit Breaker Effectivity 7.5A G500 Trim Actuator AHRS G500 G500 12V Receptacle Audio GMA 340, GMA 350 GPS Map 69X, Aera 79X GTX 328, GTX 330...
  • Page 255 AQUILA AT01-100 Electrical Power MAINTENANCE MANUAL ELECTRICAL SYSTEM WIRING - MAINTENANCE General Repairs of the electrical system wiring are limited to the replacement and splicing of electrical wires. In general all repairs have to be carried out by certified repair stations or properly certified and trained persons.
  • Page 256 AQUILA AT01-100 MAINTENANCE MANUAL...
  • Page 257 AQUILA AT01-100 MAINTENANCE MANUAL CHAPTER 25 EQUIPMENT / FURNISHINGS...
  • Page 258 AQUILA AT01-100 MAINTENANCE MANUAL...

  • Page 259: Restraint System - Maintenance

    AQUILA AT01-100 Equipment / Furnishings MAINTENANCE MANUAL TABLE OF CONTENTS Chapter Section Title Subject Page Effectivity EQUIPMENT / FURNISHINGS - GENERAL..........25-00-00 Introduction 25-00-00 General Description 25-00-00 SEATS - MAINTENANCE ................25-10-00 General 25-10-00 Seat Removal/Installation 25-10-00 Gas Spring Strut Assembly Removal/Installation 25-10-00 RESTRAINT SYSTEM - MAINTENANCE.............25-11-00...
  • Page 260 AQUILA AT01-100 Equipment / Furnishings MAINTENANCE MANUAL Page 02 25 - TOC 15.09.09...
  • Page 261 AQUILA AT01-100 Equipment / Furnishings MAINTENANCE MANUAL EQUIPMENT / FURNISHINGS - GENERAL Introduction This chapter describes removable items of equipment and interior furnishings contained in the cabin and baggage compartment. General Description The seats can be adjusted back and forward. The restraint system of each seat is attached to the fuselage structure.
  • Page 262 AQUILA AT01-100 MAINTENANCE MANUAL...
  • Page 263 AQUILA AT01-100 Equipment / Furnishings MAINTENANCE MANUAL SEATS - MAINTENANCE General The seats are made from fiber composite materials and equipped with integrated safety head rests and removable, hard-wearing seat cushions. An infinitely adjustable seat meets the requirements of a wide range of pilots. The seat track is angled upward for forward travel so that shorter people will be positioned slightly higher as they adjust the seat forward.
  • Page 264 AQUILA AT01-100 Equipment / Furnishings MAINTENANCE MANUAL Detail- Seat Installation Figure 201 Page 202 25-10-00 30.04.13...
  • Page 265 AQUILA AT01-100 Equipment / Furnishings MAINTENANCE MANUAL Gas Spring Strut Assembly Removal/Installation Remove Gas Spring Strut Assembly (1) Remove seat cushion. Remove control knob at the remote control of the gas spring locking valve and then the retaining nut which secures the remote control to attachment bracket.
  • Page 266 AQUILA AT01-100 MAINTENANCE MANUAL...
  • Page 267 AQUILA AT01-100 Equipment / Furnishings MAINTENANCE MANUAL RESTRAINT SYSTEM - MAINTENANCE General The seats are equipped with automatic, four point seat belts/shoulder harness assemblies. A central rotary buckle is used to fasten the seat belts/shoulder harness. The design incorporates an inertia reel system for the shoulder portion.
  • Page 268 AQUILA AT01-100 MAINTENANCE MANUAL...
  • Page 269 AQUILA AT01-100 MAINTENANCE MANUAL CABIN INTERIOR - MAINTENANCE General The panels, coverings and carpets can be removed for maintenance purposes. For cabin interior cleaning and care refer to chapter 12, section "Cabin interior - Cleaning and Care". Panels, Coverings and Carpets Removal and Installation...
  • Page 270 AQUILA AT01-100 Equipment / Furnishings MAINTENANCE MANUAL 211 BB 211 AB 211 FT 211 FB remove 211 FT 211 EC remove 211 FT remove 211 FB 211 GT 211 CC 211 DR remove 211 BB see 211 DL Detail- 211 DL...
  • Page 271 AQUILA AT01-100 Equipment / Furnishings MAINTENANCE MANUAL 211 IR 211 IC remove 211 IL remove 211 IR 211 IL 211 KC Detail- 211 JB Panels and Covers Figure 201 (2) Page 203 25-12-00 30.04.13...
  • Page 272 AQUILA AT01-100 Equipment / Furnishings MAINTENANCE MANUAL...
  • Page 273 AQUILA AT01-100 Equipment / Furnishings MAINTENANCE MANUAL CARGO TIE-DOWNS - MAINTENANCE General Eight cargo tie-down rings are provided to secure baggage. Baggage nets may be used to hold baggage in position during flight. The cargo tie-down rings are secured directly to the floorboard by nutplates or they secure the floorboard to the supports.
  • Page 274 AQUILA AT01-100 MAINTENANCE MANUAL...
  • Page 275 AQUILA AT01-100 Equipment / Furnishings MAINTENANCE MANUAL EMERGENCY EQUIPMENT - DESCRIPTION Introduction This section describes those items of equipment carried for use in emergencies and includes the emergency locator transmitter (ELT) and a fire extinguisher. As standard the aircraft is equipped with a Kannad 406 AF Compact ELT. Due to the multiplicity of equipment coming onto the market a different ELT may be installed.
  • Page 276 AQUILA AT01-100 Equipment / Furnishings MAINTENANCE MANUAL Detail- ELT remote control panel / indicator (RCPI) Detail- Detail- ELT antenna BNC connector red LED main switch RC connector Detail- mounting bracket Velcro strap ELT Main Components (Kannad 406 AF Compact) Figure 1...
  • Page 277 AQUILA AT01-100 Equipment / Furnishings MAINTENANCE MANUAL EMERGENCY LOCATER TRANSMITTER - MAINTENANCE General This section covers removal and installation procedures of ELT components as well necessary periodic maintenance. Consider all publications / requirements of the appropriate national authority regarding ELT operation and maintenance.
  • Page 278 AQUILA AT01-100 Equipment / Furnishings MAINTENANCE MANUAL Install ELT Antenna (1) Position antenna with gasket on topside of fuselage. (2) From inside the fuselage install mounting plate. (3) Secure antenna base to topside of fuselage using screws, nuts and washers. Reinstall ground wire.
  • Page 279 AQUILA AT01-100 Equipment / Furnishings MAINTENANCE MANUAL FIRE EXTINGUISHER - MAINTENANCE General The aircraft is equipped with a liquefied-gas type fire extinguisher AIR TOTAL HAL 1 mounted in a quick-release bracket attached to the floor board of the baggage compartment, behind the right seat.
  • Page 280 AQUILA AT01-100 MAINTENANCE MANUAL...
  • Page 281 AQUILA AT01-100 Equipment / Furnishings MAINTENANCE MANUAL FIRE EXTINGUISHER - MAINTENANCE General The aircraft is equipped with a liquefied-gas type fire extinguisher H3R Aviation RT A400 mounted in a quick-release bracket attached to the floor board of the baggage compartment, behind the right seat.
  • Page 282 AQUILA AT01-100 Equipment / Furnishings MAINTENANCE MANUAL Fire Extinguisher Removal/Installation Remove Fire Extinguisher (1) Release quick-release clamp. (2) Remove fire extinguisher from bracket assembly. Install Fire Extinguisher (1) Position fire extinguisher in bracket assembly. (2) Secure with quick release clamp.
  • Page 283 AQUILA AT01-100 MAINTENANCE MANUAL CHAPTER 27 FLIGHT CONTROLS...
  • Page 284 AQUILA AT01-100 MAINTENANCE MANUAL...

  • Page 285: Aileron Control System - Description

    AQUILA AT01-100 Flight Controls MAINTENANCE MANUAL TABLE OF CONTENTS Chapter Section Title Subject Page FLIGHT CONTROLS - GENERAL ..............27-00-00 Introduction 27-00-00 General Description 27-00-00 AILERON CONTROL SYSTEM - DESCRIPTION........27-10-00 Introduction 27-10-00 Description and Operation 27-10-00 AILERON CONTROL SYSTEM - MAINTENANCE ........27-10-00...
  • Page 286 AQUILA AT01-100 Flight Controls MAINTENANCE MANUAL TABLE OF CONTENTS (Cont.) Chapter Section Title Subject Page Inspection/Check 27-30-00 Adjustment/Test 27-30-00 ELEVATOR TRIM CONTROL - DESCRIPTION..........27-31-00 Introduction 27-31-00 Description and Operation 27-31-00 ELEVATOR TRIM CONTROL - MAINTENANCE ........27-31-00 General 27-31-00 Trim Actuator Removal/Installation...
  • Page 287 AQUILA AT01-100 Flight Controls MAINTENANCE MANUAL FLIGHT CONTROLS - GENERAL Introduction This chapter contains information about the flight controls used to manually control the aircraft in flight. It also includes functional and maintenance information about the flaps. General Description The conventionally designed flight control system is divided into aileron control, rudder control, elevator control and the wing flaps system.
  • Page 288 AQUILA AT01-100 MAINTENANCE MANUAL...
  • Page 289 AQUILA AT01-100 Flight Controls MAINTENANCE MANUAL AILERON CONTROL SYSTEM - DESCRIPTION Introduction This section describes that portion of the flight control system which controls the position and movement of the ailerons. The rigging procedure for the aileron control system is also provided.
  • Page 290 AQUILA AT01-100 Flight Controls MAINTENANCE MANUAL pushrod 4 pushrod 3 pushrod 2 pushrod 1 Aileron Control System Design and Function Figure 1 Page 2 27-10-00 30.04.13...
  • Page 291 AQUILA AT01-100 Flight Controls MAINTENANCE MANUAL AILERON CONTROL SYSTEM - MAINTENANCE General For a breakdown of components, refer to figure 201, 202 and 203. WARNING: WHEN INSTALLING COMPONENTS OF CONTROL SYSTEM, NEW SELF-LOCKING NUTS SHOULD ALWAYS BE USED. NEVER USE A SELF-LOCKING NUT MORE THAN ONCE.
  • Page 292 AQUILA AT01-100 Flight Controls MAINTENANCE MANUAL left side shown (right side analogous) Detail- Detail- Component Installation Figure 201 Page 202 27-10-00 30.04.13...
  • Page 293 AQUILA AT01-100 Flight Controls MAINTENANCE MANUAL Install Front Bellcrank (1) Position front bellcrank between brackets and secure using bolt, washer and nut. (2) Connect pushrods to front bellcrank. (3) Perform aileron control system inspection/check ( refer to “Inspection/Check” below (4) Install access plate 210 AB (refer to 06-30-00).
  • Page 294 AQUILA AT01-100 Flight Controls MAINTENANCE MANUAL left side shown (right side analogous) Detail- Detail- Component Installation Figure 202 Page 204 27-10-00 30.04.13...

  • Page 295: Inspection/Check

    AQUILA AT01-100 Flight Controls MAINTENANCE MANUAL Pushrod 4 Removal/Installation Remove Pushrod 4 (1) Remove wing (refer to 57-10-00). (2) Open access panel 520 (620) AB (refer to 06-30-00). (3) Disconnect pushrod at aileron bellcrank. (4) Remove rod end bearing. (5) Cautiously withdraw pushrod from wing.
  • Page 296 AQUILA AT01-100 Flight Controls MAINTENANCE MANUAL Detail- left side shown (right side analogous) Detail- Aileron Bellcrank Installation Figure 203 Page 206 27-10-00 30.04.13...

  • Page 297: Adjustment/Test

    AQUILA AT01-100 Flight Controls MAINTENANCE MANUAL (2) Verify minimum rod end thread engagement of 8 mm (0.312 in.). (3) Verify ailerons can be moved smoothly through the full travel. No grinding is audible. (4) Check ailerons for correct travel using an inclinometer. If necessary perform aileron control system adjustment/test ( refer to “Adjustment/Test”...
  • Page 298 AQUILA AT01-100 MAINTENANCE MANUAL...
  • Page 299 AQUILA AT01-100 Flight Controls MAINTENANCE MANUAL RUDDER CONTROL SYSTEM - DESCRIPTION Introduction This section describes that portion of the flight control system which controls the position and movement of the rudder. The rigging procedure for the rudder control system is also provided.
  • Page 300 AQUILA AT01-100 Flight Controls MAINTENANCE MANUAL Rudder Control Design And Function Figure 1 Page 2 27-20-00 30.04.13...
  • Page 301 AQUILA AT01-100 Flight Controls MAINTENANCE MANUAL RUDDER CONTROL SYSTEM - MAINTENANCE General For a breakdown of the components, refer to figure 201 and 202. WARNING: WHEN INSTALLING COMPONENTS OF THE CONTROL SYSTEM, NEW SELF- LOCKING NUTS SHOULD ALWAYS BE USED. NEVER USE A SELF-LOCKING NUT MORE THAN ONCE.
  • Page 302 AQUILA AT01-100 Flight Controls MAINTENANCE MANUAL Detail- Rudder Control Installation Figure 201 Page 202 27-20-00 30.04.13...
  • Page 303 AQUILA AT01-100 Flight Controls MAINTENANCE MANUAL (2) Reinstall lower half of middle bearing block. (3) Reconnect steering tubes to rudder bars. (4) Reconnect master cylinders to the rudder pedal assembly. (5) Reconnect control cables to rudder control actuator arms and re-rig system (refer to “Adjustment/Test“...
  • Page 304 AQUILA AT01-100 Flight Controls MAINTENANCE MANUAL Detail- Rudder Pedal / Master Cylinder Installation Figure 202 Page 204 27-20-00 30.04.13...
  • Page 305 AQUILA AT01-100 Flight Controls MAINTENANCE MANUAL (3) Verify rudder can be moved smoothly through full travel. No grinding is audible. (4) Check rudder for correct travel using an inclinometer, if necessary perform rudder control system adjustment/test (refer to “Adjustment/Test” below).
  • Page 306 AQUILA AT01-100 MAINTENANCE MANUAL...
  • Page 307 AQUILA AT01-100 Flight Controls MAINTENANCE MANUAL ELEVATOR CONTROL SYSTEM - DESCRIPTION Introduction This section describes that portion of the flight control system which controls the position and movement of the elevator. The rigging procedure for the elevator control system is also provided.
  • Page 308 AQUILA AT01-100 Flight Controls MAINTENANCE MANUAL pushrod 2 pushrod 1 Elevator Control System Design And Function Figure 1 Page 2 27-30-00 30.04.13...
  • Page 309 AQUILA AT01-100 Flight Controls MAINTENANCE MANUAL ELEVATOR CONTROL SYSTEM - MAINTENANCE General For a breakdown of the components, refer to figure 201 and 202. WARNING: WHEN INSTALLING COMPONENTS OF THE CONTROL SYSTEM NEW SELF- LOCKING NUTS SHOULD ALWAYS BE USED. NEVER USE A SELF-LOCKING NUT MORE THAN ONCE.
  • Page 310 AQUILA AT01-100 Flight Controls MAINTENANCE MANUAL Detail- Fuselage structure omitted for clarity. left side shown (right side analogous) Detail- Component Installation Figure 201 Page 202 27-30-00 30.04.13...
  • Page 311 AQUILA AT01-100 Flight Controls MAINTENANCE MANUAL (4) Check elevator control system and elevator trim system for proper operation and rig if necessary (refer to 27-30-00 and 27-31-00). (5) Install baggage compartment floor panel (refer to 25-12-00). (6) Install seats (refer to 25-10-00).
  • Page 312 AQUILA AT01-100 Flight Controls MAINTENANCE MANUAL Fuselage structure omitted for clarity. Detail- Detail- Component Installation Figure 202 Page 204 27-30-00 30.04.13...
  • Page 313 AQUILA AT01-100 Flight Controls MAINTENANCE MANUAL Adjustment/Test Adjustment/Test (1) Remove baggage compartment floor panel (refer to 25-12-00). (2) Remove access plate 211 HL and HR (refer to 25-12-00). (3) Lock elevator bellcrank in neutral position in a suitable manner (the line between pushrod attach points on bellcrank is perpendicular to the pushrod 2).
  • Page 314 AQUILA AT01-100 MAINTENANCE MANUAL...

  • Page 315: Elevator Trim Control - Description

    AQUILA AT01-100 Flight Controls MAINTENANCE MANUAL ELEVATOR TRIM CONTROL - DESCRIPTION Introduction The aircraft isequipped with an electrical spring-force trim system. An electrical trim actuator changes the pre-load of a pair of springs that applies a defined force to the elevator pushrod.
  • Page 316 AQUILA AT01-100 Flight Controls MAINTENANCE MANUAL Detail- elevator pushrod trim position sensor Fuselage structure omitted for clarity. trim actuator Elevator Trim System Design And Function Figure 1 Page 2 27-31-00 30.04.13...

  • Page 317: Elevator Trim Control - Maintenance

    AQUILA AT01-100 Flight Controls MAINTENANCE MANUAL ELEVATOR TRIM CONTROL - MAINTENANCE General For a breakdown of the components, refer to figure 201. Trim Actuator Removal/Installation Remove Trim Actuator (1) Set the elevator trim system to neutral. (2) Place the BAT switch in OFF position.
  • Page 318 AQUILA AT01-100 Flight Controls MAINTENANCE MANUAL Detail- Fuselage structure Fuselage structure omitted for clarity. omitted for clarity. Elevator Trim System Installation Figure 201 Page 202 27-31-00 30.04.13...

  • Page 319: Flap Control System - Description

    AQUILA AT01-100 Flight Controls MAINTENANCE MANUAL FLAP CONTROL SYSTEM - DESCRIPTION Introduction This section describes that portion of the flight control system which controls the position and movement of the flaps. The rigging procedure forthe flap control system is also provided.
  • Page 320 AQUILA AT01-100 Flight Controls MAINTENANCE MANUAL flap actuator torque tube Flap Control System Design and Function Figure 1 Page 2 27-50-00 30.04.13...

  • Page 321: Flap Control System - Maintenance

    AQUILA AT01-100 Flight Controls MAINTENANCE MANUAL FLAP CONTROL SYSTEM - MAINTENANCE General This section provides instructions for removal and installation of components and instruction for flap control system rigging. For a breakdown of the components, refer to figure 201, 202, 203, and 204.
  • Page 322 AQUILA AT01-100 Flight Controls MAINTENANCE MANUAL Detail- Fuselage structure omitted for clarity. Flap Control System Installation Figure 201 Page 202 27-50-00 30.04.13...

  • Page 323: Flap Pushrod Removal/Installation

    AQUILA AT01-100 Flight Controls MAINTENANCE MANUAL (2) Secure both halves to pivot bracket using bolt, washer and nut. (3) Install spacer and bolt, washer and nut connecting halves. (4) Connect torque tube assembly to flap actuator pushrod. (5) Perform flap control system inspection/check and rig system, if necessary (refer to “Inspection/Check”...
  • Page 324 AQUILA AT01-100 Flight Controls MAINTENANCE MANUAL Detail- Wing structure omitted for clarity. Flap Control System Installation Figure 201 Page 204 27-50-00 30.04.13...

  • Page 325: Adjustment/Test

    06-10-00. (e) Repeat check on right flap. NOTE: If the results of inspection do not fall within the tolerance specified in 06-10-00, contact AQUILA Aviation GmbH for disposition. (4) Install all items removed for access. Adjustment/Test Adjustment/Test (1) Remove access plate 210 AB (refer to 06-30-00).
  • Page 326 AQUILA AT01-100 MAINTENANCE MANUAL...
  • Page 327 AQUILA AT01-100 MAINTENANCE MANUAL CHAPTER 28 FUEL...
  • Page 328 AQUILA AT01-100 MAINTENANCE MANUAL...
  • Page 329 AQUILA AT01-100 Fuel MAINTENANCE MANUAL TABLE OF CONTENTS Chapter Section Title Subject Page Effectivity FUEL - GENERAL .....................28-00-00 Introduction 28-00-00 General Description 28-00-00 FUEL STORAGE - MAINTENANCE..............28-10-00 General 28-10-00 Wing Fuel Tank Leakage Test 28-10-00 FUEL DISTRIBUTION - MAINTENANCE ...........28-20-00...
  • Page 330 AQUILA AT01-100 MAINTENANCE MANUAL...

  • Page 331: Fuel - General

    AQUILA AT01-100 Fuel MAINTENANCE MANUAL FUEL - GENERAL Introduction This chapter covers those units and components which are not part of the engine but store or deliver fuel to the engine or indicate fuel quantity and pressure. For additional information on the internal engine fuel system components, refer to the respective engine manufacturer’s publications.
  • Page 332 AQUILA AT01-100 Fuel MAINTENANCE MANUAL FUEL SYSTEM SCHEMATIC fuel vent lines wing fuel tanks drain valve drain valve dual fuel level indicator return line FUEL LEFT RIGHT LIFT LIFT KNOB KNOB fuel selector / shut-off valve fuel filter return line aux.

  • Page 333: Fuel Storage - Maintenance

    The inboard fuel tank ribs are easily accessible for maintenance work through access panel 610 BB (510 BB) in the lower wing skin. he wing fuel tanks are maintenance-free. However, if a leak is suspected, AQUILA Aviation GmbH should be consulted.
  • Page 334 AQUILA AT01-100 MAINTENANCE MANUAL...

  • Page 335: Fuel Distribution - Maintenance

    AQUILA AT01-100 Fuel MAINTENANCE MANUAL FUEL DISTRIBUTION - MAINTENANCE WARNING: PERFORM ALL FUEL SYSTEM MAINTENANCE IN ACCORDANCE WITH SAFETY PRECAUTIONS CONTAINED IN 12-11-00! General The fuel distribution system consists primarily of the fuel selector / shut-off valve, an electrical fuel pump, fuel lines and the fuel pump switch.
  • Page 336 AQUILA AT01-100 Fuel MAINTENANCE MANUAL fuel return line fuel line 2 Nm 17.7 in.lbs Detail- Fuel System Components Installation Figure 201 Page 202 28-20-00 30.04.13...

  • Page 337: Electrical Fuel Pump Removal/Installation

    AQUILA AT01-100 Fuel MAINTENANCE MANUAL (6) Disconnect the fuel supply and return lines at valve. (7) Remove bolts securing valve to mounting bracket and remove the fuel selector / shut-off valve assembly from aircraft. Install Fuel Selector / Shut-Off Valve (1) Verify battery is disconnected and electrical power to aircraft is OFF.
  • Page 338 AQUILA AT01-100 Fuel MAINTENANCE MANUAL Notes: Fuel system components Detail- in left wing analogous. Fuselage structure omitted fuel return line for clarity. fuel line Fuel Selector / Shut-Off Valve Installation Figure 202 Page 204 28-20-00 30.04.13...
  • Page 339 AQUILA AT01-100 Fuel MAINTENANCE MANUAL firewall hardpoints Detail- fuel line fuel return line Electrical Fuel Pump / System Components Installation Figure 203 Page 205 28-20-00 30.04.13...

  • Page 340: Fuel System Pressure Test

    AQUILA AT01-100 Fuel MAINTENANCE MANUAL Fuel System Pressure Test Leak-test the fuel system by the following procedure: (1) Fill the wing fuel tank with approved fuel. (2) Remove engine cowling, crew seats and all other panels and covers to gain access to all fuel system components and fuel lines (refer to 25-10-00, 25-12-00 and 71-10-00).

  • Page 341: Fuel Quantity Indication - Maintenance

    AQUILA AT01-100 Fuel MAINTENANCE MANUAL FUEL QUANTITY INDICATION - MAINTENANCE WARNING: PERFORM ALL FUEL SYSTEM MAINTENANCE IN ACCORDANCE WITH SAFETY PRECAUTIONS CONTAINED IN 12-11-00! General The fuel quantity indicating system consists of two resistive type fuel quantity sensors, one in each tank, a dual fuel quantity indicator and wiring connecting the components.

  • Page 342: Adjustment/Test

    AQUILA AT01-100 Fuel MAINTENANCE MANUAL Install Fuel Quantity Sensor (1) Verify battery is disconnected and electrical power to aircraft is OFF. (2) Check ease of movement of the float arm before installing the sensor. (3) Place sensor with new gasket on to the threaded studs at inboard fuel tank rib.

  • Page 343: Fuel Quantity Indication - Maintenance

    AQUILA AT01-100 Fuel MAINTENANCE MANUAL FUEL QUANTITY INDICATION - MAINTENANCE WARNING: PERFORM ALL FUEL SYSTEM MAINTENANCE IN ACCORDANCE WITH SAFETY PRECAUTIONS CONTAINED IN 12-11-00! General Fuel quantity indication is included in the engine monitoring system. Fuel quantity is measured by two resistive type fuel quantity sensors, one in each tank, electrically connected to the engine data converter (EDC) via an interface module (RFLM-4) at the back of the instrument panel.

  • Page 344: Resistive Fuel Module Removal/Installation

    Fuel Quantity Indicating System Calibration Refer to Electronics International MVP-50 operating instructions for the fuel tank calibration procedure. The necessary password can be obtained from Aquila Aviation on request. Fuel Quantity Sensor Test (1) Prepare aircraft (a) Drain fuel from wing tanks (refer to 12-11-00).

  • Page 345: Fuel Pressure Indication - Maintenance

    AQUILA AT01-100 Fuel MAINTENANCE MANUAL FUEL PRESSURE INDICATION - MAINTENANCE WARNING: PERFORM ALL FUEL SYSTEM MAINTENANCE IN ACCORDANCE WITH SAFETY PRECAUTIONS CONTAINED IN 12-11-00! General Fuel pressure indication is included in the engine monitoring system. Fuel pressure is measured by a pressure transducer electrically connected to the engine data converter (EDC).
  • Page 346 AQUILA AT01-100 MAINTENANCE MANUAL...
  • Page 347 AQUILA AT01-100 MAINTENANCE MANUAL CHAPTER 31 INDICATING / RECORDING SYSTEMS...
  • Page 348 AQUILA AT01-100 MAINTENANCE MANUAL...
  • Page 349 AQUILA AT01-100 Indicating / Recording MAINTENANCE MANUAL TABLE OF CONTENTS Chapter Section Title Subject Page Effectivity INDICATING / RECORDING SYSTEMS - GENERAL........31-00-00 AT01-100A Introduction 31-00-00 AT01-100A General Description 31-00-00 AT01-100A INDICATING / RECORDING SYSTEMS - GENERAL........31-00-00 AT01-100B Introduction 31-00-00 AT01-100B...
  • Page 350 AQUILA AT01-100 MAINTENANCE MANUAL...

  • Page 351: Indicating / Recording Systems - General

    Basically the instruments and avionic equipment can be chosen by the customer, but it cannot be installed in any arbitrary combination. Before removing or installing equipment the airplane manufacturer AQUILA must be contacted, with the exception of replacing a unit by an identical one.
  • Page 352 AQUILA AT01-100 Indicating / Recording MAINTENANCE MANUAL Dimmer Airspeed indicator COM/NAV Attitude gyro Transponder Altimeter Manifold pressure indicator Turn coordinator Tachometer Directional gyro Fuel level indicator Vertical speed indicator CHT indicator Ignition switch Voltmeter ALT1 / BAT switch Oil temperature indicator...

  • Page 353: Indicating / Recording Systems - General

    Basically the instrument and avionic equipment can be chosen by the customer, but it cannot be installed in any arbitrary combination. Before removing or installing equipment the airplane manufacturer AQUILA must be contacted, with the exception of replacing a unit by an identical one.
  • Page 354 Fuel selector / shut-off valve Dimmer Parking brake control lever COM/NAV Note: Arrangement of instruments may be different due to varying equipment. Instrument Panel Basic Configuration for Day & Night VFR Figure 1 EFFECTIVITY Page 2 AQUILA AT01-100B 31-00-00 30.04.13...

  • Page 355: Indicating / Recording Systems - General

    Basically the instrument and avionic equipment can be chosen by the customer, but it cannot be installed in any arbitrary combination. Before removing or installing equipment the airplane manufacturer AQUILA must be contacted, with the exception of replacing a unit by an identical one.
  • Page 356 AQUILA AT01-100 Indicating / Recording MAINTENANCE MANUAL ELT remote control Garmin G-500 PFD/MFD Dimmer Attitude gyro COM/NAV Ignition switch Transponder ALT1 / BAT switch Engine monitoring system Electrical fuel pump switch Avionic master switch Circuit breaker panel NAV light switch...

  • Page 357: Instrument Panel - Maintenance

    AQUILA AT01-100 Indicating / Recording MAINTENANCE MANUAL INSTRUMENT PANEL - MAINTENANCE General The instrument panel is made from aluminum alloy and is formed in one piece with a shelf. The shelf fits between the panel and the firewall. The panel shelf is attached on the left and right sides to support consoles and secured to the fuselage with bolts.
  • Page 358 AQUILA AT01-100 Indicating / Recording MAINTENANCE MANUAL Install Instrument Panel (1) Put instrument panel assembly in position and secure to fuselage using bolts, spacers, washers and nuts. (2) Secure instrument panel to center console using bolts, spacers, washers, and nuts.
  • Page 359 AQUILA AT01-100 MAINTENANCE MANUAL CHAPTER 32 LANDING GEAR...
  • Page 360 AQUILA AT01-100 MAINTENANCE MANUAL...
  • Page 361 AQUILA AT01-100 Landing Gear MAINTENANCE MANUAL TABLE OF CONTENTS Chapter Section Title Subject Page Effectifity LANDING GEAR - GENERAL 32-00-00 Introduction 32-00-00 General Description 32-00-00 MAIN LANDING GEAR - DESCRIPTION..........32-10-00 Introduction 32-10-00 Description and Operation 32-10-00 MAIN LANDING GEAR - MAINTENANCE ..........32-10-00...
  • Page 362 AQUILA AT01-100 MAINTENANCE MANUAL TABLE OF CONTENTS - CONTINUED Chapter Section Title Subject Page Effectivity Main Gear Wheel Disassembly/Assembly 32-40-00 Cleveland/Grove Nose Gear Wheel Removal/Installation 32-40-00 Cleveland/Grove Nose Gear Wheel Disassembly/Assembly 32-40-00 Cleveland/Grove Brake Master Cylinder Removal/Installation 32-40-00 Cleveland/Grove Brake Caliper Removal/Installation...

  • Page 363: Landing Gear - General

    AQUILA AT01-100 Landing Gear MAINTENANCE MANUAL LANDING GEAR - GENERAL Introduction This chapter describes units and components which furnish a means of supporting and steering the aircraft on the ground, including the main and nose landing gears, brakes, wheels and tires.
  • Page 364 AQUILA AT01-100 MAINTENANCE MANUAL...

  • Page 365: Main Landing Gear - Description

    AQUILA AT01-100 Landing Gear MAINTENANCE MANUAL MAIN LANDING GEAR - DESCRIPTION Introduction The main landing gear consists of the main landing gear struts, the wheels with brakes and the wheel fairings. The wheel fairings are standard equipment. The main gear struts are cantilever spring legs made of spring steel and carry the landing loads.
  • Page 366 AQUILA AT01-100 MAINTENANCE MANUAL...

  • Page 367: Main Landing Gear - Maintenance

    AQUILA AT01-100 Landing Gear MAINTENANCE MANUAL MAIN LANDING GEAR - MAINTENANCE Main Gear Leg Removal/Installation WARNING: CONTACT WITH HYDRAULIC FLUID CAN CAUSE SKIN IRRITATIONS. CAUTION: EXCESSIVE HYDRAULIC FLUID WILL ATTACK THE SURFACE OF VARIOUS MATERIALS. READ AND ADHERE TO ALL MANUFACTURER’S INSTRUCTIONS.
  • Page 368 AQUILA AT01-100 Landing Gear MAINTENANCE MANUAL Detail- UHMW-insert UHMW-insert UHMW-insert UHMW-insert Main Gear Leg Installation Figure 201 Page 202 32-10-00 30.04.13...

  • Page 369: Nose Landing Gear - Description

    AQUILA AT01-100 Landing Gear MAINTENANCE MANUAL NOSE LANDING GEAR - DESCRIPTION Introduction The aircraft has a steerable nose landing gear which is equipped with a shock absorber and wheel fairing. Description and Operation The nose gear consists of a welded tubular steel strut pivotally attached to the engine mount.
  • Page 370 AQUILA AT01-100 MAINTENANCE MANUAL...

  • Page 371: Nose Landing Gear - Maintenance

    AQUILA AT01-100 Landing Gear MAINTENANCE MANUAL NOSE LANDING GEAR - MAINTENANCE Nose Gear Leg Removal/Installation (Ref. Fig. 201) Remove Nose Gear Leg (1) Jack aircraft or weight tail of aircraft to raise nose wheel (refer to 07-00-00). (2) Remove engine cowling (refer to 71-10-00).
  • Page 372 AQUILA AT01-100 Landing Gear MAINTENANCE MANUAL engine mount NOTE: Right steering rod assembly omitted for clarity. Detail- 28 Nm 248 in.lbs Nose Gear Leg Installation Figure 201 Page 202 32-20-00 30.04.13...
  • Page 373 AQUILA AT01-100 Landing Gear MAINTENANCE MANUAL Detail- Damper Assy and Nose Wheel Fork Installation Figure 202 Page 203 32-20-00 30.04.13...
  • Page 374 AQUILA AT01-100 MAINTENANCE MANUAL...

  • Page 375: Wheels And Brakes - Description

    AQUILA AT01-100 MAINTENANCE MANUAL WHEELS AND BRAKES - DESCRIPTION Introduction This section describes components and maintenance of the wheels and the brake system. For tire specifications, refer to “Landing Gear - General”. For more detailed information on the installed wheels and brakes, refer to Beringer Aero maintenance manual for 5.00-5”...
  • Page 376 AQUILA AT01-100 MAINTENANCE MANUAL...

  • Page 377: Wheels And Brakes - Maintenance

    AQUILA AT01-100 Landing Gear MAINTENANCE MANUAL WHEELS AND BRAKES - MAINTENANCE Main Gear Wheel Removal/Installation (Ref. Fig. 201) Remove a Main Gear Wheel (1) Jack aircraft or appropriate main gear wheel (refer to 07-00-00). (2) Remove screws securing wheel fairing and remove wheel fairing.
  • Page 378 AQUILA AT01-100 Landing Gear MAINTENANCE MANUAL 28 Nm 248 in.lbs 10 Nm 88 in.lbs Detail- 30 Nm 265 in.lbs Main Gear Wheel Installation / Disassembly Figure 201 (1) EFFECTIVITY Page 202 Aircraft equipped with Beringer wheel/brake system 32-40-00 30.04.13...
  • Page 379 AQUILA AT01-100 Landing Gear MAINTENANCE MANUAL 14(3ea) Detail- Inner circlip Detail- Inner bearing Inner wheel half 11(8ea) Large O-ring Tire Central spacer Outer wheel half Outer bearing Outer circlip 10 Valve 10 Nm 11 Bolt (8ea) 87 in.lbs 12 Small O-ring...
  • Page 380 AQUILA AT01-100 Landing Gear MAINTENANCE MANUAL 5 Nm 87 in.lbs Detail- Nose Gear Wheel Installation / Disassembly Figure 202 (1) EFFECTIVITY Page 204 Aircraft equipped with Beringer wheel/brake system 32-40-00 30.04.13...
  • Page 381 AQUILA AT01-100 Landing Gear MAINTENANCE MANUAL 14(3ea) Detail- Inner circlip Detail- Inner bearing Inner wheel half 11(8ea) Large O-ring Tire Central spacer Outer wheel half Outer bearing Outer circlip 10 Valve 11 Bolt (8ea) 10 Nm 87 in.lbs 12 Small O-ring...
  • Page 382 AQUILA AT01-100 Landing Gear MAINTENANCE MANUAL CAUTION: DO NOT PRY BETWEEN TIRE BEAD AND WHEEL FLANGE AS THIS MAY DESTROY STRUCTURAL AND SEALING PROPERTIES OF WHEEL AND TIRE. (4) Remove all screws holding wheel halves together. CAUTION: DO NOT USE IMPACT OR POWER WRENCHES.
  • Page 383 AQUILA AT01-100 Landing Gear MAINTENANCE MANUAL connector small O-ring central spacer axle Ø 3 mm with- out sharp edges small O-ring large O-ring outer wheel half plywood tool (lower part with supports) Wheel Assembly Figure 203 (1) EFFECTIVITY Page 207...
  • Page 384 AQUILA AT01-100 Landing Gear MAINTENANCE MANUAL conical bushing central spacer outer wheel half Tire arrangement: red spot in front of valve Wheel Assembly Figure 203 (2) EFFECTIVITY Page 208 Aircraft equipped with Beringer wheel/brake system 32-40-00 30.04.13...
  • Page 385 AQUILA AT01-100 Landing Gear MAINTENANCE MANUAL wheel assembly screws (8ea) large O-ring inner wheel half Wheel Assembly Figure 203 (3) EFFECTIVITY Page 209 Aircraft equipped with Beringer wheel/brake system 32-40-00 30.04.13...

  • Page 386: Wheel Assembly Maintenance

    AQUILA AT01-100 Landing Gear MAINTENANCE MANUAL tightening order of wheel assembly screws CAUTION: USING A WRONG THREADLOCKER MAY CAUSE LOOSE OF SCREWS OR REMOVAL PROBLEM. CAUTION: DO NOT USE IMPACT OR POWER WRENCHES. (13) Screw valve core. (14) Place wheel in a protective enclosure and inflate to maximum tire rated pressure (90 psi, 6 bar).
  • Page 387 AQUILA AT01-100 Landing Gear MAINTENANCE MANUAL max. play clip screw clip inner wheel half brake disk Removal of Clips and Clip Screws (main wheels only) (1) Remove screws and clips if they are out of tolerance. The maximum play allowed is 0.4 mm (0.016 in.).
  • Page 388 AQUILA AT01-100 Landing Gear Landing Gear MAINTENANCE MANUAL NOTE: Causes for replacement of wheel halves and central spacer are: - Signs of deep corrosion in critical areas. - Anodizing color removed on more than 15% of external surface. - Heavy nicks.

  • Page 389: Brake Master Cylinder Removal/Installation

    AQUILA AT01-100 Landing Gear MAINTENANCE MANUAL Installation of Clips and Clip Screws (main wheels only) (1) If clips (drive keys) have been removed install new clips and new screws. Secure screws using high strength threadlocker (Loctite 271 recommended). CAUTION: USING A WRONG THREADLOCKER MAY CAUSE LOOSE OF SCREWS OR REMOVAL PROBLEM.
  • Page 390 AQUILA AT01-100 Landing Gear MAINTENANCE MANUAL pedal shaft master brake cylinder Detail- pilot’s left pedal assembly Master Brake Cylinder Installation Figure 204 EFFECTIVITY Page 214 Aircraft equipped with Beringer wheel/brake system 32-40-00 30.04.13...
  • Page 391 AQUILA AT01-100 Landing Gear MAINTENANCE MANUAL CAUTION: DO NOT APPLY BRAKE PRESSURE WHILE THE CALIPER CASING IS SEPARATED. (3) Remove the old brake pads. NOTE: The disc has not to be removed during the pad change. It is recommended to leave the disc in place.
  • Page 392 AQUILA AT01-100 Landing Gear MAINTENANCE MANUAL brake pad assemblies back plate brake disc 25 Nm 220 in.lbs Brake Pad Replacement Figure 205 EFFECTIVITY Page 216 Aircraft equipped with Beringer wheel/brake system 32-40-00 30.04.13...

  • Page 393: Brake Disc Replacement

    AQUILA AT01-100 Landing Gear MAINTENANCE MANUAL Brake Disc Replacement The minimum allowable brake disc thickness is 3.8 mm (0.15 in.). Maximum coning allowed is 0.3 mm (0.012 in.). The maximum values for grooves and bumps are 0.2 mm (0.008 in.).

  • Page 394: Brake System Conditioning

    AQUILA AT01-100 Landing Gear MAINTENANCE MANUAL Brake System Conditioning When new brake pads have been installed, it is important to condition them properly to obtain the service life designed into them. Rated brake torque value is reached only after a full conditioning of brake pads and disc.
  • Page 395 AQUILA AT01-100 Landing Gear MAINTENANCE MANUAL WARNING: CONTACT WITH HYDRAULIC FLUID CAN CAUSE SKIN IRRITATIONS. CAUTION: EXCESSIVE HYDRAULIC FLUID WILL ATTACK THE SURFACE OF VARIOUS MATERIALS. READ AND ADHERE TO ALL MANUFACTURERS INSTRUCTIONS. PROVIDE A SUITABLE COLLECTING VESSEL FOR HYDRAULIC FLUID.
  • Page 396 AQUILA AT01-100 Landing Gear MAINTENANCE MANUAL bleeder cylinder Detail- piston seals pistons brake pad assemblies back plate 25 Nm 220 in.lbs assembly screws Brake Caliper Assembly Figure 206 EFFECTIVITY Page 220 Aircraft equipped with Beringer wheel/brake system 32-40-00 30.04.13...
  • Page 397 AQUILA AT01-100 Landing Gear MAINTENANCE MANUAL NOTE: Causes for replacement of caliper casing are: - Signs of deep corrosion. - Anodizing color removed on more than 15% of external surface. - Heavy nicks. - Anodizing removed on internal piston bore.
  • Page 398 AQUILA AT01-100 MAINTENANCE MANUAL...

  • Page 399: Wheels And Brakes - Description

    AQUILA AT01-100 Landing Gear MAINTENANCE MANUAL WHEELS AND BRAKES - DESCRIPTION Introduction Nose and main landing gear wheels are of conventional design. The wheels of the main landing gear are each equipped with a single brake disc, floating cylinder brake assembly.
  • Page 400 AQUILA AT01-100 MAINTENANCE MANUAL...

  • Page 401: Wheels And Brakes - Maintenance

    AQUILA AT01-100 Landing Gear MAINTENANCE MANUAL WHEELS AND BRAKES - MAINTENANCE Main Gear Wheel Removal/Installation Remove a Main Gear Wheel (1) Jack aircraft or appropriate main gear wheel (refer to 7-00-00). (2) Remove screws securing wheel fairing and remove wheel fairing.
  • Page 402 AQUILA AT01-100 Landing Gear MAINTENANCE MANUAL 28 Nm 248 in.lbs Detail- Main Gear Wheel Installation Figure 201 EFFECTIVITY Page 202 Aircraft equipped with Cleveland/Grove wheel/brake 32-40-00 system 30.04.13...

  • Page 403: Nose Gear Wheel Removal/Installation

    AQUILA AT01-100 Landing Gear MAINTENANCE MANUAL (4) Reassemble the wheel unit, including the brake disc, with bolts, washers, and nuts. Torque to 10 - 12 Nm (89 - 106 in.lbs.). (5) Inflate the tire as required (refer to “Landing Gear - General”).
  • Page 404 AQUILA AT01-100 Landing Gear MAINTENANCE MANUAL brake disc on main wheels only Detail- +/-2 Wheel Assembly Figure 202 EFFECTIVITY Page 204 Aircraft equipped with Cleveland/Grove wheel/brake 32-40-00 system 30.04.13...

  • Page 405: Brake Master Cylinder Removal/Installation

    AQUILA AT01-100 Landing Gear MAINTENANCE MANUAL NOTE When the wheel halves are joined, it is recommended to double check that the tube isn't pinched, using an inspection mirror and a flashlight. (4) Reassemble the wheel unit with bolts, washers, and nuts. Torque to 10 - 12 Nm.
  • Page 406 AQUILA AT01-100 Landing Gear MAINTENANCE MANUAL back plate torque lining plate piston inlet fitting O-ring cylinder Detail- anchor bolt bleeder assy Brake Caliper Assembly Figure 203 EFFECTIVITY Page 206 Aircraft equipped with Cleveland/Grove wheel/brake 32-40-00 system 30.04.13...

  • Page 407: Brake Disc Removal/Installation

    AQUILA AT01-100 Landing Gear MAINTENANCE MANUAL Install a Caliper (1) Slide the caliper casing anchor pins into the torque plate bushings until the lining on the pressure plate contacts the brake disc. (2) Position the back plate against the other side of the disc and thread the two caliper casing bolts with their washers into the back plate from opposite side of the caliper casing.

  • Page 408: Brake System Bleeding

    AQUILA AT01-100 Landing Gear MAINTENANCE MANUAL NOTE: Before setting the first rivet fully, start the other rivets to keep the lining aligned properly with the plate. (5) Set all the rivets fully. (6) Slide the pressure plate with its new lining material over the caliper casing anchor pins.
  • Page 409 AQUILA AT01-100 MAINTENANCE MANUAL CHAPTER 33 LIGHTS...
  • Page 410 AQUILA AT01-100 MAINTENANCE MANUAL...
  • Page 411 AQUILA AT01-100 Lights MAINTENANCE MANUAL TABLE OF CONTENTS Chapter Section Title Subject Page Effectivity LIGHTS - GENERAL..................33-00-00 Introduction 33-00-00 General Description 33-00-00 INTERIOR LIGHTS - MAINTENANCE ............33-10-00 General 33-10-00 Post Light Removal/Installation 33-10-00 Nulite Removal/Installation 33-10-00 Cockpit Light Removal/Installation 33-10-00 EXTERIOR LIGHTS - MAINTENANCE ............33-40-00...
  • Page 412 AQUILA AT01-100 MAINTENANCE MANUAL...

  • Page 413: Lights - General

    AQUILA AT01-100 Lights MAINTENANCE MANUAL LIGHTS - GENERAL Introduction This chapter describes interior and exterior lighting systems used on the aircraft, including removal and installation procedures of components and light bulb replacement instructions. General Description A cockpit light is installed for general cabin lighting, for emergency instrument panel lighting and as a reading light.
  • Page 414 AQUILA AT01-100 MAINTENANCE MANUAL...

  • Page 415: Interior Lights - Maintenance

    AQUILA AT01-100 Lights MAINTENANCE MANUAL INTERIOR LIGHTS - MAINTENANCE General If instruments do not have internal lighting, they are illuminated by post lights or Nulites. Post lights are LED lights that illuminate the instrument panel and function as instrument mounting bolts.

  • Page 416: Cockpit Light Removal/Installation

    AQUILA AT01-100 Lights MAINTENANCE MANUAL Install Nulite (1) Put Nulite in position between the instrument panel and the instrument with the wires coming out of the top. (2) Install affected instrument as described in the apropriate chapter of this manual.

  • Page 417: Exterior Lights - Maintenance

    AQUILA AT01-100 Lights MAINTENANCE MANUAL EXTERIOR LIGHTS - MAINTENANCE General The maintenance of exterior lights is limited to the removal and installation of components and light bulb replacement. The illumination unit of the navigation/position/anti-collision lights cannot be repaired. If one LED of the cluster has failed the complete illumination unit has to be replaced.
  • Page 418 AQUILA AT01-100 Lights MAINTENANCE MANUAL Navigation/Position/Anti-Collision Light Removal/Installation/Check Remove Navigation/Position/Anti-Collision Light (1) Ensure BAT, NAV light and ACL light switches are in OFF position. (2) Remove screws securing base plate to wing tip fairing. Carefully remove light. (3) Disconnect wires at connector.
  • Page 419 AQUILA AT01-100 MAINTENANCE MANUAL CHAPTER 34 NAVIGATION...
  • Page 420 AQUILA AT01-100 MAINTENANCE MANUAL...
  • Page 421 AQUILA AT01-100 Navigation MAINTENANCE MANUAL TABLE OF CONTENTS Chapter Section Title Subject Page Effectivity NAVIGATION - GENERAL ..............34-00-00 Introduction 34-00-00 General Description 34-00-00 PITOT/STATIC SYSTEM – DESCRIPTION........34-11-00 Introduction 34-11-00 Description and Operation 34-11-00 PITOT/STATIC SYSTEM – MAINTENANCE ........34-11-00 General 34-11-00...
  • Page 422 AQUILA AT01-100 Navigation MAINTENANCE MANUAL TABLE OF CONTENTS (Cont.) Chapter Section Title Subject Page Effectivity INTEGRATED FLIGHT SYSTEM – MAINTENANCE .....34-25-00 Garmin G500 General 34-25-00 Garmin G500 Garmin G500 Removal/Installation 34-25-00 Garmin G500 Inspection/Check 34-25-00 Garmin G500 INDEPENDENT POSITION DETERMINING - MAINTENANCE..................34-40-00...

  • Page 423: Navigation - General

    AQUILA AT01-100 Navigation MAINTENANCE MANUAL NAVIGATION - GENERAL Introduction This chapter describes units and components that provide aircraft navigational information. General Description Different instruments and devices offer a means of determining flight conditions, aircraft attitude and position of the aircraft over the ground.
  • Page 424 AQUILA AT01-100 MAINTENANCE MANUAL...

  • Page 425: Pitot/Static System - Description

    AQUILA AT01-100 Navigation MAINTENANCE MANUAL PITOT/STATIC SYSTEM - DESCRIPTION Introduction The static and pitot pressure system supplies static and pitot pressure for the airspeed indicator, altimeter and vertical speed indicator as well as for the AHRS sensor (optional). Description and Operation...
  • Page 426 AQUILA AT01-100 Navigation MAINTENANCE MANUAL Air Data Computer (optional) airspeed indicator altimeter vertical speed Indicator pitot pressure water traps pitot-static tube static pressure Pitot-Static System Schematic Figure 1 Page 2 34-11-00 30.04.13...

  • Page 427: Pitot/Static System - Maintenance

    AQUILA AT01-100 Navigation MAINTENANCE MANUAL PITOT/STATIC SYSTEM - MAINTENANCE General CAUTION: NEVER BLOW COMPRESSED AIR THROUGH PITOT OR STATIC LINES TOWARD INSTRUMENTS AS THIS CAN CAUSE DAMAGE TO INSTRUMENTS. Proper maintenance of the pitot/static system is essential for proper altimeter, airspeed and vertical speed indications.

  • Page 428: P/S Heat Control Box Removal/Installation (Optional)

    AQUILA AT01-100 Navigation MAINTENANCE MANUAL P/S Heat Control Box Removal/Installation (optional) CAUTION: NEVER OPERATE PITOT HEATING WITHOUT THE CONTROL BOX AS THIS CAN DESTROY THE PITOT TUBE. Remove the Control Box (1) Ensure electrical power to aircraft is OFF. (2) Disconnect battery (refer to 24-30-00).
  • Page 429 AQUILA AT01-100 Navigation MAINTENANCE MANUAL NOTE: Example View! Equipment installed on instrument panel may vary depending on aircraft configuration. cable ties electrical connector Detail- P/S Heat Control Box Figure 202 Page 203 34-11-00 30.04.13...

  • Page 430: Inspection/Check

    AQUILA AT01-100 Navigation MAINTENANCE MANUAL Inspection/Check After any component replacement or repair, the system should be checked for proper function and a leakage test should be performed. Pitot System Leak Test (1) Fasten surgical hose and sphygmomanometer bulb over pitot head.

  • Page 431: Stall Warning System - Description

    AQUILA AT01-100 Navigation MAINTENANCE MANUAL STALL WARNING SYSTEM - DESCRIPTION Introduction The aircraft is equipped in with a stall warning system. It signals an approaching stall to the pilot by an audible alarm in the cockpit. Description and Operation The stall warning system consists of a mechanical transmitter, located in the leading edge of the left wing and a warning buzzer behind the instrument panel.
  • Page 432 AQUILA AT01-100 MAINTENANCE MANUAL...

  • Page 433: Stall Warning System - Maintenance

    AQUILA AT01-100 Navigation MAINTENANCE MANUAL STALL WARNING SYSTEM - MAINTENANCE General Maintenance is limited to the removal/installation of system components. In wintry conditions, make sure that the system transmitter microplate is always clear of ice and snow. Transmitter Removal/Installation Remove Transmitter (1) Ensure electrical power to aircraft is OFF.
  • Page 434 AQUILA AT01-100 Navigation MAINTENANCE MANUAL...

  • Page 435: Attitude And Direction - Maintenance

    AQUILA AT01-100 Navigation MAINTENANCE MANUAL ATTITUDE AND DIRECTION - MAINTENANCE General CAUTION: GYROS ARE DELICATE AND CAN NOT WITHSTAND THE SHOCK OF BEING DROPPED, JARRED OR STRUCK BY PIECES OF EQUIPMENT. DO NOT PLACE GYROS ON ANY HARD SURFACE. PAD WITH GENEROUS FOAM.

  • Page 436: Attitude Indicator Removal/Installation

    (b) Check the canopy is closed. (c) Check flaps are retracted. (d) Start engine and turn ON all electrical equipment that is usually used at cruise (refer to AQUILA AT01-100 airplane flight manual). CAUTION: DUE TO INSUFFICIENT ENGINE COOLING ON THE GROUND, DO NOT CONTINUOUSLY OPERATE THE ENGINE AT CRUISE RPM FOR MORE THAN 3 MIN.
  • Page 437 AQUILA AT01-100 Navigation MAINTENANCE MANUAL (e) Run engine and set throttle at cruise position. NOTE: When performing maintenance on the magnetic compass, use a non-magnetic or plastic screwdriver. (2) Remove screws securing access plate to compass casing to reveal adjustment screws.
  • Page 438 AQUILA AT01-100 MAINTENANCE MANUAL...

  • Page 439: Integrated Flight System - Maintenance

    The actual software version is documented in the aircraft equipment list, located in chapter 6.5.1 of the AQUILA AT01-100 airplane flight manual. All Service information released from AQUILA and related to software versions has to be attached to this maintenance manual for continuing airworthiness! No special tools are required for the removal and replacement of any system LRUs.

  • Page 440: Efd Battery Replacement

    AQUILA AT01-100 Navigation MAINTENANCE MANUAL (5) Remove nut securing braided ground strap to EFD. (6) Remove pitot and static quick connectors (EFD1000 only) by pulling back outer spring loaded locking sleeve while unplugging connectors. To remove 44 pin D-sub connector unscrew both jackscrews fully and pull connector straight back.

  • Page 441: Configuration Module (Cm) Removal/Installation

    AQUILA AT01-100 Navigation MAINTENANCE MANUAL Install RSM (1) Verify electrical power to aircraft is OFF. Replace the O-ring on the RSM. Contact Aspen Avionics for O-ring replacement (256-00001-001). (3) Verify RSM shim is installed between aircraft skin and RSM if required.

  • Page 442: Inspection/Check

    AQUILA AT01-100 Navigation MAINTENANCE MANUAL Inspection/Check All units, brackets, installation hardware and wiring of the EFD1000 system should be checked as defined below during annual inspection. Items found to be defective should be repaired or replaced prior to returning the aircraft to service. The performance of this inspection should not create the need for additional protective treatment (Alodine, paint, etc) of surfaces within the aircraft.

  • Page 443: Integrated Flight System - Maintenance

    The actual software version is documented in the aircraft equipment list, located in chapter 6.5.1 of the AQUILA AT01-100 airplane flight manual. All service information released from AQUILA and related to software versions has to be attached to this maintenance manual for continuing airworthiness! For bonding checks on the AQUILA AT01-100 no procedures or equipment are necessary other than that which are commonly expected for bonding measurements on small aircraft.
  • Page 444 AQUILA AT01-100 Navigation MAINTENANCE MANUAL GMU 44 unit support bracket Detail- GMU 44 magnetometer G500 System Components Figure 201 (1) EFFECTIVITY Page 202 Aircraft equipped with Garmin G500 PFD/MFD 34-25-00 30.04.13...
  • Page 445 AQUILA AT01-100 Navigation MAINTENANCE MANUAL GDC 74A unit support bracket Detail- attachment clamp Detail- GTP 59 (OAT sensor) GDC 74A (air data computer) AHRS unit Detail- support bracket GRS 77 (AHRS sensor) G500 System Components Figure 201 (2) EFFECTIVITY Page 203...

  • Page 446: Inspection/Check

    AQUILA AT01-100 Navigation MAINTENANCE MANUAL Inspection/Check All G500 system LRUs are designed to detect internal failures. A thorough self-test is executed automatically upon application of power to the units, and built-in tests are continuously executed. Detected errors are indicated on the GDU 620 display via failure annunciations.
  • Page 447 AQUILA AT01-100 Navigation MAINTENANCE MANUAL Requirement GDU 620 — Display Unit 40 mOhm (to instrument panel) GRS 77 — Attitude, Heading 20 mOhm (to instrument panel) Reference System (AHRS) GMU 44 — Magnetometer No bond check required since the GMU is required to be isolated from it's mounting location.
  • Page 448 AQUILA AT01-100 MAINTENANCE MANUAL...

  • Page 449: Independent Position Determining - Maintenance

    AQUILA AT01-100 Navigation MAINTENANCE MANUAL INDEPENDENT POSITION DETERMINING – MAINTENANCE General This section covers that portion of the system which provides information to determine position and is mainly independent of ground installations. This includes the GPS portion of the GNS 430W or GTN 650 navigation management system (NMS).
  • Page 450 AQUILA AT01-100 MAINTENANCE MANUAL...

  • Page 451: Independent Position Determining - Maintenance

    AQUILA AT01-100 Navigation MAINTENANCE MANUAL INDEPENDENT POSITION DETERMINING – MAINTENANCE General A. This section covers that portion of the system which provides information to determine position and is mainly independent of ground installations. This includes the FlymapL multifunctional display/GPS. B. The scope of maintenance is limited to the removal and installation of the components. For further information on the FlymapL, refer to the FlymapL installation manual, doc.
  • Page 452 AQUILA AT01-100 Navigation MAINTENANCE MANUAL instrument panel - forward side unit attachment screws Note: Surrounding components and parts Detail- omitted for clarity FlymapL Unit Installation Figure 201 EFFECTIVITY Page 202 Aircraft equipped with FlymapL 34-40-00 30.04.13...

  • Page 453: Gps Antenna Removal/Installation

    AQUILA AT01-100 Navigation MAINTENANCE MANUAL Install glare shield (refer to 31-10-00). Reconnect battery (refer to 24-30-00). Conduct a functional test of the installed unit. GPS Antenna Removal/Installation (Ref. Fig. 202) A. Remove FlymapL GPS Antenna Ensure electrical power to aircraft is OFF.
  • Page 454 AQUILA AT01-100 Navigation MAINTENANCE MANUAL cable ties instrument panel - forward side adhesive tape GPS antenna Detail- FlymapL GPS Antenna Installation Figure 202 EFFECTIVITY Page 204 Aircraft equipped with FlymapL 34-40-00 30.04.13...

  • Page 455: Dependent Positioning Determining - Maintenance

    AQUILA AT01-100 Navigation MAINTENANCE MANUAL DEPENDENT POSITIONING DETERMINING - MAINTENANCE General This section covers that portion of the system which provides information to determine position and is mainly dependent on ground installations. This includes the VOR/ILS receiver portion of the GNS 430W / GTN 650 navigation management system (NMS), the VOR/ILS receiver portion of the SL30 COM/NAV transceiver as well as the Garmin GTX 328 and GTX 330 mode S transponders.

  • Page 456: Gtx 328 / Gtx 330 Transponder Removal/Installation

    AQUILA AT01-100 Navigation MAINTENANCE MANUAL E. Garmin GTX 330 Mode S Transponder The Garmin GTX 330 is a panel-mounted non-diversity mode S transponder working like a radio transmitter and receiver that operates on radar frequencies, receiving ground radar or TCAS interrogations at 1030 MHz and transmitting a coded response of pulses to ground based radar on a frequency of 1090 MHz.

  • Page 457: Transponder Antenna Removal/Installation

    AQUILA AT01-100 Navigation MAINTENANCE MANUAL Transponder Antenna Removal/Installation Remove Transponder Antenna (1) Ensure electrical power to aircraft is OFF. (2) Remove access/inspection plate 211 BB (refer to 25-12-00) to gain access to the transponder antenna. (3) Remove nuts and washers securing transponder antenna to fuselage.
  • Page 458 AQUILA AT01-100 MAINTENANCE MANUAL...
  • Page 459 AQUILA AT01-100 MAINTENANCE MANUAL CHAPTER 51 STRUCTURES...
  • Page 460 AQUILA AT01-100 MAINTENANCE MANUAL...
  • Page 461 AQUILA AT01-100 Structures MAINTENANCE MANUAL TABLE OF CONTENTS Chapter Section Title Subject Page STRUCTURES - GENERAL................51-00-00 Introduction 51-00-00 General Description 51-00-00 Structure Classes 51-00-00 FIBERGLASS LAMINATE STRUCTURES - MAINTENANCE....51-10-00 General 51-10-00 Inspection Methods 51-10-00 Damage Classification 51-10-00 REPAIR OF FIBERGLASS LAMINATE COMPONENTS ......51-20-00...
  • Page 462 AQUILA AT01-100 MAINTENANCE MANUAL...

  • Page 463: Structures - General

    Please contact AQUILA Aviation GmbH for support in case damage to the aircraft structure the cause of which is unknown or suspect, and prior to major repairs to obtain detailed information.

  • Page 464: Structure Classes

    Secondary Structure These parts are not important for the structural integrity of the aircraft. For example: panels, covers, access plates, fairings. AQUILA AT01 Primary Structure Figure 01 Page 2 51-00-00 30.04.13...

  • Page 465: Fiberglass Laminate Structures - Maintenance

    AQUILA AT01-100 Structures MAINTENANCE MANUAL FIBERGLASS LAMINATE STRUCTURES - MAINTENANCE General This section contains maintenance information and procedures such as investigation and damage classification applicable to aircraft fiberglass laminate structure components. Inspection Methods Visual Inspection Most damage to a fiberglass-laminated structure will be visually detectable. A wide variety of component surface discontinuities such as scratches, cracks, dimples, dents and creases may indicate damage.

  • Page 466: Damage Classification

    AQUILA AT01-100 Structures MAINTENANCE MANUAL Damage Classification Damage to fiberglass laminate structures can be divided into four classes: (1) Damage Class 1 Severe, extensive damage that requires partial component restoration or general component replacement. (2) Damage Class 2 Damage to primary or secondary structures with sandwich penetration such as holes or fractures.
  • Page 467 AQUILA AT01-100 Structures MAINTENANCE MANUAL roll-over bar strip around the canopy frame stabilizer root area wing root area wing root area wing root area wing spar area 1350 fuel tank 1000 4500 stabilizer root area stabilizer spar area Damages - Critical Areas...
  • Page 468 AQUILA AT01-100 MAINTENANCE MANUAL...

  • Page 469: Repair Of Fiberglass Laminate Components

    AQUILA AT01-100 Structures MAINTENANCE MANUAL REPAIR OF FIBERGLASS LAMINATE COMPONENTS General This section covers required information to complete successful repairs to aircraft components that are made from fiberglass laminate. Necessary repair data, such as ply lay-up and ply orientation for various areas, as well as repair materials and procedures are provided. Not included are...

  • Page 470: Approved Fiberglass Laminate Repair Materials

    AQUILA AT01-100 Structures MAINTENANCE MANUAL (4) Solvents used in repair processes are composed of a group of chemicals that often prove toxic. To avoid toxic poisoning, work in a well-ventilated area only and always be alert for symptoms of poisoning. If symptoms are observed, it is vital to immediately remove the person from the contaminated area.
  • Page 471 AQUILA AT01-100 Structures MAINTENANCE MANUAL Quantity Equipment Parts No. Manufacturer release film commercially required available hot glue commercially required available cotton cloth commercially required available mixing container commercially available stir sticks commercially required available scale commercially available 1 pair gloves...

  • Page 472: Material Data Sheet

    AQUILA AT01-100 Structures MAINTENANCE MANUAL Material Data Sheet The material data sheet in combination with figure 202 and 203 should be used for information on ply lay-up and ply orientation The item numbers give the order in which the layers are applied.
  • Page 473 AQUILA AT01-100 Structures MAINTENANCE MANUAL Fuselage Ply Lay-Up Figure 202 (1) Page 205 51-20-00 30.04.13...
  • Page 474 AQUILA AT01-100 Structures MAINTENANCE MANUAL Fuselage Ply Lay-Up Figure 202 (2) Page 206 51-20-00 30.04.13...
  • Page 475 AQUILA AT01-100 Structures MAINTENANCE MANUAL Remarks Item No. Layers Description Interglas 92110 strip width 110 mm, up into the bonding strip Interglas 92125 up into the bonding strip Interglas 92125 width 100 mm, up into the bonding strip, overlap in winglet area...
  • Page 476 AQUILA AT01-100 Structures MAINTENANCE MANUAL filler y=1450 1030 1900 3000 3600 Upper Wing Shell Ply Lay-Up Figure 203 (1) Page 208 51-20-00 30.04.13...
  • Page 477 AQUILA AT01-100 Structures MAINTENANCE MANUAL 1750 4100 4500 2350 1350 1350 1000 Upper Wing Shell Ply Lay-Up Figure 203 (2) Page 209 51-20-00 30.04.13...
  • Page 478 AQUILA AT01-100 Structures MAINTENANCE MANUAL 1450 1030 1030 3472 1900 3600 Lower Wing Shell Ply Lay-Up Figure 203 (3) Page 210 51-20-00 30.04.13...
  • Page 479 AQUILA AT01-100 Structures MAINTENANCE MANUAL left side only left side only drainer fitting plate tie down point 2350 1750 4050 1350 2350 1350 1000 Lower Wing Shell Ply Lay-Up Figure 203 (4) Page 211 51-20-00 30.04.13...

  • Page 480: Repair Of Sandwich Components

    (3) Solvent clean prepared area. (4) Lay up repair plies according to the existing layer direction (refer to “Material Data Sheet” above). If the layer orientation is not clear please contact AQUILA Aviation GmbH. (5) Pre-cure the repair. (6) Sand the repair surface down to contour.
  • Page 481 AQUILA AT01-100 Structures MAINTENANCE MANUAL Minor Core Damage (damaged area has a diameter of less than 1 inch Remove surface finish from damaged area (1 inch outward). (2) Remove damaged laminat e and taper laminate around core damage (3) Solvent clean prepared area.
  • Page 482 (6) Solvent clean prepared area. (7) Lay up repair plies according to the existing layer direction (refer to “Material Data Sheet” above). If the layer orientation is not clear please contact AQUILA Aviation GmbH. Overlap min. 0.5 inch between first ply and laminate edge.
  • Page 483 (8) Solvent clean prepared area. (9) Lay up repair plies according to the existing layer direction (refer to “Material Data Sheet” above). If the layer orientation is not clear please contact AQUILA Aviation GmbH. Overlap min. 0.5 inch between first ply and laminate edge.
  • Page 484 (10) Lay up outer repair plies according to the existing layer direction (refer to “Material Data Sheet” above). If the layer orientation is not clear please contact AQUILA Aviation GmbH. Overlap min. 0.5 inch between first ply and laminate edge.
  • Page 485 (13) Apply a thin coat of resin to the scarfed edges of the repair area. (14) Lay up outer repair plies according to the existing layer direction (refer to “Material Data Sheet” above). If the layer orientation is not clear please contact AQUILA Aviation GmbH. Page 217 51-20-00 30.04.13...

  • Page 486: Repair Of Non-Structural Laminate Components

    AQUILA AT01-100 Structures MAINTENANCE MANUAL (15) Pre-cure the repair. (16) Sand the repair surface down to contour. (17) Refenish the repair area as described in “Exterior Finish” below. Repair of Non-Structural Laminate Components Non-Structural Fiberglass-Laminated Component Repair (1) Remove the damage and scarf the edges of the hole.

  • Page 487: Exterior Finish

    AQUILA AT01-100 Structures MAINTENANCE MANUAL Exterior Finish Prior painting over a repair, inspect the repair to ensure that it has hardened completely and has been properly contoured. CAUTION: MASK OFF SURFACE AROUND REPAIR AREA THAT DOES NOT REQUIRE FILLING OR PAINT, PAY SPECIAL ATTENTION TO STATIC PORTS, ANTENNAS AND DRAIN HOLES.
  • Page 488 AQUILA AT01-100 Structures MAINTENANCE MANUAL...
  • Page 489 AQUILA AT01-100 MAINTENANCE MANUAL CHAPTER 52 DOORS...
  • Page 490 AQUILA AT01-100 MAINTENANCE MANUAL...
  • Page 491 AQUILA AT01-100 Doors MAINTENANCE MANUAL TABLE OF CONTENTS Chapter Section Title Subject Page DOORS - GENERAL..................52-00-00 Introduction 52-00-00 General Description 52-00-00 CANOPY - MAINTENANCE ................52-10-00 General 52-10-00 Canopy Removal/Installation 52-10-00 Canopy Latching Mechanism Maintenance 52-10-00 BAGGAGE DOOR - MAINTENANCE............52-30-00 General...
  • Page 492 AQUILA AT01-100 MAINTENANCE MANUAL...
  • Page 493 AQUILA AT01-100 Doors MAINTENANCE MANUAL DOORS - GENERAL Introduction This chapter describes the canopy and the baggage door. It includes items such as structure, latching mechanism and maintenance instructions. General Description The canopy consists of a composite frame and a large one-piece acrylic glass window which are bonded together.
  • Page 494 AQUILA AT01-100 MAINTENANCE MANUAL...
  • Page 495 AQUILA AT01-100 Doors MAINTENANCE MANUAL CANOPY - MAINTENANCE General The canopy consists of a frame fabricated from carbon fiber laminate and rovings, and a large one- piece acrylic glass window which are bonded together. The window has two direct-vision panels, one on each side.
  • Page 496 AQUILA AT01-100 Doors MAINTENANCE MANUAL Detail- Canopy Latching Mechanism Figure 201 (1) Page 202 52-10-00 30.04.13...
  • Page 497 AQUILA AT01-100 Doors MAINTENANCE MANUAL Detail- receiver latching pin push-pull road inner handle spacer locking pin canopy lock spacer shaft actuation lever spacer outer handle Detail- Canopy Latching Mechanism Figure 201 (2) Page 203 52-10-00 30.04.13...
  • Page 498 AQUILA AT01-100 Doors MAINTENANCE MANUAL Install/Adjust Locking Pin (1) Remove screws securing the covering to the canopy and remove covering. (2) Clean thread of hole and locking pin with ethyl alcohol. (3) Thoroughly apply epoxy resin to the thread tapped inside the GRP plate of the cover.
  • Page 499 AQUILA AT01-100 Doors MAINTENANCE MANUAL BAGGAGE DOOR - MAINTENANCE General The baggage door is made of glass fiber laminate. It is hinged on the forward edge via two GFRP hinge arms and latched on the rear edge. The door is locked from the outside with a key lock.
  • Page 500 AQUILA AT01-100 MAINTENANCE MANUAL...
  • Page 501 AQUILA AT01-100 MAINTENANCE MANUAL CHAPTER 53 FUSELAGE...
  • Page 502 AQUILA AT01-100 MAINTENANCE MANUAL...
  • Page 503 AQUILA AT01-100 Fuselage MAINTENANCE MANUAL TABLE OF CONTENTS Chapter Section Title Subject Page FUSELAGE - GENERAL ...................53-00-00 Introduction 53-00-00 General Description 53-00-00 FUSELAGE MAIN FRAME - DESCRIPTION ..........53-10-00 Description and Operation 53-10-00 FUSELAGE MAIN FRAME - MAINTENANCE ..........53-10-00 General 53-10-00 AUXILIARY STRUCTURE - DESCRIPTION..........53-20-00...
  • Page 504 AQUILA AT01-100 MAINTENANCE MANUAL...
  • Page 505 AQUILA AT01-100 Fuselage MAINTENANCE MANUAL FUSELAGE - GENERAL Introduction This chapter provides a description of the general fuselage structure. For systems and components installed in the fuselage structure, refer to the respective chapters in this manual. General Description The fuselage is a semi-monocoque structure made primarily of composite materials. The fuselage structure consists of two halves made from fiberglass laminate bonded along a centerline lap-joint.
  • Page 506 AQUILA AT01-100 MAINTENANCE MANUAL...
  • Page 507 AQUILA AT01-100 Fuselage MAINTENANCE MANUAL FUSELAGE MAIN FRAME - DESCRIPTION Description and Operation This section describes those structural components which make up the main frame including firewall, bulkheads and ring frames. Firewall The firewall separates the engine compartment from the rest of the fuselage and supports various aircraft components on both the forward and aft sides.
  • Page 508 AQUILA AT01-100 Fuselage MAINTENANCE MANUAL ring frames baggage compartment bulkhead carbon fiber stringers carbon fiber stringers landing gear bulkhead firewall seat bulkhead side force bulkhead Fuselage Structure Figure 201 (1) Page 2 53-10-00 30.04.13...
  • Page 509 AQUILA AT01-100 Fuselage MAINTENANCE MANUAL vertical stabilizer rear web vertical stabilizer main spar carbon fiber stringers (4x) tail end bulkhead vertical stabilizer ribs ring frames Fuselage Structure Figure 201 (2) Page 3 53-10-00 30.04.13...
  • Page 510 AQUILA AT01-100 Fuselage MAINTENANCE MANUAL Vertical Stabilizer Ribs The vertical stabilizer front and rear ribs are of rigid GFRP molding and bonded to the fuselage shells and to the vertical stabilizer main spar. The rear rib also bonds to the rear web.
  • Page 511 Refer to chapter 51 for standard repair procedures and for repair data for the fuselage shells. If the damage area is inside the fuselage AQUILA Aviation GmbH must be contacted prior to beginning repair work.
  • Page 512 AQUILA AT01-100 MAINTENANCE MANUAL...
  • Page 513 AQUILA AT01-100 MAINTENANCE MANUAL AUXILIARY STRUCTURE - DESCRIPTION Description and Operation This section describes those structural components which make up the auxiliary structure including fuselage floor structure, center console, access panels and entry step. Fuselage Floor Structure The floor structure of the aircraft consists of a forward floor, a left and right baggage compartment floor, a left and right control stick cover and a left, right and center cover of the well of the landing gear.
  • Page 514 AQUILA AT01-100 MAINTENANCE MANUAL...
  • Page 515 AQUILA AT01-100 MAINTENANCE MANUAL CHAPTER 55 STABILIZERS...
  • Page 516 AQUILA AT01-100 MAINTENANCE MANUAL...
  • Page 517 AQUILA AT01-100 Stabilizers MAINTENANCE MANUAL TABLE OF CONTENTS Chapter Section Title Subject Page STABILIZERS - GENERAL................55-00-00 Introduction 55-00-00 General Description 55-00-00 HORIZONTAL STABILIZER - MAINTENANCE.........55-10-00 General 55-10-00 ELEVATOR - MAINTENANCE ...............55-20-00 General 55-20-00 Elevator Removal/Installation 55-20-00 Adjustment - Elevator Balancing 55-20-00 VERTICAL STABILIZER - MAINTENANCE..........55-30-00...
  • Page 518 AQUILA AT01-100 MAINTENANCE MANUAL...

  • Page 519: Stabilizers - General

    AQUILA AT01-100 Stabilizers MAINTENANCE MANUAL STABILIZERS - GENERAL Introduction This chapter describes the horizontal and vertical stabilizers as well as the structure of the elevator and rudder. Maintenance information is provided. General Description The empennage consists of a horizontal stabilizer, a two-piece elevator, a vertical fin and a rudder.
  • Page 520 AQUILA AT01-100 MAINTENANCE MANUAL...

  • Page 521: Horizontal Stabilizer - Maintenance

    AQUILA AT01-100 Stabilizers MAINTENANCE MANUAL HORIZONTAL STABILIZER - MAINTENANCE General The horizontal stabilizer is of a fully cantilever, semi-monocoque design. The structure, made of composite materials, consists of a front spar, a rear shear web, root ribs and top and bottom shells.
  • Page 522 AQUILA AT01-100 MAINTENANCE MANUAL...

  • Page 523: Elevator - Maintenance

    AQUILA AT01-100 Stabilizers MAINTENANCE MANUAL ELEVATOR - MAINTENANCE General The two-piece elevator is made from composite materials. Each half has a top and a bottom shell which are bonded together. The shells have a sandwich structure with a rigid foam core. The following are bonded between the shells: a horn rip at the outer end, two hinge brackets in the front area and a rib at the inboard end.
  • Page 524 AQUILA AT01-100 Stabilizers MAINTENANCE MANUAL Elevator Balancing NOTE: Calculate the static control surface moment as follows: M = F x r [Nm] (1) Disconnect elevator assembly from elevator push-pull rod (refer to 27-30-00). (2) Weigh by means of a conventional spring balance at the given weighing point (refer to figure 201).
  • Page 525 AQUILA AT01-100 Stabilizers MAINTENANCE MANUAL (b) Raise the spring balance slowly until the control surface begins to move. Note the reading and the direction of the movement (i.e. 11,2 N up). (c) Lower the spring balance slowly until the control surface begins to move down. Note the reading and the direction of the movement to (i.e.
  • Page 526 AQUILA AT01-100 MAINTENANCE MANUAL...

  • Page 527: Vertical Stabilizer - Maintenance

    AQUILA AT01-100 Stabilizers MAINTENANCE MANUAL VERTICAL STABILIZER - MAINTENANCE General The vertical stabilizer is an integral part of the fuselage structure and is made from composite laminate materials. No servicing is required. For more information on fuselage structure, refer to 53-10-00.
  • Page 528 AQUILA AT01-100 MAINTENANCE MANUAL...

  • Page 529: Rudder - Maintenance

    AQUILA AT01-100 Stabilizers MAINTENANCE MANUAL RUDDER - MAINTENANCE General The rudder is made from composite materials. The assembly consists primarily of the left and right shells which are bonded together. The shells have a sandwich structure with a rigid foam core.
  • Page 530 AQUILA AT01-100 Stabilizers MAINTENANCE MANUAL Rudder Balancing NOTE: Calculate the static control surface moment as follows: M = F x r [Nm] (1) Remove rudder from aircraft (refer to “Rudder Removal/Installation” above). (2) Use any suitable method to support the rudder horizontally at the pivot axis so it can rotate freely around the pivot axis.
  • Page 531 AQUILA AT01-100 MAINTENANCE MANUAL CHAPTER 56 WINDOWS...
  • Page 532 AQUILA AT01-100 MAINTENANCE MANUAL...
  • Page 533 AQUILA AT01-100 Windows MAINTENANCE MANUAL TABLE OF CONTENTS Chapter Section Title Subject Page WINDOWS - GENERAL ..................56-00-00 Introduction 56-00-00 General Description 56-00-00 FLIGHT COMPARTMENT WINDOWS - MAINTENANCE......56-10-00 General 56-10-00 Tools, Equipment and Materials 56-10-00 Window Repair 56-10-00 Page 1 56 - TOC...
  • Page 534 AQUILA AT01-100 MAINTENANCE MANUAL...

  • Page 535: Windows - General

    AQUILA AT01-100 Windows MAINTENANCE MANUAL WINDOWS - GENERAL Introduction This chapter describes the acrylic glass windows of the canopy and the fuselage. Refer to 52-10-00 for information on the canopy structure. Refer to 12-23-00 for information on cleaning and care of acrylic glass windows.
  • Page 536 AQUILA AT01-100 MAINTENANCE MANUAL...

  • Page 537: Flight Compartment Windows - Maintenance

    AQUILA AT01-100 Windows MAINTENANCE MANUAL FLIGHT COMPARTMENT WINDOWS - MAINTENANCE General This section describes the repair of damaged acrylic glass windows. A properly carried out repair is essential to preserve the optical properties of acrylic glass windows. Personnel must be familiar with repair practices prior to attempting acrylic glass repairs on the aircraft.
  • Page 538 AQUILA AT01-100 Windows MAINTENANCE MANUAL Temporary Repairs (1) Stop-drill the ends of short cracks. Use a 2,5 mm (3/32 in.) drill. stop-drill 2.5 mm (3/32 in.) window crack (2) Repair the crack not later than the next 100-hour inspection. Permanent Repairs (1) Remove canopy (refer to 52-10-00).
  • Page 539 AQUILA AT01-100 Windows MAINTENANCE MANUAL (11) Cut a groove along the crack in the inner surface of the window. NOTE: This groove is less deep than the outer surface groove. It must cut into the outer layer of filler. This prevents holes in the filler.
  • Page 540 AQUILA AT01-100 MAINTENANCE MANUAL...
  • Page 541 AQUILA AT01-100 MAINTENANCE MANUAL CHAPTER 57 WINGS...
  • Page 542 AQUILA AT01-100 MAINTENANCE MANUAL...
  • Page 543 AQUILA AT01-100 Wings MAINTENANCE MANUAL TABLE OF CONTENTS Chapter Section Title Subject Page WINGS - GENERAL..................57-00-00 Introduction 57-00-00 General Description 57-00-00 WINGS - MAINTENANCE ................57-00-00 General 57-00-00 Tools, Equipment and Material 57-00-00 Wings Removal/Installation 57-00-00 Wing Attachment Bolt Removal/Installation 57-00-00 CONTROL SURFACES - MAINTENANCE ..........57-50-00...
  • Page 544 AQUILA AT01-100 MAINTENANCE MANUAL...

  • Page 545: Wings - General

    AQUILA AT01-100 Wings MAINTENANCE MANUAL WINGS - GENERAL Introduction This chapter describes the wing, flaps and aileron structures. It also provides maintenance information. General Description The wings are made from composite materials which provide very smooth and seamless flight surfaces. They are of a cantilever, semi-monocoque design, with a one-piece main spar, ribs and shear webs covered with top and bottom shells.
  • Page 546 AQUILA AT01-100 MAINTENANCE MANUAL...

  • Page 547: Wings - Maintenance

    The section provides removal and installation instructions for the wings and the wing bolts. Tools, Equipment and Material Quantity Equipment Parts No. Manufacturer 3.A./B. Wing stand AQUILA Aviation GmbH 3.A./4.A Wing attachment AQUILA Aviation GmbH bolt removal tool Wing Removal/Installation CAUTION: AT LEAST SEVEN PERSONS ARE NEEDED FOR WING REMOVAL OR INSTALLATION.
  • Page 548 AQUILA AT01-100 Wings MAINTENANCE MANUAL wing spar root ribs wing fuel tank Detail- Wing Structure Figure 201 Page 202 57-00-00 30.04.13...
  • Page 549 AQUILA AT01-100 Wings MAINTENANCE MANUAL (9) Disconnect electrical wires at connector inside the spar tunnel. (10) Disconnect fuel lines (four places). (11) Identify and disconnect pitot and static lines at water traps. (12) Disconnect aileron front from aileron rear bellcrank (refer to 27-10-00).
  • Page 550 AQUILA AT01-100 Wings MAINTENANCE MANUAL fillister-head screw 11,5 in.lb Bolt must be secured with safety wire! Safety wire should be anchored to the shown fillister-head screw. Note: The rear right location is shown. Wing Bolt Installation Figure 201 Page 204 57-00-00 30.04.13...

  • Page 551: Wing Attachment Bolt Removal/Installation

    AQUILA AT01-100 Wings MAINTENANCE MANUAL (11) Reconnect battery (refer to 24-30-00). (12) Perform aileron control system inspection/check (refer to 27-10-00). (13) Perform elevator control system and elevator trim system inspection/check and adjust system if necessary as described in 27-30-00 and 27-31-00.
  • Page 552 AQUILA AT01-100 MAINTENANCE MANUAL...

  • Page 553: Control Surfaces - Maintenance

    AQUILA AT01-100 Wings MAINTENANCE MANUAL CONTROL SURFACES - MAINTENANCE General The flap structure is shown in figure 201. The top and bottom shells have a sandwich structure with a rigid foam core. GFRP molded ribs are bonded between the shells. A flap hinge arm is bonded to each rib.
  • Page 554 AQUILA AT01-100 Wings MAINTENANCE MANUAL Detail- Detail- Flap/Aileron Structure Figure 201 Page 202 57-50-00 30.04.13...

  • Page 555: Adjustment - Control Surface Balancing

    AQUILA AT01-100 Wings MAINTENANCE MANUAL Install Aileron (1) Put the aileron in position and secure with washer and castellated nut at inboard hinge. Secure castellated nut with cotter pin. (2) Connect aileron push-pull rod to aileron horn. (3) Check proper aileron control system operation.
  • Page 556 AQUILA AT01-100 Wings MAINTENANCE MANUAL wing Detail- right flap Flap Installation Figure 202 Page 204 57-50-00 30.04.13...
  • Page 557 AQUILA AT01-100 Wings MAINTENANCE MANUAL Detail- Aileron Installation Figure 203 Page 205 57-50-00 30.04.13...
  • Page 558 AQUILA AT01-100 Wings MAINTENANCE MANUAL hinge center line weighing point r=21,1 cm (8.3 in.) Detail- hinge center line weighing point r=21,1 cm (8.3 in.) Detail- Flap / Aileron Balancing Figure 204 Page 206 57-50-00 30.04.13...
  • Page 559 AQUILA AT01-100 Wings MAINTENANCE MANUAL (a) Attach spring balance at weighing point. The initial position of the flaps for each measurement should be 35° down. (b) Raise the spring balance slowly until the control surface begins to move. Note the reading and the direction of the movement (i.e.
  • Page 560 AQUILA AT01-100 MAINTENANCE MANUAL...
  • Page 561 AQUILA AT01-100 MAINTENANCE MANUAL CHAPTER 61 PROPELLER...
  • Page 562 AQUILA AT01-100 MAINTENANCE MANUAL...
  • Page 563 AQUILA AT01-100 Propeller MAINTENANCE MANUAL TABLE OF CONTENTS Chapter Section Title Subject Page Effectivity PROPELLER - GENERAL ................61-00-00 Introduction 61-00-00 General Description 61-00-00 PROPELLER - TROUBLESHOOTING ............61-00-00 General 61-00-00 Troubleshooting 61-00-00 PROPELLER ASSEMBLY - MAINTENANCE..........61-10-00 General 61-10-00 Tools, Equipment and Material...
  • Page 564 AQUILA AT01-100 MAINTENANCE MANUAL...

  • Page 565: Propeller - General

    AQUILA AT01-100 Propeller MAINTENANCE MANUAL PROPELLER - GENERAL Introduction This chapter describes the propeller. Maintenance information is provided. Revs given in this chapter are propeller speeds. General Description The aircraft uses a mt-Propeller MTV-21-A/170-05 variable pitch, two blade wood-composite propeller. The propeller has a governor which controls propeller pitch hydraulically.
  • Page 566 AQUILA AT01-100 MAINTENANCE MANUAL...

  • Page 567: Propeller - Troubleshooting

    AQUILA AT01-100 Propeller MAINTENANCE MANUAL PROPELLER - TROUBLESHOOTING 1. General The following chart lists some of the more common troubles which may occur with the propeller, their probable causes and remedies. 2. Troubleshooting Chart Trouble Probable Cause Remedy Static rpm too low Propeller limits engine speed.

  • Page 568: Troubleshooting

    AQUILA AT01-100 Propeller MAINTENANCE MANUAL 2. Troubleshooting Chart (Cont.) Trouble Probable Cause Remedy 4. Wrong pitch stops in the Compare pitch values to those of the propeller. data sheet. Note static rotational speed. 5. Abrupt movement of Move the controls carefully and of propeller or throttle slowly.
  • Page 569 AQUILA AT01-100 Propeller MAINTENANCE MANUAL 2. Troubleshooting Chart (Cont.) Trouble Probable Cause Remedy Rpm decrease during 1. Speeder spring in the Check governor on the test bench. normal operation without governor broken. change of propeller lever 2. Dirt in the fuel system or Clean or repair.
  • Page 570 AQUILA AT01-100 MAINTENANCE MANUAL...

  • Page 571: Propeller Assembly - Maintenance

    AQUILA AT01-100 Propeller MAINTENANCE MANUAL PROPELLER ASSEMBLY - MAINTENANCE General The aircraft is equipped with a mt-Propeller MTV-21-A/170-05 variable pitch, two blade wood- composite propeller. The propeller low pitch stop is preset by mt-Propeller and therefore needs no adjustment. Maintenance is limited to the removal/installation of the propeller assembly, inspections and small repairs.

  • Page 572: Propeller Removal/Installation

    AQUILA AT01-100 Propeller MAINTENANCE MANUAL Spinner The spinner dome is a one-piece part made from fiber reinforced composite. The bulkhead is truncated aluminum alloy. Filler plates increase the stiffness of the dome on the cutouts for the blades. The dome is mounted to the bulkhead by means of screws.

  • Page 573: Inspection/Check

    AQUILA AT01-100 Propeller MAINTENANCE MANUAL Inspection/Check Inspection/Check (1) Remove screws securing spinner dome to spinner bulkhead and remove spinner. (2) Check spinner for cracks and other damage. (3) Perform a visual inspection of the propeller blades. (a) Check for critical cracks (refer to mt-Propeller E-124 operation and installation manual for hydraulically controlled variable pitch propeller) (b) Inspect for notches, dents, nicks or other damage.
  • Page 574 AQUILA AT01-100 Propeller MAINTENANCE MANUAL Trailing edge splitting can arise from a stone hit. If the split is not longer than 40 mm (1.5 in.), it can be glued with epoxy cement. If some wood is missing (not deeper than 8 mm [0.25 in.]), fill damaged area with epoxy, let it harden, grind surface smooth and cover with water-resistant varnish, preferably polyurethane.

  • Page 575: Propeller Control - Maintenance

    AQUILA AT01-100 Propeller MAINTENANCE MANUAL PROPELLER CONTROL - MAINTENANCE General The aircraft is equipped with a constant speed propeller. A mt-Propeller P-850-12 governor controls the blade pitch. The governor max. rpm screw is preset by mt-Propeller and therefore needs no adjustment.
  • Page 576 AQUILA AT01-100 Propeller MAINTENANCE MANUAL gasket governor 11-15 Nm 100-140 in.lbs Governor Installation Figure 201 Page 202 61-20-00 30.04.13...

  • Page 577: Inspection/Check

    AQUILA AT01-100 Propeller MAINTENANCE MANUAL (4) Install governor control cable to governor control arm. (5) Adjust governor (refer to “Adjustment/Test” below). (6) Install upper engine cowling (refer to 76-10-00). (7) Carry out a functional test (refer to “Adjustment/Test” below). Inspection/Check...
  • Page 578 AQUILA AT01-100 Propeller MAINTENANCE MANUAL (5) Start and warm up engine. (6) Adjust power lever for approx. 1700 rpm (propeller lever in max. rpm position). (7) Pull back propeller lever until the propeller speed drops by 200 rpm. (8) Pull back power lever in idle position.
  • Page 579 AQUILA AT01-100 MAINTENANCE MANUAL CHAPTER 71 POWER PLANT...
  • Page 580 AQUILA AT01-100 MAINTENANCE MANUAL...
  • Page 581 AQUILA AT01-100 Power Plant MAINTENANCE MANUAL TABLE OF CONTENTS Chapter Section Title Subject Page POWER PLANT - GENERAL ................71-00-00 Introduction 71-00-00 General Description 71-00-00 POWER PLANT - TROUBLESHOOTING............71-00-00 General 71-00-00 Troubleshooting 71-00-00 POWER PLANT - MAINTENANCE ..............71-00-00 General 71-00-00 Engine Removal/Installation...
  • Page 582 AQUILA AT01-100 MAINTENANCE MANUAL...

  • Page 583: Power Plant - General

    AQUILA AT01-100 Power Plant MAINTENANCE MANUAL POWER PLANT - GENERAL Introduction This chapter provides maintenance information for the power plant and associated components. Engine-related information is limited to the most important specifications. For further, more detailed information, refer to applicable ROTAX Aircraft Engines publications.
  • Page 584 AQUILA AT01-100 Power Plant MAINTENANCE MANUAL Components (1) Starter The starter is mounted at the rear lower right side of the engine. It is a direct drive 12 V DC motor. Starting a pinion gear in the starter engages the crankshaft ring gear and turns the engine over.

  • Page 585: Power Plant - Troubleshooting

    AQUILA AT01-100 Power Plant MAINTENANCE MANUAL POWER PLANT - TROUBLESHOOTING General The following chart lists some of the more common engine troubles, which may be encountered during maintenance, their probable causes and remedies. Troubleshooting Safety Precautions: (1) Before beginning troubleshooting on engine, ensure that a fire extinguisher is available.
  • Page 586 AQUILA AT01-100 Power Plant MAINTENANCE MANUAL Leak in induction Tighten all connections system in induction system. Replace any parts that are defective. Incorrect idle adjustment Adjust throttle stop to obtain correct idle. Uneven cylinder Check condition of piston compression rings and valve seats.
  • Page 587 AQUILA AT01-100 Power Plant MAINTENANCE MANUAL and corrosion. Check cables for damage, for ground contact and security. Failure of engine Leak in induction system Tighten all connections and to develop full power replace defective parts. Throttle lever out of Adjust throttle lever.
  • Page 588 AQUILA AT01-100 Power Plant MAINTENANCE MANUAL High oil Insufficient air cooling Check oil cooler for condition, temperature deformation or obstruction. Insufficient oil supply Fill to proper level with specified oil. Low grade of oil Replace with oil conforming to specifications.

  • Page 589: Power Plant - Maintenance

    AQUILA AT01-100 Power Plant MAINTENANCE MANUAL POWER PLANT - MAINTENANCE General This section provides instructions on engine removal and installation. For information beyond the scope of this section, such as repair and overhaul of the engine or components, refer to applicable ROTAX Aircraft Engines GmbH publications.
  • Page 590 (20) Disconnect Bowden cable at governor and at support. (21) Disconnect Bowden cables at carburetor. (22) Lift engine just enough to relief weight from engine mounts. (23) Remove nuts, washers, and bolts securing engine to AQUILA engine mount. (24) Remove engine from aircraft. Install Engine NOTE: Remove all protective plugs or caps and labels as each component is installed.

  • Page 591: Engine Cleaning

    AQUILA AT01-100 Power Plant MAINTENANCE MANUAL (20) Install spinner and propeller (refer to 61-10-00). (21) Replenish engine oil and coolant (refer to 75-10-00 and 79-10-00). (22) Install battery (refer to 24-30-00). (23) Place fuel selector valve to desired tank. (24) Perform operational check (refer to 05-20-00).
  • Page 592 AQUILA AT01-100 MAINTENANCE MANUAL...

  • Page 593: Cowling - Maintenance

    AQUILA AT01-100 Power Plant MAINTENANCE MANUAL COWLING - MAINTENANCE General The engine cowling is made from laminated fiberglass and comprises an upper and a lower half. The oil access door is located on the right side of the upper cowling. An air intake and the induction air filter casing are to be found on the lower cowling left side.
  • Page 594 AQUILA AT01-100 Power Plant MAINTENANCE MANUAL (5) Install flexible air hose to induction air filter casing and secure using clamp. (6) Put upper cowl in position and secure to lower cowl and fuselage with CAMLOC quick- release fasteners. Page 202 71-10-00 30.04.13...

  • Page 595: Engine Mount - Maintenance

    The vibration dampers isolate engine noise and vibration from the airframe. This section is applicable to the engine mount made by AQUILA Aviation GmbH. Maintenance not covered by this chapter is possible, if carried out according to AC 43.13-1B, September 8, 1998.
  • Page 596 AQUILA AT01-100 Power Plant MAINTENANCE MANUAL (8) Install master relay, starter relay and electrical connectors to the engine. (9) Install battery (refer to 24-30-00). (10) Install engine (refer to 71-00-00). Page 202 71-20-00 30.04.13...

  • Page 597: Air Induction System - Maintenance

    AQUILA AT01-100 Power Plant MAINTENANCE MANUAL AIR INDUCTION SYSTEM - MAINTENANCE General Induction air enters the carburetors via the air intake, the induction air filter, the air distribution box and the flexible ducts. The air intake and the induction air filter casing are located on the lower cowling left side.
  • Page 598 AQUILA AT01-100 MAINTENANCE MANUAL...
  • Page 599 AQUILA AT01-100 MAINTENANCE MANUAL CHAPTER 74 IGNITION SYSTEM...
  • Page 600 AQUILA AT01-100 MAINTENANCE MANUAL...
  • Page 601 AQUILA AT01-100 Ignition System MAINTENANCE MANUAL TABLE OF CONTENTS Chapter Section Title Subject Page IGNITION SYSTEM - GENERAL ..............74-00-00 Introduction 74-00-00 General Description 74-00-00 IGNITION SYSTEM - MAINTENANCE............74-00-00 General 74-00-00 SMD-Electronic Module Removal/Installation 74-00-00 Double Ignition Coil Assembly Removal/Installation 74-00-00...
  • Page 602 AQUILA AT01-100 MAINTENANCE MANUAL...

  • Page 603: Ignition System - General

    AQUILA AT01-100 Ignition System MAINTENANCE MANUAL IGNITION SYSTEM - GENERAL Introduction This chapter describes those units and components which generate, distribute and control an electrical current to ignite the fuel air mixture in the engine cylinders. General Description The ROTAX 912S engine is equipped with a dual ignition unit of a breakerless, capacitor ®...
  • Page 604 AQUILA AT01-100 Ignition System MAINTENANCE MANUAL IGNITION SYSTEM ignition circuit A ignition circuit B Ignition System Electrical Schematic Figure 1 Page 2 74-00-00 30.04.13...

  • Page 605: Ignition System - Maintenance

    AQUILA AT01-100 Ignition System MAINTENANCE MANUAL IGNITION SYSTEM - MAINTENANCE General Maintenance of the ignition system is limited to the removal and installation of components. Information on verification and renewal of spark plugs is also provided. For information beyond the scope of this section pertaining to the ignition system, refer to the maintenance manual for ROTAX Engine Type 912 Serie.

  • Page 606: Spark Plug Removal/Installation

    AQUILA AT01-100 Ignition System MAINTENANCE MANUAL (3) Install spark plug connectors to spark plugs. (4) Install clamps and cable ties securing ignition cables to engine. (5) Install battery (refer to 24-30-00). (6) Install engine cowling (refer to 71-10-00). Spark Plug Removal/Installation Remove Spark Plug (1) Remove engine cowling (refer to 71-10-00).
  • Page 607 AQUILA AT01-100 Ignition System MAINTENANCE MANUAL Oily, glossy coating: - Misfiring; - Too much oil in combustion chamber; - Worn cylinder and piston rings; White with melt droplets: - Mixture too lean; - Leaking valves; Ignition System Wiring (1) Check all cable connectors for tight fit and good contact.
  • Page 608 AQUILA AT01-100 MAINTENANCE MANUAL...
  • Page 609 AQUILA AT01-100 MAINTENANCE MANUAL CHAPTER 75 COOLING SYSTEM...
  • Page 610 AQUILA AT01-100 MAINTENANCE MANUAL...
  • Page 611 AQUILA AT01-100 Cooling System MAINTENANCE MANUAL TABLE OF CONTENTS Chapter Section Title Subject Page Effectivity COOLING SYSTEM - GENERAL ..............75-00-00 Introduction 75-00-00 General Description 75-00-00 COOLING SYSTEM - MAINTENANCE ............75-00-00 General 75-00-00 Water Pump Removal/Installation 75-00-00 Radiator Removal/Installation 75-00-00 Overflow Bottle Removal/Installation...
  • Page 612 AQUILA AT01-100 MAINTENANCE MANUAL...

  • Page 613: Cooling System - General

    AQUILA AT01-100 Cooling System MAINTENANCE MANUAL COOLING SYSTEM - GENERAL Introduction This chapter describes those units and components which cool and ventilate engine cylinders with cylinder heads. For cooling system servicing, such as replenishing or flushing, refer to 12-14-00. General Description The cooling system of the ROTAX 912S engine is designed for liquid cooling of the cylinder heads ®...
  • Page 614 AQUILA AT01-100 Cooling System MAINTENANCE MANUAL The expansion tank is closed by a pressure cap (with excess pressure valve and return valve). As coolant temperature rises, the excess pressure valve opens and the coolant will flow through the hose at atmospheric pressure to the transparent overflow bottle. When coolant temperature drops, the coolant will be sucked back into the cooling circuit.

  • Page 615: Cooling System - Maintenance

    AQUILA AT01-100 Cooling System MAINTENANCE MANUAL COOLING SYSTEM - MAINTENANCE General WARNING: NEVER OPEN RADIATOR, EXPANSION TANK OR OVERFLOW BOTTLE CAP WHEN THE COOLING SYSTEM IS STILL HOT! FOR REASONS OF SAFETY, COVER CAP WITH A CLOTH AND OPEN SLOWLY. SUDDEN OPENING OF THE CAP WOULD PROVOKE EXIT OF BOILING COOLANT AND RESULT IN SEVERE SCALDS.

  • Page 616: Overflow Bottle Removal/Installation

    AQUILA AT01-100 Cooling System MAINTENANCE MANUAL Overflow Bottle Removal/Installation Remove Overflow Bottle (1) Remove engine cowling (refer to 71-10-00). (2) Disconnect hose at overflow bottle. (3) Remove cable ties securing overflow bottle to bracket and remove overflow bottle from aircraft.
  • Page 617 AQUILA AT01-100 MAINTENANCE MANUAL CHAPTER 76 ENGINE CONTROLS...
  • Page 618 AQUILA AT01-100 MAINTENANCE MANUAL...
  • Page 619 AQUILA AT01-100 Engine Controls MAINTENANCE MANUAL TABLE OF CONTENTS Chapter Section Title Subject Page ENGINE CONTROLS - GENERAL ..............76-00-00 Introduction 76-00-00 General Description 76-00-00 ENGINE CONTROLS - MAINTENANCE ............76-00-00 General 76-00-00 Control Quadrant Disassembly/Assembly 76-00-00 Throttle Control Cables Removal/Installation 76-00-00...
  • Page 620 AQUILA AT01-100 MAINTENANCE MANUAL...

  • Page 621: Engine Controls - General

    AQUILA AT01-100 Engine Controls MAINTENANCE MANUAL ENGINE CONTROLS - GENERAL Introduction This chapter describes the controls with which the engine is operated, such as throttle control. It does not include units that are controlled themselves, and units or components which are specifically included in other chapters.
  • Page 622 AQUILA AT01-100 MAINTENANCE MANUAL...

  • Page 623: Engine Controls - Maintenance

    AQUILA AT01-100 Engine Controls MAINTENANCE MANUAL ENGINE CONTROLS - MAINTENANCE General For propeller speed control adjustment/test procedures, refer to 61-20-00. For carburetor heat control adjustment/test procedures, refer to 71-60-00. Control Quadrant Disassembly/Assembly For control quadrant disassembly/assembly, refer to figure 201.
  • Page 624 AQUILA AT01-100 Engine Controls MAINTENANCE MANUAL rear stop adjusting bolts Detail- Control Quadrant Assembly Figure 201 Page 202 76-00-00 30.04.13...

  • Page 625: Governor Control Cable Removal/Installation

    AQUILA AT01-100 Engine Controls MAINTENANCE MANUAL Governor Control Cable Removal/Installation Remove Governor Control Cable (1) Remove engine cowling (refer to 71-10-00). (2) Remove access panels 211 FT, 211 FB, 211 EC (refer to 25-12-00) i n the cabin (3) Disconnect governor control cable from governor control arm.

  • Page 626: Choke Control Adjustment/Test

    AQUILA AT01-100 Engine Controls MAINTENANCE MANUAL (5) Move throttle control lever between idle and full throttle positions. Ensure the throttle control lever is only limited by the throttle control arm stops on the carburetors and has positive clearance of 1 mm (0.04 in.) to the console slot in both the full forward and full aft positions.
  • Page 627 AQUILA AT01-100 MAINTENANCE MANUAL CHAPTER 77 ENGINE INDICATING...
  • Page 628 AQUILA AT01-100 MAINTENANCE MANUAL...
  • Page 629 AQUILA AT01-100 Engine Indicating MAINTENANCE MANUAL TABLE OF CONTENTS Chapter Section Title Subject Page Effectivity ENGINE INDICATING - GENERAL..............77-00-00 Introduction 77-00-00 General Description 77-00-00 POWER INDICATION - MAINTENANCE...........77-10-00 Analog instr. General 77-10-00 Analog instr. Tachometer Removal/Installation 77-10-00 Analog instr. Manifold Pressure Gauge Removal/Installation 77-10-00 Analog instr.
  • Page 630 AQUILA AT01-100 MAINTENANCE MANUAL...

  • Page 631: Engine Indicating - General

    AQUILA AT01-100 Engine Indicating MAINTENANCE MANUAL ENGINE INDICATING - GENERAL Introduction This chapter describes those systems and components which indicate engine operation. Refer to 28-00-00 for further information on fuel pressure and fuel quantity measuring systems. Refer to 79-00-00 for further information on oil pressure and oil temperature measuring systems.
  • Page 632 AQUILA AT01-100 MAINTENANCE MANUAL...

  • Page 633: Power Indication - Maintenance

    AQUILA AT01-100 Engine Indicating MAINTENANCE MANUAL POWER INDICATION - MAINTENANCE General Propeller speed is indicated by a tachometer which is mounted on the instrument panel. The tachometer receives an electrical signal from a sensor mounted on the internal alternator casing at the rear end of the engine.
  • Page 634 AQUILA AT01-100 MAINTENANCE MANUAL...

  • Page 635: Power Indication - Maintenance

    AQUILA AT01-100 Engine Indicating MAINTENANCE MANUAL POWER INDICATION - MAINTENANCE General Propeller speed indication is included in the engine monitoring system. Propeller/engine speed is measured by a sensor mounted on the internal alternator casing at the rear end of the engine and electrically connected to the engine data converter (EDC).
  • Page 636 AQUILA AT01-100 MAINTENANCE MANUAL...

  • Page 637: Temperature Indication - Maintenance

    AQUILA AT01-100 Engine Indicating MAINTENANCE MANUAL TEMPERATURE INDICATION - MAINTENANCE General Cylinder head temperature is measured by a temperature-sensitive sensor that is mounted in the no. 3 cylinder head. The indicator is located in the cluster of engine gauges on the right instrument panel.
  • Page 638 AQUILA AT01-100 Engine Indicating MAINTENANCE MANUAL Carburetor Temperature Sensor Removal/Installation (optional) Remove Carburetor Temperature Sensor (1) Ensure electrical power to aircraft is OFF. (2) Remove engine cowling (refer to 71-10-00). (3) Disconnect battery (refer to 24-30-00). (4) Disconnect electrical lead to sensor.

  • Page 639: Carburetor Temperature Sensor Removal/Installation

    AQUILA AT01-100 Engine Indicating MAINTENANCE MANUAL TEMPERATURE INDICATION - MAINTENANCE General Cylinder head temperature indication is included in the engine monitoring system. Temperature is measured by a type K thermocouple electrically connected to the engine data converter (EDC). The cylinder head temperature (CHT) is measured in the head of the no. 3 cylinder.
  • Page 640 AQUILA AT01-100 Engine Indicating MAINTENANCE MANUAL Install Carburetor Temperature Sensor (1) Install sensor head and new copper sealing washer. Secure with Loctite (medium strength). CAUTION: TIGHTEN THE SENSOR HEAD CAREFULLY TO AVOID STRIPPING THE THREAD. (2) Connect electrical connector to sensor.

  • Page 641: Engine Monitoring System - Maintenance

    AQUILA AT01-100 Engine Indicating MAINTENANCE MANUAL ENGINE MONITORING SYSTEM - MAINTENANCE General The aircraft is equipped with an Electronics International MVP-50 glass panel engine monitor. The system consists of four major components: - the MVP display, - the EDC-33 engine data converter, - the probes and transducers and - the wiring and extension cables.
  • Page 642 AQUILA AT01-100 Engine Indicating MAINTENANCE MANUAL Install Engine Data Converter (1) Position EDC at back of instrument panel and attach with screws. (2) Connect electrical connectors to EDC. (3) Install glare shield (refer to 31-10-00). (4) Reconnect battery (refer to 24-30-00).
  • Page 643 AQUILA AT01-100 MAINTENANCE MANUAL CHAPTER 78 EXHAUST...
  • Page 644 AQUILA AT01-100 MAINTENANCE MANUAL...
  • Page 645 AQUILA AT01-100 Exhaust MAINTENANCE MANUAL TABLE OF CONTENTS Chapter Section Title Subject Page Effectivity EXHAUST SYSTEM - GENERAL ..............78-00-00 Introduction 78-00-00 General Description 78-00-00 EXHAUST SYSTEM - MAINTENANCE ............78-00-00 General 78-00-00 Exhaust System Removal/Installation 78-00-00 Main Muffler Inspection/Check 78-00-00 Page 1 78 - TOC 30.04.13...
  • Page 646 AQUILA AT01-100 MAINTENANCE MANUAL...
  • Page 647 AQUILA AT01-100 Exhaust MAINTENANCE MANUAL EXHAUST SYSTEM - GENERAL Introduction This chapter describes such systems and components which direct the engine exhaust gases out of the engine compartment. General Description The exhaust system comprises four exhaust pipes (from each cylinder), a main muffler, a second muffler and a tailpipe.
  • Page 648 AQUILA AT01-100 Cooling System MAINTENANCE MANUAL...
  • Page 649 AQUILA AT01-100 Exhaust MAINTENANCE MANUAL EXHAUST SYSTEM - MAINTENANCE General Each engine cylinder has an exhaust pipe leading down to the main muffler that is located beneath the engine. The exhaust pipes and a second muffler are connected to the main muffler over ball joints.
  • Page 650 AQUILA AT01-100 Exhaust MAINTENANCE MANUAL (d) Submerge pressurized muffler in water and inspect for leaks. (e) If any leaks are detected, the muffler must be removed from service and repaired or replaced. (f) Remove muffler from water, remove test plugs and dry muffler with compressed air.
  • Page 651 AQUILA AT01-100 MAINTENANCE MANUAL CHAPTER 79...
  • Page 652 AQUILA AT01-100 MAINTENANCE MANUAL...
  • Page 653 AQUILA AT01-100 MAINTENANCE MANUAL TABLE OF CONTENTS Chapter Section Title Subject Page Effectivity OIL - GENERAL ....................79-00-00 Introduction 79-00-00 General Description 79-00-00 OIL TANK - MAINTENANCE ................79-10-00 General 79-10-00 Oil Tank Removal/Installation 79-10-00 Oil Tank Cleaning 79-10-00 OIL COOLER - MAINTENANCE ..............79-20-00...
  • Page 654 AQUILA AT01-100 MAINTENANCE MANUAL...

  • Page 655: Oil - General

    AQUILA AT01-100 MAINTENANCE MANUAL OIL - GENERAL Introduction This chapter covers those units and components which are not part of the engine but store and/or supply lubricating oil to/from the engine or indicate oil condition. For additional information on the internal engine oil system components, refer to the respective engine manufacturer’s publications.
  • Page 656 AQUILA AT01-100 MAINTENANCE MANUAL Oil Circuit The oil pump sucks the engine oil from the oil tank via the oil cooler and forces it through the oil filter to the points of lubrication in the engine. Surplus oil emerging from the points of lubrication accumulates on the bottom of the crankcase and is forced back to the oil tank by the blow-by gases.

  • Page 657: Oil Tank - Maintenance

    AQUILA AT01-100 MAINTENANCE MANUAL OIL TANK - MAINTENANCE General The oil tank is attached to the engine mount on the right-hand side of the engine. It can be removed and/or disassembled (figure 201) for maintenance. The oil tank must be removed, disassembled and cleaned when oil contamination is detected.
  • Page 658 AQUILA AT01-100 MAINTENANCE MANUAL clamp oil tank cover O-ring baffle insert partition sealing ring drain screw Oil Tank Disassembly Figure 201 Page 202 79-10-00 30.04.13...

  • Page 659: Oil Cooler - Maintenance

    AQUILA AT01-100 MAINTENANCE MANUAL OIL COOLER - MAINTENANCE General The oil cooler is mounted in front of the radiator on the inner forward part of the lower engine cowling behind the main air intake. The oil inlet and outlet hose assemblies are connected to the oil cooler casing.
  • Page 660 AQUILA AT01-100 MAINTENANCE MANUAL Detail- heat protection sleeve rubbing protection from/to engine mounting bracket Detail- oil cooler Oil Cooler Installation Figure 201 Page 202 79-20-00 30.04.13...

  • Page 661: Oil Pressure Indication - Maintenance

    AQUILA AT01-100 MAINTENANCE MANUAL OIL PRESSURE INDICATION - MAINTENANCE General The oil pressure indicating system consists of an oil pressure transducer, an oil pressure indicator and wiring connecting the two components. The oil pressure transducer is mounted on the right side of the oil pump casing. The oil pressure transducer is a membrane pressure transducer with a built-in current source.
  • Page 662 AQUILA AT01-100 MAINTENANCE MANUAL...

  • Page 663: Oil Pressure Indication - Maintenance

    AQUILA AT01-100 MAINTENANCE MANUAL OIL PRESSURE INDICATION - MAINTENANCE General Engine oil pressure indication is included in the engine monitoring system. Pressure is measured by a pressure transducer electrically connected to the engine data converter (EDC). Engine oil pressure is measured on the right side of the oil pump casing.
  • Page 664 AQUILA AT01-100 MAINTENANCE MANUAL...

  • Page 665: Oil Temperature Indication - Maintenance

    AQUILA AT01-100 MAINTENANCE MANUAL OIL TEMPERATURE INDICATION - MAINTENANCE General The oil temperature indicating system consists of a temperature sensor, an oil temperature indicator and wiring connecting the two components. Oil temperature is measured in the oil filter / oil pump area. The resistance-type sensor functions with system voltage.
  • Page 666 AQUILA AT01-100 MAINTENANCE MANUAL...

  • Page 667: Oil Temperature Indication - Maintenance

    AQUILA AT01-100 MAINTENANCE MANUAL OIL TEMPERATURE INDICATION - MAINTENANCE General Engine oil temperature indication is included in the engine monitoring system. Temperature is measured by a type K thermocouple electrically connected to the engine data converter (EDC). Engine oil temperature is measured in the oil filter / oil pump area.
  • Page 668 AQUILA AT01-100 MAINTENANCE MANUAL...
  • Page 669 AQUILA AT01-100 MAINTENANCE MANUAL CHAPTER 80 STARTING...
  • Page 670 AQUILA AT01-100 MAINTENANCE MANUAL...
  • Page 671 AQUILA AT01-100 Starting MAINTENANCE MANUAL TABLE OF CONTENTS Chapter Section Title Subject Page Effectivity STARTING - GENERAL..................80-00-00 Introduction 80-00-00 General Description 80-00-00 STARTER - MAINTENANCE................80-11-00 General 80-11-00 Starter Removal/Installation 80-11-00 Page 1 80 - TOC 30.04.13...
  • Page 672 AQUILA AT01-100 MAINTENANCE MANUAL...
  • Page 673 AQUILA AT01-100 Starting MAINTENANCE MANUAL STARTING - GENERAL Introduction This chapter describes the starter as a component of the starting system. General Description The starting system comprises the starter, a relay and the ignition/starter switch. The starter is mounted at the rear lower right side of the engine. During the engine starting process, the starter pinion gear drives the crankshaft through a freewheel ring gear and turns the engine over.
  • Page 674 AQUILA AT01-100 Cooling System MAINTENANCE MANUAL...
  • Page 675 AQUILA AT01-100 Starting MAINTENANCE MANUAL STARTER - MAINTENANCE General The aircraft is equipped with a direct-drive 12V DC starter. The starter is mounted at the rear lower right side of the engine. During starting, a starter relay is activated by the ignition key. Its contacts close and electrical current energizes the starter motor.
  • Page 676 AQUILA AT01-100 Cooling System MAINTENANCE MANUAL...
  • Page 677 AQUILA AT01-100 MAINTENANCE MANUAL CHAPTER 91 CHARTS AND DIAGRAMS...
  • Page 678 AQUILA AT01-100 MAINTENANCE MANUAL...
  • Page 679 AQUILA AT01-100 Charts and Diagrams MAINTENANCE MANUAL TABLE OF CONTENTS Chapter Section Title Subject Page Effectivity CHARTS AND DIAGRAMS - GENERAL ............91-00-00 Introduction 91-00-00 Electrical Symbols 91-00-00 Wiring Diagrams 91-00-00 Wire Routing Diagrams 91-00-00 Antenna Overview 91-00-00 Page 1 91 - TOC...
  • Page 680 AQUILA AT01-100 MAINTENANCE MANUAL...
  • Page 681 AQUILA AT01-100 Charts and Diagrams MAINTENANCE MANUAL CHARTS AND WIRING DIAGRAMS - GENERAL Introduction This chapter includes several wiring diagrams for reference purposes. Electrical Symbols Below a collection of electrical symbols used in the wiring diagrams: connector, single pole, male...
  • Page 682 AQUILA AT01-100 Charts and Diagrams MAINTENANCE MANUAL Wiring Diagrams The wiring diagrams listed below define the wiring of the basic electrical equipment. No. Wiring diagram Ref. Fig. Effectivity Ignition System and Fuel Pump Fig. 1 (2) Battery, External Alternator and S tarter Fig.
  • Page 683 AQUILA AT01-100 Charts and Diagrams MAINTENANCE MANUAL S I2 DEV582 LINE P724 7021AR18s-wh 7021AL18s-wh LOAD ignition switch 8050B16 GND M1a 7021BL18s-wh P1071 8050C16N GND M4 P1540 P1538 DEV664 brown brown violet DEV663 violet DEV662 7020D20 see: Battery, External Alternator and Starter...
  • Page 684 AQUILA AT01-100 Charts and Diagrams MAINTENANCE MANUAL ALT 1 see: Ammeter battery relay starter relay battery Battery, External Alternator and Starter Figure 2 (1) Page 4 91-00-00 24.10.13...
  • Page 685 AQUILA AT01-100 Charts and Diagrams MAINTENANCE MANUAL ALT 1 Starter Relay Excitation ground power auxiliary relay see: Warning Lights see: Warning Lights see: External Power see: External Power see: Ignition System and Fuel Pump see: Ignition System and Fuel Pump...
  • Page 686 AQUILA AT01-100 Charts and Diagrams MAINTENANCE MANUAL LINE ALT 2 25 A LOAD 8213E12 8213A20 C M1 P1512 8213F12N X M1 8213G12-ye DEV667 8213H12-ye Internal Alternator Figure 3 EFFECTIVITY Page 6 Aircraft equipped for Night-VFR 91-00-00 24.10.13...
  • Page 687 AQUILA AT01-100 Charts and Diagrams MAINTENANCE MANUAL GND M1b P1563 8212E20 P1564 J M1 P1595 P1566 P1569 P1596 8212B04 8212A04 see: Battery, External Alternator and Starter P1597 P1598 DEV674 P1594 P1567 P1568 ENABLE 8212A20 8212D20 RL M3 ground power relay...
  • Page 688 AQUILA AT01-100 Charts and Diagrams MAINTENANCE MANUAL Warning Lights voltage monitoring module ground terminals Voltage Monitoring Figure 5 EFFECTIVITY Page 8 Aircraft equipped for Night-VFR 91-00-00 24.10.13...
  • Page 689 AQUILA AT01-100 Charts and Diagrams MAINTENANCE MANUAL P1018 P1020 fuel sensor LH fuel sensor RH Fuel Indicating System Figure 6 Page 9 91-00-00 24.10.13...
  • Page 690 AQUILA AT01-100 Charts and Diagrams MAINTENANCE MANUAL Warning Lights Circuit breaker ratings that are not shown depend on the configuration. Refer to the wiring diagram of the particular option. Stall Warning Trim Control Attitude Indicator Trim Actuator Turn Coordinator Flap Control...
  • Page 691 AQUILA AT01-100 Charts and Diagrams MAINTENANCE MANUAL Circuit Breakers and Switches Figure 7 (2) Page 11 91-00-00 24.10.13...
  • Page 692 AQUILA AT01-100 Charts and Diagrams MAINTENANCE MANUAL X I1 P938 P939 ammeter TB I3 P1497 P1505 Ammeter Figure 8 EFFECTIVITY Page 12 Aircraft equipped with analog engine instruments 91-00-00 24.10.13...
  • Page 693 AQUILA AT01-100 Charts and Diagrams MAINTENANCE MANUAL P1611 MVP-0000-or P1612 MVP-0000-br Ammeter Figure 9 EFFECTIVITY Page 13 Aircraft equipped with MVP-50 91-00-00 24.10.13...
  • Page 694 AQUILA AT01-100 Charts and Diagrams MAINTENANCE MANUAL LINE Warning Lights LOAD 7030B20 7030C20 7030D20 7030E20 ALT 1 ALT 2 VOLT P/S HEAT FUEL L I1 L I2 L I3 L I4 L I5 Warning Lights Figure 10 EFFECTIVITY Page 14...
  • Page 695 AQUILA AT01-100 Charts and Diagrams MAINTENANCE MANUAL LINE Warning Lights LOAD annunciator panel FUEL TEST ALT 1 ALT 2 VOLT PRESS (red) (amber) HEAT P1714 TB I4 TB I1 P1706 8260e22 * The warning light FUEL PRESS is not used if an MVP-50 is installed.
  • Page 696 AQUILA AT01-100 Charts and Diagrams MAINTENANCE MANUAL Dome Light cabin light NAV light LH Lights Figure 12 (1) Page 16 91-00-00 24.10.13...
  • Page 697 AQUILA AT01-100 Charts and Diagrams MAINTENANCE MANUAL landing light NAV light RH Lights Figure 12 (2) Page 17 91-00-00 24.10.13...
  • Page 698 AQUILA AT01-100 Charts and Diagrams MAINTENANCE MANUAL Instruments 1 CHT (OAT) Oil temperature Engine Indicating Figure 13 (1) EFFECTIVITY Page 18 Aircraft equipped with analog engine instruments 91-00-00 24.10.13...

  • Page 699: Engine Indicating

    AQUILA AT01-100 Charts and Diagrams MAINTENANCE MANUAL Instruments 2 Fuel Gauge Oil pressure Left Right see: Fuel Indicating System Engine Indicating Figure 13 (2) EFFECTIVITY Page 19 Aircraft equipped with analog engine instruments 91-00-00 24.10.13...
  • Page 700 AQUILA AT01-100 Charts and Diagrams MAINTENANCE MANUAL LINE Panel Light dimmer IC 101 LOAD SP826 SP823 J585 P1732 9341Ba22 9341Ba22N TB I1 P1723 P 101 dimmer P1740 9341Bg22N 9341Bg22 DEV708 P1739 P1733 J586 P1742 9341Bf22N 9341Bf22 P1741 DEV709 Instrument Lighting...

  • Page 701: Stall Warning System

    AQUILA AT01-100 Charts and Diagrams MAINTENANCE MANUAL LINE Stall Warning LOAD warning buzzer J575 P1418 9410A20 9410B20-rd 9410C20-bk 9410D20 9410D20N TB I1 P1426 S F1 stall warning P1434 P1435 Stall Warning System Figure 15 Page 21 91-00-00 24.10.13...
  • Page 702 AQUILA AT01-100 Charts and Diagrams MAINTENANCE MANUAL rear fuselage end switch spindle drive trim motor Elevator Trim System Figure 16 (1) Page 22 91-00-00 24.10.13...

  • Page 703: Instrument Panel

    AQUILA AT01-100 Charts and Diagrams MAINTENANCE MANUAL instrument panel Trim Control Trim Actuator center console trim indicator trim switch Elevator Trim System Figure 16 (2) Page 23 91-00-00 24.10.13...
  • Page 704 AQUILA AT01-100 Charts and Diagrams MAINTENANCE MANUAL Flap Flap Control Actuator Cruise Takeoff Landing Flap Control System Figure 17 (1) Page 24 91-00-00 24.10.13...
  • Page 705 AQUILA AT01-100 Charts and Diagrams MAINTENANCE MANUAL LED takeoff position LED cruise position Cruise Takeoff Landing LED landing position Flap Control System Figure 17 (2) Page 25 91-00-00 24.10.13...
  • Page 706 AQUILA AT01-100 Charts and Diagrams MAINTENANCE MANUAL heated pitot-static tube Pitot Heating System Figure 18 (1) EFFECTIVITY Page 26 Aircraft equipped with pitot heating system 91-00-00 24.10.13...
  • Page 707 AQUILA AT01-100 Charts and Diagrams MAINTENANCE MANUAL Relay NO Relay C Heater 1 Heater 2 control box for heated pitot-static tube Pitot Heating System Figure 18 (2) EFFECTIVITY Page 27 Aircraft equipped with pitot heating system 91-00-00 24.10.13...
  • Page 708 AQUILA AT01-100 Charts and Diagrams Charts and Diagrams MAINTENANCE MANUAL LINE 12V DC Receptacle LOAD +12V TB I1 12V Power Supply Figure 19 Page 28 91-00-00 24.10.13...
  • Page 709 AQUILA AT01-100 Charts and Diagrams MAINTENANCE MANUAL Headset Console Figure 20 Page 29 91-00-00 24.10.13...
  • Page 710 AQUILA AT01-100 Charts and Diagrams MAINTENANCE MANUAL C36b Instruments 1 ground terminals resistive fuel module see: Fuel Indicating System Engine Monitoring System Figure 21 (1) EFFECTIVITY Page 30 Aircraft equipped with MVP-50 91-00-00 24.10.13...
  • Page 711 AQUILA AT01-100 Charts and Diagrams MAINTENANCE MANUAL X M8 engine connector fuel pressure sensor oil pressure sensor oil temp. sensor outboard temp. sensor carburetor temp. sensor engine connector eng. speed sensor Engine Monitoring System Figure21 (2) EFFECTIVITY Page 31 Aircraft equipped with MVP-50 91-00-00 24.10.13...
  • Page 712 AQUILA AT01-100 Charts and Diagrams MAINTENANCE MANUAL Wire Routing Diagrams The wire routing diagrams listed below define the wiring of the basic electrical equipment. No. Wire routing diagram Ref. Fig. Effectivity (1) Antennas Fig. 1 300 - 306 (2) Antennas Fig.
  • Page 713 AQUILA AT01-100 Charts and Diagrams MAINTENANCE MANUAL Legend: ELT antenna ROD ELT antenna WHP GPS antenna COM2 antenna FLARM antenna ADSB antenna marker beacon antenna XPDR antenna NAV antenna COM1 antenna Antennas - Wire Routing Figure 1 EFFECTIVITY Page 33...
  • Page 714 AQUILA AT01-100 Charts and Diagrams MAINTENANCE MANUAL Legend: ELT antenna ROD ELT antenna WHP combined GPS/COM2 antenna GPS antenna NAV antenna COM1 antenna FLARM antenna ADSB antenna marker beacon antenna 10 XPDR antenna Antennas - Wire Routing Figure 1 EFFECTIVITY...
  • Page 715 AQUILA AT01-100 Charts and Diagrams MAINTENANCE MANUAL Legend: ELT antenna ROD ELT antenna WHP combined GPS/COM2 antenna GPS antenna NAV antenna COM1 antenna FLARM antenna ADSB antenna marker beacon antenna 10 XPDR antenna Antennas - Wire Routing Figure 1 EFFECTIVITY...
  • Page 716 AQUILA AT01-100 Charts and Diagrams MAINTENANCE MANUAL Legend: GMU 44 GRS 77 GTP 59 GDC 741 GDU 620 fuselage connector G500 Garmin G500 - Wire Routing Figure 2 Page 36 91-00-00 24.10.13...
  • Page 717 AQUILA AT01-100 Charts and Diagrams MAINTENANCE MANUAL Legend: dome light connector, dome light connector landing light landing light NAV lights LH Pitot heat fuel sensor LH stall warning sensor fuel sensor RH NAV lights RH Wings and Lights - Wire Routing...
  • Page 718 AQUILA AT01-100 Charts and Diagrams MAINTENANCE MANUAL Legend: alternator 1 ignition box engine connector fuselage connector trim indicator to flap actuator to trim motor wing connector head set console 10 alt. rectifier reg. unit 11 fuel pump 12 ext. power receptacle 13 alternator 2 Misc.
  • Page 719 AQUILA AT01-100 Charts and Diagrams MAINTENANCE MANUAL Antenna Overview The diagram below defines the position of the various antennas. Legend: ELT antenna ROD ELT antenna WHP GPS antenna COM2 antenna FLARM antenna ADSB antenna marker beacon antenna XPDR antenna NAV antenna...
  • Page 720 AQUILA AT01-100 Charts and Diagrams MAINTENANCE MANUAL Legend: ELT antenna ROD ELT antenna WHP combined GPS/COM2 antenna GPS antenna NAV antenna COM1 antenna FLARM antenna ADSB antenna marker beacon antenna XPDR antenna Antenna Overview Figure 1 EFFECTIVITY Page 40 307 - 999 91-00-00 24.10.13...

This manual is also suitable for:

At01-100aAt01-100c

Table of Contents