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0.687
0.75
0.812
0.875
0.937
1.0
RIVET LENGTH L
(INCHES)
FRACTION DASH
0.156
0.187
0.250
0.312
0.375
0.437
0.50
0.562
0.625
0.687
0.75
0.812
0.875
0.937
1.0
3
Cracks due to overheating are not acceptable, and rivets having these vertical cracks on either head must
be rejected. The batch which was overheated must be segregated and scrapped because the ductility
cannot be repaired by reheat treatment.
C. Removal.
(1) Remove rivets by drilling off the head and punching out the shank (refer to Figure 1). The procedure is as follows:
(a) File a flat area on the manufactured head of nonflush rivets.
Copyright © Textron Aviation Inc.
Retain printed data for historical reference only. For future maintenance, use only current data.
-11
0.469
-12
0.526
-13
0.598
-14
0.649
-15
0.716
-16
0.773
1/4 DIAMETER GRIP T
(INCHES)
MINIMUM MAXIMUM MINIMUM MAXIMUM MINIMUM MAXIMUM
-2.5
-3
-4
-5
0.091
-6
0.104
-7
0.176
-8
0.217
-9
0.266
-10
0.340
-11
0.386
- 12
0.446
-13
0.492
-14
0.549
-15
0.603
-16
0.676
A14937
Average Nominal Projection
Before Driving for
Rivets Up To One−Half Inch Long
Rivet
Diameter
C
(Inches)
(Inches)
0.062
0.093
0.093
0.120
0.125
0.156
0.156
0.156
0.187
0.180
0.250
0.150
0.312
0.256
0.375
0.406
FOR TRAINING PURPOSES ONLY
ISSUE 02 , JAN 2018
Model 510 Structural Repair Manual (Rev 2)
0.525
0.482
0.530
0.597
0.531
0.587
0.648
0.588
0.638
0.715
0.639
0.702
0.772
0.703
0.758
0.840
0.759
0.810
5/16 DIAMETER GRIP
T (INCHES)
0.103
0.175
0.216
0.265
0.242
0.298
0.339
0.299
0.355
0.385
0.356
0.410
0.445
0.411
0.467
0.491
0.468
0.524
0.548
0.525
0.581
0.602
0.582
0.630
0.675
0.631
0.687
0.728
0.688
0.744
C
(mm)
2.3
3.0
4.0
4.0
4.6
6.3
6.5
10.3
Print Date: Wed Mar 21 05:10:19 CDT 2018
51-40-03-0 (Rev 1)
0.454
0.513
0.514
0.569
0.570
0.625
0.626
0.680
0.681
0.736
0.737
0.791
3/8 DIAMETER GRIP T
(INCHES)
0.188
0.250
0.251
0.313
0.314
0.437
0.376
0.437
0.438
0.563
0.501
0.563
0.564
0.625
C
T
5582T1025
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