Cessna 510 Mustang Structural Repair Manual page 55

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A63506
Nominal
Fastener
Diameter
5/32
3/16
1/4
5/16
3/8
NOTE:
Same inspection procedure must be used for oversize diameters.
Above Fastener Head
Above Fastener Head
Copyright © Textron Aviation Inc.
Retain printed data for historical reference only. For future maintenance, use only current data.
Figure 2 : Sheet 2 : Check Blind Rivets for Collar and Stem Flushness
Spindle Position
B, Maximum
A, Maximum
Inch (mm)
0.010 (0.25)
0.012 (0.30)
0.015 (0.38)
0.019 (0.48)
0.023 (0.58)
A
C
Huck Blind Fasteners
FOR TRAINING PURPOSES ONLY
ISSUE 02 , JAN 2018
Inch (mm)
C, Maximum
0.010 (0.25)
Shall be flush
0.012 (0.30)
or below the
0.015 (0.38)
spindle top
0.019 (0.48)
land.
0.023 (0.58)
Spindle
Position
Below Fastener Head
Locking
Collar
Position
Below Fastener Head
Model 510 Structural Repair Manual (Rev 2)
51-40-03-0 (Rev 1)
Collar Position
D, Maximum
Inch (mm)
0.017 (0.43)
0.022 (0.56)
0.029 (0.74)
0.037 (0.94)
0.045 (1.14)
B
D
Print Date: Wed Mar 21 05:10:19 CDT 2018
6282T1121
Page 9 of 20

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