Cessna 510 Mustang Structural Repair Manual page 19

A60932
Maximum +0.05 or −0.05 Inch (+1.3 or −1.3 mm)
from Loft Contour
(adjusted for skin thickness)
Refer to Table 1.
NOTE:
Refer to Sheet 1 for zone locations.
Copyright © Textron Aviation Inc.
Retain printed data for historical reference only. For future maintenance, use only current data.
Figure 1 : Sheet 2 : Flushness Requirements and Tolerances
Loft Contour (corrected for
norminal skin thickness).
6.00 Inches
(152 mm)
FOR TRAINING PURPOSES ONLY
ISSUE 02 , JAN 2018
Model 510 Structural Repair Manual (Rev 2)
Maximum Local Deviation
(Waviness)
Print Date: Wed Mar 21 05:09:51 CDT 2018
51-00-03-0 (Original Issue)
Actual Contour
6782T1030
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