Eagle ICA-D212-725, Instructions Manual

Page: 324 / 729

ICA-D212-725 (53)
Page 19 of 19
CHAPTER 53 – FUSELAGE (53-00-00)

COPYRIGHT

2007 BY DART AEROSPACE LTD.

THIS DOCUMENT IS PRIVATE AND CONFIDENTIAL AND IS SUPPLIED ON THE EXPRESS CONDITION THAT IT IS NOT TO BE USED FOR ANY PURPOSE OR COPIED OR COMMUNICATED TO ANY
OTHER PERSON WITHOUT WRITTEN PERMISSION FROM DART AEROSPACE LTD.
Revision: 4
Date: 11.06.01
No.
Characteristic Inspection
Method
Limit
4 Mechanical
damage on one
spot face
Measure For a mechanical damage of <=0.040 inch (1.02 mm), remove
the depth of the damage. Do not remove more than 0.040 inch
(1.02 mm) from the cross hatched area.
5 Mechanical
damage to the
lug hole (not the
bushing hole)
Measure For a mechanical damage depth of <=0.020 inch (0.51 mm),
uniformly remove the depth of the damage around the periphery
of the hole. Do not remove more than 0.020 inch (0.51 mm)
from any part of the lug hole surface. Maintain original lug hole
centerline. Be-bush hole.
6 Mechanical
damage to the
bushing hole
Not allowed. Replace bushing.
Figure 53-10. Tail Rotor Gearbox Support Fitting - Damage and Corrosion Limits (Sheet 3 of 3)