Raytheon Beechcraft Bonanza 35 Series, Руководство по ремонту

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BONANZA 35 SERIES SHOP MANUAL
Page 23
B21 Aug 29/03
Section 7
INSPECTION AFTER HARD LANDING (Continued)
e. Inspect nose drag legs and gear door retract
linkage for damage.
f. Inspect landing gear lift leg attach bracket at
the main spar for deformation, cracks, etc.
g. Inspect area around landing gear attach
points.
Nose Structure a. Inspect external skin surfaces for distortion,
loose or missing rivets.
b. Check cowling attachment for alignment or
damage.
c. Inspect engine control cables for smooth
operation and check plumbing and wiring for
security and attachment.
d. Inspect engine support fittings for cracks or
structural failure.
e. Check tips of propeller for damage.
f. Check propeller spinner and backplate for
evidence of interference with cowling.
g. Inspect wheel well structure for damage or
cracks. Check area surrounding the landing
gear attachment points.
Wing Carry-thru Structure a. Check wing attachment fittings for cracks.
Perform a Dye Penetrant inspection.
b. Inspect plumbing, wiring and actuator for
damage and security of attachment.
c. Check keel, front and rear spar on the lower
side of fuselage for damage and alignment.
Wings a. Inspect external wing surface skin for
cracks, abnormal wrinkles and loose or
missing rivets.
b. Check wing attachment fittings for cracks
Perform a Dye Penetrant inspection.
c. Inspect internal structure.
d. Inspect plumbing and wiring for security of
attachment.
ITEM INSPECTION REQUIREMENT INSPECTION INTERVAL