Raytheon Beechcraft Bonanza 35 Series, Руководство по ремонту

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BONANZA 35 SERIES SHOP MANUAL
Page 24
Aug 29/03
B21
Section 7
INSPECTION AFTER HARD LANDING (Continued)
Fuselage Center Section a. Inspect external skin surface for cracks,
abnormal wrinkles and loose or missing rivets.
b. Inspect around cabin windows for structural
cracks.
Fuselage, Aft a. Check external skin surface the entire
length for cracks, abnormal wrinkles and loose
or missing rivets.
b. Inspect empennage and control surfaces for
freedom of movement.
SECOND LEVEL INSPECTION As required
NOTE
Because shock loading may be transmitted along one structural member to another, carefully inspect the
surrounding and supporting structure in any damaged area found in the first level inspection.
Landing Gear a. Place airplane on jacks and check shock
strut for free up and down movement.
b. Remove tires and inspect internally for cuts
or broken areas.
c. Disassemble and examine wheels (rims) for
cracks or distortion.
d. Visually inspect axle with 10-power glass. If
suspect, dye check or magnaflux.
e. Remove and replace or magnaflux the
landing gear attach bolts, check bolt holes for
cracks or elongation.
f. Remove and replace or magnaflux drag link
bolts and supports.
g. Perform landing gear retraction test.
Nose Structure a. If tips of propeller have been damaged, refer
to the applicable Engine Maintenance Manual
for engine inspection procedure.
b. Inspect areas surrounding the engine
support fittings.
c. Check the internal structure of the wheel
well for cracks or damage.
d. Test plumbing and wiring for proper
operation.
ITEM INSPECTION REQUIREMENT INSPECTION INTERVAL