Raytheon Beechcraft Bonanza 35 Series, Руководство по ремонту

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BONANZA 35 SERIES SHOP MANUAL
Page 21
B21 Aug 29/03
Section 7
WHEN OPERATING IN AREAS OF HIGH HUMIDITY (Continued)
Wing Remove wing and center section access
covers and check for corrosion. At a scheduled inspection.
Empennage Remove all fuselage access covers and check
for corrosion. At a scheduled inspection.
AFTER RECEIPT OF THE AIRPLANE
Wing Check torque of the wing attach bolts. After the first 100 hours and at the
first 100 hours after adjustment of
the wing.
OPERATING FROM VERY SOFT OR UNUSUAL TERRAIN
LANDING GEAR
Tires Visually check for cuts, wear, deterioration
and inflation. Routine.
Main Landing Gear Check strut inflation.
a. Wheels 1. Check for obvious damage. Routine.
2. Remove and clean; inspect for abrasions,
cracks and chipped rims, bearing for wear,
corrosion, fretting and bluing; check seals for
distortion, deterioration, and proper fit and
security. Every 100 hours and/or annually.
b. Brake Units 1. Check cylinders and associated lines for
damage and leaks. Routine.
2. Check for evidence of overheating. Every 100 hours and/or annually.
3. Check discs for scoring, distortion,
damaged plating and evidence of overheating. Every 100 hours and/or annually.
c. Shock Absorber Check surfaces for cleanliness, free from oil or
grease deterioration. Every 100 hours and/or annually.
d. Wheel Wells Clean foreign material (dirt, etc.) from wheel
wells. Inspect supports between main and aft
spars in upper wheel well and the lift leg attach
bracket at the main spar for deformation,
cracks, etc. As required.
Nose Landing Gear
a. Wheel 1. Visually check for obvious damage. Routine.
2. Remove and clean. Inspect for abrasions,
cracks and chipped rims, bearings for wear,
corrosion, fretting and bluing; check seals for
distortion, deterioration, proper fit and
security. Every 100 hours.
ITEM INSPECTION REQUIREMENT INSPECTION INTERVAL