Raytheon Beechcraft Bonanza 35 Series, Руководство по ремонту

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BONANZA 35 SERIES SHOP MANUAL
Page 27
B21 Aug 29/03
Section 7
INSPECTION AFTER ENCOUNTERING TURBULENT AIR (Continued)
c. Inspect aileron, aileron tab and flaps for
wrinkles or cracks.
d. Inspect internal structure and fuel cells
through access panels.
e. Inspect plumbing and wiring for security of
attachment.
Nose Structure a. Check external skin surface for cracks,
wrinkles and loose or missing rivets.
b. Inspect area forward of windshield for
evidence of structural deformation or failure.
Fuselage, Center Section Inspect external skin surface for cracks,
abnormal wrinkles and loose or missing rivets.
Fuselage, Aft a. Inspect the entire length of the external skin
surface for cracks, stress wrinkles and loose
or missing rivets.
b. Check the empennage surfaces for damage
and free movement.
c. Inspect for skin wrinkles at the juncture of
the fuselage and empennage.
SECOND LEVEL INSPECTION As required
NOTE
Because G 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.
Wing Carry-thru Structure a. Dye check wing attachment fittings,
examine (magnaflux or replace) attachment
bolts and check bolt holes for alignment and
correct dimension.
b. Remove floorboards and access plates and
inspect the front and rear spar and keel
structure for evidence of deformation or
structural failure.
c. Operational test plumbing, wiring, flaps,
control cables, pulley mounts and any other
system found in this area.
Nose Structure a. Inspect areas surrounding the engine
support fittings.
b. Inspect internal structure for cracks or
damage.
ITEM INSPECTION REQUIREMENT INSPECTION INTERVAL