Raytheon Beechcraft Bonanza 35 Series, Руководство по ремонту

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BONANZA 35 SERIES SHOP MANUAL
Page 15
B21 Aug 29/03
Section 7
D. WINGS AND CARRY-THROUGH STRUCTURE (Continued) MECH INSP
LH RH
13. WING SPAR CAP - Inspect the wing spar cap for corrosion. Refer to Section 4. See
Service Bulletin 2538.
14. WING BOLTS - Check wing bolts for proper torque at the first 100-hour inspection and
at the first 100-hour inspection after each reinstallation of the wing attach bolts. Refer to
Section 3 of this shop manual for wing bolt, nut and fitting inspection criterion and
frequency.
15. RADAR ANTENNA COVER - Check the fiberglass for security, attachment and cracks.
16. FUEL VENTS AND AIR INLETS, PITOT TUBE AND STALL WARNING VANE - Check
for condition and obstruction.
17. Perform the INSPECTION OF MAIN FUEL CELL FLAPPER VALVE procedure. Refer
to Section 3. NOTE - This inspection is to be performed at every second 100-Hour
inspection or every second Annual inspection.
E. NOSE GEAR MECH INSP
1. WHEEL AND TIRE - Check wheel for cracks and tire for wear, damage and proper
inflation. Check wheel bearings for condition and wear and lubrication.
2. LANDING GEAR STRUT - Inspect the shock strut and components for cracks,
attachment, proper inflation and evidence of leakage.
3. ACTUATING LINKAGE - Check for wear at attach points. Check for cracks and
security.
4. GEAR DOORS AND LINKAGE - Check doors for damage and cracks to the structure
and skins. Check linkage for wear and cracks at the attach points. Check for condition
and security.
5. NOSE GEAR STEERING LINKAGE - Inspect linkage for tightness, condition and
security. Inspect linkage boots for condition.
6. SHIMMY DAMPER - Check for condition and attachment. Check attach points for
cracks. Check fluid level per Section 2.
7. STRUT FLUID LEVEL - Check and maintain the proper fluid level in the strut as outlined
in Section 2.
8. STRUT AND A-FRAME HINGE BOLTS - Inspect for corrosion and security of
attachment.
9. STATIC CABLE (If installed) - Inspect for condition, proper clearances and attachment.
10. VISUAL INDICATOR - Check for condition.
11. NOSE LANDING GEAR DRAG BRACE (P/N 002-820016-31, P/N 002-820018-3, or
with Kit 35-4012-1 Installed) - Check that the two drag brace bracket attachment bolts
are secure. Check drag brace assembly for shear stress, wear and corrosion. At 2,000
hours, remove and inspect the two bracket attachment bolts. Replace all hardware with
evidence of shear stress, wear and/or corrosion.
100-HOUR OR ANNUAL INSPECTION (Continued)