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AIRCRAFT MAINTENANCE MANUAL
G: MAIN LANDING GEAR
Check the main landing gear attach-fittings and
1.
pivot bolts. Replace bolts if worn.
Check the tires and tubes, wheels, and brake
2.
discs and lining for general condition.
3.
Check the spindle for straightness and tightness.
Inspect rubber shock biscuits for distortion, splits
or evidence of compound deterioration. Inspect
4.
shock strut attachment bolts and replace if worn or
distorted. Use proper close tolerance NAS bolts
for replacements, not AN hardware.
Check tripod for cracks, especially in the area of
5.
welds.
Check condition of wheel bearings and lubricate
with MIL-G-81322 (Aeroshell 22) grease as
6.
required. Reassemble all wheel bearings. (See
chapter 6 for pertinent data.)
H: HYDRAULIC SYSTEM
Check the master cylinders, parking brake valves,
brake lines, brake calipers, all brake fittings, and
1.
brake bleeders for leakage, general condition, and
security.
Check brake fluid level in each master cylinder
2.
and top off with fresh MIL-H-5606 aviation
hydraulic fluid as required.
Check the operation and holding ability of the
3.
brake pedal and parking brakes. Bleed hydraulic
systems if required.
Remove, clean, and inspect leaf spring forward
attach bolt P/N NAS6206-38D every 100 hours.
Upon reassembly lubricate bolt and leaf spring
hole with Snap-on™ General Purpose Anti-seize
1.
or equivalent or MIL-G-81322 (Aeroshell 22)
grease.
Torque to specifications I/A/W Torque
chart (figure 2-7). Replace MS24665-300 cotter
pin after each inspection.
Effective: 03/26/2010
THRUSH AIRCRAFT, INC – MODEL S2R-G10
J: TAIL GEAR
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