Thrush Aircraft S2RHG-T65 TURBO THRUSH, Руководство по обслуживанию

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THRUSH AIRCRAFT, INC – MODEL S2RHG-T65 TURBO THRUSH
AIRCRAFT MAINTENANCE MANUAL
2-22
Effective 05/25/05
MAIN LANDING GEAR
(Continued)
Da
ily
50
HRS
100
HRS
400
HRS
5.
Check the master cylinders, parking brake valves,
brake lines, brake calipers, all brake fittings, and
brake bleeders for leakage, general condition, and
security.
X
6.
Check brake fluid level in each master cylinder
and top off with fresh MIL-H-5606 aviation
hydraulic fluid as required.
X
7.
Check the operation and holding ability of the
pedal and parking brakes. Bleed hydraulic
systems if required.
X X
TAIL GEAR
Da
ily
50
HRS
100
HRS
400
HRS
1.
Remove, clean, and inspect leaf spring forward
attach bolt P/N NAS6207-54D every 100 hours.
Upon reassembly lubricate bolt and leaf spring
hole with Snap-on™ General Purpose Antiseize 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 each
inspection.
X
2.
Inspect all bolts holes for elongation. As a general
rule, replace components with holes that are out-
of-round by 0.005” or more.
** CAUTION **
Replacement of the leaf spring
forward attach P/N NAS6207-54D
bolt with a larger diameter is not
approved. The leaf spring may not
be “drilled out” for a larger bolt.
X
3.
Inspect main spring leaf for corrosion and cracks.
Replace leaf spring as needed.
X
4.
Inspect P/N 95434-11 Acetal (Delrin®) lower
support block spacer for wear and cracks.
X