THRUSH AIRCRAFT, INC – MODEL S2R-G10
AIRCRAFT MAINTENANCE MANUAL
Page
6-14 Effective: 03/26/2010
FIGURE 6-6: TAIL LANDING GEAR
After the components have been installed,
seal the contact edges where the spring
P/N 5079-1 upper support block P/N
94131-9, lower support block P/N 94131-
11 and spacer P/N 95207-1 come together
with a high quality flexible silicone sealant
or fuel tank sealant to AMS-S-8802
(formerly MIL-S-8802) to help block the
collection of potential corrosive
contaminants in this area.
A. Place elevator in a 17 (±1) degrees
down position.
B. Connect lock cable to pivot arm.
C. Assure lock pin is flush with bottom of
lock pin guide when making final
adjustment to lock cable turnbuckle.
D. Adjust top plate as required to assure
straight travel of aircraft tail wheel when
tail gear is locked.
DISASSEMBLY OF SPINDLE HOUSING
ASSEMBLY Carefully lower aircraft to ground and
remove Jack. Ref. figure 6-7
Recheck tire inflation pressure (12.5x4.5
10pr) is 55psi max.
A. If desired, remove bolts, nuts and
washers that bolt tail wheel fork to
spindle.
TAIL LANDING GEAR RIGGING
B. Remove bolts, nuts, and washers that
bolt centering arm to top of spindle
and remove centering arm. Note
orientation for proper reassembly.
Rigging will be required if lock cable or
elevator travel stops have been altered in
any way. Rig as follows:
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