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(4) S 835-010Make sure you can install the eccentric drum rig pin NS6 through the rig pin hole (24, View C-C, Fig. 501) in the forward bracket (23) and the eccentric drum (25).
NOTE:____ You must turn the eccentric hub on the interconnect mechanism to the air mode, against the pull of the interconnect springs, to install rig pin NS6.
(5) S 825-180Make sure the piston position rig pin NS7 (40, Detail A, Fig. 502) can be installed easily when there is no weight on the spring cartridge piston (45, Detail A, Fig. 502). Measure the free length of the spring cartridge (45) between the rod end centerlines. Make sure it is 17.20|0.01 inches for the 275N2059-1 and -2 spring cartridges and 16.51|0.01 inches for the 275N2059-3 spring cartridge.
(6) S 095-011Remove the rig pins NS6 and NS7.
(7) S 825-012Make sure the tension in the cables NGPPA (2) and NGPPB (5) is in tolerance (Table 501). Use the cable tensiometer. It is convenient to measure the NGPP cable tension at the back of the nose gear above the piston position quadrant.
(8) S 435-271Connect the torsion links (42 and 44, Fig. 502) (AMM 32-21-09/401).
(9) S 435-013Examine all of the adjustable rod ends in the piston position/rudder interconnect system to make sure the threads are engaged correctly. The end of the rod must fill at least half of the inspection hole.
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TASK 32-51-00-835-152
4. Rigging of the NGPP/Rudder Interconnect System (Fig. 501, 502)______________________________________________
A. General
(1)
There must be no more than a 5°F difference between the inner and the outer temperatures of the airplane. The temperatures must be stable for one hour or more before you do the rigging and also during the rigging.
(2)
Rig Pins from Set B20003-XX (AMM 20-10-24/201):
(a)
NS6 - P/N B20003-5
(b)
NS7 - P/N B20003-15
(3)
Cable Tensiometer, 0 to 200 pound range for
3/32 inch diameter cable - Commercially
Available
(4)
Line to hold the NLG Top Torsion Link (Rope or
Cord)
B.
Consumable Materials
(1)
C00308 Compound, Corrosion Preventive -MIL-C-11796
(2)
D00015 Grease, Corrosion Preventive - BMS 3-24
C.
References
(1)
AMM 07-11-02/201, Jacking Airplane Nose
(2)
AMM 20-10-24/201, Rig Pins
(3)
AMM 32-51-08/401, Nose Wheel Steering Spring Cartridge
D.
Access
(1)
Location Zones
115 NLG Wheel Well (Left)
116 NLG Wheel Well (Right)
119 Main Equipment Center (Left)
120 Main Equipment Center (Right)
211 Control Cabin (Left)
212 Control Cabin (Right)
711 Nose Landing Gear (NLG)
E.
Do the Rigging of the NGPP/Rudder Interconnect System
S 865-176
(1) Look at the indicator (58) on the steering collar (Detail E, Fig. 502) to make sure the nose wheels are less than 1/2 degree from the center.
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S 585-177
(2) If the indicator (58) is not there, lift the airplane nose on jacks (AMM 07-11-02/201) to put the nose wheels in the center.
NOTE: The nose wheels and the steering collar will go to the center
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本文鏈接地址：757 AMM 飛機維護手冊 起落架 CHAPTER 32 - LANDING GEAR 3(105)
