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MAINTENANCE MANUAL
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CAUTION: DO NOT MAKE A STEERING INPUT GREATER THAN 45 DEGREES WITH THE
_______ UPPER TORSION LINKS LOWERED (AIR MODE). THIS CAN CAUSE DAMAGE TO THE AIRPLANE.
(9)
Turn the captain's tiller handle (31) clockwise from the center until it touches the stop. Hold it against the stop and make sure the angular movement of the steering collar (41, Detail E, Fig. 502) is 65 |1 degrees clockwise.
S 735-107
(10)
Release the captain's tiller (3) and let it go to the center without manual aid. Make sure the conditions that follow occur:
(a)
The tiller goes to the center in less than 4 seconds.
(b)
The steering collar (41) is less than |1 1/2 degrees from the center.
(c)
If the nose landing gear is more than |1-1/2 degrees from the center, do the steps that follow: 1) Adjust the tension in the cables NWSA and NWSB until the
nose landing gear is less than |1-1/2 degrees from the center (the tension of the cables must be in the limits shown in Table 502).
NOTE: Adjust one cable, then the other, in small
____
increments.
2) Remove the pressure from the left hydraulic system (AMM 29-11-00/201).
3) Put the nose landing gear to a position less than |1/4 degrees from the center. Make sure the rig pins NS1, NS2, NS3, and NS5 have a free fit.
4) Pressurize the left hydraulic system (AMM 29-11-00/201).
(d) If you adjusted the cables with step (a), make sure the rig pins NS1 through NS5 have a free fit. The nose landing gear must be less than |1/4 degree from the center when you do this.
NOTE: The rig pins have a free fit if you can remove or
____ install them with two fingers. It is possible that you will feel some resistance.
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(11) Do the tests in the two steps before this (9 and 10), but turn the Captain's tiller handle counterclockwise.
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CAUTION: DO NOT MAKE A STEERING INPUT GREATER THAN 45 DEGREES WITH THE
_______ UPPER TORSION LINKS LOWERED (AIR MODE). THIS CAN CAUSE DAMAGE TO THE AIRPLANE.
(12) Turn the captain's tiller handle clockwise until the tiller stop (14B, View B-B, Fig. 501) touches the stop bolt (14C). Make sure the maximum torque is not more than 30 pound-inches.
S 735-110
CAUTION: DO NOT MAKE A STEERING INPUT GREATER THAN 45 DEGREES WITH THE
_______ UPPER TORSION LINKS LOWERED (AIR MODE). THIS CAN CAUSE DAMAGE TO THE AIRPLANE.
(13)
Turn the captain's tiller handle counterclockwise until the tiller stop (14B) touches the stop bolt (14C). Make sure the maximum torque is not more than 30 pound-inches.
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(14)
Remove the pressure from the left hydraulic system
(AMM 29-11-00/201).
S 865-112
(15)
Put the airplane back to its initial condition if the tests are completed.
H.
Do the Test of the Rudder Pedal Steering
S 035-113
(1) Make sure the torsion links for the nose landing gear (42 and 44, View A, Fig. 502) are disconnected.
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(2) Make sure the upper torsion link (44) is held in a position to be clear of the nose wheel tires during movement.
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WARNING: MAKE SURE ALL PERSONS AND EQUIPMENT ARE AWAY FROM THE SYSTEM
_______ FOR THE NOSE WHEEL STEERING BEFORE YOU SUPPLY HYDRAULIC POWER TO THE SYSTEM. PARTS OF THE SYSTEM FOR THE NOSE WHEEL STEERING CAN TURN AND CAUSE INJURY TO PERSONS OR DAMAGE TO EQUIPMENT.
(3)
Pressurize the left hydraulic system to 2850 to 3150 psig
(AMM 29-11-00/201).
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(4)
Make sure the Captain's tiller handle is in the center, then do the steps that follow:
(a)
Push and hold the right rudder pedal on the Captain's side.
(b)
Make sure the steering collar turns 5 +2/-1 degrees clockwise.
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(5)
Release the Captain's rudder pedal and let the steering collar go back to the center without manual aid.
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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(114)
