S 034-010
(7)
Remove the pin (1) to disconnect the brake rods from the inner cylinder of the shock strut.
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S 024-011
(8) Remove the brake rod (5).
TASK 32-11-19-404-012
3. Install the Brake Rod for the Main Landing Gear (Fig. 401)
_______________________________________________
A. Consumable Materials
(1)
C00174 Compound - Corrosion Prevention,
MIL-C-16173 grade 4
(2)
D00528 Grease - Royco 11MS
B.
Parts
~.............................................................................. | MM | | IPC | ................. ............................ | FIG | ITEM | NOMENCLATURE | SUBJECT |FIG | ITEM | ................................................................................ | 401 | 1 | Pin | 32-11-01 | 10 | 135 | | | 2 | End Cap | | | 130 | | | 3 | Nut | | | 125 | | | 4 | Washer | | | 124 | | | 5 | Brake Rod | | | 168 | | | 6 | Bolt | | | 123 | | | 7 | Pin | | | 145 | | | 8 | End Cap | | | 140 | | | 9 | Nut | | | 125 | | | 10 | Washer | | | 124 | | | 11 | Bolt | | | 123 | 2......…........…...................................…...........…....….........1
C. References
(1)
AMM 07-11-03/201, Jacking Airplane Axles
(2)
AMM 12-21-14/301, Main Gear and Actuating Mechanisms
(3)
AMM 32-00-20/201, Landing Gear Downlocks
(4)
AMM 32-45-01/401, Main Gear Wheel and Tire
D.
Access
(1)
Location Zones
211/212 Control Cabin
731/741 Main Landing Gear (MLG)
732/742 MLG Body Doors
733/743 MLG Oleo Doors
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E. Install the Brake Rods
S 624-013
(1)
Apply corrosion prevention compound to the inner diameter of the pins.
S 434-014
(2)
Apply Royco 11MS grease to the pin (1), the end cap (2), the lockbolt (6), the washer (4), and the nut (3). Install the parts to connect the brake rod to the inner cylinder of the shock strut.
(a)
Tighten the nut (3) to 100-200 pound-inches (View A-A).
(b)
Install the cotter pin through the nut (3).
S 424-015
(3)
Install the wheel and the tire on the main landing gear
(AMM 32-45-01/401).
S 844-016
(4)
Make sure the brake rod (5) does not touch the ground as the main landing gear is lowered to the ground.
S 584-017
(5)
Lower the main landing gear and remove the jack (AMM 07-11-03/201).
S 424-018
(6)
Connect the brake rod (5) to the brake by the subsequent steps:
(a)
Apply Royco 11MS grease to the pin (7), end cap (8), lockbolt (11), washer (10), nut (9), and the cotter pin.
(b)
Insert the pin (7) through the brake rod (5) and the brake assembly joint as shown on Fig. 401.
(c)
Insert the lockbolt (11) through the hole at the bottom of the recess in pin (7).
(d)
Insert the end cap (8) over the threaded end of the bolt (11).
(e)
Install the lockbolt (11) and the end cap (8) with the washer (10), and the nut (9) to the pin (7). 1) Tighten the nut (9) to 100-200 pound-inches (View B-B).
32-11-19 中国航空网 www.aero.cn 航空翻译 www.aviation.cn 本文链接地址：757 AMM 飞机维护手册 起落架 CHAPTER 32 - LANDING GEAR 1(119)
