(5)
AMM 32-09-07/201, Main Gear Truck Tilt Sensors
(6)
AMM 32-11-19/401, Main Gear Brake Rod
(7)
AMM 32-12-04/401, Main Gear Strut Door
(8)
AMM 32-41-10/401, Main Gear Wheel Brake
(9)
AMM 32-42-06/401, Antiskid Transducer
(10)
AMM 32-45-01/401, Main Gear Wheel and Tire
E.
Access
(1)
Location Zones
211/212 Control Cabin
731/741 Main Landing Gear (MLG)
732/742 MLG Body Doors
733/743 MLG Oleo Doors
F.
Install the Truck Assembly
S 844-031
(1)
Put the truck assembly in the correct position under the shock strut.
(2)
Lower the inner cylinder to align the holes for the pivot pin.
S 584-032
32-11-17
ALL ú ú 04 Page 408 ú Jan 28/00
A
757
MAINTENANCE MANUAL
(3) S 624-033Apply the corrosion prevention compound to the inner diameter of the pins (1, 8).
(4) S 424-034Install the thread protector. Apply Royco 11MS lubricant to the pin (8), the washer (9) and the nut (13). Install these parts to connect the truck assembly (7) to the inner cylinder of the shock strut. Tighten the nut (13) to 150-200 pound-feet. Loosen the nut, then tighten to 5-10 pound-feet until there is clearance between the washer and the nut. Loosen to the nearest lock position to install the antirotation bolts (View B-B).
(5) S 414-035Install the antirotation bolts (10), the washers (11), and the nuts (12).
(6) S 844-036Put the axle jacks under the truck. Lift the truck beam with the jacks until there is clearance for the installation of the wheels and the tires (AMM 07-11-03/201).
(7) S 434-037Apply grease (BMS 3-33) to the pin (1), antirotation bolt (3), collar (4), washers (2, 5), nut (6), and the cotter pin. Install these parts to connect the rod end of the truck positioner actuator to the truck beam (View A-A).
(8) S 434-038Connect the proximity sensors for the truck tilt.
(9) S 414-039Install and tighten the clamps to install the shield to the truck beam.
S 414-040
(10) Install the junction boxes on each end of the truck beam. Connect the electrical lines.
32-11-17
ALL ú ú 05 Page 409 ú May 28/00
A
757
MAINTENANCE MANUAL
S 824-078
(11)
Make sure the clamps on the flexible electrical conduit are installed just below or just aft of the location band on the conduit(s) (Fig. 403).
S 414-042
(12)
Install the disconnect brackets for the hydraulic line (with hoses attached) to the main landing gear (Fig. 402).
S 844-043
(13)
Make sure the pressure is removed from the left hydraulic system (AMM 29-11-00/201). Connect the hydraulic lines and the electrical lines to the brackets on the side of the truck beam.
S 414-044
(14)
Install the wheel brakes (AMM 32-41-10/401).
S 434-044
(15)
AIRPLANES WITH BRAKE TEMPERATURE MONITORING SYSTEM;
connect the electrical lines to brake temperature sensors.
S 414-046
(16)
Install the brake rods (AMM 32-11-19/401).
S 844-047
(17)
Push the antiskid wires through the axles. Install the antiskid transducers (AMM 32-42-06/401).
S 414-048
(18)
Install the wheels and the tires (AMM 32-45-01/401).
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(115)