PLASTISOL END TOWARD LEVER ARM JOINT1
Free-play Measurement for the Nose Landing Gear Figure 601 (Sheet 1)
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
32-21-03
ALL ú ú 01 Page 602 ú Oct 10/91
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400
MAINTENANCE MANUAL
A-A
TOOL
Free-play Measurement for the Nose Landing Gear
Figure 601 (Sheet 2)
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
32-21-03
ALL ú ú 01 Page 603 ú Oct 10/91
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400 MAINTENANCE MANUAL
S 866-052
WARNING: YOU MUST CAREFULLY INSTALL THE GROUND LOCKS IN ALL LANDING
_______ GEAR. AN ACCIDENTAL RETRACTION OF THE LANDING GEAR CAN CAUSE INJURY TO PERSONS AND DAMAGE TO EQUIPMENT.
(2) Install the ground locks in all landing gear (AMM 09-11-00/201).
S 496-053
WARNING: YOU MUST CAREFULLY DO THE STEPS IN THE TASK BELOW TO INSTALL
_______ THE DOOR LOCKS ON THE LANDING GEAR DOORS. THE DOORS CAN CLOSE QUICKLY IF YOU DO NOT INSTALL THE DOOR LOCKS CORRECTLY. THIS CAN CAUSE INJURY TO PERSONS OR DAMAGE TO EQUIPMENT.
(3)
Do this task: "Installation of the Door Locks on the Nose Landing Gear" (AMM 32-00-30/201).
S 866-033
(4)
Remove the hydraulic power from the system No. 1 (AMM 29-11-00/201).
S 586-034
(5)
Lift the nose of the airplane with the fuselage jack until the dimension X on the NLG servicing chart (AMM 12-15-05/301) is approximately six inches (AMM 07-11-02/201).
S 876-060
(6)
Deflate the shock strut for the nose landing gear.
(a)
Remove the air valve cap.
WARNING: DO NOT LOOSEN THE AIR VALVE BODY UNLESS YOU FULLY DEFLATED
_______ THE SHOCK STRUT. THE INTERNAL PRESSURE CAN BLOW THE VALVE OUT. THIS WILL CAUSE INJURY TO PERSONS.
(b) Loosen the air valve nut two turns maximum.
NOTE: The fluid in the shock strut will release bubbles
____ immediately when you decrease the pressure. Deflate the shock strut slowly to prevent a flow of fluid through the air valve.
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
32-21-03
ALL ú ú 03 Page 604 ú Oct 18/99
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400 MAINTENANCE MANUAL
(7) S 496-035Install the jack attached tool to the bottom of the axle.
(8) S 946-038Put the axle jack below the inner cylinder of the nose landing gear.
(9) S 586-037Lift the inner cylinder with the axle jack until the dimension X on the NLG servicing chart (Ref 12-15-05/301) is 4 |0.25 inches. (a) Make sure the nose gear tires are off the ground. (b) Adjust the fuselage jack and the axle jack if it is necessary.
S 496-040
(10)
Install the tow pin at the summing mechanism to move away the hydraulic pressure from the metering valve (AMM 09-11-00/201).
S 496-039
(11)
Install the torsional play tool.
NOTE:____The torsional play tool has 4 parts. Figure 601, Sht 2 shows these parts.
(a)
Install the lock assemblies (Parts 3 and 4) on the steering actuators.
(b)
Install the dial indicator to read the axle nut motion.
(c)
Install the torsional play tool into the jack attached tool. 1) Install the bare end of the reversible extension assembly (Part 2) into the jack attached tool.
2) Make the hole larger in the jack attached tool if it is necessary.
NOTE: The reversible extension assembly is installed 5.00
____ inches into the jack attached tool. This distance is the distance from the end of the extension assembly to the outer edge of the stop collar.
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
中國航空網 www.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：747-400 AMM 飛機維護手冊 起落架 LANDING GEAR 3(132)
