S 034-169
(19)
Remove the plugs and the caps and connect the upper hydraulic lines.
S 434-055
(20)
Install the clamps (8) and the hydraulic lines (7) on the main landing gear (Fig. 401).
S 034-170
(21)
Remove the plugs and the caps.
S 434-171
(22)
Connect all the lines.
S 424-054
(23)
Install the actuator and the actuator walking beam of the main landing gear (AMM 32-32-11/401).
NOTE: If the stabilizing beam of the main landing gear was
____ installed, you can remove it to make the installation of the actuator assembly easier, and install it again after the installation of the actuator assembly.
S 434-179
WARNING: EXAMINE THE ELECTRICAL HARNESS BELOW THE AXLE FOR DAMAGE OR
_______ REPAIRS DONE BEFORE. DAMAGED OR SPLICED WIRES CAN CAUSE ELECTRICAL SHOCK OR INJURY TO PERSONS.
ú (24) Install the electrical harness (9), (Fig. 402).
S 414-052
(25)
Install the shock strut doors (AMM 32-13-11/401).
(26)
Adjust the shock strut doors (AMM 32-13-11/401).
(27)
Lubricate the main landing gear (AMM 12-21-11/301).
S 434-119
(28)
If you installed the right main landing gear, connect the interlock valve cable of the ground spoiler (AMM 27-62-51/401).
S 824-050
S 644-049
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
32-11-00
ALL ú ú 01.1 Page 427 ú Jul 12/02
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
S 864-047
(29)
Pressurize the hydraulic systems A and B (AMM 29-15-00/201).
S 714-188
(30)
Operate the brake pedals four to six times to bleed the brake.
S 794-120
(31)
Examine the connections of the hydraulic brake line for leakage.
S 714-046
(32)
Examine the operation of the skid detectors of the new main landing gear you installed (AMM 32-42-00/501).
S 094-121
(33)
Remove the ground lock assemblies (AMM 32-00-01/201).
S 714-194
(34)
Do the Operation Test of the APU Fire Detection System (AMM 26-15-00/501).
S 714-172
(35)
Do a retraction test of the main landing gear (AMM 32-32-00/501).
S 714-045
(36)
Do a test of the manual extension system of the main landing gear (AMM 32-34-00/501).
(37)
Install the ground lock assemblies (AMM 32-00-01/201).
S 584-043
(38)
Lower the airplane to the ground and remove the jacks (AMM 07-11-11/201).
(39)
Set the parking brake.
S 494-044
S 844-042
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
32-11-00
ALL ú ú 01 Page 428 ú Mar 12/02
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
S 424-221
(40)
Install the door on the main landing gear shock strut (AMM 32-13-11/401).
S 414-222
(41)
Install the hydraulic access panel (8401 left or 8501 right) on the bottom of the wing.
S 614-187
(42)
Service the shock struts with oil and nitrogen (AMM 12-15-31/301).
S 844-041
(43)
If it is not necessary for other work, remove electrical power from the airplane.
S 844-040
(44)
If it is not necessary for other work, remove hydraulic power from the airplane (AMM 29-15-00/201).
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本文链接地址：737-300 400 500 AMM 飞机维护手册 起落架 LANDING GEAR 1(54)
