B. References
(1)
AMM 08-10-00/201, Leveling
(2)
AMM 24-22-00/201, Manual Control
(3)
AMM 27-81-00/201, Leading Edge Flap and Slat Locks Installation
(4)
AMM 33-42-21/401, Inboard Landing and Runway Turnoff Light Lens Assembly (Cover) - Removal/Installation
C. Access
(1) Location Zone 303 Left Wing Inboard Leading Edge Including Slats 403 Right Wing Inboard Leading Edge Including Slats
D. Procedure
S 865-009
WARNING: YOU MUST CAREFULLY DO THE STEPS IN THE TASK BELOW TO INSTALL
_______ THE LEADING EDGE FLAP AND SLAT LOCKS CORRECTLY. THE LEADING EDGE FLAPS AND SLATS CAN MOVE QUICKLY IF YOU DO NOT INSTALL THE LOCKS CORRECTLY. THIS CAN CAUSE INJURY TO PERSONS OR DAMAGE TO EQUIPMENT.
(1) Do this task: "Leading Edge Flap and Slat Locks Installation" (AMM 27-81-00/201).
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
33-42-31
ALL ú ú 01 Page 501 ú Mar 15/95
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A 737-300/400/500MAINTENANCE MANUAL
(2) S 035-011Remove the lens of the inboard landing and runway turnoff lights (AMM 33-42-21/401).
(3) S 865-013Make sure the airplane and the test area are on level ground.
(4) S 865-047Make sure the airplane is approximately level (AMM 08-10-00/201).
(5) S 945-003Set the light aligner in its position (Fig. 502). (a) Measure the height of the light from the ground. (b) Use the height of the light to adjust the height of the light aligner (Fig. 502).
(6) S 865-010Supply electrical power (AMM 24-22-00/201).
(7) S 825-019Adjust the light.
CAUTION:_______ DO NOT MAKE THE LIGHTS COME ON FOR MORE THAN FIVE MINUTES. AFTER YOU MAKE THE LIGHTS COME ON, MAKE THE LIGHTS GO OFF FOR AN EQUAL TIME. BECAUSE OF THE HEAT, THE CONTINUED OPERATION OF THE LIGHTS CAN DECREASE THE LIFE OF THE LAMPS.
(a) (b) At the overhead panel, P5, set the switch for the landing light to the on position.Turn the adjustment screws of the light until the indicators on the light aligner change colors from yellow to black.
NOTE:____ The indicator in the center of the light aligner will stay yellow. All the other indicators must become black at the same time.
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
33-42-31
ALL ú ú 01 Page 502 ú Mar 15/95
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A 737-300/400/500MAINTENANCE MANUAL
LIGHT (REF)
LEFT INBOARD LANDING LIGHT (THE RIGHT LIGHT IS SYMMETRICAL)
Adjustment of the Inboard Landing Lights
Figure 501
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
33-42-31
ALL ú ú 02 Page 503 ú Jul 15/91
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A 737-300/400/500MAINTENANCE MANUAL
LOCATION OF THE LIGHT ALIGNER FOR THE RIGHT INBOARD LANDING LIGHT
(LEFT LIGHT IS SYMMETRICAL)
Inboard Landing Lights (Adjustment with a Light Aligner)
Figure 502 (Sheet 1)
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
33-42-31
ALL ú ú 01 Page 504 ú Jul 15/95
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
LIGHT
SEE A (BACK VIEW) LIGHT ALIGNER
BEAM LIGHT
LIGHT BEAM
HEIGHT
OF THE
ALIGNER LIGHT CENTER OF THE LIGHT BEAM
中國航空網 www.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：737-300 400 500 AMM 飛機維護手冊 燈 LIGHTS(65)
