737-300 400 500 AMM 飞机维护手册 SERVICING(133)

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 B.  There is an outboard landing light in each outboard fairing.
 C.  The outboard landing lights can be extended and retracted.
 TASK 12-25-95-643-009
 2.  Outboard Landing Light Lubrication (Fig. 301)__________________________________
 A.  Consumable Materials
 (1) D01063 Lubricant - Dow Corning 77 (DC77) or Molycote 77 (M77)
 B.  References
 (1)  AMM 24-22-00/201, Manual Control
 C.  Access
 (1)  Location Zone 307 Left Wing Trailing Edge, Outboard Flap and Spoilers 407 Right Wing Trailing Edge, Outboard Flap and Spoilers
 D.  Procedure
 S 863-010
 (1)  
Supply electrical power (AMM 24-22-00/201).

 S 863-011

 (2)  
At the overhead panel, P5, set each switch for the outboard landing lights to the extend position.

 (a)  Make sure the outboard landing lights extend fully down.
 S 863-012
 (3) Open these circuit breakers and attach the DO-NOT-CLOSE tags:
 (a)  On the load control center panel, P18: 1) RIGHT OUTBOARD LANDING LIGHT 2) LEFT OUTBOARD LANDING LIGHT
 S 643-013
 (4)  Lubricate the sector gear of each outboard landing light (Fig. 301).
 E.  Put the Airplane to Its Usual Condition
 S 863-014
 (1)  Remove the DO-NOT-CLOSE tag and close each circuit breaker that was opened.
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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A 737-300/400/500MAINTENANCE MANUAL

M77 IS OPTIONAL TO DC77
OUTBOARD LANDING LIGHT
(EXTENDED)

Outboard Landing Light Lubrication
Figure 301

B55362
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 ú  01  Page 302
 ú  Jul 15/95 

BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A 737-300/400/500MAINTENANCE MANUAL
 (2)  S 863-015Set each switch to the retract position. (a) Make sure the outboard landing lights retract.
 (3)  S 863-008Remove electrical power if it is not necessary (AMM 24-22-00/201).

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 ALL  ú ú 01 Page 303 ú Mar 15/94
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
 CABLE LUBRICATION - SERVICING
_____________________________
 1.  General_______
 A.  There is one task in this procedure, the lubrication of the control cables.
 TASK 12-26-00-603-001
 2.  Control Cable Lubrication_________________________
 A.  Consumable Materials
 (1)  
D00015 Grease - Corrosion Preventive, BMS 3-24, BMS 3-33

 (2)  
G01043 Cloth - Lint-Free

 B.  Access
 (1)  Location Zone
 200 Lower Half of the Fuselage
 300 Left Wing
 400 Right Wing
 500 Left Nacelle
 600 Right Nacelle
 700 Empenage

 C.  Procedure
 S 163-002
 CAUTION: DO NOT USE SOLVENT OR HEAT TO THIN THE GREASE ON THE CONTROL
_______ CABLES. DO NOT USE SOLVENT TO CLEAN THE CONTROL CABLES. THE SOLVENT REMOVES GREASE FROM THE CABLE. DO NOT APPLY OR SPRAY BMS 3-23 ON THE CONTROL CABLES.
 (1)  Use a lint-free cloth that is clean and dry to clean the control cables.
 NOTE: Remove the old grease and dirt from the surface of the
____ control cable. Clean the control cable for the full length of the cable for the full length of travel through fairleads, air pressure seals, over pulleys, quadrants, and drums.
 S 643-003
 (2)  Lubricate the control cables:
 (a)  Carbon Steel Cables:
 CAUTION: THE CONTROL CABLES IN THE WING AND NACELLE AREA ARE
　
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