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 (5)  Use a clean applicator to apply anti-seize compound to the surfaces where the latch and notch engage.
 (a)  Move the reverse thrust lever to make sure all the surfaces are lubricated.
 S 753-007
 (6)  Move the reverse thrust lever forward and back and listen for a metallic scraping sound as the latch moves out of the notch.
 (a)  If no sound is heard, the latch is correctly lubricated.
 S 643-008
 (7)  
Do the procedure again for the other latch.

 S 093-009

 (8)  
Remove the cloth.

 S 863-013

 (9)  
Put the reverse thrust lever back to the forward and down position.

 S 413-010

 (10)
 Install the rail, the center cover seal, and the cover seal onto the control stand (AMM 76-11-04/401).

 S 863-011

 (11)
 Remove the DO-NOT-CLOSE identifier and close these circuit breaker on the overhead panel P11:

 (a)  11G11, AUTO SPEEDBRAKE

 (12)
 Do the Thrust Reverser Activation Procedure (AMM 78-31-00/201).

 S 443-012
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 ALL  ú ú 01A Page 304 ú Dec 20/93
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
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757 MAINTENANCE MANUAL
 ENGINE STARTER - SERVICING (OIL CHANGE)
_______________________________________
 1.  General_______
 A. This procedure contains two tasks.
 (1)  
The first task examines the chip detector and drains the oil from the starter.

 (2)  
The second task fills the starter with oil.

 TASK 12-22-02-683-002
 2.  Drain the Engine Starter Oil____________________________
 A. General
 WARNING:_______DO NOT LET THE OIL TOUCH YOUR SKIN FOR A LONG TIME. THE SYNTHETIC OIL USED IN THIS ENGINE CONTAINS ADDITIVES WHICH CAN BE TOXIC IF THEY ARE ABSORBED THROUGH THE SKIN.
 CAUTION: DO NOT LET THE OIL FLOW ON TO PARTS THAT DO NOT USUALLY TOUCH
_______ THE OIL. THE OIL CAN CAUSE DAMAGE TO PAINT AND SOME TYPES OF RUBBER. ANY OIL THAT GETS ON TO THESE PARTS MUST BE CLEANED IMMEDIATELY.
 VERY SMALL QUANTITIES OF SOME TYPES OF ALKALINE CLEANING FLUIDS CAN CAUSE FAILURE OF THE SYNTHETIC OIL. USE VERY CLEAN CONTAINERS AND EQUIPMENT.
 DO NOT PUT OIL THAT YOU HAVE DRAINED INTO THE ENGINE.
 (1) You must follow this WARNING and CAUTION for the entire task.
 B. Equipment
 (1)  Clean Container - minimum capacity:
 1.2 U.S. pints
 1 Imperial pint

 0.568 Litres
 C. Consumable Materials
 (1)  Lockwire
 British Spec - DTD. 189A 22. S.W.G.
 American Spec - 21 A.W.G.
 OMat No. - 238

 D. References
 (1)  
AMM 70-02-01/201, Identification, Lubrication and Fitting of Rubber Sealing Rings

 (2)  
AMM 71-11-04/201, Fan Cowl Panels

 (3)  
AMM 80-11-01/401, Engine Starter

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 ALL  ú ú 01 Page 301 ú Sep 28/99
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A

757
MAINTENANCE MANUAL

 (4)  AMM 80-11-01/601, Starter Inspection/Check.
 E.  Access
 (1)  
Location Zones

 (a)  
413 Fan Cowl Panel (Left)

 (b)  
414 Fan Cowl Panel (Right)

 (c)  
423 Fan Cowl Panel (Left)

 (d)  
424 Fan Cowl Panel (Right)

 

 (2)  
Access Panels

 (a)  
413AL Fan Cowl Panel (Left)

 (b)  
414AL Fan Cowl Panel (Right)

 (c)  
423AL Fan Cowl Panel (Left)

 (d)  
424AL Fan Cowl Panel (Right)

 

 F.  Drain the Starter Oil (Fig. 301)
 S 013-011
 CAUTION: OBEY THE PRECAUTIONS FOR THE KEVLAR WRAPPING WHEN YOU OPEN THE
_______ FAN COWL PANEL. IF THE PRECAUTIONS ARE NOT OBEYED, DAMAGE TO THE KEVLAR WRAPPING CAN OCCUR.
　
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