(c)
11H23, FLAP/SLAT ALTN DR SHUTOFF ARM
(d)
11J33, WARN ELEX A
S 863-225
(4)
Remove the circuit breaker locks and the DO-NOT-CLOSE tags, and close these circuit breakers on the P6 panel:
(a)
6D20, ALTN SLAT PWR
(b)
6D23, ALTN FLAP PWR
(5)
Remove the DO-NOT-OPERATE tag from the flap control lever.
S 863-221
(6)
Make sure the TE flaps and LE slats are fully retracted with the flap control lever in the zero (FLAPS UP) detent (AMM 27-81-00/201).
S 863-222
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
12-21-08
ALL ú ú 01 Page 321 ú Sep 28/00
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
757 MAINTENANCE MANUAL
S 843-037
WARNING:_______USE AMM 32-00-15/201 TO REMOVE THE DOOR LOCKS. THE DOORS OPEN AND CLOSE QUICKLY AND CAN CAUSE INJURIES TO PERSONS OR DAMAGE TO EQUIPMENT.
(7)
Remove the door locks from the main landing gear doors and close the doors (Ref 32-00-15/201).
S 863-226
(8)
Remove the electrical power if it is not necessary
(Ref 24-22-00/201).
S 443-227
(9)
Do the activation procedure for the thrust reverser
(Ref 78-31-00/201).
TASK 12-21-08-643-030
7. Lubricate the Leading Edge (LE) Slat Power Drive Unit (PDU) Gears_________________________________________________________________
A. Equipment
(1)
Trailing Edge Flap Power Drive Unit Lock - B27008-1
(2)
Circuit Breaker Lockout Clip
(Commercially Available)
(3)
LE Slat Drive Lock Set - B27020-31
(includes CB Locks B27020-25 and B27065-1. Valve Locks B27020-32 or B27077-1 are not used in this procedure)
B. Consumable Materials
(1)
D00014 Grease - MIL-G-21164 (Recommended)
(2)
D00013 Grease - MIL-G-23827 (Optional)
C. References
(1)
06-44-00/201, Wing Access Doors and Panels
(2)
24-22-00/201, Electrical Power - Control
(3)
AMM 27-81-00/201, LE Slat System - Maintenance Practices
(4)
29-11-00/201, Main (Left, Right, and Center) Hydraulic Systems
(5)
32-00-15/201, Landing Gear Door Locks
(6)
32-00-20/201, Landing Gear Downlocks
(7)
78-31-00/201, Thrust Reverser System
D. Access
(1) Location Zones 193/194 Wing to Body - Forward Lower Half 211/212 Control Cabin 510/610 Wing Leading Edge - Forward of Front Spar and Inboard
of Nacelle Strut 520/620 Wing Leading Edge - Forward of Front Spar and
Outboard of Nacelle Strut 730/740 Left and Right Main Landing Gears and Doors 732/742 Left and Right Main Landing Gear Wheel Well
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
12-21-08
ALL ú ú 01 Page 322 ú May 28/01
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
757 MAINTENANCE MANUAL
(2) Access Panels
511CB or 193BL LE Slat Power Drive Unit and Hydraulics
E. Prepare for the Lubrication
NOTE: The LE Slat PDU is found aft of the left wing strakelet and
____
is installed on the left wing front spar.
S 043-228
WARNING: DO THE THRUST REVERSER DEACTIVATION PROCEDURE TO PREVENT THE
_______ OPERATION OF THE THRUST REVERSER. ACCIDENTAL OPERATION OF THE THRUST REVERSER CAN CAUSE INJURY TO YOU OR DAMAGE TO EQUIPMENT.
(1)
Do this procedure: Thrust Reverser Deactivation for Ground
Maintenance (Ref 78-31-00/201).
S 863-229
(2)
Make sure the trailing edge (TE) flaps and LE slats are fully extended (AMM 27-81-00/201).
S 863-230
(3)
Make sure the flap control lever is in the 30-unit detent.
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