27-11-00
ALL ú ú 01 Page 508 ú Dec 20/89
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
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757 MAINTENANCE MANUAL
(c)
A3 - P/N B20003-23
(d)
A4 - P/N B20003-23Consumable Materials
(1)
D00015 Grease, Corrosion Preventive - BMS 3-24References
(1)
06-41-00/201, Fuselage Access Doors and Panels
(2)
06-44-00/201, Wing Access Doors and Panels
(3)
20-10-03/401, Control Cables
(4)
20-10-24/201, Rig Pins
(5)
24-22-00/201, Electrical Power - Control
(6)
27-51-00/201, Trailing Edge Flap System
(7)
27-51-00/501, Trailing Edge Flap System
(8)
29-11-00/201, Pressurize/Depressurize Main Hydraulic Systems
(9)
32-00-15/201, Landing Gear Door Locks
(10)
32-00-20/201, Landing Gear DownlocksAccess
(1)
Location Zones 113 Area forward of NLG wheel well (Left) 561 Rear spar to TE (Left) 661 Rear spar to TE (Right)
(2)
Access Panels 113AL Flight/Landing Gear/Engine Control Components 561AB Aileron Quadrant (Left) 561CB Aileron Power Limit (Left) 661AB Aileron Quadrant (Right) 661CB Aileron Power Limit (Right)
Prepare for Adjustment
S 015-031
(1)
Open access door 113AL (Ref. 06-41-00).
S 015-032
(2)
Open access panels 561AB and 561CB (left aileron) and 661AB and 661CB (right aileron) (Ref. 06-44-00).
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
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ALL ú ú 01 Page 509 ú Sep 28/99
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
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757 MAINTENANCE MANUAL
S 865-033
(3)
Supply electrical power (Ref. 24-22-00).
S 865-034
(4)
Retract the trailing edge flaps.
S 865-035
(5)
Do the deactivation procedure for the flaps (Ref. 27-51-00).
S 495-036
(6)
Make sure the downlocks for the nose and main landing gear are installed (Ref. 32-00-20).
S 495-037
WARNING:_______MAKE SURE THAT THE DOOR LOCKS ARE INSTALLED CORRECTLY. FAST MOVEMENT OF THE DOORS CAN CAUSE INJURY TO PERSONS AND DAMAGE TO EQUIPMENT.
(7)
Open the main gear doors and install the door locks (Ref. 32-00-15).
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Adjust the Control Wheels (Fig. 501)
S 825-231
(1) Put the captain's and first officer's control wheel in neutral.
NOTE: Neutral is achieved by clamping a straight edge across the
____
lower surface of each wheel.
S 825-039
(2)
Use a clamp to attach the rigging beam to the control wheels.
(a)
Make sure the lower surfaces of the two control wheels touch the rigging beam.
S 035-038
(3)
Disconnect the bus-force-limiter rod from the first-officer's drum assembly.
S 035-040
(4)
Remove the lockwire and loosen the locknut on the bus-force-limiter rod.
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757 MAINTENANCE MANUAL
(5) S 825-041Adjust the length of the bus-force-limiter rod until the attach bolt can be easily installed.
(6) S 435-043Tighten the locknut to 75-100 pound-inches (8.5-11.3 newton-meters) and install the lockwire. (a) Make sure the rod end threads cover at least 1/2 of the inspection holes at each end of the bus-force-limiter rod.
(7) S 435-042Install the bolt, bushing, washer, and nut at the rod end. grease if it is necessary. Apply
(8) S 085-232Remove the rigging beam from the control wheels.
(9) S 435-233If you are installing or replacing the column and/or drum installations, do the steps that follow:
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