(2)
24-22-00/201, Electrical Power - Control
(3)
25-50-01/401, Cargo Compartment Ceiling Lining
(4)
32-00-15/201, Landing Gear Door Locks
(5)
32-00-20/201, Landing Gear Downlocks
B.
Access
(1)
Location Zones
730 Left Main Landing Gear and Doors
740 Right Main Landing Gear and Doors
668 Aileron
(2)
Access Panel 661AB Aileron Quadrant and Override Mechanism
C.
Prepare for the Removal
S 864-002
(1)
Supply electrical power (Ref 24-22-00/201).
S 494-003
(2)
Make sure the landing gear downlocks are installed (Ref 32-00-20/201).
S 494-004
WARNING: USE THE PROCEDURE IN AMM 32-00-15 TO INSTALL THE DOOR LOCKS. THE DOORS OPEN AND CLOSE QUICKLY AND CAN CAUSE INJURY TO PERSONS OR DAMAGE TO EQUIPMENT.
(3)
Open the main gear doors and install the door locks (Ref 32-00-15/201).
(4)
Open the access panel, 661AB (Ref 06-44-00/201).
S 014-006
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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
757 MAINTENANCE MANUAL
AILERON QUADRANT AND OVERRIDE MECHANISM
FEEL, CENTERING,
AND TRIM MECHANISM LATERAL CONTROL OVERRIDE MECHANISM
SEE A
BUS ROD (TO THE FEEL, CENTERING, AND TRIM MECHANISM)
WING CABLE
A2B BOLT, WASHER, NUT (4 LOCATIONS)
OVERRIDE ARM
BODY CABLE A2A UPPER NUT
LOWER NUT
SUPPORT ROD
5.10 INCHES
(129.5 mm)
A2 RIG PIN
HOLES
OVERRIDE SPRING
SUPPORT
BRACKET BODY CABLE A2B
WING CABLE A2A
AFT BEARING
WASHER
CONTROL
RODNUT
INSPECTION AUTOPILOT COTTER PIN
SEE B HOLE CRANK
BOLT, WASHER, NUT
(3 LOCATIONS) INBD FWD
LATERAL CONTROL OVERRIDE MECHANISM
A
Lateral-Control Override Mechanism Installation Figure 401 (Sheet 1)
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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A 757 MAINTENANCE MANUAL
INSPECTION
THROUGH THE INSPECTION HOLES AFTER YOU DO THE ALCS ADJUSTMENT
Lateral-Control Override Mechanism Installation Figure 401 (Sheet 2)
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ALL ú ú 02 Page 403 ú Jan 28/02
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
757
MAINTENANCE MANUAL
AILERON QUADRANT AND OVERRIDE MECHANISM
SEE A
FEEL, CENTERING, AND
TRIM MECHANISM
SEE B
A4 RIG
PIN HOLE
(RIGHT)
A1 RIG PIN HOLES
AILERON QUADERANT AND OVERRIDE MECHANISM
A
FWD INBD
FEEL, CENTERING AND TRIM MECHANISM
B
Lateral Control Override Mechanism Installation
Figure 402
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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
757 MAINTENANCE MANUAL
D. Lateral Control Override Mechanism - Removal
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