(2)
AMM 76-11-01/401, Thrust Levers.
(3)
AMM 76-11-02/401, Start Levers.
B. Access
(1) Location Zones
101 Control Cabin - Left
102 Control Cabin - Right
C. Procedure
S 864-002-C03
(1)
Remove hydraulic power (AMM 29-15-00/201).
S 864-003-C03
(2)
Put the thrust levers in the IDLE position.
S 864-004-C03
(3)
Put the start levers in the CUTOFF position.
S 864-005-C03
(4)
Put a protective cover on the Aft Electronics Panel, P8.
NOTE: This will prevent damage to the switches and the glass
____ surfaces of the indicators and the displays.
S 024-006-C03
(5) Do these steps to remove the covers, seals, and lightplates (Fig. 401):
(a) Remove the stabilizer trim control wheels: 1) Remove the bolt from the left stabilizer trim control wheel. 2) Remove the left stabilizer trim control wheel from the spline shaft. 3) Remove the bolt from the right stabilizer trim control wheel.
4) Remove the right stabilizer trim control wheel from the spline shaft.
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. AIRPLANES WITH EFIS-REINFORCED CONTROL ú
76-11-11
STANDS WITH A STABLIZER TRIM SHAFT WITH ú CONFIG 3 A SELF-LOCKING INSERT-AND-BOLT ú C02 Page 401 ú Mar 12/02
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
////////////////////////A / /
CFM56 ENGINES
737-300/400/500/ /MAINTENANCE MANUAL ////////////////////////
SCREW (9 LOCATIONS) THRUST LEVER COVERS AND SEALS
FORWARD THRUST LEVER STOP
SPEED BRAKE LEVER COVER LIGHT PLATE SCREW
SPEED BRAKE (4 LOCATIONS)LEVER COVER
SCREW
(8 LOCATIONS)
AFT THRUST LEVER STOP 1
SCREW (3 LOCATIONS) FLAP LEVER
HORN CUTOUT SWITCH KNOB
DETENT QUADRANT SCREW (8 LOCATIONS) FLAP LEVER COVER LIGHT PLATE SCREW SCREW
(2 LOCATIONS) (4 LOCATIONS)
STABILIZER TRIM COVER FLAP LEVER COVERAND LIGHT PLATE
STABILIZER TRIM SCREW
INDICATOR LIGHT PLATE
(4 LOCATIONS) STABILIZER TRIM COVER
STABILIZER
TRIM CUTOUT
STABILIZER TRIMSWITCH PLATE SPLINED CONTROL WHEEL SHAFT
SCREW
(2 LOCATIONS)
START LEVER
COVER AND SEALS
SCREW AFT GUARD PLATE
SCREW
(2 LOCATIONS)
STABILIZER TRIMFWD CONTROL WHEEL
1
MAKE SURE THE TABS ON THE AFT THRUST LEVER STOP
POINT AFT AND DOWN.
Control Stand Access Installation
Figure 401
F14101
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. AIRPLANES WITH EFIS-REINFORCED CONTROL ú
76-11-11
STANDS WITH A STABLIZER TRIM SHAFT WITH ú CONFIG 3 A SELF-LOCKING INSERT-AND-BOLT ú C01 Page 402 ú Mar 12/02
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
////////////////////////A / /
CFM56 ENGINES
737-300/400/500/ /MAINTENANCE MANUAL ////////////////////////
(b)
Remove the aft guard plate: 1) Remove the two screws from the aft guard plate. 2) Remove the aft guard plate.
(c)
Remove the start lever cover and the dust seals: 1) Remove the two screws from the start lever cover and the
dust covers.
2) Remove the start lever cover and the dust seals.
(d)
Remove the aft thrust lever stop: 1) Remove the three screws from the aft thrust lever stop. 2) Remove the aft thrust lever stop.
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