C. References
(1) AMM 12-31-11/201, Body Section 41 Access Doors and Panels
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(2)
AMM 12-31-71/201, Wing Upper Surface Access Doors and Panels
(3)
AMM 27-81-00/201, Leading Edge Flap and Slat Control System
(4)
AMM 52-61-00/001, Forward Airstair
(5)
AMM 78-31-00/201, Thrust Reverser System
(6)
AMM 78-34-02/201, Feedback Push-Pull Cables
D. Access
(1)
Location Zones
101/102 Control Cabin, Left and Right
205 Electronic Compartment
208 Forward Cargo Compartment
504/604 Thrust Reverser - Left
505/605 Thrust Reverser - Right
507/607 Strut Area
(2)
Access Panels
4404 Forward Cargo Door
6301/6401 Leading Edge Access Panel
E. Prepare for the Adjustment
S 045-112-C00
WARNING: DO THE DEACTIVATION PROCEDURE TO PREVENT THE OPERATION OF THE
_______ THRUST REVERSER. THE ACCIDENTAL OPERATION OF THE THRUST REVERSER CAN CAUSE INJURIES TO PERSONS OR DAMAGE TO THE EQUIPMENT.
(1) Do the deactivation procedure for the thrust reverser
(AMM 78-31-00/201).
S 865-113-C00
WARNING: REFER TO AMM 27-81-00/201 FOR THE INSTALLATION OF THE LOCK FOR
_______ THE LEADING EDGE FLAP. THE FLAPS CAN MOVE QUICKLY AND CAUSE INJURY TO PERSONS AND DAMAGE TO THE EQUIPMENT.
(2) AIRPLANES WITHOUT THROTTLE CONTROL CABLE TURNBUCKLES IN THE FUSELAGE; AIRPLANES PRE-SB 76-1023; Extend the leading edge flaps and install the flap locks (AMM 27-81-00/201).
NOTE: Extend the leading edge flaps to get access to the
____
control cable turnbuckles.
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INTEGRATED AUTOTHROTTLE SERVOMECHANISMS ( SEE
B FOR RIG PIN LOCATIONS)
Engine Control Cables
Figure 504 (Sheet 1)
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G66423
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"PT PWR" RIG PIN HOLE (80` PLA-UNDER SEAL)
STRUT DRUM
CONTROL BOX
RETAINER
PIN STOP
"IDLE" RIG PIN PLATE
HOLE (55` PLA- FUEL
UNDER SEAL) SHUTOFF
ASSEMBLY
FWD FUEL SHUTOFFSTART CONTROL QUADRANTPUSH-PULL CABLE
CABLE SUPPORT BRACKET
JAMNUTS
A
RIG PIN
TORQUE SWITCH MECHANISM
RIG PIN
CABLES CONTROL THRUST T1B T1A
FWD MECHANISM TORQUE SWITCH
CABLES CONTROL THRUST T2A T2B B ASSEMBLY SUPPORT ASSEMBLY (TYP) ACTUATOR
Figure 504 (Sheet 2) Engine Control System Adjustment Locations
G66433
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