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MAINTENANCE MANUAL
CAUTION
THE INBOARD THRUST REVERSER HALVES MUST NOT BE OPENED UNLESS INBOARD LEADING EDGE SLATS ARE RETRACTED TO CRUISE POSITION AND PLACARDED AS FOLLOWS:
1.
RETRACT INBOARD LEADING EDGE SLATS.
2.
ATTACH DO-NOT-OPERATE IDENTIFIER TO FLAP
CONTROL LEVER.
3.
CHECK THAT ALTERNATE FLAP SLAT POSITION SELECTOR ON PILOTS P3-1 PANEL IS IN NORM POSITION AND ATTACH DO-NOT-OPERATE IDENTIFIER.
IF EXTENSIVE ENGINE WORK IS BEING ACCOMPLISHED, IT MAY BE DESIRABLE TO DEACTIVATE THE PRIMARY AND ALTERNATE LEADING EDGE DRIVE SYSTEMS PER MM 27-81-00.
MAX TORQUE 165 IN LBS
STOW
DEPLOY 165 IN LBS MAX TORQUE
LEFT SIDE IS SHOWN LEFT SIDE IS SHOWN
(RIGHT SIDE IS EQUIVALENT) (RIGHT SIDE IS EQUIVALENT)
Fan C-Duct and Thrust Reverser Cowl Markings
Figure 201 (Sheet 3)
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MAINTENANCE MANUAL
Fan C-Duct and Thrust Reverser Cowl Markings
Figure 201A (Sheet 1)
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G95408
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MAINTENANCE MANUAL
INTERNAL SURFACE OF THE ACCESS DOOR
Fan C-Duct and Thrust Reverser Cowl Markings
Figure 201A (Sheet 2)
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G95410
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MAINTENANCE MANUAL
LEFT SIDE IS SHOWN (RIGHT SIDE IS EQUIVALENT)
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