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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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Fan C-Duct and Thrust Reverser Cowl Markings
Figure 201A (Sheet 1)

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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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LEFT SIDE IS SHOWN (RIGHT SIDE IS EQUIVALENT)
　
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