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S 092-059-N00
 (4) Remove the sling assembly from the thrust reverser (Fig. 204).
 NOTE: Make sure to install the bolts at the attach points after
____
 you remove the sling assembly.

 S 412-060-N00
 CAUTION: MAKE SURE THE T-BOLT IS CORRECTLY ENGAGED IN THE RECEIVER OF
_______ THE VEE-GROOVE LATCH BAND BEFORE YOU CLOSE THE T-BOLT LATCH HANDLE. FAILURE TO OBEY THIS INSTRUCTION CAN CAUSE DAMAGE TO THE T-BOLT OR THE RECEIVER ON THE VEE-GROOVE LATCH BAND.
 (5)  
Close the T-bolt latch handle to lock the vee-groove latch band around the thrust reverser (Fig. 201).

 S 412-061-N00

 (6)  
Close the four tension latches on the bottom of the engine.

 NOTE: Start with the front tension latch on the torque box and
____ continue aft until you close all four tension latches.
 S 412-062-N00
 (7)
Close the louvered exhaust door on the bottom of the engine.

 G.
Put the Airplane Back to Its Usual Condition

 S 412-063-N00
 (1)  
Install the core cowl panels (AMM 71-11-06/401).

 S 412-064-N00

 (2)  
Close the fan cowl panels (AMM 71-11-04/201).

 S 412-065-N00

 (3)  
Close the fan cowl panel (AMM 71-11-04/201).

 (4)  
Remove the DO-NOT-OPERATE tags from the thrust levers.

 S 442-067-N00

 (5)  
Do the activation procedure for the thrust reverser
 (AMM 78-31-00/201).

 S 862-066-N00
 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

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S 442-068-N00
 (6)  
Do the activation procedure for the leading edge flaps (AMM 27-81-00/201).

 S 442-069-N00

 (7)  
Do the activation procedure for the Speed Brake Control System (AMM 27-62-00/201).

 TASK 78-31-00-862-070-N00
 6.  Thrust Reverser Operation - Deployment (Manual Procedure) (Fig. 205)_________________________________________________________
 A. References
 (1)  
AMM 27-62-00/201, Speed Brake Control System

 (2)  
AMM 27-81-00/201, Leading Edge Flap System

 (3)  
AMM 71-11-04/201, Fan Cowl Panels

 B.
Access

 (1)  
Location Zone 415 and 416 Engine 1 - Thrust Reverser Halves 425 and 426 Engine 2 - Thrust Reverser Halves 435 and 436 Engine 3 - Thrust Reverser Halves 445 and 446 Engine 4 - Thrust Reverser Halves

 (2)  
Access Panel
 413 and 414 Fan Cowl Panels - Engine 1
 423 and 424 Fan Cowl Panels - Engine 2
 433 and 434 Fan Cowl Panels - Engine 3
 443 and 444 Fan Cowl Panels - Engine 4

 C.
Procedure

 S 042-071-N00
 WARNING:_______MAKE SURE YOU CORRECTLY DISCONNECT THE SPEED BRAKE. AN ACCIDENTAL SPEED BRAKE MOVEMENT CAUSED BY THE THRUST LEVERS CAN CAUSE INJURY TO PERSONS.
 (1)  Do this task: "Speed Brake Control System Deactivation" (AMM 27-62-00/201).
 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

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SEE  B  HYDRAULIC SUPPLY LINE 
SHAFT TUBE ROTARY FLEX  RING GIMBAL 
SEE  A  TORQUE BOX 
ACTUATOR 
SYNC LOCK 
A NON-LOCKING HYDRAULIC ACTUATOR INSTALLATION 
LVDT FEEDBACK  ACTUATOR LOCK PROXIMITY SENSOR  TARGET  LEVER LOCK 

TARGET
ACTUATOR DEPLOY PROXIMITY SENSOR
LOCKING HYDRAULIC ACTUATOR
LOCKING ACTUATOR INSTALLATION
B

Manual Operation of Thrust Reverser Translating Sleeve Figure 205
M49446
　
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