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TASK 27-00-00-440-805
11. MMEL 27-12 (DDPG) Restoration - Auto Slat System Inoperative
A. General
(1) This task puts the airplane back to its usual condition after operation with an auto slat system
inoperative.
B. Location Zones
Zone Area
211 Flight Compartment - Left
212 Flight Compartment - Right
C. Procedure
SUBTASK 27-00-00-440-001
(1) Close the auto slat system circuit breakers:
(a) For the number 1 auto slat system,
Remove the safety lock and close this circuit breaker:
F/O Electrical System Panel, P6-2
Row Col Number Name
C 14 C01068 FLIGHT CONTROL AUTOSLAT DC 1
(b) For the number 2 auto slat system,
Remove the safety lock and close this circuit breaker:
F/O Electrical System Panel, P6-2
Row Col Number Name
B 14 C01070 FLIGHT CONTROL AUTOSLAT DC 2
SUBTASK 27-00-00-810-004
(2) Correct the fault.
(a) Find the fault code or description of the fault that occurred.
(b) If you find a fault code, then do these steps:
1) Go to the Fault Code Index in the applicable chapter of the FIM and find the fault code.
NOTE: The first two digits of the fault code is the FIM chapter.
2) Find the task number on the same line as the fault code.
3) Go to the task in the FIM and do the steps in the task.
(c) If you find a description of the fault, then do these steps:
1) Go to the Observed Fault List at the beginning of the FIM and find the best description
for the fault.
2) Find the task number on the same line as the fault description.
3) Go to the task in the FIM and do the steps in the task.
SUBTASK 27-00-00-210-004
(3) Verify that the auto slat systems and AUTO SLAT FAIL light operates normally:
737-600/700/800/900
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EFFECTIVITY
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(a) Push the MASTER CAUTION light switch.
1) Make sure the AUTO SLAT FAIL, FLT CONT, and MASTER CAUTION lights come on.
(b) Push the MASTER CAUTION light switch.
1) Make sure the AUTO SLAT FAIL, FLT CONT, and MASTER CAUTION lights go off.
SUBTASK 27-00-00-930-013
(4) Remove the ONE AUTO SLAT SYSTEM INOP placard from the AUTO SLAT FAIL light.
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TASK 27-00-00-040-806
12. MMEL 27-13 (DDPG) Preparation - Stall Warning System Inoperative
A. General
(1) This task gives the maintenance steps which prepare the airplane for flight with a stall warning
system inoperative.
B. Location Zones
Zone Area
211 Flight Compartment - Left
212 Flight Compartment - Right
C. Procedure
SUBTASK 27-00-00-040-002
(1) Do these steps to deactivate the failed stall warning system:
(a) For the number 1 stall warning system,
Open these circuit breakers and install safety locks:
CAPT Electrical System Panel, P18-2
Row Col Number Name
E 4 C01392 STICK SHAKER LEFT
E 6 C01205 SMYD-1 SNSR EXC AC
(b) For the number 2 stall warning system,
Open these circuit breakers and install safety locks:
F/O Electrical System Panel, P6-1
Row Col Number Name
B 4 C01207 SMYD-2 SNSR EXC AC
B 6 C01393 STICK SHAKER RIGHT
SUBTASK 27-00-00-930-014
(2) Attach a placard on the test switch associated with the inoperative stall warning system which
states - NO. 1 or NO. 2 STALL WARNING SYSTEM INOP.
SUBTASK 27-00-00-740-003
(3) Do these steps to make sure that the other stall warning system operates normally:
(a) Push and hold the applicable STALL WARNING TEST switch on the stall warning test
module (P5-18 panel).
(b) Make sure the control column shaker operates.
(c) Release the switch.
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
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(d) Make sure the control column shaker stops.
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TASK 27-00-00-440-806
13. MMEL 27-13 (DDPG) Restoration - Stall Warning System Inoperative
A. General
(1) This task puts the airplane back to its usual condition after operation with a stall warning system
inoperative.
B. Location Zones
Zone Area
211 Flight Compartment - Left
212 Flight Compartment - Right
C. Procedure
SUBTASK 27-00-00-440-002
(1) Close the stall warning system circuit breakers:
(a) For the number 1 stall warning system,
Remove the safety locks and close these circuit breakers:
　
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