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2) Push the stall warning test switches No. 1 and 2.
3) Make sure the stick shakers operate satisfactory.
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(4) Do the following task, MMEL 27-4 (DDPG) Restoration - Leading Edge Flap/Slat Position Light
Systems Inoperative, TASK 27-00-00-440-801.
------------------------- END OF TASK ---------------------------
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Leading Edge Flap and Slat Position Light Location
Figure 901/27-00-00-990-801
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TASK 27-00-00-440-801
3. MMEL 27-4 (DDPG) Restoration - Leading Edge Flap/Slat Position Light Systems Inoperative
(Figure 901)
A. General
(1) This task puts the airplane back to its usual condition after operation with the leading edge (LE)
flap/slat position light systems inoperative.
B. References
Reference Title
29-11-00-860-805 Hydraulic System A or B Power Removal (P/B 201)
C. Location Zones
Zone Area
211 Flight Compartment - Left
212 Flight Compartment - Right
D. Procedure
SUBTASK 27-00-00-960-001
(1) Replace the bulbs from the applicable lights.
SUBTASK 27-00-00-810-001
(2) If the LE flap/slat position light was not the problem, then do these steps to 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 27-00-00-930-004
(3) Remove the INOP placard from the applicable lights.
SUBTASK 27-00-00-930-005
(4) Remove the placard that has the LE flap and slat positions.
E. Put the Airplane Back to Its Usual Condition
SUBTASK 27-00-00-860-043
(1) If you open the circuit breaker, then do this step:
(a) Remove the safety tag and close this circuit breaker:
CAPT Electrical System Panel, P18-2
Row Col Number Name
E 7 C01208 STALL WARN ASYM MODE
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SUBTASK 27-00-00-860-044
(2) Remove power from hydraulic system B. To remove power from hydraulic system B, do this
task: Hydraulic System A or B Power Removal, TASK 29-11-00-860-805.
------------------------- END OF TASK ---------------------------
TASK 27-00-00-040-802
4. MMEL 27-7 (DDPG) Preparation - Auto Spoiler System Inoperative
A. General
(1) This task gives the maintenance steps which prepare the airplane for flight with the auto spoiler
system inoperative.
B. Location Zones
Zone Area
211 Flight Compartment - Left
212 Flight Compartment - Right
C. Procedure
SUBTASK 27-00-00-010-001
(1) Open this circuit breaker and install safety lock:
F/O Electrical System Panel, P6-2
Row Col Number Name
B 9 C00440 FLIGHT CONTROL AUTO SPEED BRAKE
SUBTASK 27-00-00-930-006
(2) Attach an AUTO SPOILER INOP placard to the speed brake control lever.
------------------------- END OF TASK ---------------------------
TASK 27-00-00-440-802
5. MMEL 27-7 (DDPG) Restoration - Auto Spoiler System Inoperative
A. General
(1) This task puts the airplane back to its usual condition after operation with the auto spoiler
system inoperative.
B. References
Reference Title
27-62-00-710-801 Speed Brake Control System Operational Test (P/B 501)
C. Location Zones
Zone Area
211 Flight Compartment - Left
212 Flight Compartment - Right
D. Procedure
SUBTASK 27-00-00-710-002
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737-600/700/800/900 AIRCRAFT MAINTENANCE MANUAL飞机维护手册1(44)
