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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,
Remove the safety locks and close these circuit breakers:
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 27-00-00-810-005
(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.
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
GUN ALL 27-00-00
Page 917
Jun 10/2007
D633A101-GUN
BOEING PROPRIETARY - Copyright#Unpublished Work - See title page for details
SUBTASK 27-00-00-740-004
(3) Do these steps to make sure that the stall warning systems operate normally:
(a) Push and hold the NO. 1 STALL WARNING TEST switch on the stall warning test module
(P5-18 panel).
(b) Make sure the pilot’s control column shaker operates.
(c) Release the switch.
(d) Make sure the control column shaker stops.
(e) Push and hold the NO. 2 STALL WARNING TEST switch on the stall warning test module
(P5-18 panel).
(f) Make sure the first officer’s control column shaker operates.
(g) Release the switch.
(h) Make sure the control column shaker stops.
SUBTASK 27-00-00-930-015
(4) Remove the STALL WARNING SYSTEM INOP placard from the STALL WARNING TEST switch.
------------------------- END OF TASK ---------------------------
TASK 27-00-00-040-807
14. MMEL 27-14 (DDPG) Preparation - Rudder Trim Indicator Inoperative
A. General
(1) This task gives the maintenance steps which prepare the airplane for flight with the rudder trim
indicator inoperative.
B. References
Reference Title
27-21-00-800-801 Rudder Hydraulic System A, B, or Standby Pressurization (P/B 201)
27-21-00-840-801 Put the Rudder Hydraulic systems A, B, and Standby Back to the
Condition Before the Pressurization (P/B 201)
C. Location Zones
Zone Area
211 Flight Compartment - Left
212 Flight Compartment - Right
325 Vertical Fin - Rudder
D. Procedure
SUBTASK 27-00-00-860-009
(1) Pressurize rudder hydraulic systems A and B. To pressurize them, do this task: Rudder
Hydraulic System A, B, or Standby Pressurization, TASK 27-21-00-800-801.
SUBTASK 27-00-00-040-003
(2) Do a test of the rudder trim actuator:
(a) Turn the rudder trim knob to the NOSE LEFT position.
(b) Make sure the captain’s left rudder pedal moves forward and right rudder pedal moves aft.
(c) Turn the rudder trim knob to the NOSE RIGHT position.
(d) Make sure the captain’s left rudder pedal moves aft and right rudder pedal moves forward.
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
GUN ALL 27-00-00
Page 918
Jun 10/2007
D633A101-GUN
BOEING PROPRIETARY - Copyright#Unpublished Work - See title page for details
SUBTASK 27-00-00-710-003
(3) Do a test of the rudder trim centering:
(a) Turn the rudder trim knob until the captain’s rudder pedals are aligned with each other.
(b) Make sure the rudder is in the neutral position.
1) If it is necessary, move the captain’s rudder pedals lightly to set the rudder to the
neutral position.
SUBTASK 27-00-00-930-016
(4) Attach a INDICATOR INOP placard to the rudder trim indicator.
SUBTASK 27-00-00-860-010
(5) Do this task: Put the Rudder Hydraulic systems A, B, and Standby Back to the Condition
Before the Pressurization, TASK 27-21-00-840-801.
------------------------- END OF TASK ---------------------------
TASK 27-00-00-440-807
15. MMEL 27-14 (DDPG) Restoration - Rudder Trim Indicator Inoperative
A. General
(1) This task puts the airplane back to its usual condition after operation with the rudder trim
indicator inoperative.
B. References
Reference Title
27-11-94-000-803 Rudder Trim Indicator Removal (P/B 401)
27-11-94-400-803 Rudder Trim Indicator Installation (P/B 401)
C. Location Zones
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737-600/700/800/900 AIRCRAFT MAINTENANCE MANUAL飞机维护手册1(50)
