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(1) Make sure the speed brake control system is operational, do this task: Speed Brake Control
System Operational Test, TASK 27-62-00-710-801.
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
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SUBTASK 27-00-00-860-004
(2) Remove the safety lock and close this circuit breaker:
F/O Electrical System Panel, P6-2
Row Col Number Name
B 9 C00440 FLIGHT CONTROL AUTO SPEED BRAKE
SUBTASK 27-00-00-810-002
(3) 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 27-00-00-930-007
(4) Remove the AUTO SPOILER INOP placard from the speed brake control lever.
------------------------- END OF TASK ---------------------------
TASK 27-00-00-040-803
6. MMEL 27-10 (DDPG) Preparation - FEEL DIFF PRESS Light Inoperative
A. General
(1) This task gives the maintenance steps which prepare the airplane for flight with the FEEL DIFF
PRESS light on the forward overhead panel inoperative.
B. References
Reference Title
27-31-00-700-801 Null Procedure - Mach Trim Actuator (P/B 201)
27-31-00-800-801 Elevator Hydraulic System A and B - Pressurization (P/B 201)
27-31-00-840-801 Put the Elevator Hydraulic systems A and B Back to the Condition
Before the Pressurization (P/B 201)
C. Tools/Equipment
NOTE: When more than one tool part number is listed under the same "Reference" number, the
tools shown are alternates to each other within the same airplane series. Tool part numbers
that are replaced or non-procurable are preceded by "Opt:", which stands for Optional.
737-600/700/800/900
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EFFECTIVITY
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Reference Description
SPL-1674 Assembly - Adapter, Control Wheel, Torque and Force Test
(Part #: F72867-1, Supplier: 81205, A/P Effectivity: 737-100, -200,
-200C, -300, -400, -500, -600, -700, -700C, -700ER, -700QC, -800, -900,
-900ER, -BBJ)
SPL-1680 Protractor - Assembly, Control Column
(Part #: 4MIT65B80307-1, Supplier: 81205, A/P Effectivity: 737-100,
-200, -200C, -300, -400, -500, -600, -700, -700C, -700ER, -700QC, -800,
-900, -900ER, -BBJ)
(Part #: A27021-29, Supplier: 81205, A/P Effectivity: 737-100, -200,
-200C, -300, -400, -500, -600, -700, -700C, -700ER, -700QC, -800, -900,
-900ER, -BBJ)
SPL-1742 Regulator - Air Pressure, Elevator Feel Computer
(Part #: F72928-58, Supplier: 81205, A/P Effectivity: 737-600, -700,
-700C, -700ER, -700QC, -800, -900, -900ER, -BBJ)
STD-1100 Gauge - Push/Pull, Dial, 0-50 Lb Capacity
D. Consumable Materials
Reference Description Specification
G00252 Film, Plastic Sheeting, Polyethylene L-P-512
G00270 Tape - Masking, General Purpose - 3M #250 A-A-883
G02219 Tape - Yellow Vinyl Adhesive - Scotch Brand No.471
G02443 Tape - Barricade, Orange, 3 inches Wide, 4 mils
Thick, "REMOVE BEFORE FLIGHT"
G02447 Tag - Red Paper, "PITOT PROBES COVERED"
E. Location Zones
Zone Area
211 Flight Compartment - Left
212 Flight Compartment - Right
311 Area Aft of Pressure Bulkhead - Left
312 Area Aft of Pressure Bulkhead - Right
323 Vertical Fin - Front Spar To Rear Spar
F. Access Panels
Number Name/Location
311BL Stabilizer Trim Access Door
G. Feel System Test
SUBTASK 27-00-00-860-005
WARNING: MAKE SURE THAT PERSONS AND EQUIPMENT ARE CLEAR OF ALL CONTROL
SURFACES BEFORE YOU SUPPLY HYDRAULIC POWER. AILERONS, RUDDERS,
ELEVATORS, FLAPS, SLATS, SPOILERS, LANDING GEAR, AND THRUST REVERSERS
CAN MOVE QUICKLY WHEN YOU SUPPLY HYDRAULIC POWER. THIS CAN CAUSE
INJURY TO PERSONS AND DAMAGE TO EQUIPMENT.
(1) Pressurize the elevator hydraulic systems A and B. To pressurize them, do this task: Elevator
Hydraulic System A and B - Pressurization, TASK 27-31-00-800-801.
　
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本文鏈接地址：737-600/700/800/900 AIRCRAFT MAINTENANCE MANUAL飛機維護手冊1(45)