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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.
Reference Description
SPL-1675 Assembly - Lock, Flight Controls
(Part #: F80049-18, Supplier: 81205, A/P Effectivity: 737-100, -200,
-200C, -300, -400, -500, -600, -700, -700C, -700ER, -700QC, -800, -900,
-900ER, -BBJ)
(Opt Part #: F80049-12, Supplier: 81205, A/P Effectivity: 737-100, -200,
-200C, -300, -400, -500, -600, -700, -700C, -700ER, -700QC, -800, -900,
-900ER, -BBJ)
SPL-1676 Assembly - Lock, Flight Controls
(Part #: F80049-17, Supplier: 81205, A/P Effectivity: 737-100, -200,
-200C, -300, -400, -500, -600, -700, -700C, -700ER, -700QC, -800, -900,
-900ER, -BBJ)
C. Location Zones
Zone Area
133 Main Landing Gear Wheel Well, Body Station 663.75 to Body Station
727.00 - Left
134 Main Landing Gear Wheel Well, Body Station 663.75 to Body Station
727.00 - Right
210 Subzone - Control Compartment - Body Station 178.00 to Body
Station 259.50
D. Procedure
SUBTASK 27-31-00-080-002
(1) Remove the flight controls hydraulic module locks from the flight controls shutoff valves.
(a) Remove the lockpins.
(b) Remove the lock, SPL-1675 or lock, SPL-1676 from the two flight controls shutoff valves.
(c) Put the manual override lever at the two flight controls shutoff valves in the position 1 (ON
position).
(d) Connect the electrical connector to the flight controls shutoff valve at the flight controls
hydraulic modules A and B.
SUBTASK 27-31-00-860-012
(2) Set the FLT CONTROL A and B switches on the forward overhead panel to the ON position.
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
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Page 211
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D633A101-GUN
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SUBTASK 27-31-00-860-013
(3) Remove the safety tags and close these circuit breakers:
F/O Electrical System Panel, P6-2
Row Col Number Name
B 13 C00363 FLIGHT CONTROL SHUTOFF VALVES FLT CONT
C 11 C00362 FLIGHT CONTROL SHUTOFF VALVES STBY RUD
C 13 C01074 FLIGHT CONTROL SHUTOFF VALVES FLT CONT
SUBTASK 27-31-00-860-014
(4) If it is necessary, fill the hydraulic reservoirs. To fill them, do this task: Hydraulic Reservoir
Servicing, TASK 12-12-00-610-801.
------------------------- END OF TASK ---------------------------
TASK 27-31-00-700-801
6. Null Procedure - Mach Trim Actuator
A. References
Reference Title
22-11-00-820-802 Elevator Rigging Test (P/B 501)
24-22-00-860-811 Supply Electrical Power (P/B 201)
29-11-00-860-801 Hydraulic System A or B Pressurization (P/B 201)
B. 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.
Reference Description
SPL-1677 Assembly - Trammel Bar, Stabilizer Trim Actuator
(Part #: F80055-1, Supplier: 81205, A/P Effectivity: 737-100, -200,
-200C, -300, -400, -500, -600, -700, -700C, -700ER, -700QC, -800, -900,
-900ER, -BBJ)
C. Location Zones
Zone Area
211 Flight Compartment - Left
212 Flight Compartment - Right
D. Access Panels
Number Name/Location
311BL Stabilizer Trim Access Door
E. Prepare for the Test
SUBTASK 27-31-00-860-146
(1) Do this task: Supply Electrical Power, TASK 24-22-00-860-811.
SUBTASK 27-31-00-860-147
(2) Set the autopilot stab trim cutout switch, on the control stand, to the CUTOUT position.
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
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Page 212
Oct 10/2007
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SUBTASK 27-31-00-860-148
(3) Make sure that the VHF NAV and IRS switches, on the P5 forward overhead panel, are in the
NORMAL positions.
SUBTASK 27-31-00-860-149
(4) Set the left and right IRS select switches, on the P5 aft overhead panel, to the ALIGN or NAV
position.
SUBTASK 27-31-00-860-150
WARNING: KEEP PERSONS AND EQUIPMENT AWAY FROM THE FLIGHT CONTROL SURFACES.
THE AILERONS, ELEVATORS, RUDDER, FLAPS, SLATS, SPOILERS, STABILIZER AND
NOSE GEAR CAN MOVE SUDDENLY WHEN YOU SUPPLY HYDRAULIC POWER. THIS
CAN CAUSE INJURY TO PERSONS AND DAMAGE TO EQUIPMENT.
(5) Supply hydraulic power to hydraulic systems A and B. To supply hydraulic power, do this task:
Hydraulic System A or B Pressurization, TASK 29-11-00-860-801.
　
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本文鏈接地址：737-600/700/800/900 AIRCRAFT MAINTENANCE MANUAL飛機維護手冊2(127)