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(Part #: FDIX 50, Supplier: 0BFD9, A/P Effectivity: 737-ALL)
(Part #: FDV 50, Supplier: 0BFD9, A/P Effectivity: 737-ALL)
(Opt Part #: FDI 100, Supplier: 0BFD9, A/P Effectivity: 737-ALL)
COM-1914 Test Set - Air Data Model FLMTS (Flight Line Maintenance)
(Part #: 01-0987-00, Supplier: 41364, A/P Effectivity: 737-100, -200,
-200C, -300, -400, -500, -600, -700, -700C, -700ER, -700QC, -800, -900,
-900ER, -ALL, -BBJ)
(Part #: 01-1046-00, Supplier: 41364, A/P Effectivity: 737-100, -200,
-200C, -300, -400, -500, -600, -700, -700C, -700ER, -700QC, -800, -900,
-900ER, -ALL, -BBJ)
(Part #: 01-1047-00, Supplier: 41364, A/P Effectivity: 737-ALL)
(Part #: 18910920001, Supplier: 89944, A/P Effectivity: 737-ALL)
(Part #: 6005KTQA1-103, Supplier: 35012, A/P Effectivity: 737-ALL)
(Part #: ADC800, Supplier: 41364, A/P Effectivity: 737-ALL)
(Part #: ADTS405F, Supplier: 0R667, A/P Effectivity: 737-ALL)
(Part #: ADTS505, Supplier: 0R667, A/P Effectivity: 737-ALL)
(Part #: D60340, Supplier: K1474, A/P Effectivity: 737-ALL)
(Part #: D60383, Supplier: K1474, A/P Effectivity: 737-100, -200, -200C,
-300, -400, -500, -600, -700, -700C, -700ER, -700QC, -800, -900, -900ER,
-ALL, -BBJ)
(Part #: DPS500, Supplier: 21844, A/P Effectivity: 737-ALL)
(Part #: MODEL 6300, Supplier: 0RD25, A/P Effectivity: 737-ALL)
(Part #: TES9463, Supplier: 88277, A/P Effectivity: 737-ALL)
(Opt Part #: 18910480000, Supplier: 89944, A/P Effectivity: 737-ALL)
(Opt Part #: D60302, Supplier: K1474, A/P Effectivity: 737-ALL)
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)
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
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Jun 10/2007
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BOEING PROPRIETARY - Copyright#Unpublished Work - See title page for details
(Continued)
Reference Description
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)
D. 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
334 Left Horizontal Stabilizer - Elevator
344 Right Horizontal Stabilizer - Elevator
E. Access Panels
Number Name/Location
311BL Stabilizer Trim Access Door
F. Prepare for the Test
SUBTASK 27-31-00-860-090
WARNING: MAKE SURE THAT PERSONS AND EQUIPMENT ARE CLEAR OF ALL CONTROL
SURFACES BEFORE YOU SUPPLY HYDRAULIC POWER. AILERONS, RUDDERS,
ELEVATORS, FLAPS, SPOILERS, SLATS, 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.
SUBTASK 27-31-00-860-091
(2) Do this task: Null Procedure - Mach Trim Actuator, TASK 27-31-00-700-801.
SUBTASK 27-31-00-480-014
(3) At the two pitot probes on the vertical fin, do the following:
(a) Seal the drain hole on each pitot probe.
CAUTION: MAKE SURE THAT THE PITOT PROBE HAS NO ADDED WEIGHT ON IT FROM THE
TEST HOSE. THE WEIGHT OF THE TEST HOSE CAN BEND OR TWIST THE PITOT
PROBE OUT OF TOLERANCE.
(b) Connect the pressure lines from the air data model test set, COM-1914 or regulator,
SPL-1742 to the two pitot probes on the vertical fin.
SUBTASK 27-31-00-010-020
(4) Open this access panel:
Number Name/Location
311BL Stabilizer Trim Access Door
SUBTASK 27-31-00-480-015
(5) Inside the aft unpressurized compartment, below the elevator feel computer, do the following:
(a) Remove the restrictor valves from the bottom of the pitot lines.
(b) If you are using the regulator, SPL-1742, or equivalent, do the following:
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
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1) Connect the pressure gage lines from the regulator, SPL-1742, or equivalent, to the
drain holes of the pitot lines.
(c) If you are using the air data model test set, COM-1914, then do the following:
1) Install plugs over the ends of the pitot lines.
2) Install a highly visible streamer on the opening of the aft unpressurized compartment.
a) Make sure that you can easily see the streamer from the ground.
　
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