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Reference Description
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)
COM-1916 Adapter - Pitot Probe
(Part #: P75701M2-3, Supplier: 38002, A/P Effectivity: 737-600, -700,
-700C, -700ER, -700QC, -800, -900, -900ER, -BBJ)
STD-883 Test Set - Air Data, RVSM Compatible
D. Location Zones
Zone Area
117 Electrical and Electronics Compartment - Left
118 Electrical and Electronics Compartment - Right
121 Forward Cargo Compartment - Left
122 Forward Cargo Compartment - Right
211 Flight Compartment - Left
212 Flight Compartment - Right
E. Access Panels
Number Name/Location
117A Electronic Equipment Access Door
F. Prepare for the Test
SUBTASK 27-51-00-860-076
(1) Do this task: Supply Electrical Power, TASK 24-22-00-860-811.
SUBTASK 27-51-00-860-077
WARNING: KEEP PERSONS AND EQUIPMENT CLEAR OF THE FLIGHT CONTROL SURFACES, THE
THRUST REVERSERS, AND THE LANDING GEAR. THESE COMPONENTS CAN MOVE
SUDDENLY WHEN YOU SUPPLY HYDRAULIC POWER. THIS CAN CAUSE INJURIES TO
PERSONS AND DAMAGE TO EQUIPMENT.
(2) Supply system B hydraulic power, do this task: Hydraulic System A or B Pressurization,
TASK 29-11-00-860-801.
SUBTASK 27-51-00-010-015
(3) To get access to the main equipment center, do this task.
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
GUN ALL 27-51-00
Page 559
Oct 10/2007
D633A101-GUN
BOEING PROPRIETARY - Copyright#Unpublished Work - See title page for details
Open this access panel:
Number Name/Location
117A Electronic Equipment Access Door
G. Trailing Edge Flap Load Relief System Functional Test
SUBTASK 27-51-00-740-009
(1) Push the ON/OFF button on the front panel of the FSEU to turn on the display.
NOTE: The display will show EXISTING FAULTS?
SUBTASK 27-51-00-000-001
(2) Open these circuit breakers and install safety tags:
CAPT Electrical System Panel, P18-3
Row Col Number Name
C 2 C00238 HEATERS TEMP PROBE
D 3 C01071 HEATERS ALPHA VANE RIGHT
D 5 C00525 HEATERS F/O PITOT
D 6 C00524 HEATERS AUX PITOT
SUBTASK 27-51-00-740-010
(3) Do the BITE test of the load relief system:
(a) Push the down arrow until GROUND TESTS? shows on the display.
(b) Push the YES button to select GROUND TESTS? on the FSEU.
(c) Push the down arrow until TE FLAP LD REL? shows on the display.
(d) Push the YES button to select TE FLAP LD REL? from the menu.
(e) Follow the instructions on the FSEU display to complete the test.
NOTE: It will be necessary to operate the trailing edge flaps when the FSEU requests that
they be in a different position.
GUN 155, 201-999
1) Make sure the FLAP LOAD RELIEF light on the P3-1 panel comes on during the test.
GUN ALL
(f) Make sure that TEST PASSED shows at the end of the test.
SUBTASK 27-51-00-860-078
(4) Push the ON/OFF button on the front panel of the FSEU to turn it off.
SUBTASK 27-51-00-480-010
(5) Connect a pitot/static system tester to the left pitot probe to supply airspeed output from the left
ADIRU. To connect the tester, do this task: Captain’s Total Air Pressure System -
Pressurization, TASK 34-11-00-790-803.
SUBTASK 27-51-00-720-013
(6) Do a test of the load relief system with the flaps at 40 units:
(a) Use the primary system to extend the flaps to the 40-unit position. To retract the flaps, do
this task: Trailing Edge Flap System Operation With Primary Control,
　
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