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211 Flight Compartment - Left
212 Flight Compartment - Right
C. Access Panels
Number Name/Location
117A Electronic Equipment Access Door
D. Prepare for the Test
SUBTASK 27-81-00-860-037
(1) Do this task: Supply Electrical Power, TASK 24-22-00-860-811.
SUBTASK 27-81-00-860-038
WARNING: MAKE SURE ALL PERSONS AND EQUIPMENT ARE 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 INJURY TO PERSONS AND DAMAGE TO EQUIPMENT.
(2) To pressurize hydraulic system B, do this task: Hydraulic System A or B Pressurization,
TASK 29-11-00-860-801.
SUBTASK 27-81-00-860-039
(3) If the flap control lever is not in the UP position, do these steps:
WARNING: MAKE SURE PERSONS AND EQUIPMENT ARE CLEAR OF THE LEADING EDGE
FLAPS AND SLATS AND THE TRAILING EDGE FLAPS. THE FLAPS AND SLATS
CAN MOVE QUICKLY. THIS CAN CAUSE INJURY TO PERSONS AND DAMAGE TO
EQUIPMENT.
(a) Move the flap control lever to the UP position.
(b) Let the leading edge flaps and slats and the trailing edge flaps move to the retract position.
SUBTASK 27-81-00-010-002
(4) Open this access panel:
Number Name/Location
117A Electronic Equipment Access Door
E. Leading Edge Flap and Slat Operational Test in Primary Mode
SUBTASK 27-81-00-740-002
(1) Do this task: FSEU Display and Existing Faults Test, TASK 27-51-00-740-801.
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
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SUBTASK 27-81-00-730-001
WARNING: MAKE SURE PERSONS AND EQUIPMENT ARE CLEAR OF THE LEADING EDGE FLAPS
AND SLATS AND THE TRAILING EDGE FLAPS. THE FLAPS AND SLATS WILL MOVE
DURING THIS TEST. THIS CAN CAUSE INJURY TO PERSONS AND DAMAGE TO
EQUIPMENT.
(2) Do a test of the leading edge flap and slat operational test in primary mode:
(a) Use the FSEU front panel to do a check of the position of the leading edge flaps and slats
(Figure 504):
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?.
2) Push the down arrow until OTHER FUNCTNS? shows on the display.
3) Push the YES button to select OTHER FUNCTNS? on the FSEU.
4) Push the down arrow until I/O MONITOR? shows on the display.
5) Push the YES button to select I/O MONITOR? from the menu.
6) Push the YES button to select PROX SENSORS? from the I/O MONITOR? menu.
(b) Push the down arrow to step through the proximity sensor states at the LE flaps and slats
UP position.
(c) Make sure these displays and the proximity sensor states show on the FSEU (Table 504):
Table 504/27-81-00-993-815
Display State
S1 OUTBD GAP NEAR
S1 INBD GAP NEAR
S2 OUTBD GAP FAR
S2 INBD GAP FAR
S2 RETR GAP NEAR
S3 OUTBD GAP FAR
S3 INBD GAP FAR
S3 RETR GAP NEAR
S4 OUTBD GAP FAR
S4 INBD GAP FAR
S4 RETR GAP NEAR
S5 OUTBD GAP FAR
S5 INBD GAP FAR
S5 RETR GAP NEAR
S6 OUTBD GAP FAR
S6 INBD GAP FAR
S6 RETR GAP NEAR
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
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(Continued)
Display State
S7 OUTBD GAP FAR
S7 INBD GAP FAR
S7 RETR GAP NEAR
S8 OUTBD GAP NEAR
S8 INBD GAP NEAR
F1 RETR GAP NEAR
F1 EXT GAP FAR
F2 RETR GAP NEAR
F2 EXT GAP FAR
F3 RETR GAP NEAR
F3 EXT GAP FAR
F4 RETR GAP NEAR
F4 EXT GAP FAR
(d) Move the flap control lever to the 1-unit detent position.
1) Make sure these lights come on during the flaps and slats extension and go off after
extension (Figure 505);
a) The LE FLAPS TRANSIT light on the center instrument panel, P2
b) All the LE flaps and slats TRANSIT lights on the aft overhead panel, P5.
2) Push the down arrow on the FSEU to step through the proximity sensor states.
3) Make sure these displays and the proximity sensor states show on the FSEU
(Table 505):
Table 505/27-81-00-993-816
Display State
S1 OUTBD GAP FAR
S1 INBD GAP NEAR
S2 OUTBD GAP FAR
S2 INBD GAP NEAR
S2 RETR GAP FAR
S3 OUTBD GAP FAR
S3 INBD GAP NEAR
S3 RETR GAP FAR
S4 OUTBD GAP FAR
S4 INBD GAP NEAR
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
GUN ALL 27-81-00
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Feb 10/2006
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