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时间:2010-08-25 15:35来源:蓝天飞行翻译 作者:admin
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SUBTASK 27-51-63-720-003
(11) Do this task:Stabilizer Trim Motor Test, TASK 27-41-71-700-801
GUN 155, 156
SUBTASK 27-51-63-710-011
(12) Do this test of the passenger information signs:SUBTASK 33-20-00-710-006-001
GUN ALL
SUBTASK 27-51-63-860-018
(13) Remove system B hydraulic power, do this task: Hydraulic System A or B Power Removal,
TASK 29-11-00-860-805.
SUBTASK 27-51-63-940-001
(14) Close this access panel:
Number Name/Location
117A Electronic Equipment Access Door
------------------------- END OF TASK ---------------------------
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AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
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BOEING PROPRIETARY - Copyright#Unpublished Work - See title page for details
Flap Limit Switch Test
Figure 502 (Sheet 1 of 3)/27-51-63-990-803
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
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Page 514
Jun 10/2007
D633A101-GUN
BOEING PROPRIETARY - Copyright#Unpublished Work - See title page for details
Flap Limit Switch Test
Figure 502 (Sheet 2 of 3)/27-51-63-990-803
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
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BOEING PROPRIETARY - Copyright#Unpublished Work - See title page for details
Flap Limit Switch Test
Figure 502 (Sheet 3 of 3)/27-51-63-990-803
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EFFECTIVITY
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TASK 27-51-63-720-802
4. Flaps DOWN Limit Switch, S246 Functional Test
(Figure 502)
A. General
(1) This task is applicable to the Flaps DOWN Limit Switch, S246.
B. References
Reference Title
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)
29-11-00-860-805 Hydraulic System A or B Power Removal (P/B 201)
C. Location Zones
Zone Area
117 Electrical and Electronics Compartment - Left
118 Electrical and Electronics Compartment - Right
211 Flight Compartment - Left
212 Flight Compartment - Right
D. Access Panels
Number Name/Location
117A Electronic Equipment Access Door
E. Flaps DOWN Limit Switch, S246 Test
SUBTASK 27-51-63-860-019
(1) Do this task: Supply Electrical Power, TASK 24-22-00-860-811.
SUBTASK 27-51-63-010-004
(2) To gain access to the Electronic Equipment Center, do this step:
Open this access panel:
Number Name/Location
117A Electronic Equipment Access Door
SUBTASK 27-51-63-860-020
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.
(3) Supply system B hydraulic power, do this task: Hydraulic System A or B Pressurization,
TASK 29-11-00-860-801.
SUBTASK 27-51-63-860-021
WARNING: MAKE SURE PERSONS AND EQUIPMENT ARE AWAY FROM THE TRAILING EDGE
FLAPS AND THE LEADING EDGE FLAPS AND SLATS. THE FLAPS AND SLATS WILL
MOVE. THIS CAN CAUSE INJURIES TO PERSON AND DAMAGE TO EQUIPMENT.
(4) Move the flap control lever to the 30-unit position. Wait for the flaps to move to the 30-unit
position.
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
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SUBTASK 27-51-63-710-006
(5) Move the ALTERNATE FLAPS ARM switch to the ARM position.
SUBTASK 27-51-63-860-027
(6) Move the flap control lever to the 40-unit position.
NOTE: The flaps should not move when you move the flap control lever.
SUBTASK 27-51-63-710-009
(7) Move the ALTERNATE FLAPS control switch to the DOWN position and hold it until the trailing
edge flaps stop moving.
SUBTASK 27-51-63-740-002
(8) Use the FSEU to do a check of the position of the trailing edge flaps:
(a) Push the ON/OFF button on the front panel of the FSEU to turn on the display.
NOTE: The display will show EXISTING FAULTS?.
(b) Push the down arrow until OTHER FUNCTNS? shows on the display.
(c) Push the YES button to select OTHER FUNCTNS? on the FSEU.
(d) Push the down arrow until I/O MONITOR? shows on the display.
(e) Push the YES button to select I/O MONITOR? from the menu.
(f) Push the down arrow until SYNCHRO INPUTS? shows on the display.
(g) Push the YES button to select SYNCHRO INPUTS? from the menu.
 
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