曝光臺 注意防騙 網(wǎng)曝天貓店富美金盛家居專營店坑蒙拐騙欺詐消費(fèi)者

SUBTASK 27-51-00-860-035
(1) Push the ON/OFF button on the front panel of the FSEU to turn it off.
SUBTASK 27-51-00-410-007
(2) For the main equipment center, do this task.
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
GUN ALL 27-51-00
Page 548
Oct 10/2006
D633A101-GUN
BOEING PROPRIETARY - Copyright#Unpublished Work - See title page for details
Close this access panel:
Number Name/Location
117A Electronic Equipment Access Door
------------------------- END OF TASK ---------------------------
TASK 27-51-00-740-803
8. Trailing Edge Flap Load Relief System BITE Test
(Figure 501)
A. General
(1) This test does a check of the load relief functions for the trailing edge flaps.
(2) In this procedure it is necessary to move the flap control lever to move the trailing edge flaps.
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
212 Flight Compartment - Right
D. Access Panels
Number Name/Location
117A Electronic Equipment Access Door
E. Prepare for the Test
SUBTASK 27-51-00-860-036
(1) Do this task: Supply Electrical Power, TASK 24-22-00-860-811.
SUBTASK 27-51-00-860-037
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 27-51-00-010-007
(3) To get access to the main equipment center, do this task.
Open this access panel:
Number Name/Location
117A Electronic Equipment Access Door
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
GUN ALL 27-51-00
Page 549
Oct 10/2006
D633A101-GUN
BOEING PROPRIETARY - Copyright#Unpublished Work - See title page for details
F. Trailing Edge Flap Load Relief System BITE Test
SUBTASK 27-51-00-740-006
(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 27-51-00-740-008
(2) 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.
G. Put the Airplane Back to Its Usual Condition
SUBTASK 27-51-00-860-039
(1) Push the ON/OFF button on the front panel of the FSEU to turn it off.
SUBTASK 27-51-00-410-008
(2) For the main equipment center, do this task.
Close this access panel:
Number Name/Location
117A Electronic Equipment Access Door
SUBTASK 27-51-00-860-040
(3) Move the flap control lever to the UP position to retract the flaps.
SUBTASK 27-51-00-860-041
(4) Remove system B hydraulic power, do this task: Hydraulic System A or B Power Removal,
TASK 29-11-00-860-805.
------------------------- END OF TASK ---------------------------
TASK 27-51-00-720-801
9. Flap Priority Valve Test
(Figure 501)
A. General
(1) This test does a check of the flap priority valve.
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
GUN ALL 27-51-00
Page 550
Jun 10/2007
D633A101-GUN
BOEING PROPRIETARY - Copyright#Unpublished Work - See title page for details
B. References
Reference Title
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
211 Flight Compartment - Left
212 Flight Compartment - Right
D. Prepare for the Test
SUBTASK 27-51-00-860-042
WARNING: KEEP PERSONS AND EQUIPMENT CLEAR OF THE FLIGHT CONTROL SURFACES, THE
THRUST REVERSERS, AND THE LANDING GEAR. THESE COMPONENTS CAN MOVE
　
中國航空網(wǎng) www.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：737-600-700-800-900 AIRCRAFT MAINTENANCE MANUAL飛機(jī)維護(hù)手冊4(56)