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D. Access Panels
Number Name/Location
117A Electronic Equipment Access Door
E. Procedure
SUBTASK 27-51-01-860-001
(1) Open these circuit breakers and install safety tags:
F/O Electrical System Panel, P6-2
Row Col Number Name
A 6 C00566 FLIGHT CONTROL FLAP LOAD RELIEF
A 7 C00210 FLIGHT CONTROL FLAP SHUTOFF VALVES
A 8 C00211 FLIGHT CONTROL FSEU DC 1
A 9 C01468 FLIGHT CONTROL FSEU DC 2
A 11 C01443 FC TE FLAP POS/SKEW SNSR & IND RIGHT
A 12 C00213 FC TE FLAP POS/SKEW SNSR & IND LEFT
SUBTASK 27-51-01-010-001
(2) To get access to the main equipment center, do this step:
Open this access panel:
Number Name/Location
117A Electronic Equipment Access Door
SUBTASK 27-51-01-020-001
(3) Remove the FSEU [1] from the E1-1 shelf, do this task: E/E Box Removal,
TASK 20-10-07-000-801.
------------------------- END OF TASK ---------------------------
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Figure 401 (Sheet 1 of 2)/27-51-01-990-801
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Figure 401 (Sheet 2 of 2)/27-51-01-990-801
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TASK 27-51-01-400-801
3. Flap/Slat Electronics Unit Installation
(Figure 401)
A. General
(1) The FSEU [1] is installed on the E1-1 shelf in the main equipment center.
B. References
Reference Title
20-10-07-400-801 E/E Box Installation (P/B 201)
24-22-00-860-811 Supply Electrical Power (P/B 201)
27-51-00-740-801 FSEU Display and Existing Faults Test (P/B 501)
27-51-00-740-802 Trailing Edge Flap Asymmetry Skew System BITE Test (P/B 501)
27-51-00-740-803 Trailing Edge Flap Load Relief System BITE Test (P/B 501)
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)
32-09-00-860-801 Put the Airplane in the Air Mode (P/B 201)
32-09-00-860-802 Return the Airplane to the Ground Mode (P/B 201)
C. Expendables/Parts
AMM Item Description AIPC Reference AIPC Effectivity
1 FSEU 27-51-01-01-005 GUN 001-028, 101-121,
155-157, 201-999
D. Location Zones
Zone Area
117 Electrical and Electronics Compartment - Left
118 Electrical and Electronics Compartment - Right
E. Access Panels
Number Name/Location
117A Electronic Equipment Access Door
F. Flap/Slat Electronic Unit Installation
SUBTASK 27-51-01-420-001
(1) Install the FSEU [1] on the E1-1 shelf, do this task: E/E Box Installation, TASK 20-10-07-400-801.
SUBTASK 27-51-01-860-002
(2) Remove the safety tags and close these circuit breakers:
F/O Electrical System Panel, P6-2
Row Col Number Name
A 6 C00566 FLIGHT CONTROL FLAP LOAD RELIEF
A 7 C00210 FLIGHT CONTROL FLAP SHUTOFF VALVES
A 8 C00211 FLIGHT CONTROL FSEU DC 1
A 9 C01468 FLIGHT CONTROL FSEU DC 2
A 11 C01443 FC TE FLAP POS/SKEW SNSR & IND RIGHT
A 12 C00213 FC TE FLAP POS/SKEW SNSR & IND LEFT
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G. Flap/Slat Electronic Unit Installation Test
SUBTASK 27-51-01-860-003
(1) Do this task: Supply Electrical Power, TASK 24-22-00-860-811.
SUBTASK 27-51-01-860-004
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 27-51-01-740-001
(3) Do the Existing Faults BITE test with the FSEU [1]. To do the BITE test, do this task: FSEU
Display and Existing Faults Test, TASK 27-51-00-740-801.
SUBTASK 27-51-01-740-002
(4) Do the Load Relief BITE test with the FSEU [1]. To do the BITE test, do this task: Trailing Edge
Flap Load Relief System BITE Test, TASK 27-51-00-740-803.
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737-600-700-800-900 AIRCRAFT MAINTENANCE MANUAL飞机维护手册4(66)
