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AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
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BOEING PROPRIETARY - Copyright#Unpublished Work - See title page for details
Flap Control Lever Position Sensor Installation
Figure 201 (Sheet 3 of 3)/27-51-06-990-801
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AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
GUN ALL 27-51-06
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Oct 10/2003
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TASK 27-51-06-400-802
3. Flap Control Lever Position Sensor Installation
(Figure 201)
A. Location Zones
Zone Area
211 Flight Compartment - Left
212 Flight Compartment - Right
B. Flap Control Lever Position Sensor Installation
SUBTASK 27-51-06-860-012
(1) Make sure that this circuit breaker is open and has safety tag:
F/O Electrical System Panel, P6-2
Row Col Number Name
A 12 C00213 FC TE FLAP POS/SKEW SNSR & IND LEFT
SUBTASK 27-51-06-010-008
(2) Install the flap control lever position sensor [20] on the position sensor assembly [2]:
NOTE: The position sensor assembly [2] includes the position sensor [20], bracket
assembly [23], bracket [24] and the crank [18].
(a) Put the bracket assembly [23] in its position on the bracket [24].
(b) Put the crank [18] in its position through the slot in the bracket [24].
(c) Put the crank [18] on the shaft of the position sensor [20] and put the position sensor [20] in
its position on the bracket [24].
(d) Install the screw [27], washers [28] and nut [29] to attach the crank [18] to the position
sensor [20].
(e) Install the screws [25] and washers [26] to attach the position sensor [20] to the bracket [24].
NOTE: Make sure the wire for the electrical connector [9] is approximately 1808 from the
crank [18].
SUBTASK 27-51-06-420-006
(3) Install the flap control lever position sensor assembly [2]:
(a) Put the flap control lever position sensor assembly [2] in its position on the control stand
[7].
(b) Install the screws [19] that attach the flap control lever position sensor assembly [2].
(c) Install the bolt [22] and nut [21] to attach the link [17] to the crank [18].
SUBTASK 27-51-06-420-007
(4) Connect the electrical connector [9] for the flap control lever position sensor [20].
SUBTASK 27-51-06-420-008
(5) Install the clamps [10] with the bolts [11], washers [12] and nuts [13] to attach the wire for the
electrical connector [9] to the control stand [1].
SUBTASK 27-51-06-420-009
(6) Install the clamp [14] with the bolt [15] and washers [16] to attach the wire for the electrical
connector [9] to the control stand [1].
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EFFECTIVITY
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Oct 10/2003
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SUBTASK 27-51-06-860-013
(7) Remove the safety tag and close this circuit breaker:
F/O Electrical System Panel, P6-2
Row Col Number Name
A 12 C00213 FC TE FLAP POS/SKEW SNSR & IND LEFT
SUBTASK 27-51-06-820-003
(8) Do this task: Flap Control Lever Position Sensor Adjustment, TASK 27-51-06-820-802.
SUBTASK 27-51-06-730-007
(9) Do this task: Flap Control Lever Position Sensor System Test, TASK 27-51-06-730-802.
C. Put the Airplane Back to Its Usual Condition
SUBTASK 27-51-06-410-007
(1) Install the side cover [3] on the lower right side of the control stand [7]:
(a) Put the side cover [3] in its position on the control stand [7].
NOTE: The lower side cover [3] goes under the upper side cover [1].
(b) Install the screws [4] that attach the side cover [3] to the control stand [7].
(c) Tighten the lower screws [8] that attach the upper side cover [1]
(d) Install the pocket assembly [6] with the screws [5] on the side cover [3].
------------------------- END OF TASK ---------------------------
TASK 27-51-06-820-802
4. Flap Control Lever Position Sensor Adjustment
A. References
Reference Title
24-22-00-860-811 Supply Electrical Power (P/B 201)
29-11-00-860-805 Hydraulic System A or B Power Removal (P/B 201)
B. Location Zones
Zone Area
117 Electrical and Electronics Compartment - Left
118 Electrical and Electronics Compartment - Right
211 Flight Compartment - Left
212 Flight Compartment - Right
C. Access Panels
Number Name/Location
117A Electronic Equipment Access Door
D. Prepare for the Adjustment
SUBTASK 27-51-06-860-014
(1) Do this task: Supply Electrical Power, TASK 24-22-00-860-811.
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AIRCRAFT MAINTENANCE MANUAL
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737-600-700-800-900 AIRCRAFT MAINTENANCE MANUAL飞机维护手册4(75)
