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D633A101-GUN
BOEING PROPRIETARY - Copyright#Unpublished Work - See title page for details
Flap Limit Switch Installation
Figure 401 (Sheet 1 of 4)/27-51-63-990-801
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AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
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D633A101-GUN
BOEING PROPRIETARY - Copyright#Unpublished Work - See title page for details
Flap Limit Switch Installation
Figure 401 (Sheet 2 of 4)/27-51-63-990-801
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AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
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D633A101-GUN
BOEING PROPRIETARY - Copyright#Unpublished Work - See title page for details
Flap Limit Switch Installation
Figure 401 (Sheet 3 of 4)/27-51-63-990-801
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EFFECTIVITY
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Flap Limit Switch Installation
Figure 401 (Sheet 4 of 4)/27-51-63-990-801
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D633A101-GUN
BOEING PROPRIETARY - Copyright#Unpublished Work - See title page for details
TASK 27-51-63-400-801
3. Flap Limit Switch Installation
(Figure 401)
A. General
(1) This task is applicable to the TE Flaps UP switch, S245, the TE Flaps DOWN switch, S246 and the
TE Flaps UP switch S1051.
B. References
Reference Title
27-31-00-700-811 Feel Differential Pressure Light - Test (P/B 501)
27-51-00-440-801 Trailing Edge Flap System Reactivation (P/B 201)
27-51-63-720-801 Flaps UP Limit Switch, S245 Functional Test (P/B 501)
27-51-63-720-802 Flaps DOWN Limit Switch, S246 Functional Test (P/B 501)
27-51-63-820-801 Flaps Limit Switch Adjustment (P/B 501)
C. Consumable Materials
Reference Description Specification
C00913 Compound - Nondrying Resin Mix Corrosion
Inhibiting Material
BMS3-27
D. Location Zones
Zone Area
134 Main Landing Gear Wheel Well, Body Station 663.75 to Body Station
727.00 - Right
E. Flap Limit Switch Installation
SUBTASK 27-51-63-420-001
(1) Install the limit switch [9]:
(a) Remove the roller guide lock ring [12], roller guide [11], nut [13] and washer [14] from the
limit switch [9].
(b) Put the limit switch [9] with the washer [15] and nut [13] in its location on the flap control unit
[1].
(c) Install the washer [14] and nut [13] to hold the limit switch [9] in its position.
(d) Put the roller guide [11] in its position on the limit switch [9].
(e) Install the roller guide lock ring [12] to hold the roller guide [11] in its position.
SUBTASK 27-51-63-420-002
(2) Install the limit switch [10]:
(a) Remove the roller guide lock ring [17], roller guide [16], nut [18] and washer [19] from the
limit switch [10].
(b) Put the limit switch [10] with the washer [20] and nut [18] in its location on the flap control
unit [1].
(c) Install the washer [19] and nut [18] to hold the limit switch [10] in its position.
(d) Put the roller guide [16] in its position on the limit switch [10].
(e) Install the roller guide lock ring [17] to hold the roller guide [16] in its position.
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D633A101-GUN
BOEING PROPRIETARY - Copyright#Unpublished Work - See title page for details
SUBTASK 27-51-63-760-001
(3) Make sure the resistance between the limit switch and the flap control unit [1] is less than 2.5
milliohms.
SUBTASK 27-51-63-420-003
(4) Attach the electrical wires for the limit switch:
(a) Connect the switch leads to the connectors [6].
(b) Attach the connectors [6].
(c) Install new wire bundle ties on the wire bundle [2].
(d) Put the clamps [3] in their locations on the wire bundle [2].
(e) install the screws [4] to attach the clamps [3].
GUN ALL; AIRPLANES WITH TRAILING EDGE FLAPS UP SWITCH S00245
SUBTASK 27-51-63-860-005
(5) Remove the safety tags and close these circuit breakers:
CAPT Electrical System Panel, P18-1
Row Col Number Name
C 7 C00285 YAW DAMPER AC
CAPT Electrical System Panel, P18-3
Row Col Number Name
D 11 C00442 PASSENGER CABIN SIGNS PASS SIGN CONT
F/O Electrical System Panel, P6-2
Row Col Number Name
A 7 C00210 FLIGHT CONTROL FLAP SHUTOFF VALVES
B 10 C00207 FLIGHT CONTROL STAB TRIM CONT
GUN ALL; AIRPLANES WITH TRAILING EDGE FLAPS UP SWITCH S00246
SUBTASK 27-51-63-860-006
(6) Remove the safety tag and close this circuit breaker:
　
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