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F/O Electrical System Panel, P6-2
Row Col Number Name
A 7 C00210 FLIGHT CONTROL FLAP SHUTOFF VALVES
GUN ALL; AIRPLANES WITH TRAILING EDGE FLAPS UP SWITCH S01051
SUBTASK 27-51-63-860-007
(7) Remove the safety tags and close these circuit breakers:
F/O Electrical System Panel, P6-2
Row Col Number Name
A 15 C01081 HYDRAULIC SYSTEM PTU VALVE CONT 1
A 16 C01085 HYDRAULIC SYSTEM PTU VALVE CONT 2
B 8 C01464 FLIGHT CONTROL ELEV TAB VLV RIGHT
B 13 C00363 FLIGHT CONTROL SHUTOFF VALVES FLT CONT
C 13 C01074 FLIGHT CONTROL SHUTOFF VALVES FLT CONT
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AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
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Jun 10/2005
D633A101-GUN
BOEING PROPRIETARY - Copyright#Unpublished Work - See title page for details
GUN ALL; AIRPLANES WITH TRAILING EDGE FLAPS UP SWITCH S01051 (Continued)
F/O Electrical System Panel, P6-3
Row Col Number Name
E 14 C00316 INDICATOR MASTER DIM SECT 4
F/O Electrical System Panel, P6-4
Row Col Number Name
GUN 101-122
A 8 C00265 AIR CONDITIONING RAM AIR MOD CONT LEFT
GUN ALL
SUBTASK 27-51-63-820-001
(8) Adjust the applicable limit switch [9] or limit switch [10]. To adjust the limit switch, do this task:
Flaps Limit Switch Adjustment, TASK 27-51-63-820-801.
SUBTASK 27-51-63-420-004
(9) Install lockwire on the nuts [18] for the limit switch [10].
SUBTASK 27-51-63-420-005
(10) Install lockwire on the nuts [15] for the limit switch [9].
SUBTASK 27-51-63-410-001
(11) Install the switch cover [8] on the flap control unit [1]:
(a) Put the switch cover [8] in its location on the flap control unit [1].
(b) Apply compound, C00913 to the shank and threads of the screws [7].
(c) Install the washer [21] and screws [7] that attach the switch cover [8].
F. Put the Airplane Back to Its Usual Condition
SUBTASK 27-51-63-440-001
(1) Do this task: Trailing Edge Flap System Reactivation, TASK 27-51-00-440-801.
SUBTASK 27-51-63-720-001
(2) Do the applicable test of the limit switch:
(a) For the TE Flap UP switch [9], S245, do this task: Flaps UP Limit Switch, S245 Functional
Test, TASK 27-51-63-720-801.
(b) For the TE Flap Down switch [10], S246, do this task: Flaps DOWN Limit Switch, S246
Functional Test, TASK 27-51-63-720-802.
(c) For the TE Flap UP switch [9], S1051, do this task: Feel Differential Pressure Light - Test,
TASK 27-31-00-700-811.
------------------------- END OF TASK ---------------------------
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EFFECTIVITY
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FLAP LIMIT SWITCHES - ADJUSTMENT/TEST
1. General
A. This procedure has these tasks:
(1) An adjustment of the flap limit switches
(2) A functional test of the Flaps UP limit switch S245
(3) A functional test of the Flaps DOWN limit switch S246.
TASK 27-51-63-820-801
2. Flaps Limit Switch Adjustment
(Figure 501)
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.
(2) The flap drive system and the cables must be correctly adjusted before you do this task.
B. References
Reference Title
27-31-00-700-815 Elevator Tab Control System - Operational Test (P/B 501)
27-51-00-040-801 Trailing Edge Flap System Deactivation (P/B 201)
27-51-00-440-801 Trailing Edge Flap System Reactivation (P/B 201)
27-51-00-860-803 Extend the Trailing Edge Flaps (P/B 201)
27-51-00-860-804 Retract the Trailing Edge Flaps (P/B 201)
29-22-00-710-801 Power Transfer Unit Operational Test (P/B 501)
32-00-01-480-801 Landing Gear Downlock Pins Installation (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. Consumable Materials
Reference Description Specification
A02315 Sealant - Low Density, Synthetic Rubber. 2 Part BMS5-142
C00913 Compound - Nondrying Resin Mix Corrosion
Inhibiting Material
BMS3-27
D. Location Zones
Zone Area
133 Main Landing Gear Wheel Well, Body Station 663.75 to Body Station
727.00 - Left
134 Main Landing Gear Wheel Well, Body Station 663.75 to Body Station
727.00 - Right
E. Prepare for the Adjustment
SUBTASK 27-51-63-860-008
(1) If the trailing edge flaps are not in the retracted position, do this task: Retract the Trailing Edge
Flaps, TASK 27-51-00-860-804.
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EFFECTIVITY
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