(2)
A00911 Adhesive - BMS 5-126, Type I
B.
Access
(1)
Location Zones 306/406 Wing Trailing Edge, Aileron and Control Tab
C.
Procedure
S 428-012
(1)
Install the index plate:
(a)
Put the index plate on the wing rib and make a mark for the rivet locations.
(b)
Drill and countersink the rivet holes on the index plate.
WARNING: DO NOT GET SOLVENTS IN YOUR MOUTH, OR YOUR EYES, OR ON
_______ YOUR SKIN. DO NOT BREATHE THE FUMES FROM SOLVENTS. SOLVENTS ARE HAZARDOUS MATERIALS. SOLVENTS MAY BE FLAMMABLE OR HARMFUL TO THE ENVIRONMENT. REFER TO PRODUCT MATERIAL SAFETY DATA SHEETS (MSDS) AND LOCAL REQUIREMENTS FOR PROPER HANDLING PROCEDURES.
(c)
Clean the faying surfaces to be bonded with solvent, Series 99 (AMM 20-30-99/201).
(d)
Apply the adhesive.
(e)
Install the index plate.
(f)
Install the rivets, MS20605B-3, that attach the index plate to the wing rib.
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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
D. Put the Airplane Back to Its Usual Condition
S 868-008
(1)
Remove the DO-NOT-CLOSE tags and close these circuit breakers:
(a)
P6-2 Circuit Breaker Panel
1) FLT CONT SHUTOFF VALVES
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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
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737-300/400/500MAINTENANCE MANUAL
AILERON POWER CONTROL UNIT LINKAGE - REMOVAL/INSTALLATION
_________________________________________________________
1. General
_______
A. There are two tasks in this procedure. There is one task for the removal and one task for the installation of the linkage of the power control unit. The procedure has these parts:
(1)
The removal of the power control unit
(2)
The removal of the linkage
(3)
The disassembly of the linkage
(4)
The assembly of the linkage
(5)
The installation of the linkage
(6)
the installation of the power control unit.
B.
You do not have to remove the linkages of system A and system B together.
TASK 27-11-14-004-001
2. Aileron Power Control Unit Linkage Removal
__________________________________________
A. Special Tools and Equipment
(1) F70207-93 Rigging Pins Kit:
~.............................................................................. | | | DIAMETER | LENGTH | | | REF NO. | F70207-( )| (INCHES) | (INCHES) | FUNCTION | ................................................................................
| A/S-3 | -8 | 0.309-0.311 | 3.7 |0.25 | SPOILER CONTROL QUADRANT |
| | | | | LOWER LEVER |
| A/S-4 | -11 | 0.309-0.311 | 6.7 |0.25 | AILERON BUS DRUM |
2.........…...........….............…............….............................1
B. References
(1)
27-11-71/401, Aileron Power Control Unit
C.
Access
(1)
Location Zone
101 Control Cabin, LH
102 Control Cabin, RH
216 Main Wheel Well, LH
217 Main Wheel Well, RH
D.
Remove the Aileron Power Control Unit Linkage
S 024-002
(1)
Do this task: "Aileron Power Control Units Removal" (Ref 27-11-71/401).
S 024-003
(2)
Remove the linkage (Fig. 401):
(a)
Disconnect the cables ABSA and ABSB at the turnbuckles.
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