(3)
Remove torque wrench adapter from aileron control wheel.
(4)
Replace medallion on aileron control wheel.
501
May 15/70 BOEING PROPRIETARY - Copyright . - Unpublished Work - See title page for details. 27-11-51 Page 503
T52454
Aileron Deflection Diagram 523
27-11-51 Figure 502 Aug 01/95
Page 504
BOEING PROPRIETARY - Copyright . - Unpublished Work - See title page for details.
1. General
A. This data consists of illustration and wear limits charts. No procedure is given for gaining access to permit inspection. For this information, refer to component removal/installation.
2. Aileron Control Wheel Drum Wear Limits
G03322 G05246 G44591
580 Aileron Control Wheel Drum Wear Limits
Nov 15/79 Figure 601 (Sheet 1) BOEING PROPRIETARY - Copyright . - Unpublished Work - See title page for details. 27-11-51 Page 601
Aileron Control Wheel Drum Wear Limits 500
27-11-51 Page 602 Figure 601 (Sheet 2) BOEING PROPRIETARY - Copyright . - Unpublished Work - See title page for details. Aug 15/73
500 Aileron Control Wheel Drum Wear Limits
Aug 15/73 Figure 601 (Sheet 3) BOEING PROPRIETARY - Copyright . - Unpublished Work - See title page for details. 27-11-51 Page 603
AILERON TRANSFER MECHANISM - REMOVAL/INSTALLATION
1. Equipment and Materials
A. Control Column Protractor Assembly-4MIT65B80307-1 (Preferred) or F52485-500 (Optional) which is used with the following adapters:
(1)
Control Wheel Protractor Mount-F72790
(2)
Forward Thrust Lever Protractor Adapter-F72952-2
B. Rigging Pins Kit-F70207-84, or 98:
REF NO. F70207-( ) DIAMETER (INCHES) LENGTH (INCHES) FUNCTION
A/S-1 A/S-1A A/S-3 A/S-4 -13 -19 -8 -11 0.309-0.311 0.309-0.311 0.309-0.311 0.309-0.311 2.35 +0.06 8.25 +0.25 3.7 +0.25 6.7 +0.25 AILERON TRANSFER MECHANISM AILERON TRANSFER MECHANISM SPOILER CONTROL QUADRANT LOWER LEVER AILERON BUS DRUM
C. Control Wheel Straightedge-SE27-0001
D. Grease-Mil-G-25760 (Ref 20-30-21)
E. Torque and Force Test Control Wheel Adapter-F72867-1
2. Prepare to Remove Aileron Transfer Mechanism
A. Ensure hydraulic systems A and B are depressurized (Ref 27-11-0 MP).
B. Place aileron control wheels and aileron trim control wheel in neutral positions.
C. Insert rigging pins A/S-1 and A/S-1A in aileron transfer mechanism (Fig. 401).
NOTE: Rigging pin A/S-1 must be fully put into transfer mechanism and held to keep it from falling out.
D. Insert rigging pin A/S-4 in aileron bus drums.
E. Insert rigging pin A/S-3 in right aileron control quadrant shaft.
3. Remove Aileron Transfer Mechanism
A. Remove cable shields and disconnect cables ACBA and ACBB at turnbuckles. Secure disconnected cables and tag cables to facilitate reassembly.
542
May 01/99 BOEING PROPRIETARY - Copyright . - Unpublished Work - See title page for details. 27-11-61 Page 401
G42342 G03372
Aileron Transfer Mechanism Installation 500
27-11-61 Page 402 Figure 401 (Sheet 1) BOEING PROPRIETARY - Copyright . - Unpublished Work - See title page for details. Aug 15/69
500 Aileron Transfer Mechanism Installation
Nov 01/75 Figure 401 (Sheet 2) BOEING PROPRIETARY - Copyright . - Unpublished Work - See title page for details. 27-11-61 Page 403
B. Disconnect right cables AA and AB at turnbuckles. Secure disconnected cables and tag cables to facilitate reassembly .
C. Remove nuts, washers and bolts securing transfer mechanism to structure.
D. Slide transfer mechanism downward while guiding cables ACBA and ACBB through cutouts until assembly is separated from structure.
E. Remove nut, washers and screws securing cable guards, and remove cable guards.
F. Disengage cables AA and AB from aileron transfer mechanism.
G. Remove cables ACBA and ACBB from transfer mechanism.
4. Install Aileron Transfer Mechanism
A. Lubricate cables AA and AB with grease and secure to spoiler drum.
B. Install cable guards and secure with screws, washers and nuts. (See figure 401.)
C. Lubricate cables ACBA and ACBB and secure cables to bus drum.
D. Guide ends of cables ACBA and ACBB through cutouts, and simultaneously position transfer mechanism into place.
E. Secure transfer mechanism with bolts, washers and nuts.
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