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Page 602
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(Continued)
NAME OF THE PARTS
THAT ARE IN CONTACT
DIM.
DIAMETER DESIGN LIMITS WEAR LIMITS
MINIMUM
inches/mm
MAXIMUM
inches/mm
PERMITTED
MAXIMUM I.D./
MINIMUM O.D. OF
WORN PART
MAXIMUM
SERVICE
DIAMETRIC
CLEARANCE
#7 BOLT O.D. 0.2485 in
6.3119 mm
0.2495 in
6.3373 mm
0.2475 in
6.2865 mm
0.0127 mm
#8 BUSHING I.D. 0.2500 in
6.3500 mm
0.2505 in
6.3627 mm
0.2525 in
6.4135 mm
0.0005 in
#8 BOLT O.D. 0.2485 in
6.3119 mm
0.2495 in
6.3373 mm
0.2475 in
6.2865 mm
0.0127 mm
SUBTASK 27-11-21-020-005
(4) Do this task: Aileron Balance Tab Installation, TASK 27-11-21-400-801 or Aileron Tab Control
Rods Installation, TASK 27-11-34-400-801.
------------------------- END OF TASK ---------------------------
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
GUN ALL 27-11-21
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Aileron Balance Tab Wear Limits
Figure 601 (Sheet 1 of 2)/27-11-21-990-803
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
GUN ALL 27-11-21
Page 604
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D633A101-GUN
BOEING PROPRIETARY - Copyright#Unpublished Work - See title page for details
Aileron Balance Tab Wear Limits
Figure 601 (Sheet 2 of 2)/27-11-21-990-803
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
GUN ALL 27-11-21
Page 605
Oct 10/2003
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AILERON WING QUADRANT - REMOVAL/INSTALLATION
1. General
A. This procedure has these tasks:
(1) A removal of the aileron wing quadrant
(2) An installation of the aileron wing quadrant.
TASK 27-11-24-000-801
2. Aileron Wing Quadrant Removal
(Figure 401)
A. References
Reference Title
27-11-00-860-801 Remove Pressure from the Aileron Hydraulic Systems A and B
(P/B 201)
B. Tools/Equipment
NOTE: When more than one tool part number is listed under the same "Reference" number, the
tools shown are alternates to each other within the same airplane series. Tool part numbers
that are replaced or non-procurable are preceded by "Opt:", which stands for Optional.
Reference Description
SPL-1585 Kit - Rigging Pins, All Systems
(Part #: F70207-109, Supplier: 81205, A/P Effectivity: 737-600, -700,
-700C, -700ER, -700QC, -800, -900, -900ER, -BBJ)
C. 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
572 Left Wing - Aileron
672 Right Wing - Aileron
D. Access Panels
Number Name/Location
571AT Upper Outboard Fixed Trailing Edge, Quadrant Bolt Access Panel
571DB Lower Outboard Fixed Trailing Edge Access Panel
671AT Upper Outboard Fixed Trailing Edge, Quadrant Bolt Access Panel
671DB Lower Outboard Fixed Trailing Edge Access Panel
E. Prepare for the Removal
SUBTASK 27-11-24-860-001
WARNING: MAKE SURE THE DOWNLOCK PINS ARE INSTALLED ON ALL THE LANDING GEARS.
WITHOUT THE DOWNLOCK PINS, THE LANDING GEARS COULD RETRACT AND
CAUSE INJURIES TO PERSONS AND DAMAGE TO EQUIPMENT.
(1) Do this task: Remove Pressure from the Aileron Hydraulic Systems A and B,
TASK 27-11-00-860-801.
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
GUN ALL 27-11-24
Page 401
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SUBTASK 27-11-24-480-001
(2) Install the rig pin A/S-4, from the rig pin kit, SPL-1585, in the aileron bus drum.
SUBTASK 27-11-24-010-001
(3) Remove the applicable panel:
(a) On the left wing, open this access panel:
Number Name/Location
571DB Lower Outboard Fixed Trailing Edge Access Panel
(b) On the right wing, open this access panel:
Number Name/Location
671DB Lower Outboard Fixed Trailing Edge Access Panel
F. Aileron Wing Quadrant Removal
SUBTASK 27-11-24-020-001
(1) Remove the aileron wing quadrant assembly [9]:
(a) Disconnect the cable ABSA [2] and cable ABSB [4] at the turnbuckles [1].
(b) Safety the disconnect cable ABSA [2] and cable ABSB [4].
(c) Remove the nuts [39], washers [38] and bolts [37] to remove the cable guard [36].
　
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