曝光台 注意防骗
网曝天猫店富美金盛家居专营店坑蒙拐骗欺诈消费者
STD-1097 Caliper - Vernier, 0-6 Inch, Readable to 1/1000 Inch
D. Location Zones
Zone Area
572 Left Wing - Aileron
672 Right Wing - Aileron
E. Procedure
SUBTASK 27-11-34-020-004
(1) Do this task: Aileron Balance Tab Removal, TASK 27-11-21-000-801 or Aileron Tab Control
Rods Removal, TASK 27-11-34-000-801.
SUBTASK 27-11-34-020-005
(2) Use these tools to do a check for wear on the parts of the aileron tab control rods:
(a) micrometer (0-1 Inch, readable to 1/1000 Inch), STD-1096
(b) readable to 1/1000 inch vernier 0 - 6 inch caliper, STD-1097.
SUBTASK 27-11-34-020-006
(3) Examine the parts of the aileron tab control rods for worn areas:
(a) Remove the parts you want to do a check.
(b) Measure the parts with a micrometer (0-1 Inch, readable to 1/1000 Inch), STD-1096 or a
readable to 1/1000 inch vernier 0 - 6 inch caliper, STD-1097.
(c) Compare the dimensions you measured with the permitted wear dimensions.
(d) If the parts are out of tolerance, replace or repair the parts.
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Table 601/27-11-34-993-801
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
#1 ROD END BEARING I.D. 0.2495 in
6.3373 mm
0.2500 in
6.3500 mm
0.2520 in
6.4008 mm
0.0000 in
#1 BOLT O.D. 0.2485 in 0.2495 in 0.2475 in 0.0000 mm
6.3119 mm 6.3373 mm 6.2865 mm
#2 BUSHING I.D. 0.3750 in
9.5250 mm
0.3756 in
9.5402 mm
0.3773 in
9.5834 mm
0.0005 in
#2 BUSHING O.D. 0.3740 in
9.4996 mm
0.3745 in
9.5123 mm
0.3728 in
9.4691 mm
0.0127 mm
#3 BUSHING I.D. 0.2500 in
6.3500 mm
0.2505 in
6.3627 mm
0.2525 in
6.4135 mm
0.0005 in
#3 BOLT O.D. 0.2485 in
6.3119 mm
0.2495 in
6.3373 mm
0.2475 in
6.2865 mm
0.0127 mm
#4 BUSHING I.D. 0.2500 in
6.3500 mm
0.2505 in
6.3627 mm
0.2525 in
6.4135 mm
0.0005 in
#4 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 27-11-34-020-007
(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 ---------------------------
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Aileron Tab Control Rods Wear Limits
Figure 601 (Sheet 1 of 2)/27-11-34-990-802
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Aileron Tab Control Rods Wear Limits
Figure 601 (Sheet 2 of 2)/27-11-34-990-802
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AILERON CONTROL WHEEL - REMOVAL/INSTALLATION
1. General
A. This procedure has these tasks:
(1) A removal of the aileron control wheel
(2) An installation of the aileron control wheel.
B. This procedure is applicable for the captain’s and first officer’s aileron control wheel.
TASK 27-11-41-000-801
2. Aileron Control Wheel Removal
A. References
Reference Title
22-11-41-000-801 Autopilot Disengage Switch Removal (P/B 401)
23-51-04-000-801 Control Wheel PTT Switch Removal (P/B 401)
24-22-00-860-812 Remove Electrical Power (P/B 201)
27-11-00-860-801 Remove Pressure from the Aileron Hydraulic Systems A and B
(P/B 201)
27-41-97-000-801 Stabilizer Trim Control Switch Removal (P/B 401)
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
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