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Removal/Installation for procedures to remove and install the flight spoiler actuator.
TASK 27-61-51-200-801
2. Flight Spoiler Actuator Inspection
(Figure 601)
A. General
(1) This procedure gives wear limits and repair data for the flight spoiler actuators.
B. References
Reference Title
27-61-51-000-801 Flight Spoiler Actuator Removal (P/B 401)
27-61-51-400-801 Flight Spoiler Actuator Installation (P/B 401)
C. Tools/Equipment
Reference Description
STD-1096 Micrometer - Depth, 0-1 Inch, Readable to 1/1000 Inch
STD-1097 Caliper - Vernier, 0-6 Inch, Readable to 1/1000 Inch
D. Location Zones
Zone Area
562 Left Wing - Spoiler No. 5
563 Left Wing - Spoiler No. 4
564 Left Wing - Spoiler No. 3
565 Left Wing - Spoiler No. 2
662 Right Wing - Spoiler No. 8
663 Right Wing - Spoiler No. 9
664 Right Wing - Spoiler No. 10
665 Right Wing - Spoiler No. 11
E. Procedure
SUBTASK 27-61-51-020-006
(1) To inspect the flight spoiler actuator, you will need to remove it. To remove it, do this task: Flight
Spoiler Actuator Removal, TASK 27-61-51-000-801.
SUBTASK 27-61-51-020-007
(2) Use these tools to check for wear on the parts of the flight spoiler actuator:
(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 27-61-51-020-008
(3) Examine the parts of the flight spoiler actuator for worn areas:
(a) Remove the parts to be checked.
(b) Measure the parts as necessary 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.
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(c) Compare the dimensions you measured with the permitted wear dimensions that follow.
(d) If the parts are not in the tolerance, replace or repair the part as required.
Table 601/27-61-51-993-801
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 BUSHING I.D. 0.7500 in 0.7515 in 0.7520 in
19.050 mm 19.088 mm 19.101 mm 0.0057 in
#1 PIN O.D. 0.7475 in 0.7480 in 0.7458 in 0.146 mm
18.987 mm 18.999 mm 18.943 mm
#2 BEARING I.D. 0.7495 in 0.7500 in 0.7505 in
19.037 mm 19.050 mm 19.063 mm 0.0042 in
#2 PIN O.D. 0.7475 in 0.7480 in 0.7458 in 0.107 mm
18.987 mm 18.999 mm 18.943 mm
#3 BUSHING I.D. 0.2500 in 0.2515 in 0.2525 in
6.350 mm 6.388 mm 6.414 mm 0.0040 in
#3 BOLT O.D. 0.2485 in 0.2495 in 0.2475 in 0.102 mm
6.312 mm 6.337 mm 6.287 mm
#4 BRACKET I.D. 0.3765 in 0.3771 in 0.3777 in
9.563 mm 9.578 mm 9.594 mm 0.0028 in
#4 BUSHING O.D. 0.3755 in 0.3761 in 0.3743 in 0.072 mm
9.538 mm 9.553 mm 9.507 mm
#5 BEARING I.D. 0.2497 in 0.2500 in 0.2510 in
6.342 mm 6.350 mm 6.375 mm 0.0025 in
#5 BOLT O.D. 0.2485 in 0.2495 in 0.2475 in 0.063 mm
6.312 mm 6.337 mm 6.287 mm
#6 BUSHING I.D. 0.2500 in 0.2515 in 0.2525 in
6.350 mm 6.388 mm 6.414 mm 0.0040 in
#6 BOLT O.D. 0.2485 in 0.2495 in 0.2475 in 0.102 mm
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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
6.312 mm 6.337 mm 6.287 mm
SUBTASK 27-61-51-020-009
(4) Reassemble the flight spoiler actuator, as necessary.
SUBTASK 27-61-51-020-010
(5) Install the flight spoiler actuator. To install it, do this task: Flight Spoiler Actuator Installation,
TASK 27-61-51-400-801.
------------------------- END OF TASK ---------------------------
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Flight Spoiler Actuator Wear Limits
Figure 601 (Sheet 1 of 3)/27-61-51-990-802
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