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SUBTASK 27-51-22-020-005
(3) Examine the parts of the outboard aft flap (Table 601):
(a) Remove the parts that you will measure.
(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 not in tolerance, replace or repair the parts.
Table 601/27-51-22-993-804
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
CLEARANCE
inches/mm
#1 BUSHING I.D. 0.2500 in 0.2505 in 0.2505 in
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AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
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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
CLEARANCE
inches/mm
6.3500 mm 6.3627 mm 6.3627 mm 0.0015 in
#1 BOLT O.D. 0.2490 in 0.2495 in 0.2490 in 0.0381 mm
6.3246 mm 6.3373 mm 6.3246 mm
#2 BUSHING I.D. 0.3750 in 0.3756 in 0.3756 in
9.5250 mm 9.5402 mm 9.5102 mm 0.0016 in
#2 BUSHING O.D. 0.3740 in 0.3745 in 0.3740 in 0.0406 mm
9.4996 mm 9.5123 mm 9.4996 mm
#3 ROD END I.D. 0.2500 in 0.2500 in 0.2500 in
6.3500 mm 6.3500 mm 6.3500 mm 0.0010 in
#3 BOLT O.D. 0.2490 in 0.2495 in 0.2490 in 0.0254 mm
6.3246 mm 6.3373 mm 6.3246 mm
#4 BUSHING I.D. 0.2500 in 0.2506 in 0.2506 in
6.3500 mm 6.3652 mm 6.3652 mm 0.0016 in
#4 BOLT O.D. 0.2490 in 0.2495 in 0.2490 in 0.0406 mm
6.3246 mm 6.3373 mm 6.3246 mm
#5 BUSHING I.D. 0.2500 in 0.2505 in 0.2505 in
6.3500 mm 6.3627 mm 6.3627 mm 0.0015 in
#5 BOLT O.D. 0.2490 in 0.2495 in 0.2490 in 0.0381 mm
6.3246 mm 6.3373 mm 6.3246 mm
#6 BUSHING I.D. 0.3750 in 0.3756 in 0.3756 in
9.5250 mm 9.5402 mm 9.5402 mm 0.0016 in
#6 BUSHING O.D. 0.3740 in 0.3745 in 0.3740 in 0.0406 mm
9.4996 mm 9.5123 mm 9.4996 mm
#7 ROD END I.D. 0.2500 in 0.2500 in 0.2500 in
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AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
GUN ALL 27-51-22
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D633A101-GUN
BOEING PROPRIETARY - Copyright#Unpublished Work - See title page for details
(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
CLEARANCE
inches/mm
6.3500 mm 6.3500 mm 6.3500 mm 0.0010 in
#7 BOLT O.D. 0.2490 in 0.2495 in 0.2490 in 0.0254 mm
6.3246 mm 6.3373 mm 6.3246 mm
#8 BUSHING I.D. 0.2500 in 0.2505 in 0.2505 in
6.3500 mm 6.3627 mm 6.3627 mm 0.0015 in
#8 BOLT O.D. 0.2490 in 0.2495 in 0.2490 in 0.0381 mm
6.3246 mm 6.3373 mm 6.3246 mm
#9 BUSHING I.D. 0.2500 in 0.2505 in 0.2545 in
6.3500 mm 6.3627 mm 6.4643 mm 0.0050 in
#9 BOLT O.D. 0.2485 in 0.2495 in 0.2455 in 0.1270 mm
6.3119 mm 6.3373 mm 6.2357 mm
#10 TRACK I.D. 0.2500 in 0.2505 in 0.2545 in
6.3500 mm 6.3627 mm 6.4643 mm 0.0050 in
#10 BOLT O.D. 0.2485 in 0.2495 in 0.2455 in 0.1270 mm
6.3119 mm 6.3373 mm 6.2357 mm
#11 BUSHING I.D. 0.3750 in 0.3756 in 0.3756 in
9.5250 mm 9.5402 mm 9.5402 mm 0.0016 in
#11 BUSHING O.D. 0.3740 in 0.3745 in 0.3740 in 0.0406 mm
9.4996 mm 9.5123 mm 9.4996 mm
#12 BUSHING I.D. 0.2500 in 0.2505 in 0.2545 in
6.3500 mm 6.3627 mm 6.4643 mm 0.0050 in
#12 BOLT O.D. 0.2485 in 0.2495 in 0.2455 in 0.1270 mm
6.3119 mm 6.3373 mm 6.2357 mm
#13 BUSHING I.D. 0.3125 in 0.3131 in 0.3170 in
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
GUN ALL 27-51-22
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D633A101-GUN
BOEING PROPRIETARY - Copyright#Unpublished Work - See title page for details
(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
CLEARANCE
inches/mm
7.9375 mm 7.9527 mm 8.0518 mm 0.0050 in
#13 BOLT O.D. 0.3110 in 0.3120 in 0.3081 in 0.1270 mm
7.8994 mm 7.9248 mm 7.8257 mm
　
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