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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
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
541 Left Wing - Fairing Flap Support No. 4
641 Right Wing - Fairing Flap Support No. 5
E. Procedure
SUBTASK 27-51-13-020-009
(1) Do this task: Inboard Flap Inboard Carriage Removal, TASK 27-51-13-000-802.
SUBTASK 27-51-13-020-010
(2) Use these tools to do a check for wear on the part of the inboard flap inboard carriage:
(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 27-51-13-020-011
(3) Examine the parts of the inboard flap inboard carriage (Table 602):
(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.
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Table 602/27-51-13-993-806
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. 1.1870 in 1.1878 in 1.1915 in
30.150 mm 30.170 mm 30.264 mm 0.0050 in
#1 PIN O.D. 1.1855 in 1.1865 in 1.1828 in 0.1270 mm
30.112 mm 30.137 mm 30.043 mm
#2 ROLLER I.D. 1.1868 in 1.1875 in 1.1915 in
30.145 mm 30.163 mm 30.264 mm 0.0050 in
#2 PIN O.D. 1.1855 in 1.1865 in 1.1825 in 0.1270 mm
30.112 mm 30.137 mm 30.036 mm
#3 ROLLER O.D. 2.9990 in 3.0010 in 2.9970 in
76.175 mm 76.225 mm 76.124 mm
#4 ECCENTRIC
BUSHING
I.D. 1.2500 in
31.750 mm
1.2520 in
31.801 mm
1.2540 in
31.852 mm
0.0050 in
#4 PIN O.D. 1.2480 in 1.2490 in 1.2470 in 0.1270 mm
31.699 mm 31.725 mm 31.674 mm
#5 BUSHING I.D. 3.3000 in 3.3020 in 3.3040 in
88.820 mm 83.871 mm 83.922 mm 0.0050 in
#5 CARTRIDGE O.D. 3.2980 in 3.2990 in 3.2970 in 0.1270 mm
83.769 mm 83.795 mm 83.744 mm
#6 ROLLER I.D. 1.2493 in 1.2500 in 1.2540 in
31.732 mm 31.750 mm 31.852 mm 0.0050 in
#6 PIN O.D. 1.2480 in 1.2490 in 1.2450 in 0.1270 mm
31.699 mm 31.725 mm 31.623 mm
#7 ROLLER O.D. 2.9990 in 3.0010 in 2.9970 in
76.175 mm 76.225 mm 76.124 mm
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SUBTASK 27-51-13-420-007
(4) Do this task: Inboard Flap Inboard Carriage Installation, TASK 27-51-13-400-802.
------------------------- END OF TASK ---------------------------
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Inboard Flap Inboard Carriage Inspection
Figure 602 (Sheet 1 of 2)/27-51-13-990-804
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Inboard Flap Inboard Carriage Inspection
Figure 602 (Sheet 2 of 2)/27-51-13-990-804
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INBOARD AFT FLAP ACTUATING MECHANISM - REMOVAL/INSTALLATION
1. General
A. This procedure has these tasks:
(1) A removal of the inboard aft flap actuating mechanism
(2) An installation of the inboard aft flap actuating mechanism.
B. The aft flap actuating mechanism includes these parts:
(1) The aft flap drive rod
(2) The interconnect pushrod
(3) The crankshaft
(4) The aft flap pushrods
(5) The cables
(6) The outboard bellcrank
(7) The inboard bellcrank
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737-600-700-800-900 AIRCRAFT MAINTENANCE MANUAL飞机维护手册4(108)
