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27-11-14
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A 737-300/400/500MAINTENANCE MANUAL
RIGGING
PIN A/S-3
AILERON
SPRING
AILERON BODY TURNBUCKLE CARTRIDGE
QUADRANT CABLE AB
CABLE AA CABLE
ABSA
RIGGING
PRESSURE PIN A/S-4
DECK
TURNBUCKLE
CABLE ABSB
SEE A
AILERON
BUS DRUMS
TURNBUCKLE
RETAINING PLATE
(4 LOCATIONS)
CABLE TURNBUCKLE
ABSB
FWD INBD
CABLE
ABSA
Aileron Power Control Unit Linkage Installation
Figure 401 (Sheet 1)
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A
737-300/400/500
MAINTENANCE MANUAL
SAFETY LINK REACTION LINK(TOP) (TOP)
SAFETY LINK
(LOWER) AILERON POWER CONTROL UNIT (SYSTEM B)
SUPPORT (TOP)
SUPPORT SPACER (TOP)
DIAGONAL SUPPORT (TOP)
LEVER ASSEMBLY (TOP)
REACTION LINK SPACER (2 EACH) (TOP)
SUPPORT ASSEMBLY
(TOP) AILERON POWER CONTROL UNIT
SPRING CARTRIDGE(SYSTEM A) LEVER (TOP ONLY)
REACTION LINK (LOWER)
ALIGNMENT PIN
DIAGONAL
FWD SUPPORT
SUPPORT (LOWER)
(LOWER) BUS DRUMS
INBD
A
Aileron Power Control Unit Linkage Installation
Figure 401 (Sheet 2)
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
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A 737-300/400/500MAINTENANCE MANUAL
(b)
Remove the nuts, washers, and screws that hold the plates to the aileron bus drum.
(c)
Disengage the cables ABSA and ABSB from the aileron bus drum.
(d)
Safety the disconnected cables.
(e)
On system B, remove the cotter pin, nut, washer, and bolt to disconnect the spring cartridge at the inboard end.
(f)
Remove the alignment pins between the support assemblies.
(g)
Remove the nuts, washers, and bolts to disengage the diagonal support from the structure.
(h)
Remove the nut, washer, spacer and bolt to disconnect the safety link from the outboard end of the reaction link.
(i)
Remove the nuts, washers, and bolts to disconnect the support from the structure.
(j)
Remove the linkage from the airplane.
S 034-004
(3)
Disassemble the linkage:
(a)
Remove the cotter pin, nut, and washer to remove the support.
(b)
Remove the support spacer.
(c)
Remove the nut, washer, and bolt from the lever assembly.
(d)
Remove the reaction link, spacers, and lever assembly.
(e)
On system B, remove the nut, washer, and bolt from the spring cartridge lever.
(f)
Remove the lever.
(g)
On system A, remove the spacer.
(h)
Remove the support assembly.
(i)
Remove the lockbolts and the collars to remove the bus drum from the shaft.
TASK 27-11-14-404-005
3. Aileron Power Control Unit Linkage Installation
_______________________________________________
A. Special Tools and Equipment
(1) F70207-93 Rigging Pins Kit:
~.............................................................................. | | | DIAMETER | LENGTH | | | REF NO. | F70207-( )| (INCHES) | (INCHES) | FUNCTION | ................................................................................
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本文链接地址：737-300 400 500 AMM 飞机维护手册 飞行操纵 FLIGHT CONTROLS 1(108)
