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
plates [14] from the aileron bus drum [20].
(c) Disengage the cable ABSA [19] and cable ABSB [22] from the aileron bus drum [20].
(d) Safety the disconnected cable ABSA [19] and cable ABSB [22] to secure them.
(e) Remove the cotter pin [6], washers [5] to remove the cable retention pins [4] between the
support frames [7] and [21].
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(f) Remove the nuts [23] and screws [25] to disconnect the System B upper quadrant
assembly from the System A lower quadrant assembly.
(g) For system A, do these steps:
1) Remove the nut [47], washer [46], washer [45] and bolt [44] to disconnect the diagonal
support [39] from the structure.
2) Remove the nut [34], washer [33], washer [32] and bolt [31] to remove the diagonal
support [39] from the support frame [21].
3) Remove the nuts [49] to remove the hydraulic fittings.
4) Remove the nut [30], washer [29], washer [28], bolt [27], nut [38], washer [37], washer
[36], and bolt [35] to remove the support frame [21] from the structure.
(h) For system B, do these steps:
1) Remove the nut [12], washer [11], bushing [10], washer [9] and bolt [8] to disconnect the
spring cartridge [13] at the inboard end;
2) Remove the nut [68], washer [69], bushing [70], shims [67], washer [72] and bolt [71] to
disconnect the diagonal support [62] from the structure;
3) Remove the nut [55], washer [54], washer [53] and bolt [52] to remove the diagonal
support [62] from the support assembly [56];
4) Remove the nut [30], washer [29], washer [28], bolt [27] and nut [66], washer [65],
washer [64], bolt [63] to remove the support frame [7] from the structure.
(i) For system A, do these steps:
1) Remove the nuts [43], washers [42], washers [41] and bolts [40] to disconnect the
support assembly [50] from the structure;
2) Remove the linkage [1] from the airplane.
(j) For system B, do these steps:
1) Remove the nuts [43], washers [42], washers [41] and bolts [40] to disconnect the
support assembly [56] from the structure.
2) Remove the linkage [2] from the airplane.
------------------------- END OF TASK ---------------------------
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Aileron Power Control Unit Linkage Installation
Figure 401 (Sheet 1 of 4)/27-11-14-990-801
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Aileron Power Control Unit Linkage Installation
Figure 401 (Sheet 2 of 4)/27-11-14-990-801
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Aileron Power Control Unit Linkage Installation
Figure 401 (Sheet 3 of 4)/27-11-14-990-801
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Aileron Power Control Unit Linkage Installation
Figure 401 (Sheet 4 of 4)/27-11-14-990-801
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TASK 27-11-14-400-801
3. Aileron Power Control Unit Linkage Installation
(Figure 401)
A. References
Reference Title
27-11-00-700-809 Aileron Travel Test (P/B 501)
27-11-00-820-801 Aileron Cables Adjustment (P/B 501)
27-11-71-400-801 Aileron Power Control Unit Installation (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
(Part #: F70207-109, Supplier: 81205, A/P Effectivity: 737-600, -700,
-700C, -700ER, -700QC, -800, -900, -900ER, -BBJ)
C. Consumable Materials
Reference Description Specification
中国航空网 www.aero.cn
航空翻译 www.aviation.cn
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737-600/700/800/900 AIRCRAFT MAINTENANCE MANUAL飞机维护手册1(143)
