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时间:2011-03-27 12:54来源:蓝天飞行翻译 作者:航空
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

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 4 Attach the clamp (10) and the clamp (25) to the bracket on the
_ HCU with the screw (15) and nut (20).
 5 TORQUE the nut (20) to between 20 and 25 lbf.in (0.22 and 0.28
_
 m.daN).

 6 Connect the generator harness connector 400VCA to the forward
_ pylon junction box. (Ref. Fig. 404/TASK 71-00-00-991-913)
 a Do not clean the contacts with abrasive material.
_ R b_ Do a pin retention check of the sockets (Ref. ESPM 20-48-R 23). c Tighten the connector by hand until the orange (or red)
_ color is visible in the lock display (window).
 7 Connect the electrical connectors 450VCA, 452VCA, 454VCA, and
_ 457VCA to the aft pylon junction box Tighten the connectors fingertight plus one-eighth turn with soft nose pliers. (Ref. Fig. 403/TASK 71-00-00-991-912)
 8 Install the two clamps which attach the core harness to the
_
 pylon.

 NOTE : Make sure that you install the correct clamps on the
____ core harness. Two clamp sizes (diameter) can be found depending on the core harness diameter.
 **ON A/C 153-153,
 Subtask 71-00-00-410-094-A
 B. Install these components: CAUTION : USE 2 WRENCHES TO REMOVE OR INSTALL THE TUBE COUPLING NUTS.
_______ ONE WRENCH TO HOLD THE UNION AND ONE TO LOOSEN OR TIGHTEN THE COUPLING NUT. THIS WILL PREVENT DAMAGE TO THE HARDWARE.
 (1) Install these components on the left side of the engine :
 (a) Connect the fan lower zone extinguishing line forward of the hydraulic junction box. TORQUE union to between 800 and 900 lbf.in (9.04 and 10.17 m.daN).
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 (b) Connect the pylon interface duct to the pylon duct with the coupling (65). (Ref. Fig. 406A/TASK 71-00-00-991-915-A)

 (c) TORQUE the coupling as follows:


 1 TORQUE the coupling nut to the value shown on the coupling.
_
 2 Lightly hit the coupling perimeter in different places with a
_
 fiber hammer.

 3 TORQUE the coupling again to the specified value.
_
 4 Lightly hit the coupling perimeter again.
_
 5 TORQUE the coupling again to the specified value.
_
 (d) Connect the pressure tube (70) to the union installed in the upper high-pressure manifold duct (engine 1 only). (Ref. Fig. 406A/TASK 71-00-00-991-915-A)

 (e) TORQUE the hose coupling to 100 lbf.in (1.13 m.daN).

 (f) Connect the sense tubes (75) and (80) to the pylon interface tubes. (Ref. Fig. 406A/TASK 71-00-00-991-915-A)

 (g) TORQUE the tube coupling to between 100 and 125 lbf.in (1.13 and


 1.41 m.daN).
 (h) Install a new gasket (15) and the main fuel supply hose (20) to the fluid disconnect panel with the four bolts (25) and washers (30). (Ref. Fig. 405/TASK 71-00-00-991-914)
R (i) TORQUE the four bolts (25) to between 65 and 85 lbf.in (0.73 and
R 0.96 m.daN). Safety with lockwire 0.032 in. (0.8 mm) dia.
R (Material No. CP8001).

 (j) Install a new gasket (10) and the fuel/return by-pass hose (45) to the fluid disconnect panel with the bolts (35) and washers (40). (Ref. Fig. 405/TASK 71-00-00-991-914)

 (k) TORQUE the four bolts (35) to between 24 and 36 lbf.in (0.27 and


 0.40 m.daN).
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 (l) Connect the upper case drain hose (50) to the fluid disconnect panel. (Ref. Fig. 405/TASK 71-00-00-991-914)

 (m) TORQUE the hose coupling to between 215 and 245 lbf.in (2.42 and


 2.76 m.daN).
 (n) Connect the hydraulic pressure hose (55) to the fluid disconnect panel. (Ref. Fig. 405/TASK 71-00-00-991-914)

 (o) TORQUE the hose coupling to between 855 and 945 lbf.in (9.66 and


 10.67 m.daN)
 (p) Connect the suction hose (60) to the coupling half installed on the fluid disconnect panel and tighten the coupling nut handtight. (Ref. Fig. 405/TASK 71-00-00-991-914)

 (q) Connect hose/tube (175) to the PRV interface.
 (Ref. Fig. 405/TASK 71-00-00-991-914)


 (r) TORQUE the hose coupling to between 85 and 100 lbf.in (0.96 and


 1.13 m.daN).
 (s) Connect the thrust reverser harness connector 4100KSA and 4100KSB to electrical junction box. Tighten the connector fingertight plus one-eighth turn with soft nose pliers . (Ref. Fig. 405/TASK 71-00-00-991-914)
 
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