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时间:2011-03-27 17:13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

R -------------------------------------------------------------------------------
R REMOVE | FROM | NOTE
R | |
R Bolt (80) | Bracket (70) | On flange S, at the 10:15 o'clock position
R | | (Detail C)
R | |
R Clamp (90) | |
R Bolt (120) | Bracket (110) | On flange S, at the 8:30 o'clock position
R | | (Detail E)
R | |
R Clamp (130) | |
R Nuts (30) | Flange S | At the 9:15 o'clock position
R | | (Detail B)
R | |
R Bolts (50) | |
R (6) Remove the main junction box (20) from the engine.
R (7) Install the blanking plugs and caps on the connectors and R receptacles. R
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R R  Main Junction Box Figure 403/TASK 77-21-10-991-305- 13 (SHEET 1)
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R R  Main Junction Box Figure 403/TASK 77-21-10-991-305- 23 (SHEET 2)
 F EEFF : E E ECES  ALL  『E 77-21-10EEE Page 427 Aug 01/04

 


R R  Main Junction Box Figure 403/TASK 77-21-10-991-305- 33 (SHEET 3)
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 TASK 77-21-10-400-025


R Installation of the Main Junction Box
 1. Reason for the Job
__________________
 Self Explanatory
 2. Job Set-up Information
______________________
 A. Fixtures, Tools, Test and Support Equipment
 -------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
R No specific warning notice No specific Torque Wrench : range 36.00 to 220.00 lbf.in
 (0.40 to 2.60 m.daN)
 B. Consumable Materials
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
Material No. CP2101 USA MIL-T-5544
 graphite grease (Ref. 70-30-00)
 Material No. CP8001 *
 lockwire 0.032 in (0.8 mm) dia (Ref. 70-30-00)
 Material No. CP8002 *
 lockwire 0.032 in (0.8 mm) dia (Ref. 70-30-00)

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 C. Referenced Information

 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
R  31-60-00-860-001 EIS Start Procedure
R  31-60-00-860-002 EIS Stop Procedure 71-13-00-010-040 Opening of the Fan Cowl Doors 71-13-00-410-040 Closing of the Fan Cowl Doors 73-29-00-710-040 Operational Test of the FADEC on the Ground (with
 Engine Non motoring)
 78-30-00-081-041 Make the Thrust Reverser Serviceable after
 Maintenance
 78-30-00-481-041 Make the Thrust Reverser Unserviceable for

 Maintenance
 78-36-00-010-040 Opening of the Thrust Reverser Doors
 78-36-00-410-040 Closing of the Thrust Reverser Doors

R  77-21-10-991-305 Fig. 403
 3. Job Set-up
__________
 Subtask 77-21-10-860-059
 A. Aircraft Maintenance Configuration
 (1) On the center pedestal, on the ENG panel 115VU, make sure that a warning notice is in position to tell persons not to start the engine.

 (2) On the overhead maintenance panel 50VU, make sure that the ON legend of the ENG/FADEC GND PWR/1(2) pushbutton switch is off. Make sure that a warning notice is in position to tell persons not to energize the FADEC 1(2).


 Subtask 77-21-10-010-085
 B. Get Access
 (1) Make sure that the fan cowl doors are open: (Ref. TASK 71-13-00-010-040) FOR 1000EM1 437AL, 438AR FOR 1000EM2 447AL, 448AR
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 (2) Make sure that the thrust reverser doors are open: (Ref. TASK 78-36-00-010-040) FOR 1000EM1 451AL, 452AR FOR 1000EM2 461AL, 462AR

 Subtask 77-21-10-040-069
 C. Make sure that the thrust reverser is unserviceable (Ref. TASK 78-30-00-481-041).
 4. Procedure
_________
R (Ref. Fig. 403/TASK 77-21-10-991-305)
 Subtask 77-21-10-420-059
 
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