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时间:2011-03-26 09:12来源:蓝天飞行翻译 作者:admin
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

_______ WORK ON THE PNEUMATIC SYSTEM.
 WARNING : BE CAREFUL WHEN YOU WORK ON THE ENGINE COMPONENTS IMMEDIATELY AFTER
_______ THE ENGINE IS SHUTDOWN. THE ENGINE COMPONENTS CAN STAY HOT FOR UP TO ONE HOUR.
 1. Reason for the Job
__________________
 Self Explanatory
 2. Job Set-up Information
______________________
 A. Fixtures, Tools, Test and Support Equipment
 -------------------------------------------------------------------------------REFERENCE QTY DESIGNATION
 -------------------------------------------------------------------------------
No specific blanking plugs
 No specific circuit breaker(s) safety clip(s)
 No specific warning notice
 No specific access platform 0.5 m (1 ft. 8 in.)

 B. Referenced Information
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
24-41-00-861-002 Energize the Aircraft Electrical Circuits from the
 External Power 71-13-00-010-040 Opening of the Fan Cowl Doors 78-30-00-481-041 Make the Thrust Reverser Unserviceable for
 Maintenance 78-36-00-010-040 Opening of the Thrust Reverser Doors 36-11-49-991-302 Fig. 403
 1EFF : ALL 1 36-11-49Page 423 1 1 May 01/00R 1 1 1CES 1


 3. Job Set-up
__________
 Subtask 36-11-49-861-065
 A. Energize the aircraft electrical circuits
 (Ref. TASK 24-41-00-861-002).

 Subtask 36-11-49-941-054
 B. Safety Precautions
 (1)
 Make sure that the engine 1(2) shutdown occurred not less than 5 minutes before you do this procedure.

 (2)
 On the AIR COND panel 30VU:


 -make sure that the ENG 1(2) BLEED pushbutton switch is released
 (the OFF legend is on), R - make sure that the APU BLEED pushbutton switch is released (the ON R legend is off),
 -put a warning notice to tell persons not to operate the pneumatic system.
 (3)
 On the ENG panel 115VU:

 -put a warning notice to tell persons not to start the engine 1(2).

 (4)
 On the HP ground connector:

 -Put a warning notice to tell persons not to pressurize the pneumatic system.

 (5)
 On the ENG section of the maintenance panel 50VU:


 -make sure that the ON legend of the ENG/FADEC GND PWR 1(2) pushbutton switch is off,
 -put a warning notice to tell persons not to energize the FADEC 1(2).
 Subtask 36-11-49-865-056
 C. Open, safety and tag this(these) circuit breaker(s):
 -------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------49VU AIR BLEED/ENG 1/CTL 3HA1 D12 49VU AIR BLEED/ENG 1/MONG 2HA1 D11 122VU AIR BLEED/ENG 2/CTL 3HA2 Z23 122VU AIR BLEED/ENG 2/MONG 2HA2 Z22


 Subtask 36-11-49-010-052
 D. Get Access
 (1)
 Open the fan cowl doors (Ref. TASK 71-13-00-010-040):
 FOR 1000EM1
 437AL, 438AR
 FOR 1000EM2
 447AL, 448AR


 (2)
 Put the access platform in position in zone 450 for engine 1 and in zone 460 for engine 2.


 Subtask 36-11-49-040-059
 E. Make the thrust reverser unserviceable (Ref. TASK 78-30-00-481-041). Subtask 36-11-49-010-095
 F. Open the thrust reverser cowl doors (Ref. TASK 78-36-00-010-040):
 FOR 1000EM1
 451AL, 452AR
 FOR 1000EM2
 461AL, 462AR

 4. Procedure
_________
 (Ref. Fig. 403/TASK 36-11-49-991-302) Subtask 36-11-49-020-052
 A. Removal of the High Pressure (HP) Tee Duct
 (1)
 Remove the coupling (10) and the E-seal (5) that connect the HP tee duct (15) to the upper HP duct.

 (2)
 Remove the coupling (10) and the E-seal (5) that connect the HP tee duct (15) to the lower HP duct.

 (3)
 Remove the coupling (30) and the E-seal (25) that connect the HP tee duct (15) to the HP bleed valve (20).

 (4)
 Remove the HP tee duct (15) from the engine.

 (5)
 Put blanking plugs on the open ends of the HP tee duct (15).


 1EFF : ALL 1 36-11-49Page 425 1 1 May 01/00R 1 1 1CES 1


 High Pressure (HP) Tee Duct Figure 403/TASK 36-11-49-991-302
 1EFF : 1 1R 1CES  ALL  1 11 1 36-11-49 Page 426 May 01/00

 

 (6) Put blanking plugs on the upper HP duct, the lower HP duct, and the HP bleed valve (20).
 1EFF : ALL 1 36-11-49Page 427 1 1 May 01/00R 1 1 1CES 1
 
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