D. Referenced Information

 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
05-57-00-200-001  Aircraft Stability
 20-28-00-912-002  Electrical Bonding of Components With Conductive
 Bolts and Screws in the Tanks
 20-28-00-912-003  Electrical Bonding of Electrical Connectors
 20-28-00-912-004  Electrical Bonding of Components With Conductive
 Bolts and Screws and Bonding Straps in the Fuselage
 and in the Wings (this does not include the tanks)-
26-21-41-400-001  Installation of the Engine Fire-Extinguisher Bottle
 (6WE1,8WE1,6WE2,8WE2)
 28-00-00-910-001  Fuel Safety Procedures
 29-00-00-910-002  Safety Procedures of the Hydraulic System
 29-10-00-864-001  Depressurize the Green Hydraulic System
 29-10-00-864-002  Depressurize the Yellow Hydraulic System
 29-10-00-864-003  Depressurize the Blue Hydraulic System
 29-14-00-614-001  Depressurization of the Hydraulic Reservoirs
 54-54-00-400-001  Installation of the Aft Fixed Fairing
 54-55-00-400-001  Installation of the Aft Movable Fairing
 54-56-00-400-001  Installation of the Lower Fairing
 71-00-00-400-040  Installation of the Power Plant
 78-32-11-400-040  Installation of the Left or Right Half Door of Thrust
 Reverser
 54-50-00-991-001  Fig. 401
 54-50-00-991-005  Fig. 402
 54-50-00-991-006  Fig. 403
 54-50-00-991-012  Fig. 404
 54-50-00-991-013  Fig. 405
 54-50-00-991-014  Fig. 406
 54-50-00-991-015  Fig. 407
 54-50-00-991-020  Fig. 408
 54-50-00-991-019  Fig. 409
 FOR FIN 1000EM2
 71-13-11-400-040  Installation of the Fan Cowl Doors

 1EFF : ALL 1 54-50-00Page 426 1 1 Nov 01/03R 1 1 1CES 1

 3. Job Set-up__________
 Subtask 54-50-00-941-056
 A. Safety Precautions
 (1) Make sure that the engine (1) and (2) shutdown occurred not less than 5 minutes before you do this procedure. 
R R  (2) Make sure that a warning notice in position is in the cockpit to tell persons not to start engine.
 (3) Make sure that the ON legend of the ENG/FADEC GND PWR/1(2) pushbutton switch is off, and put a warning notice to tell persons not to use it.
 (4) Make sure that the APU BLEED pushbutton switch is released (on legend OFF) and install a warning notice to tell persons not to use it. 
R R  (5) Make sure that the fuel safety procedure instructions are obeyed (Ref. TASK 28-00-00-910-001).
 (6) Make sure that the hydraulic safety procedure instructions are obeyed (Ref. TASK 29-00-00-910-002). 
R  (7) Make sure that an access platform is in position at zone 811.
 (8) Make sure that hydraulic systems are depressurized (Ref. TASK 29-10-00-864-001) (Ref. TASK 29-10-00-864-002) (Ref. TASK 29-10-00-864-003)
 (9) Make sure that the hydraulic reservoirs are depressurized (Ref. TASK 29-14-00-614-001).
 (10) Make sure that the aircraft is stable (Ref. TASK 05-57-00-200-001).

 Subtask 54-50-00-865-051

 B. Make sure that this(these) circuit breaker(s) is(are) open, safetied and tagged
 -------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------49VU ENGINE/2/HP FUEL SOV 1KC2 A02 49VU ENGINE/1/HP FUEL SOV 1KC1 A01 49VU ANTI ICE/PROBES/AOA/1 4DA1 D04 49VU ANTI ICE/PROBES/PHC/1 2DA1 D03 49VU ANTI ICE/PROBES/PITOT/1 3DA1 D02 121VU HYDRAULIC/HYD POWER/Y 3803GX N30 122VU ANTI ICE/ENG/2 1DN2 W10 122VU ANTI ICE/PROBES/PHC/3 2DA3 Y16 122VU ANTI ICE/PROBES/2/TAT 1DA2 Y15 122VU ANTI ICE/PROBES/2/PITOT 3DA2 Y14 122VU ANTI ICE/PROBES/2/AOA 4DA2 Y13 122VU ANTI ICE/PROBES/2/PHC 2DA2 Y12 122VU ANTI ICE/PROBES/2/STATIC 5DA2 Y11 122VU ANTI ICE/PROBES/3/PITOT 3DA3 Z16 122VU ANTI ICE/PROBES/3/AOA 4DA3 Z15 122VU ANTI ICE/PROBES/1/STATIC 5DA1 Z13 122VU ANTI ICE/PROBES/1/TAT 1DA1 Z12 123VU Y HYD/ELEC/PUMP 3802GX AB06 123VU Y HYD/ELEC/ELEC PUMP/NORM 3801GX AB03
 4. Procedure
_________
R NOTE : This procedure is applicable to the left pylon. Data between
____ R parentheses are for the right pylon.
 Subtask 54-50-00-480-051
 A. Installation of the Tool
 (1)
 Put a crane in position with the characteristics that follow:

 -height 5 m (16.40 ft.),
 -capacity 1000 daN (2248.0890 lbf).
　
中國航空網(wǎng) www.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：A320飛機維護手冊 AMM NACELLES/PYLONS(13)