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).
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