1EFF : ALL 1 52-71-00Page 546 1 1 May 01/05 1 1 1CES 1 D. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
24-41-00-861-002 Energize the Aircraft Electrical Circuits from the
External Power
24-41-00-862-002 De-energize the Aircraft Electrical Circuits Supplied
from the External Power
31-60-00-860-001 EIS Start Procedure
31-60-00-860-002 EIS Stop Procedure
52-10-00-010-001 Opening of the Passenger/Crew Door
52-10-00-410-001 Closing of the Passenger/Crew Door
52-10-00-860-001 Special Precautions before Work on the Passenger/Crew
Door
52-10-00-860-002 Special Precautions after Work on the Passenger/Crew
Door
52-71-00-991-005 Fig. 506
FOR FIN 4WN1
25-23-46-000-001 Removal of the Door Linings at the FWD Passenger/Crew
Doors
25-23-46-400-001 Installation of the Door Linings at the FWD
Passenger/Crew Doors
FOR FIN 4WN2
25-23-46-000-001 Removal of the Door Linings at the FWD Passenger/Crew
Doors
25-23-46-400-001 Installation of the Door Linings at the FWD
Passenger/Crew Doors
FOR FIN 7WN1
25-23-46-000-002 Removal of the Door Linings at the AFT Passenger/Crew
Doors
25-23-46-400-002 Installation of the Door Linings at the AFT
Passenger/Crew Doors
FOR FIN 7WN2
25-23-46-000-002 Removal of the Door Linings at the AFT Passenger/Crew
Doors
25-23-46-400-002 Installation of the Door Linings at the AFT
Passenger/Crew Doors
FOR FIN 13WV1
25-23-46-000-001 Removal of the Door Linings at the FWD Passenger/Crew
Doors
25-23-46-400-001 Installation of the Door Linings at the FWD
Passenger/Crew Doors
FOR FIN 13WV2
25-23-46-000-001 Removal of the Door Linings at the FWD Passenger/Crew
Doors
1EFF : ALL 1 52-71-00Page 547 1 1 May 01/04R 1 1 1CES 1
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
25-23-46-400-001 Installation of the Door Linings at the FWD
Passenger/Crew Doors FOR FIN 17WV1 25-23-46-000-002 Removal of the Door Linings at the AFT Passenger/Crew
Doors 25-23-46-400-002 Installation of the Door Linings at the AFT
Passenger/Crew Doors FOR FIN 17WV2 25-23-46-000-002 Removal of the Door Linings at the AFT Passenger/Crew
Doors 25-23-46-400-002 Installation of the Door Linings at the AFT
Passenger/Crew Doors FOR FIN 13WV1, 13WV2, 17WV1, 17WV2 52-71-00-710-001 Operational Test of the Door Warning System FOR FIN 4WN1, 4WN2, 7WN1, 7WN2 52-73-00-710-001 Operational Test of the Emergency Escape Slide
Release System of the Passenger/Crew Doors
3. Job Set-up
__________
Subtask 52-71-00-861-052
A. Energize the aircraft electrical circuits (Ref. TASK 24-41-00-861-002)
Subtask 52-71-00-010-070
B. Get Access
WARNING : DO NOT OPEN THE PASSENGER/CREW DOOR IF THE WIND SPEED IS MORE
_______
THAN 65 KNOTS.
WARNING : BEFORE YOU START WORK ON THE DOOR, MAKE SURE THAT:
_______
-
THE EMERGENCY CONTROL HANDLE IS IN THE DISARMED POSITION WITH THE SAFETY PIN INSTALLED.
-
THE PERCUSSION LEVER OF THE DOOR-DAMPER AND EMERGENCY-OPERATION CYLINDER IS IN THE DISARMED POSITION WITH THE SAFETY PIN INSTALLED.
WARNING : STOP THE OPENING PROCEDURE IF THE RED WARNING LIGHT FLASHES.
_______ RESIDUAL PRESSURE COULD CAUSE THE DOOR TO OPEN WITH A SUDDEN FORCE AND INJURE PERSONS AND/OR DAMAGE THE AIRCRAFT.
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