R -------------------------------------------------------------------------------R REFERENCE DESIGNATION R -------------------------------------------------------------------------------
R 24-42-00-861-001 R R 25-62-47-000-002 R 25-62-47-400-001 R 25-62-49-000-001 R 25-62-49-400-001 R 52-22-00-010-001 R R 52-22-00-410-001 R R 52-22-00-614-002 R R R 52-22-00-860-002 R R 52-22-00-860-004 R R 25-62-00-991-011
R 3. Job Set-up
__________
R Subtask 25-62-00-860-058 Energize the Ground Service Network from the External Power Escape-Slide - Removal after Inflation Escape-Slide Enclosure - Installation Inflation Reservoir, Escape-Slide - Removal Inflation Reservoir, Escape-Slide - Installation Opening of the Emergency Exit Doors from the Passenger Compartment Closing of the Emergency Exit Doors from the Passenger Compartment Charging of the Door Damper and Emergency Operation Cylinders (1600WM, 1601WM, 1602WM, 1603WM) at the Emergency Exit Doors Diaphragm Replacement at the Door Damper and Emergency Operation Cylinder Special Precaution after Maintenance on the Door Damper and Emergency Operation Cylinder Fig. 504
R A. Aircraft Maintenance Configuration
R (Ref. Fig. 504/TASK 25-62-00-991-011)
R NOTE : We recommend that you do the operational test in a maintenance
____ R hanger.
R (1) Make sure that the ground service network is energized (Ref. TASK 24-R 42-00-861-001).
R (2) Open the applicable emergency exit door (referred to as door) from R the passenger compartment (Ref. TASK 52-22-00-010-001).
R (3) Fuselage protection procedure:
R CAUTION : MAKE SURE THAT THE PROTECTION IS IN POSITION ON THE
_______ R FUSELAGE BELOW THE DOOR SILL. R DEPLOYMENT OF THE ESCAPE-SLIDE CAN CAUSE DAMAGE TO THIS R AREA.
EFF : 301-399, 25-62-00Page 518 May 01/04
CES
INTENTIONALLY BLANK
R R Escape-Slide Deployment - Preparation Figure 504/TASK 25-62-00-991-011- 12 (SHEET 1)
EFF : 301-399, 25-62-00 Page 520 May 01/04
CES
R R Escape-Slide Deployment - Preparation Figure 504/TASK 25-62-00-991-011- 22 (SHEET 2)
EFF : 301-399, 25-62-00 Page 521 May 01/04
CES
(a)
Do not use bubble wrap as protection for the aircraft fuselage. NOTE : The protection is a laminate of fiberglass-reinforced
____ polyester SPECIAL MATERIALS (Material No. 05-109), which has a minimum thickness of 1.2 mm (0.06 in.). It is thin, impact resistant and applies the load equally to prevent damage to the fuselage.
(b)
Put an ACCESS PLATFORM 5M (16 FT)- ADJUSTABLE in position to help you attach the protection.
(c)
Attach the protection in position: CAUTION : MAKE SURE THAT THE PROTECTION IS CORRECLTY ATTACHED
_______
WITH TAPE TO THE AIRCRAFT STRUCTURE.
THIS PREVENTS THE SUCTION OF LOOSE MATERIAL INTO THE
ASPIRATOR DURING DEPLOYMENT.
LOOSE MATERIAL CAN CAUSE DAMAGE TO THE ASPIRATOR.
1_ Refer to the FIGURE for the dimensions and position of the
protection.
2_ Use tacky tape SPECIAL MATERIALS (Material No. 05-069) and
attach the protection on to the surface of the fuselage below
the door sill.
(4) Ground safety procedure:
WARNING : PUT SAFETY BARRIERS IN POSITION TO KEEP THE TRAVEL RANGE OF
_______ THE ESCAPE-SLIDE CLEAR. IF YOU DO NOT, INJURY TO PERSONNEL AND/OR DAMAGE TO EQUIPMENT CAN OCCUR.
(a)
Below the applicable door, make sure that an area with approximately 12.0 m (39.37 ft.) radius is clear of all miscellaneous equipment.
(b)
Put the safety barriers in position.
(c)
Put plastic sheet in position where the escape-slide hits the ground.
(d)
Put WARNING NOTICE in position to tell persons not to go into the area behind the safety barrier.
EFF : 301-399, 25-62-00Page 522
Aug 01/04
R
CES
(5)
Push the release button (5), and pull the door with the assist handle
(4)
until you can get access to the door-damper and emergency-operation cylinder:
中國航空網 www.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：A320飛機維護手冊 AMM EQUIPMENT/FURNISHINGS 設備4(75)
