Pack-Assembly - Preparation for Installation Figure 403/TASK 25-62-44-991-003- 13 (SHEET 1) 
R  EFF :  ALL  25-62-44 Page 440 Feb 01/02
 CES 

 Pack-Assembly - Preparation for Installation Figure 403/TASK 25-62-44-991-003- 23 (SHEET 2) 
R  EFF :  ALL  25-62-44 Page 441 Feb 01/02
 CES 

 Pack-Assembly - Preparation for Installation Figure 403/TASK 25-62-44-991-003- 33 (SHEET 3) 
R  EFF :  ALL  25-62-44 Page 442 Feb 01/02
 CES 

 (d)
 Pull open the burr-strips (Velcro) (54), (55) and (56).

 (e)
 Connect the quick-release connector (23).

 (f)
 Install the electrical harness (22) as shown:

 -
See DETAIL C for the right door.

 -
See DETAIL E for the left door.
 NOTE : Refer to the instructions on the soft-cover of the

____ pack-assembly (9). Make sure that the quick-release connector (23) is installed next to the 'STOW PLUG HERE' mark/placard.
 (g) Close the burr-strips (54), (55) and (56).
 (8) Make sure that the two connectors (58) and (61) are connected:
 -Between the cable and loop assembly (57), and the cover release-cable (59).
 -Between the pull-handle cable (62), and the inflation cable (60). R **ON A/C 003-049, 051-099, 101-149, 151-199, 201-299, 301-399, 401-499,
 Subtask 25-62-44-710-055
 B. Operational Test Procedure before Installation
 (Ref. Fig. 404/TASK 25-62-44-991-016)

 (1)
 Do an operational test of the girt bar (10) before it is installed in the girt assembly:

 (a)
 Hold the girt bar (10).

 (b)
 While holding the girt bar (10) pull the trigger lever (37) in the direction shown.

 (c)
 While holding the trigger lever (37) move the telescopic end-fitting (41) in and out of the girt bar (10).

 (d)
 Make sure that the telescopic end-fitting (41) can move freely in the girt bar (10).

 (2)
 Do a visual inspection of the pin (69). Make sure that there is no corrosion.

 EFF : ALL
25-62-44Page 443

 Girt Bar - Operational Test and Pin Inspection Figure 404/TASK 25-62-44-991-016 
R  EFF : 003-049, 051-099, 101-149, 151-199, 201-299, 301-399, 401-499,  25-62-44 Page 444 Aug 01/05
 CES 

 **ON A/C 001-002,
 Subtask 25-62-44-420-062
R C. Installation of the Escape-Slide Pack-Assembly (Ref. Fig. 402/TASK 25-62-44-991-021)
 WARNING : MAKE SURE THAT THERE IS A GOOD FLOW OF AIR THROUGH THE WORK
_______ AREA WHEN YOU USE SPECIAL MATERIALS. IF YOU GET ONE OF THESE MATERIALS ON YOUR SKIN, IN YOUR MOUTH OR IN YOUR EYES : -FLUSH IT AWAY WITH A FLOW OF CLEAN WATER FOR BETWEEN 10 AND 15 MINUTES. -GET IMMEDIATE MEDICAL AID IF IRRITATION OCCURS. DO NOT BREATHE THE FUMES FROM THE MATERIAL. DO NOT SMOKE WHEN YOU USE THE MATERIAL. DO NOT USE THE MATERIAL NEAR A FLAME, SPARKS OR SOURCES OF HEAT. THESE MATERIALS ARE DANGEROUS : THEY ARE POISONOUS, FLAMMABLE AND SKIN IRRITANTS.
 (1) Install The girt bar (10) in the girt assembly (11):
 CAUTION : DO NOT PULL THE GIRT ASSEMBLY. IF YOU DO, YOU WILL OPEN THE
_______
 PACK ASSEMBLY.

 (a)
 If the girt assembly (11) is in an unlaced condition, refer to the FIGURE for the girt bar (10) installation sequence. (Ref. Fig. 405/TASK 25-62-44-991-019)

 (b)
 If the girt assembly (11) is in a laced-up condition, install the girt bar (10) as follows:

 1 Carefully push the girt bar (10) through the girt assembly
_
 (11).

 2 Make sure that the visual indicator (30) points inboard, and
_ is on the side of the girt assembly (11) that points in the flight direction.
 3 Put the loop of the mooring line (32) on the end of the girt
_
 bar (10).

 4 Make sure that the loop is on the left side of the girt bar
_
 (10) when you look outboard.

R  Installation Procedure of the Girt Bar Figure 405/TASK 25-62-44-991-019- 12 (SHEET 1)
 EFF :  001-002,  25-62-44 Page 446 May 01/04
 CES 

R  Installation Procedure of the Girt Bar Figure 405/TASK 25-62-44-991-019- 22 (SHEET 2)
 EFF :  001-002,  25-62-44 Page 447 May 01/04
 CES 

 5 If you cannot push the girt bar (10) through the girt assembly
_
 (11), do these steps:
　
中國(guó)航空網(wǎng) m.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：A320飛機(jī)維護(hù)手冊(cè) AMM EQUIPMENT/FURNISHINGS 設(shè)備4(119)