(i)
 Install the overheat sensing element 19HF (Ref. TASK 36-22-17-400-001).

 (j)
 Install the sleeve (2), the sleeve (11) and the lock sleeve (12).

 (6)
 Connect the hydraulic hoses 1102GM, 1103GM 3102GM and 3103GM: (Ref. Fig. 404/TASK 53-58-11-991-016)

 (a)
 Remove the blanking plugs from the hoses.

 (b)
 Connect the hoses (Ref. TASK 20-21-12-911-001) and paint a red telltale mark on the connections.

 (c)
 Remove any hydraulic fluid leakage (Ref. TASK 51-78-00-615-002).

 (7)
 Remove the blanking caps and connect the electrical equipment: (Ref. Fig. 401/TASK 53-58-11-991-008, 402/TASK 53-58-11-991-009)

 (a)
 Put the electrical harnesses 6533VN/DC1 and 4643VB/3P in position between FR78 and FR79 and install and tighten the clamps.

 (b)
 Install the electrical connector 7138VC/3E and safety the connector with corrosion-resistant steel lockwire 0.6 mm (0.0236 in.) dia.

 (c)
 Put the electrical harness 4210VB/3E in position and install and tighten the clamps.

 (d)
 Connect the electrical connectors 7120VC-A/1M and 7118VC-A/1S.

 (e)
 Connect the electrical connectors 7116VC and 11LJ.

 (f)
 Connect the electrical wiring to the switch 8QC.

 (g)
 Connect the electrical connectors 11WF-A and 12WF-A.

 (h)
 Install the electrical harnesses 6528VN/DC2, 6760VN/B1 and 6761VN/DC1.

 (i)
 Install and tighten the clamps on the electrical harnesses 4213VB/1M and 4207VB/1M.

 (j)
 Install the electrical harness 7519VP.

 (k)
 Connect the electrical cable 6750VN/DC1.

 (l)
 Connect the electrical connector 21WG-A and 22WG-A.

 (m)
 Connect the electrical cable 6757VN/DC1.

 (n)
 Install the electrical harness 4622VB/3G and connect it to the terminal block 7508VT.

 (o)
 Install and tighten the clamps on the electrical harness
 4622VB/3G between FR77 and FR79.

 (p) Install and tighten the clamps on the electrical harnesses
 4631VB/1M and 4622VB/3G.
 (q) Connect the connector 7527VC to the APU air-intake actuator.
 (r) Install and tighten the clamps on the electrical harness
 4631VB/1M.
 (8) Apply STORAGE PRESERVATION (Material No. 15-007) to the inside of the
 tail cone (Ref. TASK 51-75-13-916-002). 
R  **ON A/C 301-399, 
R  Subtask 53-58-11-420-052-C 
R  B. Installation 
R  (1) Install the Tail Cone: 
R  (Ref. Fig. 407/TASK 53-58-11-991-013, 408/TASK 53-58-11-991-014) 
R  (a) Put the crane in position. 
R  (b) Attach the SLING - R/I TAILCONE to the crane. 
R  (c) Attach the sling to the hoisting lugs on the tail cone. 
R  (d) Lift the tail cone into position. 
R  (e) Make sure that the tail cone bearing (67) aligns with the 
R  fuselage spigot (66). 
R  (f) Remove the installation adaptors (77) from the EXTRACTOR - ATTACH 
R  BOLTS, TAIL CONE (98A53407566005) kit and install the adaptors on 
R  the attach bolts (70). 
R  NOTE : The tool kit with the partnumber 98A53407566005 supersedes____ 
R  the tool kit with the partnumber 98A53407566002. If only 
R  the tool kit with the partnumber 98A53407566002 is 
R  available, then it is recommended to continue to use this 
R  tool kit. 
R  (g) Apply the COMMON GREASE (Material No. 04-004) to the attach bolts 
R  (70). 
R  (h) Install the attach bolts (70) in the upper attach fittings. 

 CES

R  (i) Remove the installation adaptors from the upper attach bolts (70) 
R  and install the nuts (72). 
R  (j) Install the attach bolts (70) in the lower attach fittings. 
R  (k) Remove the installation adaptors from the lower attach bolts (70) 
R  and install the nuts (72). 
R  (l) TORQUE the nuts (72) to between 0.57 and 0.79 m.daN (50.44 and 
R  69.91 lbf.in). 
R  (m) Safety the nuts (72) with the new cotter pins (73). 
R  (n) Apply the STORAGE PRESERVATION (Material No. 15-007) to the 
R  threads of the bolts. (Ref. TASK 51-75-13-916-002) 
R  (o) Protective treatment. 
　
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 FUSELAGE 機身3(149)