A320飞机维护手册 AMM PNEUMATIC 气源 2(126)

 TASK 36-22-16-000-007

 Removal of the Cables 25HF(41HF),52HF(68HF)
 WARNING : PUT THE SAFETY DEVICES AND THE WARNING NOTICES IN POSITION BEFORE YOU_______ START A TASK ON OR NEAR: - THE FLIGHT CONTROLS - THE FLIGHT CONTROL SURFACES - THE LANDING GEAR AND THE RELATED DOORS - COMPONENTS THAT MOVE.
 WARNING : MAKE SURE THAT THE GROUND SAFETY-LOCKS ARE IN POSITION ON THE LANDING_______ GEAR.
 1. Reason for the Job__________________ 
R R  Self Explanatory
 2. Job Set-up Information______________________
 A. Fixtures, Tools, Test and Support Equipment
 -------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
No specific No specific No specific No specific No specific 98D27803000000  blanking capscircuit breaker(s) safety clip(s)safety barrierswarning noticeaccess platform 3.6 m (11 ft. 10 in.)1 LOCKING TOOL - FLAP/SLAT CONTROL LEVER
 B. Referenced Information
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
R R  27-80-00-866-004 36-22-16-991-001 36-22-16-991-002 36-22-16-991-004 36-22-16-991-005  Extending the Slats on the GroundFig. 401Fig. 402 Fig. 404 Fig. 405

 3. Job Set-up
__________

 (Ref. Fig. 401/TASK 36-22-16-991-001, 402/TASK 36-22-16-991-002) Subtask 36-22-16-941-056
 A. Safety Precautions
 (1)
 Put the safety barriers in position.

 (2)
 Put a warning notice in position in the cockpit to tell persons not to operate the slat controls.

 Subtask 36-22-16-860-063
 B. Aircraft Maintenance Configuration
 (1)
 Extend the slats fully (Ref. TASK 27-80-00-866-004).

 (2)
 Install the LOCKING TOOL - FLAP/SLAT CONTROL LEVER (98D27803000000) on the flap/slat control lever on panel 114VU.

 Subtask 36-22-16-865-074
 C. Open, safety and tag this(these) circuit breaker(s):
 -------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------49VU FLIGHT CONTROLS/SLT/CTL AND MONG/SYS1 5CV B06 49VU AIR BLEED/ENG 1/CTL 3HA1 D12 49VU AIR BLEED/ENG 1/MONG 2HA1 D11
 121VU FLIGHT CONTROLS/SLT/CTL/SYS2 7CV R21 122VU AIR BLEED/ENG 2/CTL 3HA2 Z23 122VU AIR BLEED/ENG 2/MONG 2HA2 Z22
 1EFF : ALL 1 36-22-16Page 441 1 1 May 01/05R 1 1 1CES 1

 Subtask 36-22-16-010-056

 D. Get Access
 (1)
 Put the access platform in position below the applicable access panel.

 (2)
 Remove the applicable access panels:

 -
FOR 25HF, 52HF
 remove 522EB, 522FB

 -
FOR 41HF, 68HF
 remove 622EB, 622FB.

 4. Procedure
_________ R (Ref. Fig. 404/TASK 36-22-16-991-004, 405/TASK 36-22-16-991-005) Subtask 36-22-16-020-056
 A. Removal of the Cables CAUTION : MAKE MATCH MARKS ON ALL THE ELECTRICAL WIRES BEFORE YOU
_______ DISCONNECT THEM. INCORRECT CONNECTION OF WIRES WILL CAUSE DAMAGE TO EQUIPMENT.
 (1)
 Remove the bolts (35) and the clamps (33) from the applicable cable

 (15) or (16).

 (2)
 Remove the applicable cable (15) or (16) from the electrical raceway.

 (3)
 Cut the electrical cable (15) or (16) at the in-line splice connector.

 (a)
 For the cable 25HF:

 -at the connector 4013VS in route 1S.

 (b)
 For the cable 41HF:

 -at the connector 4012VS in route 1S.

 (c)
 For the cable 52HF:

 -at the connector 4021VS in route 2S.

 (d)
 For the cable 68HF:

 -at the connector 4020VS in route 2S.

 (4)
 Remove and discard the lockwire from the connectors (19), (23) and

 (24) and the nut (20).

 (5)
 For the cables 25HF(41HF):

 -disconnect the connector (24) from the connector (22).

 (6)
 For the cables 52HF(68HF):

 -disconnect the connector (19) from the connector (23)
 -
remove the nut (20) from the connector (23)

 -
remove the connector (23) from the flanged attachment (21).

 (7)
 Remove the applicable cable assembly (15) or (16).

 (8)
 Put blanking caps on the disconnected connectors.