R (Ref. Fig. 401/TASK 36-22-16-991-001, 402/TASK 36-22-16-991-002, 403/TASK R 36-22-16-991-003, 404/TASK 36-22-16-991-004, 405/TASK 36-22-16-991-005)
 Subtask 36-22-16-941-053
 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. R
 Subtask 36-22-16-860-060
 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 36-22-16-865-053

 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
 Subtask 36-22-16-010-053
 D. Get Access 
R  (1) Put the access platform in position in the zone 522(622). 
R R  (2) Remove the applicable access panels (Ref. TASK 57-41-37-000-003), (Ref. TASK 57-41-37-000-004), (Ref. TASK 57-41-37-000-006): - FOR 26HF, 53HF remove 522AT, 522AB, 522CB, 522EB, 522FB
 - FOR 42HF, 69HF remove 622AT, 622AB, 622CB, 622EB, 622FB.
 4. Procedure_________ 
R
 Subtask 36-22-16-020-053
 A. Removal of the Overheat Sensing Elements 26HF(42HF) and 53HF(69HF) 
R R  CAUTION : REMOVE OR INSTALL THE SENSING ELEMENTS CAREFULLY. DO NOT TWIST,_______ BEND OR CAUSE KINKS IN THE SENSING ELEMENTS.
 (1) Release the quick-release fasteners (27) and open the clamps (25). Retain the protective sleeves (26).
 (2) At the pylon outboard closing-rib: 
R R R  WARNING : WEAR GOGGLES WHEN YOU REMOVE OR INSTALL THE LOCKWIRE. CUT,_______ REMOVE AND DISCARD THE LOCKWIRE AS YOU DO THE TASK. LOOSE LOCKWIRE CAN CUT OR BLIND YOU.

 (a) Remove and discard the lockwire from the connectors (19) and (22) and the nuts (20).
 (b) Disconnect the connector (19) from the connector (22).
 (c) Remove the nut (20) from the connector (22) and remove the connector (22) from the flanged attachment (21).
 (3) At the outboard telescope-rib: 
R R R  WARNING : WEAR GOGGLES WHEN YOU REMOVE OR INSTALL THE LOCKWIRE. CUT,_______ REMOVE AND DISCARD THE LOCKWIRE AS YOU DO THE TASK. LOOSE LOCKWIRE CAN CUT OR BLIND YOU.
 (a) Remove and discard the lockwire from the connectors (19), (22) and (24) and the nut (20).
 (b) Disconnect the connectors (19) and (24) from the connectors (22) and (23).
 (c) Remove the nut (20) from the connectors (22) and (23).
 (d) Remove the connectors (22) and (23) from the flanged attachment (21).
 (4) Put blanking caps on the disconnected connectors (19), (22), (23) and (24).
 (5) Remove the applicable overheat sensing element (14) or (17), and retain the applicable grommets (37).

 TASK 36-22-16-400-004

 Installation of the Overheat Sensing Elements 26HF(42HF),53HF(69HF)
 WARNING : MAKE SURE THAT THE FLIGHT CONTROL SAFETY-LOCKS AND THE WARNING
_______
 NOTICES ARE IN POSITION.

 WARNING : MAKE SURE THAT THE GROUND SAFETY-LOCKS ARE IN POSITION ON THE LANDING
_______
 GEAR.

 1. Reason for the Job
__________________
 Self Explanatory
 2. Job Set-up Information
______________________
 A. Fixtures, Tools, Test and Support Equipment
 -------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
No specific safety barriers
 No specific warning notice
 No specific access platform 2.8 m (9 ft. 2 in.)

R No specific Torque Wrench : range 0.00 to 1.20 m.daN R (0.00 to 9.00 lbf.ft) 98D27803000000 1 LOCKING TOOL - FLAP/SLAT CONTROL LEVER
 B. Consumable Materials
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
Material No. 11-026 GB DEF-STAN 68-148/1
　
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 PNEUMATIC 氣源 2(129)