(3)
Install the connector (22) in the flanged attachment (21). Install the nut (20) on the connector (22).
(4)
TORQUE the nut (20) to between 0.56 and 0.68 m.daN (49.55 and 60.17 lbf.in).
(5)
Install the connector (19) on the connector (22).
(6)
TORQUE the connector (19) to between 0.56 and 0.68 m.daN (49.55 and
60.17 lbf.in). R WARNING : WEAR GOGGLES WHEN YOU REMOVE OR INSTALL THE LOCKWIRE. CUT,
_______ R REMOVE AND DISCARD THE LOCKWIRE AS YOU DO THE TASK. LOOSE R LOCKWIRE CAN CUT OR BLIND YOU.
(7)
Safety the connectors (19) and (22) and the nut (20) with MISCELLANEOUS (Material No. 19-010).
(8)
Install the support-plugs (29) on the overheat sensing elements (11) and (12) and install the support-plugs in the RIB7 and the RIB8.
(9)
Put the cable-ties (30) in the support-plugs (29) and install the retainers (28).
(10)
Install a protective sleeve (26) at each clamp (25) and the fairlead (34).
(11)
Tighten the clamps (25) and lock the quick-release fasteners (27).
(12)
Install the removable part of the fairlead (34) with the bolt (33) and the nut (35).
Subtask 36-22-16-865-069
C. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): 3HA1, 2HA1, 3HA2, 2HA2.
Subtask 36-22-16-710-054
D. Test
(1) Do an operational test of the overheat detection system (Ref. TASK 36-22-00-710-001).
5. Close-up
________
(Ref. Fig. 401/TASK 36-22-16-991-001)
Subtask 36-22-16-410-054
A. Close Access
(1) Make sure that the work area is clean and clear of tool(s) and other items.
R (2) Install the applicable access panels (Ref. TASK 57-41-37-400-003), R (Ref. TASK 57-41-37-400-002):
-
FOR 27HF, 50HF
install 521BT, 522AT, 521HB, 522AB
-
FOR 43HF, 66HF
install 621BT, 622AT, 622HB, 622AB
-
FOR 54HF, 23HF install 521BT, 522AT, 521HB, 522AB, 521EB, 521GB
-
FOR 70HF, 39HF install 621BT, 622AT, 621HB, 621AB, 621EB, 621GB.
Subtask 36-22-16-865-070
B. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): 5CV, 7CV.
Subtask 36-22-16-860-072
C. Aircraft Configuration
(1) Retract the slats fully (Ref. TASK 27-80-00-866-005).
Subtask 36-22-16-942-054
D. Removal of Equipment
(1)
Remove the safety barriers.
(2)
Remove the warning notice(s).
(3)
Remove the access platform(s).
(4)
Remove the ground support and maintenance equipment, the special and
standard tools and all other items.
1EFF : ALL 1 36-22-16Page 470 1 1 May 01/05R 1 1 1CES 1
TASK 36-22-16-000-006
Removal of the Overheat Sensing Elements 28HF(44HF),49HF(65HF),55HF(71HF), 22HF(38HF)
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 blanking caps
No specific circuit breaker(s) safety clip(s)
No specific safety barriers
No specific warning notice
No specific access platform 3 m (9 ft. 10 in.)
98D27803000000 1 LOCKING TOOL - FLAP/SLAT CONTROL LEVER
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本文鏈接地址：A320飛機維護手冊 AMM PNEUMATIC 氣源 2(134)
