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时间:2011-02-24 09:55来源:蓝天飞行翻译 作者:admin
曝光台 注意防骗 网曝天猫店富美金盛家居专营店坑蒙拐骗欺诈消费者

____ do the operational test of the pack temperature control system:
 -the air outlet flap has full and free movement.
 -no damage to the aircraft structure or to the air outlet flap can occur.
 (1)
 Disconnect the electrical connector (2).

 (2)
 Put blanking caps on the disconnected electrical connectors.

 (3)
 Hold the air outlet flap (1) and the actuator (3) and remove the nut (7), the bolt (4) and the bush (5).

 (4)
 Let the air outlet flap move to the fully open position and make sure that:

 (a)
 The air outlet flap is not cracked or damaged.

 (b)
 When you move the air outlet flap it does not cause damage to the aircraft structure or to itself.

 

 (5)
 If the air outlet flap is cracked or damaged you must:

 (a)
 Remove the air outlet flap (Ref. TASK 21-61-52-000-002).

 (b)
 To the aircraft structure temporarily attach:

 -
the disconnected actuator (3) and,

 -
the disconnected electrical connector (2).
 NOTE : The work steps which follow are not necessary if the air

 

 

 

____
 outlet flap has been removed.

 (6)
 Put the lever (6) in position on the actuator (3) and install the bush (5), the bolt (4) and the nut (7).

 (7)
 Remove the blanking caps and connect the electrical connector (2).


R 1EFF : 001-003, 051-054, 1 21-61-00Page 417 1 1 May 01/05 1 1 1CES 1 Subtask 21-61-00-865-061


 D. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s):
 -------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------FOR 9HH
 122VU AIR COND/PACK TEMP/CTL SYS1/1/115VAC 1HH X22 122VU AIR COND/PACK TEMP/CTL SYS1/1/28VDC 3HH X21 122VU AIR COND/PACK TEMP CTL SYS2/1/28VDC 4HH Y19 122VU AIR COND/PACK TEMP CTL SYS2/1/115VAC 2HH Y18
 FOR 29HH 122VU AIR COND/PACK TEMP/CTL SYS1/2/115VAC 21HH W22 122VU AIR COND/PACK TEMP/CTL SYS1/2/28VDC 23HH W21 122VU AIR COND/PACK TEMP CTL SYS2/2/28VDC 24HH Y21 122VU AIR COND/PACK TEMP CTL SYS2/2/115VAC 22HH Y20
 Subtask 21-61-00-040-051
 E. Deactivation of the Air Outlet Flap
 NOTE : The work steps which follow are not necessary if the air outlet
____
 flap has been removed.

 NOTE : For the following procedure 2 persons, each with an
____ intercommunication set, are necessary. One person in the cockpit to control the movement of the related air outlet flap. One person at the related air outlet flap to monitor its movement.
 (1) Do the operational test of the pack temperature-control system (Ref. TASK 21-61-00-710-001)
 NOTE : During the test the person at the air outlet flap must monitor
____ its movement. He must inform the person in the cockpit when the air-outlet flap gap is 40 mm (1.5748 in.) or more (dimension A) (Ref. Fig. 403/TASK 21-61-00-991-008) The person in the cockpit must then open these circuit breakers:-
FOR 9HH
 1HH, 2HH.

 FOR 29HH
R 1EFF : 001-003, 051-054, 1 21-61-00Page 418 1 1 May 01/05 1 1 1CES 1 21HH, 22HH


 This should stop the air outlet flap at the necessary open position.
 (2) If the air outlet flap does not move during the test you must:
 -remove the air outlet flap (Ref. TASK 21-61-52-000-002).
 -temporarily secure the air-outlet flap actuator and the disconnected electrical connector to the aircraft structure.
 -retain the removed components and the air outlet flap.
 NOTE : These must remain with the aircraft until you do the
____
 reactivation of the air outlet flap.

 Subtask 21-61-00-865-062
 F. Make sure that this(these) circuit breaker(s) is(are) open, safetied and tagged
 -------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------FOR 9HH
 122VU AIR COND/PACK TEMP/CTL SYS1/1/115VAC 1HH X22 122VU AIR COND/PACK TEMP CTL SYS2/1/115VAC 2HH Y18
 FOR 29HH 122VU AIR COND/PACK TEMP/CTL SYS1/2/115VAC 21HH W22 122VU AIR COND/PACK TEMP CTL SYS2/2/115VAC 22HH Y20
 Subtask 21-61-00-020-053
 G. Electrical Connector Disconnection
 (Ref. Fig. 402/TASK 21-61-00-991-002)

 (1)
 Disconnect the electrical connector (2).

 (2)
 Put blanking caps on the disconnected electrical connectors.

 (3)
 Temporarily attach the disconnected electrical connector (2) to the aircraft structure.
 
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