(b)
Hold the jumper lead in position on the dummy connector with a backshell E0080-01-14C.
(c)
Paint the dummy connector red with STRUCTURE PAINTS (Material No. 16-018) to make sure that it is easily identified.
(4)
Connect the dummy connector to the connector 7527VC.
(5)
Put a warning notice in position in the cockpit to tell the flight crew that the air intake flap is deactivated in the open position.
(6)
Make an entry in the logbook to show that the air intake flap is deactivated in the open position and add the time which the MMEL 49-10-02 permits for the operation in this condition.
5. Close-up
________ Subtask 49-16-00-410-052-A
A. Close Access
(1)
Put the catwalk panel in position on the service frame and secure with the fasteners.
(2)
Make sure that the work area is clean and clear of tool(s) and other items.
(3)
Close the maintenance door 314AR.
(4)
Remove the access platform(s). Subtask 49-16-00-865-055
B.
Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): 1KD, 2KD.
TASK 49-16-00-440-001
Reactivation of the APU Air Intake Flap (GTCP 36-300)
1. Reason for the Job
__________________
Refer to the MMEL TASK: 49-10-02
Power Plant - Air Intake Flap
2. Job Set-up Information
______________________
A. Fixtures, Tools, Test and Support Equipment
-------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
No specific circuit breaker(s) safety clip(s) No specific access platform 3.0 m (9 ft. 10 in.)
B. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
49-16-00-210-001 Detailed Inspection of the Air Intake, Diffuser Elbow, Seals and Felt Metal (GTCP 36-300) 49-16-00-991-008 Fig. 401
3. Job Set-up
__________ Subtask 49-16-00-865-056
A. Open, safety and tag this(these) circuit breaker(s):
-------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------121VU APU/APU/CTL 2KD L42 121VU APU/ECB/SPLY 1KD L41
Subtask 49-16-00-860-057
B. Get Access
(1)
Put the access platform below the maintenance door 314AR.
(2)
Open the maintenance door 314AR.
(3)
Release the fasteners of the catwalk panel and remove it from the service frame.
4. Procedure
_________
(Ref. Fig. 401/TASK 49-16-00-991-008) Subtask 49-16-00-440-052
A. Connection of the Electrical Connectors
(1)
Disconnect the dummy connector from the electrical connector 7527VC.
(2)
Remove and discard the cable-tie which holds the electrical connector 7527VC-A to the service frame.
(3)
Remove the blanking cap from the electrical connector 7527VC-A.
(4)
Make sure that the electrical connectors are clean and in the correct condition.
(5)
Connect the electrical connector 7527VC-A to the connector 7527VC. Subtask 49-16-00-865-057
B.
Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s):
-------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------121VU APU/APU/CTL 2KD L42 121VU APU/ECB/SPLY 1KD L41
中国航空网 www.aero.cn
航空翻译 www.aviation.cn
本文链接地址:A320飞机维护手册 AMM 机载辅助动力 AIRBORNE AUXILIARY POWER2(133)