A320飞机维护手册 AMM 时间限制/维护检查 2(152)_航空信息_民用航空_通用航空

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A. Fixtures, Tools, Test and Support Equipment
-------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
R No specific circuit breaker(s) safety clip(s) No specific safety barriers No specific safety plug - ref MS21913-4 No specific safety streamer No specific warning notices No specific O-ring - ref NAS1612-4
B. Consumable Materials
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
No specific leak-detection soap solution
C. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
12-33-21-618-001 Pre-conditioning through the HP Ground Connection 12-33-21-618-001 Pre-conditioning with the APU 23-44-00-700-001 Operational Test of the Service Interphone 24-41-00-861-002 Energize the Aircraft Electrical Circuits from the
External Power 24-41-00-862-002 De-energize the Aircraft Electrical Circuits Supplied from the External Power
R 31-36-00-740-008 Access to the Parameter Call-Up Menus 31-60-00-860-001 EIS Start Procedure 31-60-00-860-002 EIS Stop Procedure 34-10-00-860-002 ADIRS Start Procedure 34-10-00-860-005 ADIRS Stop Procedure 35-12-41-000-002 Removal of the Full-Face/Quick-Donning Oxygen-Mask 35-12-41-400-002 Installation of the Full-Face/Quick-donning
Oxygen-Mask 3. Job Set-up

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Subtask 05-53-00-865-072

A. Open, safety and tag this(these) circuit breaker(s):
-------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------

R **ON A/C 062-099, 106-149, 151-199, 201-299, 301-399, 401-499,
122VU DOORS/PAX/MONG 1MQ T13 **ON A/C ALL
Subtask 05-53-00-860-057
B. Aircraft configuration
(1)
Put the safety barriers and the warning notices in position to keep persons out of the work area.

(2)
Make sure that the static probe covers are not installed.

(3)
Energize the aircraft electrical circuits (Ref. TASK 24-41-00-861-002).

(4)
Make sure that the avionics equipment ventilation operates correctly. NOTE : if during this test, the avionics equipment ventilation stops,

____
you must stop the test.

(5)
In the avionics compartment:

(a)
Put the safety plug - ref MS21913-4 with its O-ring - ref NAS1612-4 on the air inlet of the pressure switch 16WR.

(b)
Put a safety streamer on the safety plug.

(6)
We recommend that you remove the crew oxygen masks (Ref. TASK 35-12-41-000-002)

NOTE : This test requires an absolute pressure higher than the cabin
____ pressures you get during usual aircraft operations.

The crew masks have an aneroid capsule that is usually resistant to the absolute pressures you can get during this test. But, to prevent high stress on the aneroid capsule, we recommend the removal of the crew oxygen masks.
(7)
On the AIR COND panel 30VU:

-make sure that the PACK 1 and PACK 2 pushbutton switches are pushed (the FAULT legends are on).

(8)
On the CABIN PRESS section of the panel 25VU:

-release the MODE SEL pushbutton switch (the MAN legend is on).

(9)
On the EXT LT section of the panel 25VU:

-set the BEACON switch to ON.

(10)
Do the EIS start procedure (Ref. TASK 31-60-00-860-001)

(11)
On the lower ECAM display unit, on the CAB PRESS page:

-make sure that the outflow valve 10HL is in the fully open position.

(12)
On the VENTILATION section of the panel 22VU:

-
release the EXTRACT pushbutton switch (the OVRD legend comes on).

-
release the CAB FANS pushbutton switch (the OFF legend comes on).

(13)
On the CARGO HEAT section of the panel 22VU: