-
the cabin pressure is value A (Pamb + 300 mbar (4.35 psi)).
On the vertical speed indicator:
-
the cabin vertical speed must not be
more than 500 ft.min (152.39 m.min). On the pressure indicator:
-
the cabin pressure increases to value B (Pamb + 550 mbar (7.97 psi)).
On the vertical speed indicator:
-
the cabin vertical speed is 0. On the pressure indicator:
-
the cabin pressure is value B (Pamb + 550 mbar (7.97 psi)).
Record possible leaks.
1EFF : ALL 1 05-53-00Page 523 1 1 Feb 01/00R 1 1 1CES 1
-------------------------------------------------------------------------------ACTION RESULT -------------------------------------------------------------------------------NOTE : The cabin vertical speed
____
must not be more than 500
ft.min (152.39 m.min).
On the vertical speed indicator:
-
the cabin vertical speed must not be
more than 500 ft.min (152.39 m.min). On the pressure indicator:
-
the cabin pressure indication decreases to the external ambient pressure.
8. Wait until the cabin is fully
depressurized then fully open the
outflow valve.
5. Close-up
________
Subtask 05-53-00-865-063
A. Remove the safety clip(s) and the tag(s) and close 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 05-53-00-860-056
B. Put the aircraft back to its initial configuration.
(1)
Shut down the APU (Ref. TASK 12-33-21-618-001) or stop the HP ground-air supply unit (Ref. TASK 12-33-21-618-001).
(2)
On the EXT LT section of the panel 25VU:
-set the BEACON switch to OFF position.
(3)
remove the pressure indicator and the vertical speed indicator.
(4)
remove the safety plug from the pressure switch 16WR.
(a) In the avionics compartment:
-
Remove the safety streamer from the safety plug.
-
Remove the safety plug with its O-ring from the air inlet of the pressure switch 16WR.
(5)
If you removed the crew oxygen masks, install them (Ref. TASK 35-12-41-400-002)
(6)
Put the system and the aircraft back to the serviceable configuration.
(7)
Do the EIS stop procedure (Ref. TASK 31-60-00-860-002).
(8)
De-energize the aircraft electrical circuits (Ref. TASK 24-41-00-862-002).
(9)
Remove the warning notices and the safety barriers.
1EFF : ALL 1 05-53-00Page 525 1 1 Aug 01/03R 1 1 1CES 1
TASK 05-53-00-780-002- 01
Test for Leakage in the Repair Area at a Differential Pressure of 550 mbar (7.97 psi) (with AIDS)
R R WARNING : MAKE SURE THAT:_______ - ONLY THE PERSONS NECESSARY FOR THE PRESSURIZATION TEST ARE IN THE AIRCRAFT DURING THE TEST. - THE PERSONS IN THE AIRCRAFT HAVE MEDICAL APPROVAL TO DO THIS TYPE OF TEST (REFER TO YOUR LOCAL REGULATION). BE CAREFUL WHEN YOU CONTROL THE PRESSURE. SUDDEN CHANGES IN PRESSURE CAN CAUSE PAIN AND INJURY.
WARNING : THERE MUST BE TWO PERSONS IN THE COCKPIT DURING THE PRESSURIZATION_______ TEST. IF A CHANGE IN PRESSURE HAS AN UNWANTED EFFECT (PAIN, NOISE IN THE EARS , HEADHACHE, OR OTHER) ON ONE PERSON, THE OTHER PERSON CAN ADJUST THE PRESSURE TO AVOID INJURY.
WARNING : DO NOT OPEN OR GO NEAR PRESSURE-SEALED DOORS WHEN THE AIRCRAFT IS_______ PRESSURIZED. A PRESSURE-SEALED DOOR THAT OPENS WHEN THE AIRCRAFT IS PRESSURIZED. - WILL CAUSE EXPLOSIVE DECOMPRESSION. - CAN KILL OR CAUSE INJURY TO PERSONS AND/OR CAUSE DAMAGE TO THE AIRCRAFT/EQUIPMENT.
WARNING : DO NOT OPEN THE DOORS WHILE THE RED WARNING LIGHT FLASHES. IF THE RED_______ WARNING LIGHT FLASHES, REMAINING PRESSURE COULD CAUSE THE DOOR TO OPEN SUDDENLY AND COULD : - KILL OR CAUSE SERIOUS INJURY TO PERSONS - CAUSE DAMAGE TO THE AIRCRAFT.
1. Reason for the Job__________________
To find possible leaks in the repair area after large structural repairs.
R R NOTE : The pressure test that follows is only necessary after the repair if____ the repair procedure in the SRM or in the repair instruction directly tells you to do it.
2. Job Set-up Information 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 时间限制/维护检查 2(151)
