(9)
Close the access doors of the air conditioning units 191BB, 192FB.
1EFF : ALL 1 36-11-00Page 557 1 1 Feb 01/05R 1 1 1CES 1
Subtask 36-11-00-410-060
B. Close Access
(1)
In the AFT cargo compartment, install the sidewall panels 151CW, 151DW, 151EW, 151HW, 151JW, 161AW, 161BW and 161CW.
(2)
Close the AFT cargo-compartment door 825 (Ref. TASK 52-30-00-860-002) and the access door 312AR.
(3)
Close the left thrust-reverser cowl door (Ref. TASK 78-36-00-410-040):
FOR 1000EM1
451AL.
FOR 1000EM2
461AL.
(4) Close the left fan cowl door (Ref. TASK 71-13-00-410-040):
FOR 1000EM1
437AL.
FOR 1000EM2
447AL.
(5)
Close the access doors under the leading edge of the wing and belly fairings:
(a)
For the left wing and belly fairing: 521AB, 521CB, 521EB, 521BT 191BT, 197BB.
(b)
For the right wing and belly fairing: 621AB, 621CB, 621EB, 621BT, 192BT.
(6)
Close the access doors on the pylon:
FOR 1000EM1
413DL, 414FR.
FOR 1000EM2
423DL, 423FL.
(7)
Remove the warning notice(s).
(8)
Remove the access platform(s).
1EFF : ALL 1 36-11-00Page 558 1 1 Feb 01/05R 1 1 1CES 1
Subtask 36-11-00-862-072
C. De-energize the aircraft electrical circuits (Ref. TASK 24-41-00-862-002).
1EFF : ALL 1 36-11-00Page 559 1 1 Feb 01/05R 1 1 1CES 1
TASK 36-11-00-720-007
Functional Test of the Sense Lines Upstream of the Bleed Pressure Regulator Valve (4001HA) and Connected to the Control Solenoid (10HA1,10HA2)
1. Reason for the Job
__________________
To make sure that there are no leaks on the sense lines:
-upstream of the bleed pressure regulator valve and connected to the control solenoid (no pressure change).
2. Job Set-up Information
______________________
A. Fixtures, Tools, Test and Support Equipment
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
No specific blanking plug
No specific crow foot wrench
No specific warning notice(s)
No specific access platform 1.6 m (5 ft. 3 in.)
98D36003000000 1 TEST SET - ENGINE BLEED SYSTEM
98F36003002000 1 TEST SET - ENGINE BLEED SYSTEM
B. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
71-13-00-010-040 Opening of the Fan Cowl Doors
71-13-00-410-040 Closing of the Fan Cowl Doors
78-36-00-010-040 Opening of the Thrust Reverser Doors
78-36-00-410-040 Closing of the Thrust Reverser Doors
36-11-00-991-026 Fig. 503
**ON A/C 001-049, 051-099, 101-149, 201-299, 301-399,
36-11-00-991-023 Fig. 504
R **ON A/C 151-199, 401-499,
36-11-00-991-023-A Fig. 504A **ON A/C ALL
3. Job Set-up
__________
Subtask 36-11-00-941-088
A. Safety Precautions
(1)
On the ENG panel 115VU:
-put warning notice(s) to tell persons not to start the engine 1(2).
(2)
On the HP ground connector:
-put warning notice(s) to tell persons not to pressurize the pneumatic system.
Subtask 36-11-00-860-060
B. Aircraft Maintenance Configuration
(1)
Make sure that the engine 1(2) shutdown occurred not less than 5 minutes before you do this procedure.
(2)
On the ENG section of the maintenance panel 50VU:
-make sure that the ON legend of the FADEC GND PWR/1 (2) pushbutton switch is off,
-put warning notice(s) to tell persons not to operate the FADEC 1(2).
(3)
On the AIR COND panel 30VU:
-
make sure that the ENG 1(2) BLEED pushbutton switch is pushed (OFF legend is off).
-
make sure that the APU BLEED pushbutton switch is released (the ON legend is off),
-put warning notice(s) to tell persons not to operate the pneumatic system.
Subtask 36-11-00-010-070
C. Get Access
(1) Open the fan cowl doors (Ref. TASK 71-13-00-010-040):
FOR 1000EM1
437AL, 438AR
中國航空網 www.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：A320飛機維護手冊 AMM PNEUMATIC 氣源 1(65)
