(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 m.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)