-Install the access panel 151CW.
(8)
For the APU bleed-air ducts between the FR49 and FR52:
-Install the access panel 151DW.
(9)
For the APU bleed-air ducts between the FR52 and FR55:
-Install the access panel 151EW.
(10)
For the APU bleed-air ducts between the FR55 and FR58:
-Install the access panel 151HW.
(11)
For the APU bleed-air ducts between FR58 and FR59:
-Install the access panel 151JW.
(12)
For the APU bleed-air ducts between the FR59 and FR62:
-Install the access panel 161AW.
(13)
For the APU bleed-air ducts between the FR62 and FR63:
-Install the access panel 161BW.
(14)
For the APU bleed-air ducts between the FR63 and FR65:
-Install the access panel 161CW.
(15)
For the APU bleed-air ducts between the FR65 and FR70:
-Install the partition panel 161DW (Ref. TASK 25-55-12-400-001).
(16)
Close the AFT cargo compartment door (Ref. TASK 52-30-00-860-002).
(17)
For the APU bleed-air ducts between the FR70 and FR77:
-Close the access door 312AR.
(18)
For the APU bleed-air ducts aft of FR77:
-Close the access door 314AR.
(19)
Remove the access platform from below the rear fuselage.
(20)
Remove the warning notice(s).
1EFF : 301-399, 1 36-12-00Page 527 1 1 Aug 01/05R 1 1 1CES 1
R **ON A/C 001-049, 051-099, 101-105, 151-199, 201-210,
TASK 36-12-00-790-002
Leak Check on APU Bleed Air Ducting (Upstream the APU Bleed Check Valve)
WARNING : MAKE SURE THAT THE GROUND SAFETY-LOCKS ARE IN POSITION ON THE LANDING
_______
GEAR.
1. Reason for the Job
__________________
Refer to the MPD TASK: 361200-02
2. Job Set-up Information
______________________
A. Fixtures, Tools, Test and Support Equipment
-------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
No specific access platform 2.0 m (6 ft. 7 in.)
No specific access platform 3.0 m (9 ft. 10 in.)
B. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
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 25-55-11-000-001 Removal of the AFT Cargo-Compartment Partition FR47 25-55-11-400-001 Installation of the AFT Cargo-Compartment Partition
FR47 25-55-12-000-001 Removal of the AFT Cargo Compartment Partition FR65 25-55-12-400-001 Installation of the AFT Cargo Compartment Partition
FR65
31-60-00-860-001 EIS Start Procedure
31-60-00-860-002 EIS Stop Procedure
36-12-41-000-001 Removal of a Bleed-Air Duct
36-12-41-400-001 Installation of a Bleed-Air Duct
R 49-00-00-860-003 APU Start by External Power (GTCP 36-300)
R 49-00-00-860-004 APU Shutdown by External Power (GTCP 36-300)
R 1EFF : 001-049, 051-099, 101-105, 151-199, 1 36-12-00Page 528 1201-210, 1May 01/05 1 1 1CES 1
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
49-00-00-860-008 APU Start by External Power (131-9(A)) 49-00-00-860-009 APU Shutdown by External Power (131-9(A)) 52-30-00-860-001 Open the FWD or AFT Cargo-Compartment Door with the
Yellow Electric Pump 52-30-00-860-002 Close the FWD or AFT Cargo-Compartment Door with the Yellow Electric Pump 53-35-13-000-002 Removal of the Quick-Release Access Panels from the Belly Fairing Structure 53-35-13-400-002 Installation of the Quick-Release Access Panels on the Belly Fairing Structure 20-26-00-910-002 Installation of Expansion Joints (for corrective action)
R **ON A/C 001-049, 051-099, 101-105, 201-210,
36-12-00-991-001 Fig. 501
**ON A/C 151-199,
36-12-00-991-001-A Fig. 501A
R **ON A/C 001-049, 051-099, 101-105, 151-199, 201-210,
3. Job Set-up
__________
R **ON A/C 001-049, 051-099, 101-105, 201-210,
Subtask 36-12-00-010-053
A. Get Access
(Ref. Fig. 501/TASK 36-12-00-991-001)
(1) Get access to the APU bleed-air ducts between FR47 and FR50. 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 PNEUMATIC 气源 2(67)
