(2)
Pressurize the reservoirs of the hydraulic systems.
(Ref. TASK 29-14-00-614-002).
(3)
Make an entry in the technical logbook.
(4)
Remove the warning notice(s).
TASK 49-11-00-350-002
Repair of the Turbine Plenum Insulation Blanket (GTCP 36-300)
WARNING : DO NOT TOUCH THE APU UNTIL IT IS SUFFICIENTLY COOL TO PREVENT BURNS
_______ WHEN YOU DO THE MAINTENANCE TASK(S).
WARNING : LOCK THE MECHANISM OF THE ACCESS DOOR 316AR WITH THE PIP PIN WHEN YOU
_______ OPEN THE ACCESS DOOR. THIS WILL PREVENT INJURY.
CAUTION : MAKE SURE THAT YOU HAVE THE CORRECT FIRE FIGHTING EQUIPMENT
_______ AVAILABLE. THE APU FIRE EXTINGUISHING SYSTEM IS NOT SUFFICIENT TO EXTINGUISH A FIRE IF THE ACCESS DOORS 315AL AND 316AR ARE OPEN/ REMOVED. KEEP OPERATION OF THE APU TO A MINIMUM WHEN THE ACCESS DOORS ARE OPEN/REMOVED.
CAUTION : MAKE SURE THAT THE FUEL-FEED SYSTEM DOES NOT HAVE ANY LEAKS. LEAKS IN
_______ THE FUEL-FEED SYSTEM CAN CAUSE A FIRE.
1. Reason for the Job
__________________
A.
A number of incidences of rubber surge duct separations have occured which
in some cases has resulted in damage to the turbine-plenum
insulation-blankets.
B.
The rubber duct separations direct the high velocity load-control
discharge-air over the external surge-duct portion of the turbine plenum. In
some cases this results in localized damage to the insulation blanket. With
the APU inlet temperature above 125 deg.F (51.66 deg.C) the exposed skin
temperature may exceed a 450 deg.F (232.22 deg.C) specification limit
established during aircraft certification.
C.
This repair authorizes the modification of the existing damaged plenum
blanket P/N 3846330-10 to allow the incorporation of the P/N 3846643-1
repair blanket. In addition, this repair provides instructions for the
replacement of the plenum surge blanket P/N 3846330-2 as necessary.
2. Job Set-up Information
______________________
Not Applicable
3.
Job Set-up
4.
Procedure
_________
5.
Close-up
__________ ________
Subtask 49-11-00-865-075
A. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s):
-------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------121VU APU/APU/CTL 2KD L42 121VU APU/ECB/SPLY 1KD L41
POWER PLANT ((131-9(A))) - REPAIRS
__________________________________ TASK 49-11-00-400-005 Installation of the APU Substitution Kit (131-9(A)) WARNING : ISOLATE THE ELECTRICAL CIRCUITS FROM THE RELATED EQUIPMENT AND THE
_______ ENVIRONMENT.
WARNING : DO NOT TOUCH THE APU UNTIL IT IS SUFFICIENTLY COOL TO PREVENT BURNS
_______ WHEN YOU DO THE MAINTENANCE TASK(S).
1.
Reason for the Job
__________________
Self Explanatory
2.
Job Set-up Information
______________________
A. Fixtures, Tools, Test and Support Equipment
-------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
No specific blanking caps No specific blanking plug
B. Consumable Materials
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
Material No. 06-001A USA MIL-L-23398 SOLID FILM LUBRICANT AIR DRYING (Ref. 20-31-00)
Material No. 19-010 USA AMS 5687 LOCKWIRE STAINLESS STEEL ANNEALED 0.8MM DIA (Ref. 20-31-00)
R EFF : 001-049, 101-105, 107-107, 151-199, 49-11-00Page 801 201-210, Config-2 Aug 01/05
CES
C. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
24-42-00-861-001 Energize the Ground Service Network from the External Power 24-42-00-862-001 De-energize the Ground Service Network Supplied from the External Power 29-00-00-864-001 Put the Related Hydraulic System in the Depressurized Configuration before Maintenance Action 29-14-00-614-002 Pressurization of the Hydraulic Reservoirs through
中國航空網(wǎng) m.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：A320飛機維護手冊 AMM 機載輔助動力 AIRBORNE AUXILIARY POWER2(5)
