2.
Get access to the APU menu page in the SYSTEM REPORT/TEST (Ref. TASK 31-32-00-860-001).
3.
On the MCDU:
-push the line key adjacent to the APU DATA/OIL indication.
4. On the MCDU:
-push the line key adjacent to the RETURN indication.
5. On the MCDU:
-push the line key adjacent to the SYSTEM SELF-TEST indication.
6. On the MCDU:
-push the line key adjacent to the RETURN indication until the CFDS menu comes into view.
7. On the APU section on the panel 25VU:
-push the APU START pushbutton switch.
On the APU section on the panel 25VU:
-
the ON legend in the APU MASTER SWpushbutton switch comes ON.
On the MCDU:
-
the APU menu page comes on.
On the MCDU:
-
the APU DATA/OIL page comes on, withthe indication OIL LEVEL : OK
On the MCDU:
-
the APU menu page comes on.
On the MCDU:
-
the APU SYSTEM SELF-TEST page comeson with the indicationTEST IN PROGRESS and then TEST OK
On the MCDU:
-
the CFDS MENU page comes on.
On the APU section on the panel 25VU:
-
the ON legend in the APU STARTpushbutton switch comes on .
R EFF : 001-049, 101-105, 107-107, 151-199, 49-00-00Page 219 201-210, Config-2 Aug 01/05
CES
-------------------------------------------------------------------------------ACTION RESULT -------------------------------------------------------------------------------NOTE : The ECB (59KD) controls and
____ monitors the APU start.
On the APU page on the lower ECAM DU:
-all indications show that the APU operates in the specified limits during the start sequence (no red and/or amber indications).
At the end of the APU start sequence:
On the panel 25VU:
-
the ON legend in the APU START pushbutton switch goes off.
-
the AVAIL legend in the APU START pushbutton switch comes on.
On the APU page on the lower ECAM DU:
-
the AVAIL message comes on.
-all indications show that the APU operates in the specified limits (no red and/or amber indications).
On the ENGINE/WARNING page on the upper ECAM DU:
-the APU AVAIL message comes on.
NOTE : If necessary, the APU generator can energize the aircraft
____
electrical circuits (Ref. TASK 24-41-00-861-002).
NOTE : If necessary, the APU can supply bleed air for the
____
pre-conditioning (Ref. TASK 12-33-21-618-001).
R EFF : 001-049, 101-105, 107-107, 151-199, 49-00-00Page 220 201-210, Config-2 Aug 01/05
CES
TASK 49-00-00-860-008- 01
APU Start by Batteries (131-9(A))
WARNING : WHILE THE APU OPERATES, DO NOT GO INTO THESE AREAS:
_______
-
THE AREA BEHIND THE APU EXHAUST DUCT: 25m (82ft.) REARWARD OF THE
DUCT, MORE THAN 3m (10ft.) ABOVE THE GROUND, AND THE WIDTH OF THE
HORIZONTAL STABILIZER
-
THE AREA AROUND THE APU AIR-INTAKE: 2m (7ft) AROUND THE INTAKE
-
THE AREA OF THE OIL-COOLER OUTLET.
THERE IS A RISK OF INJURY IF YOU GO INTO THESE AREAS.
CAUTION : DO NOT USE THE APU DURING FLUID DE-ICING OPERATIONS. DE-ICING FLUID
_______ CAN CONTAMINATE THE INSIDE OF THE APU.
CAUTION : DO NOT TRY TO START THE APU A FOURTH TIME UNTIL THE STARTER MOTOR IS
_______ COOL (60 MINUTES MINIMUM). WE RECOMMEND THAT YOU TRY TO START THE APU THREE TIMES, WITH AN INTERVAL OF ONE MINUTE BETWEEN EACH TIME THAT YOU TRY.
CAUTION : DO NOT START THE APU WITH ACCESS DOORS 315AL AND 316AR OPEN/REMOVED.
_______ THE APU FIRE EXTINGUISHER SYSTEM IS NOT SUFFICIENT TO EXTINGUISH A FIRE IF THE ACCESS DOORS 315AL AND 316AR ARE OPEN/REMOVED.
CAUTION : DO NOT TRY TO START THE APU AGAIN DURING A REFUEL/DEFUEL PROCEDURE
_______ AFTER AN AUTOMATIC SHUTDOWN OR FAILED APU START. IF YOU DO, THERE IS A RISK OF INJURY AND/OR DAMAGE.
CAUTION : OBEY THE SAFETY PRECAUTIONS.
_______
1. Reason for the Job
__________________
NOTE : Refer to SIL 00-085 for APU operation in extreme hot weather
____
condition
2. Job Set-up Information
______________________
A. Fixtures, Tools, Test and Support Equipment
-------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
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 机载辅助动力 AIRBORNE AUXILIARY POWER1(103)
