(2)
Make sure that hydraulic systems are depressurized (Ref. TASK 29-00-00-864-001).
(3)
Do the EIS start procedure (Upper ECAM DU and lower ECAM DU only) (Ref. TASK 31-60-00-860-001).
Subtask 49-16-00-865-075
B. Open, safety and tag this(these) circuit breaker(s):
-------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------49VU APU/FUEL/BLOW OFF/PUMP 2QC B14 121VU APU/FUEL/BLOW OFF/CTL 1QC K39 121VU APU/FUEL/LP VALVE/CTL 1QF M40 121VU APU/FUEL/LP VALVE/SPLY 2QF M39 121VU APU/FUEL/PUMP/CTL 3QC M38
Subtask 49-16-00-865-076
C. Make sure that this(these) circuit breaker(s) is(are) closed:
-------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------121VU APU/APU/CTL 2KD L42 121VU APU/ECB/SPLY 1KD L41
Subtask 49-16-00-010-063
D. Get Access
(1)
Put the access platform below the APU access doors 315AL and 316AR.
(2)
Make sure that the APU intake blanking plug is removed.
R EFF : 001-049, 101-105, 107-107, 151-199, 49-16-00Page 502 201-210, Config-2 Aug 01/05
CES
(3) Make sure that the work area is clean and clear of tool(s) and other items.
NOTE : Open the circuit breakers 1KD and 2KD if adjustments are
____
necessary.
4. Procedure
_________ Subtask 49-16-00-710-052-A
A. Operational Test of the Air Intake Flap and Diverter NOTE : For adjustment of the air-intake flap (Ref. TASK 49-16-43-400-
____
003).
-------------------------------------------------------------------------------ACTION RESULT -------------------------------------------------------------------------------
1. On the overhead panel 25VU:
-push the APU MASTER SW pushbutton switch to the ON position.
2. On the ECAM panel:
-push the pushbutton APU.
3. Examine the contour of the air intake flap and the air intake structure.
On the overhead panel 25VU:
-
the ON legend in the APU MASTER SWpushbutton switch comes on.
-
the air intake flap opens.
On the ECAM systems page:
-
the FLAP OPEN indication comes on.
-
the contour should be in line. Themaximum deviation B of the flap is
1.0 mm (0.0393 in.).
NOTE : If the air intake flap is not in line with the structure, remove the
____ rubber cover on the lower part of the flap actuator rod for access. Disconnect the cotter pin, nut and the bolt that attaches the lower part of the actuator rod to the air intake flap. Adjust the actuator rod length to get the correct position.Then connect the actuator rod
to the air intake flap.
4. On the overhead panel 25VU:
-release the APU MASTER SW pushbutton to the off position.
5. Measure the clearance C between the air intake nose and the air intake flap.
On the overhead panel 25VU:
-
the ON legend in the APU MASTER SWpushbutton switch goes off.
-
the air intake flap closes.
-
the clearance C should be between 0.5mm (0.0196 in.) to 1.5 mm (0.0590in.) with the air intake flap
R EFF : 001-049, 101-105, 107-107, 151-199, 49-16-00Page 503 201-210, Config-2 Aug 01/05
CES
-------------------------------------------------------------------------------ACTION RESULT
-------------------------------------------------------------------------------flexible seal compressed lightly with a maximum of 0.5 mm (0.0196 in.).
5. Close-up
________
Subtask 49-16-00-865-077
A. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): 1QC, 2QC, 3QC, 1QF, 2QF.
Subtask 49-16-00-410-065
B. Aircraft Maintenance Configuration
(1)
On the ECAM control panel 11VU put the two brightness control knobs to the OFF position.
(2)
Pressurize the reservoirs of the hydraulic systems.
(Ref. TASK 29-14-00-614-002).
(3)
De-energize the ground service network
(Ref. TASK 24-42-00-862-001)
(4)
Make sure that the work area is clean and clear of tool(s) and other items.
(5)
Remove the ground support and maintenance equipment, the special and standard tools and all other items.
(6)
Remove the access platform(s).
R EFF : 001-049, 101-105, 107-107, 151-199, 49-16-00Page 504 201-210, Config-2 Aug 01/05 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 機載輔助動力 AIRBORNE AUXILIARY POWER2(140)
