Air Intake System Measurements Figure 501/TASK 49-16-00-991-005-A
R  EFF : 001-049, 101-105, 107-107, 151-199, 49-16-00Page 505 201-210, Config-2 Aug 01/05
 CES

 AIR INTAKE SYSTEM ((APS 3200)) - ADJUSTMENT/TEST
________________________________________________ TASK 49-16-00-710-002 Operational Test of the Air Intake Flap and Diverter (APS 3200)
 1.
 Reason for the Job

__________________
 Refer to the MPD TASK: 491600-A2

 2.
 Job Set-up Information

______________________
 A. Fixtures, Tools, Test and Support Equipment
 -------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
No specific circuit breaker(s) safety clip(s) No specific access platform 3.5 m (11 ft. 6 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 31-60-00-860-001 EIS Start Procedure 49-16-43-400-002 Installation of the Air Intake Flap (APS 3200) 49-16-00-991-003 Fig. 501
 3. Job Set-up
__________ Subtask 49-16-00-860-056
 A. Aircraft Maintenance Configuration
 (1)
 Energize the aircraft electrical circuits
 (Ref. TASK 24-41-00-861-002).

 (2)
 Do the EIS start procedure (Upper ECAM DU and lower ECAM DU only) (Ref. TASK 31-60-00-860-001).

 Subtask 49-16-00-865-062
 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 49-16-00-865-063
 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 49-16-00-010-056
 D. Get Access
 (1) Put the access platform below the APU Air Intake.

 4. Procedure
_________
 (Ref. Fig. 501/TASK 49-16-00-991-003) Subtask 49-16-00-710-051
 A. Operational Test of the Air Intake Flap and Diverter NOTE : For adjustment of the air-intake flap (Ref. TASK 49-16-43-400-
____
 002).

 -------------------------------------------------------------------------------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 flexible seal compressed lightly with a maximum of 0.5 mm (0.0196 in.).

 Air Intake System - Measurements
 Figure 501/TASK 49-16-00-991-003
　
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(jī)維護(hù)手冊 AMM 機(jī)載輔助動力 AIRBORNE AUXILIARY POWER2(141)