- SFCC-2 (22CV)
- FPPU-SLAT (28CV)
- aircraft wiring
2. Job Set-up Information
______________________
A. Fixtures, Tools, Test and Support Equipment
-------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
No specific ARINC Connector Breakout Box
B. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION
-------------------------------------------------------------------------------
AMM 27-51-34-000-001 Removal of the SFCC (21CV,22CV)
AMM 27-51-34-400-001 Installation of the SFCC (21CV,22CV)
AMM 27-81-00-740-002 Bite Test of the Slat and Flap Control Computers
(Slat System) AMM 27-81-19-000-001 Removal of the Feed Back Position Pick-Off Unit AMM 27-81-19-400-001 Installation of the Feed Back Position Pick-Off Unit ASM 27-81/06 ASM 27-81/07
「一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一1 EFF : ALL ∞∞27-81-00∞∞∞∞∞∞∞∞∞∞Page 217
Feb 01/03 CES
3. Fault Confirmation
__________________
A. Test
(1) Do a BITE test on the SFCC 1 (2) (Ref. AMM TASK 27-81-00-740-002).
(a) If the message SLT FPPU 28CV OR WIRING TO SFCC is shown, do the fault isolation.
4. Fault Isolation
_______________
A. Procedure
(1) Interchange the two SFCCs (Ref. AMM TASK 27-51-34-000-001) (Ref. AMM TASK 27-51-34-400-001).
(2) Do the test in Para. 3 A.
(3) If the fault moves with the SFCC:
(a) Replace the applicable SFCC-1 (21CV) or SFCC-2 (22CV).
(4) If the fault does not move with the SFCC:
(a) replace the FPPU-SLAT (28CV), (Ref. AMM TASK 27-81-19-000-001) R and (Ref. AMM TASK 27-81-19-400-001).
(5) If the fault continues:
(a) Use an ARINC Connector Breakout Box and do a check of the aircraft wiring, (Ref. ASM 27-81/06) and (Ref. ASM 27-81/07).
(b) Do the repair.
(c) Do the test in Para. 3. A.
5. Close-up
________
A. Remove the ground support and maintenance equipment, the special and standard tools and all other items.
B. Put the aircraft back to its initial configuration.
「一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一1 EFF : ALL ∞∞27-81-00∞∞∞∞∞∞∞∞∞∞Page 218
Nov 01/00 CES
R Loss of SLAT LH/RH APPU or Wiring/interface to SFCC1 (2).
WARNING : PUT THE SAFETY DEVICES AND THE WARNING NOTICES IN POSITION BEFORE YOU
_______
START A TASK ON OR NEAR:
- THE FLIGHT CONTROLS
- THE FLIGHT CONTROL SURFACES
- THE LANDING GEAR AND THE RELATED DOORS
- COMPONENTS THAT MOVE.
WARNING : MAKE SURE THAT THE TRAVEL RANGES OF THE FLIGHT CONTROL SURFACES ARE
_______
CLEAR BEFORE YOU PRESSURIZE/DEPRESSURIZE A HYDRAULIC SYSTEM.
WARNING : MAKE SURE THAT THE GROUND SAFETY-LOCKS ARE IN POSITION ON THE LANDING
_______
GEAR.
1. Possible Causes
_______________
- SFCC-1 (21CV)
- SFCC-2 (22CV)
- APPU-L SLAT (31CV)
- APPU-R SLAT (32CV)
- aircraft wiring
2. Job Set-up Information
______________________
A. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION
-------------------------------------------------------------------------------
AMM 27-51-34-000-001 Removal of the SFCC (21CV,22CV)
AMM 27-51-34-400-001 Installation of the SFCC (21CV,22CV)
AMM 27-81-00-740-002 Bite Test of the Slat and Flap Control Computers
(Slat System) AMM 27-81-18-000-001 Removal of the Asymmetry-Position Pick-Off Unit 31CV (32CV) AMM 27-81-18-400-001 Installation of the Asymmetry-Position Pick-Off Unit 31CV (32CV) ASM 27-81/06
3. Fault Confirmation
__________________
A. Test.
(1) Do a BITE test with the applicable SFCC (Ref. AMM TASK 27-81-00-740-002).
(2) If a message that includes the APPU 31CV (32CV) or the SFCC is shown on the MCDU, do the fault isolation procedure.
「一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一1 EFF : ALL ∞∞27-81-00∞∞∞∞∞∞∞∞∞∞Page 219
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本文链接地址：A320 Trouble Shooting Manual 排故手册 飞行操纵 2(61)
