「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 ∞∞27-51-00∞∞∞∞∞∞∞∞∞∞Page 221
Feb 01/03R CES
3. Fault Confirmation
__________________
A. SFCC system test.
(1) Do a BITE test on the SFCC 1 (2) (Ref. AMM TASK 27-51-00-740-002).
(2) If the fault data "APPU disconnected or faulty and WTB set" is displayed, page block 301 Table 7 gives the SFCC test menu selection details.
(3) Do the fault isolation.
4. Fault Isolation
_______________
A. Procedure.
(1) Swop the SFCC 1 with the SFCC 2.
(a) Wait 60 seconds and examine the UPPER ECAM and the SD FLT/CTL page for the fault warnings and status data.
(b) Access the FLP ON GROUND FAULTS and do a check for faults.
(2) If the fault moves with the SFCC, replace the applicable SFCC-1 (21CV) SFCC-2 (22CV) (Ref. AMM TASK 27-51-34-000-001) (Ref. AMM TASK 27-51-34-400-001).
(3) If the fault does not move to the other SFCC.
(a) Replace the applicable APPU-L(R) FLAP 29CV (30CV) (Ref. AMM TASK 27-51-18-000-001) (Ref. AMM TASK 27-51-18-400-001).
(b) Access the FLP ON GROUND FAULTS and do a check for faults.
(4) If the fault stays.
(a) Use an ARINC Connector Breakout Box and do a check of the A/C Wiring between the SFCC 1 (2) and the APPU connectors 29CV-A (30CV-B) (Ref. ASM 27-51/06) (Ref. ASM 27-51/07).
(b) Do the repair.
(5) Do the SYSTEM TEST (BITE) (Ref. para 3.A.(1)).
(6) If the BITE test shows NO FAULTS.
(7) Do a check of the UPPER ECAM and the SD FLT/CLT page for the fault warning and status data.
(8) If the fault warning and status data fields are clear.
「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 ∞∞27-51-00∞∞∞∞∞∞∞∞∞∞Page 222
Feb 01/03R CES
(9) Do the operational test of the flap system (Ref. AMM TASK 27-54-00-710-001).
(10) Access the FLP ON GROUND FAULTS and make sure there are no faults shown.
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 ∞∞27-51-00∞∞∞∞∞∞∞∞∞∞Page 223
Feb 01/03R
CES Flap System Jam.
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.
1. Possible Causes
_______________
- POWER CONTROL UNIT (6201CM)
- BRAKE-L WING TIP (33CV)
- BRAKE-R WING TIP (34CV)
- Transmission Assembly
- Rotary Actuators
- PCU hydraulic motor
2. Job Set-up Information
______________________
A. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
AMM 27-50-00-866-010 Reset of the Torque Limiters of the Flap System on
the Ground
AMM 27-51-51-000-001 Removal of the Flap Wing-Tip Brake
AMM 27-51-51-400-001 Installation of the Flap Wing-Tip Brake
AMM 27-54-00-200-001 Detailed Visual Inspection of the Transmission
Assembly (Including Part of the Transmission in Zone
140) AMM 27-54-00-710-001 Operational Test of the Flap System AMM 27-54-49-000-001 Removal of the Flap Track 1 Actuator 6205CM(6255CM) AMM 27-54-49-400-001 Installation of the Flap Track 1 Actuator
6205CM(6255CM) AMM 27-54-51-000-001 Removal of the Power Control Unit 6201CM of the Flap System AMM 27-54-51-400-001 Installation of the Power Control Unit 6201CM of the Flap System
中國航空網 m.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：A320 Trouble Shooting Manual 排故手冊 飛行操縱 1(90)
