B. If the message AIL TEST NOT POSSIBLE and BITE code 3F3F for ELAC1 and/or ELAC2 are shown on the MCDU:
- replace the SSTU-ROLL CTL, CAPT (4CE1) and SSTU-ROLL CTL, F/O (4CE2) (Ref. AMM TASK 27-92-41-000-002) (Ref. AMM TASK 27-92-41-400-002).
C. Do the test given in para. 3.
「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 ∞∞27-10-00∞∞∞∞∞∞∞∞∞∞Page 278
May 01/04 CES
R MCDU Procedure of the Aileron Damping Test Figure 201/TASK 27-10-00-991-001
「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 ∞∞27-10-00∞∞∞∞∞∞∞∞∞∞Page 279
May 01/04 CES
R Decoding Table of the Aileron Damping Test Not Possible Figure 202/TASK 27-10-00-991-002
「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 ∞∞27-10-00∞∞∞∞∞∞∞∞∞∞Page 280
May 01/04 CES Roll Jerk
1. Possible Causes
_______________
- ELAC-1 (2CE1)
- SERVO CTL-R AILERON, INBD G (33CE2)
- SERVO CTL-L AILERON, OUTBD B (33CE3)
- wiring SOL VLV signal from SERVO CTL-R AILERON, INBD G and SERVO CTL-L AILERON, OUTBD B to the ELAC1
- wiring POS XDCR signal from SERVO CTL-R AILERON, INBD G and SERVO CTL-L AILERON, OUTBD B to the ELAC1
2. Job Set-up Information
______________________
A. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
AMM 27-14-51-000-001 Removal of the Aileron Servo Control
AMM 27-14-51-400-001 Installation of the Aileron Servo Control
AMM 27-93-34-000-001 Removal of the ELAC (2CE1,2CE2)
AMM 27-93-34-400-001 Installation of the ELAC (2CE1,2CE2)
ASM 27-93/02
3. Fault Confirmation
__________________
A. Test
Not applicable, you cannot confirm this fault on ground.
4. Fault Isolation
_______________
A. If the fault symptom is identified by the crew observation F/CTL - Roll Jerk
(1) Replace the ELAC-1 (2CE1) (Ref. AMM TASK 27-93-34-000-001) and (Ref. AMM TASK 27-93-34-400-001).
(2) Replace SERVO CTL-R AILERON, INBD G (33CE2) and SERVO CTL-L AILERON, OUTBD B (33CE3), (Ref. AMM TASK 27-14-51-000-001) and (Ref. AMM TASK 27-14-51-400-001).
(3) Do a check of the wiring SOL VLV signal from SERVO CTL-R AILERON, INBD G and SERVO CTL-L AILERON, OUTBD B to the ELAC1 COM and MON side (Ref. ASM 27-93/02).
(4) Do a check of the wiring POS XDCR signal from SERVO CTL-R AILERON, INBD G and SERVO CTL-L AILERON, OUTBD B to the ELAC1 COM and MON side (Ref. ASM 27-93/02).
「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 ∞∞27-10-00∞∞∞∞∞∞∞∞∞∞Page 281
May 01/04 CES RUDDER - FAULT ISOLATION PROCEDURES
___________________________________
TASK 27-20-00-810-801
CAPT and F/O Pedals Stiffness
WARNING : MAKE SURE THAT THE GROUND SAFETY-LOCKS ARE IN POSITION ON THE LANDING
_______
GEAR.
WARNING : MAKE SURE THAT THE CONTROLS AGREE WITH THE POSITION OF THE ITEMS THEY
_______
OPERATE BEFORE YOU PRESSURIZE A HYDRAULIC SYSTEM.
WARNING : MAKE SURE THAT THE TRAVEL RANGES OF THE FLIGHT CONTROL SURFACES ARE
_______
CLEAR BEFORE YOU PRESSURIZE/DEPRESSURIZE A HYDRAULIC SYSTEM.
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.
1. Possible Causes
_______________
2. Job Set-up Information
______________________
A. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
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本文鏈接地址：A320 Trouble Shooting Manual 排故手冊 飛行操縱 1(28)
