Loss of the Left Elevator because of its Two Servocontrols
1. Possible Causes
_______________
- SERVO CTL-L ELEVATOR, INBD G (34CE1)
- SERVO CTL-L ELEVATOR, OUTBD B (34CE3)
2. Job Set-up Information
______________________
A. Referenced Information
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REFERENCE DESIGNATION
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AMM 27-34-00-200-001 Check of the Elevator Servo Controls and Hinge
Bearings for too much Play and Condition
AMM 27-34-00-710-001 Operational Test of the Elevator and Hydraulic
Actuation
R AMM 27-34-51-000-001 Removal of the Elevator Servo Control
R AMM 27-34-51-400-001 Installation of the Elevator Servo Control AMM 27-96-00-710-008 Operational Test of the Damping Measurement (Elevator)
3. Fault Confirmation
__________________
A. Test
(1) Not applicable, you cannot confirm this fault on the ground.
4. Fault Isolation
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A. Do a check of the left elevator servocontrols and hinge bearings for too much play and condition (Ref. AMM TASK 27-34-00-200-001).
(1) Do an operational test of the damping measurement (Elevator) (Ref. AMM TASK 27-96-00-710-008):
- if the result of the test is not in the tolerances, see Para. (a)
- if the result of the test is in the tolerances, see Para. (b).
(a) Replace the SERVO CTL-L ELEVATOR, INBD G (34CE1) and the SERVO CTL-L ELEVATOR, OUTBD B (34CE3) of the left elevator (Ref. AMM TASK 27-34-51-000-001) and (Ref. AMM TASK 27-34-51-400-001).
NOTE : The resistance of primary and secondary windings must be
____ between 30 ohms and 500 ohms.
(b) Do the operational test of the elevator and hydraulic actuation (Ref. AMM TASK 27-34-00-710-001).
「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 ∞∞27-30-00∞∞∞∞∞∞∞∞∞∞Page 207
Aug 01/03 CES Loss of the Signal of the Left Elevator Position Transducer (MON) by the SEC 1
1. Possible Causes
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- SEC-1 (1CE1)
- wiring of the POS XDCR MON (ANI 2-1) signal from the SEC 1 (1CE1) MON part to the first terminal block
2. Job Set-up Information
______________________
A. Referenced Information
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REFERENCE DESIGNATION
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27-90-00-810-818 Loss of the ACS1 Signal of the SEC1 MON Side
AMM 27-94-34-000-001 Removal of the SEC (1CE1,1CE2,1CE3)
AMM 27-94-34-400-001 Installation of the SEC (1CE1,1CE2,1CE3)
AMM 27-96-00-710-020 Operational Test of the Side Stick Assembly
(Activation for the BITE Test) R AMM 27-96-00-740-001 BITE Test of the EFCS (Ground Scanning) ASM 27-94/07
3. Fault Confirmation
__________________
A. Test
(1) Do the operational test of the side stick assembly (Activation for the BITE test) (Ref. AMM TASK 27-96-00-710-020).
NOTE : Before you start the operational test procedure, release the
____ FLT CTL/ELAC 1, FLT CTL/ELAC 2 and FLT CTL/SEC 2 pushbutton switches (on these pushbutton switches the OFF legends come on).
(2) Do the BITE test of the EFCS (ground scanning) (Ref. AMM TASK 27-96-00-740-001).
(a) If the ground scanning gives the maintenance message: SEC1 OR WIRING FROM L ELEV POS MON XDCR
- refer to Para. Fault Isolation.
(b) If the ground scanning gives at least two maintenance messages of the list below: SEC1 OR WIRING FROM L ELEV POS MON XDCR SEC1 OR WIRING FROM R ELEV POS MON XDCR SEC1 MON OR WIRING FROM THS ACTR XDCR2 9CE SEC1 OR WIRING FROM L G ELEV MODE XDCR 34CE1 SEC1 OR WIRING FROM R Y ELEV MODE XDCR 34CE2 中國航空網 www.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(39)
