1 Quickly move a side stick (CAPT or F/O) in full nose up then
_
in full nose down position:
- on the lower ECAM DU, the two elevator indexes move at the
same time with the same travel speed.
2 If the left elevator does not move or if the travel speed is
_ less than the travel speed of the right elevator: R - do the action in Para. (2)(a)1_
R 3_ If the right elevator does not move or if the travel speed is
R less than the travel speed of the left elevator:
R - do the action in Para. (2)(b)1_
(2) If the test stops during the second sequence (one servocontrol is controlled by the SEC2):
(a) For the test of the left elevator:
- replace the SERVO CTL-L ELEVATOR, OUTBD B (34CE3) (Ref. AMM TASK 27-34-51-000-001) and (Ref. AMM TASK 27-34-51-400-001).
1 If the fault continues:
_
- replace the SERVO CTL-L ELEVATOR, INBD G (34CE1) (Ref. AMM TASK 27-34-51-000-001) and (Ref. AMM TASK 27-34-51-400-001).
「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 292
May 01/01 CES
(b) For the test of the right elevator:
- replace the SERVO CTL-R ELEVATOR, OUTBD B (34CE4) (Ref. AMM TASK 27-34-51-000-001) (Ref. AMM TASK 27-34-51-400-001).
1_ If the fault continues:
- replace the SERVO CTL-R ELEVATOR, INBD Y (34CE2) (Ref. AMM
TASK 27-34-51-000-001) (Ref. AMM TASK 27-34-51-400-001).
(3) If the test stops during the third sequence (one servocontrol is controlled by the SEC1):
(a) For the test of the left elevator:
- replace the SERVO CTL-L ELEVATOR, INBD G (34CE1) (Ref. AMM TASK 27-34-51-000-001) (Ref. AMM TASK 27-34-51-400-001).
1 If the fault continues:
_
- replace the SERVO CTL-L ELEVATOR, OUTBD B (34CE3) (Ref. AMM TASK 27-34-51-000-001) (Ref. AMM TASK 27-34-51-400-001).
(b) For the test of the right elevator:
- replace the SERVO CTL-R ELEVATOR, INBD Y (34CE2) (Ref. AMM TASK 27-34-51-000-001) (Ref. AMM TASK 27-34-51-400-001).
1 If the fault continues:
_
- replace the SERVO CTL-R ELEVATOR, OUTBD B (34CE4) (Ref. AMM TASK 27-34-51-000-001) (Ref. AMM TASK 27-34-51-400-001).
B. If the message TEST NOT POSSIBLE is shown related to an another code (different of 03FF):
- do the trouble shooting procedure (Ref. TASK 27-30-00-810-851).
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 ∞∞27-30-00∞∞∞∞∞∞∞∞∞∞Page 293
Aug 01/00R
CES Vibrations Felt Along the Cabin and in the Cockpit
1. Possible Causes
_______________
- elevator servo control
2. Job Set-up Information
______________________
A. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
05-50-00-810-801 Identification of the Cause of In-Flight Airframe
Vibrations and/or Noises
AMM 27-34-00-200-002 Check of the Elevator Servo Control Oscillations.
3. Fault Confirmation
__________________
A. Test
Make sure that the identification of the cause of the vibrations is
correct (Ref. TASK 05-50-00-810-801)
4. Fault Isolation
_______________
A. If you feel vibrations along the cabin and in the cockpit:
- do a check of the elevator servo control oscillations (Ref. AMM TASK 27-34-00-200-002).
「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 ∞∞27-30-00∞∞∞∞∞∞∞∞∞∞Page 294
Aug 01/00R
CES Vibrations Felt in the Rear Cabin
1. Possible Causes
_______________
- elevator servo controls and hinge bearings
2. Job Set-up Information
______________________
A. Referenced Information
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本文鏈接地址：A320 Trouble Shooting Manual 排故手冊 飛行操縱 1(70)
