Loss of the Four Elevator Servocontrols
1. Possible Causes_______________
2. Job Set-up Information______________________
A. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
AMM 27-96-00-740-001 BITE Test of the EFCS (Ground Scanning)
3. Fault Confirmation__________________
A. Test Not applicable.
4. Fault Isolation_______________
R R R R A. This warning is shown after the failure of the four elevator servocontrols. To do the trouble shooting refer to the POST FLIGHT REPORT and start the trouble shooting from the first F/CTL ELEV SERVO FAULT warning and its related maintenance message. After this step, on the upper ECAM DU the F/CTL L ELEV FAULT or F/CTL R ELEV FAULT warning will go out of view and be replaced by F/CTL L ELEV FAULT and F/CTL ELEV SERVO FAULT or F/CTL R ELEV FAULT and F/CTL ELEV SERVO FAULT warning with a related maintenance message. Do the BITE test of the EFCS (ground scanning) (Ref. AMM TASK 27-96-00-740-001), to know the related maintenance message. Do the trouble shooting procedure related to this message.
Elevator Damping Test not Possible
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 CONTROLS ARE CLEAR.
_______
MOVEMENT OF FLIGHT CONTROLS CAN CAUSE INJURY TO PERSONS AND/OR
DAMAGE.
1. Possible Causes
_______________
- SERVO CTL-L ELEVATOR, OUTBD B (34CE3)
- SERVO CTL-L ELEVATOR, INBD G (34CE1)
- SERVO CTL-R ELEVATOR, OUTBD B (34CE4)
- SERVO CTL-R ELEVATOR, INBD Y (34CE2)
2. Job Set-up Information
______________________
A. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
27-30-00-810-851 Elevator Damping Test Not Possible (Decoding) 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)
27-30-00-991-001 Fig. 201
3. Fault Confirmation
__________________
A. Test
(1) Do the operational test of the damping measurement (elevator) (Ref. AMM TASK 27-96-00-710-008).
4. Fault Isolation
_______________
A. If the message TEST NOT POSSIBLE is shown related to the normal engagement codes (03FF):
- the right (left) elevator damping test consists of 3 sequences as follows: (Ref. Fig. 201/TASK 27-30-00-991-001)
「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 ∞∞27-30-00∞∞∞∞∞∞∞∞∞∞Page 290
Aug 01/03 CES
Elevator Damping Test Sequences
Figure 201/TASK 27-30-00-991-001
「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 ∞∞27-30-00∞∞∞∞∞∞∞∞∞∞Page 291
Aug 01/00R CES
(1) If the test stops during the first sequence (the 2 servocontrols are controlled by the SEC1 and SEC2):
(a) Do an elevator operational test as follows:
- make sure that the Green, Blue and Yellow hydraulic systems are pressurized
- make sure that the SEC1 is engaged (the ELAC1 is disengaged)
- disengage the SEC2 (the ELAC2 is disengaged).
(b) Do an elevator operational test as follows:
- make sure that the Green, Blue and Yellow hydraulic systems are pressurized
- make sure that the SEC2 is engaged (the ELAC2 is disengaged)
- disengage the SEC1 (the ELAC1 is disengaged).
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
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本文链接地址：A320 Trouble Shooting Manual 排故手册 飞行操纵 1(69)
