On the lower ECAM display unit, on the F/CTL page:
-the PITCH TRIM indicator shows 0 DEG plus or minus 0.3 .
After approximately five seconds, the pitch-trim control wheel goes back automatically to the O position.
On the lower ECAM display unit, on the F/CTL page:
-
the PITCH TRIM indicator shows 0 DEG plus or minus 0.3 .
On the upper ECAM display unit:
-
the F/CTL ELAC 1 FAULT and F/CTL ELAC 2 FAULT messages come into view.
On the lower ECAM display unit, on the F/CTL page:
-
the indexes which show the position of the elevators and spoilers 2, 3 and 4 move in relation to the side stick orders.
On the overhead panel 23VU:
-
the OFF legend of the FLT CTL/SEC 1 comes on.
On the overhead panel 24VU:
-
the OFF legend of the FLT CTL/SEC 2 goes off.
On the lower ECAM display unit, on the F/CTL page:
-
the indexes which show the position of the elevators and spoilers N. 2
R 1EFF : 001-049, 051-099, 101-105, 201-203, 1 27-96-00Page 583 1 1 Aug 01/05 1 1 1CES 1
-------------------------------------------------------------------------------ACTION RESULT -------------------------------------------------------------------------------
R - full nose down R - full right turn R - full left turn R - move the side stick back to R the neutral position.
R 60. Close the circuit breakers 15CE1 R and 15CE2. R
R **ON A/C 106-149, 204-299,
R Post SB 27-1113 For A/C 204-210, R Post SB 31-1115 For A/C 204-210,
R Subtask 27-96-00-710-081-E and 5 move in relation to the side stick orders.
On the upper ECAM display unit:
-the F/CTL ELAC 1 FAULT and F/CTL ELAC 2 FAULT messages go out of view.
R A. Operational Test of the Logics that activates the ELAC 1 & 2 and SEC1 R STBY PWR SPLY and Ability of the ELAC 1 and SEC 1 & 2 to Achieve Pitch R Control
R NOTE : During the test, ignore the MASTER CAUT legend and single shime.
____
R -------------------------------------------------------------------------------R ACTION RESULT R -------------------------------------------------------------------------------
R 1. Open the circuit breakers 15CE1 On the overhead panel 23VU:
R and 21CE1. - the FAULT legends of the FLT CTL/ELAC
R 1 and FLT CTL/SEC 1 pushbutton
R switches are off.
R 2. On the panel 50VU: On the panel 50VU:
R - release the BLUE PUMP OVRD - the ON legend of the BLUE PUMP OVRD
R pushbutton switch. pushbutton switch goes off.
R On the overhead panel 23VU:
R - the FAULT legends of the FLT CTL/ELAC
R 1 and FLT CTL/SEC 1 pushbutton
R switches are off.
R After approximately 30 seconds the
R FAULT legends come on.
R 1EFF : 001-049, 051-099, 101-149, 201-299, 1 27-96-00Page 584 1 1 Aug 01/05 1 1 1CES 1
-------------------------------------------------------------------------------ACTION RESULT -------------------------------------------------------------------------------
R R R
R R R
R R R 3. On the panel 50VU: - push the BLUE PUMP OVRD pushbutton switch.
R R
R R R R 4. Close the circuit breakers 15CE1 and 21CE1.
R R R
R R R
R R R R R R 5. Open the circuit breakers 1GA, 52GA and 15CE2. NOTE : Ignore the warning related____ to the other systems
R R
R R
R R R 6. Open the circuit breaker 19CE1.
On the upper ECAM display unit, the ELAC 1 FAULT and SEC 1 FAULT warnings come into view.
On the lower ECAM display unit, the ELAC 1 and SEC 1 legends change to amber.
On the overhead panel 50VU:
-the ON legend of the BLUE PUMP OVRD pushbutton switch comes on.
The above mentioned warnings are still shown.
On the overhead panel 23VU:
-the FAULT legends of the FLT CTL/ELAC 1 and FLT CTL/SEC 1 pushbutton switches go off.
On the upper ECAM display unit, the ELAC 1 FAULT and SEC 1 FAULT warnings go out of view.
On the lower ECAM display unit, the ELAC 1 and SEC 1 legends change to green.
On the overhead panel 24VU:
-the FAULT legend of the FLT CTL/ELAC 2 pushbutton switch comes on.
On the upper ECAM display unit, the ELAC 2 FAULT warning comes into view.
中國航空網 www.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：A320飛機維護手冊 AMM FLIGHT CONTROLS 飛行操縱9(146)
