51.
On the overhead panel 23VU:
-release and push again the FLT CTL/SEC 1 pushbutton switch.
52.
Set the pitch-trim control wheel to the 3 DN position.
53.
On the overhead panel 23VU:
-release and push again the FLT CTL/SEC 1 pushbutton switch.
54.
Open the circuit breakers 15CE1 and 15CE2.
55.
On the CAPT or F/O side:
-give the orders below one after the other:
-
full nose up
-
full nose down
-
full right turn
-
full left turn
-move the side stick back to the neutral position.
56.
On the overhead panel 23VU:
-release the FLT CTL/SEC 1 pushbutton switch.
After approximately five seconds, thepitch-trim control wheel goes backautomatically 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 .
After approximately five seconds, thepitch-trim control wheel goes backautomatically 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 theF/CTL page:
-
the indexes which show the positionof the elevators and spoilers 2, 3and 4 move in relation to the sidestick orders.
On the overhead panel 23VU:
-
the OFF legend of the FLT CTL/SEC 1comes on.
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ACTION RESULT -------------------------------------------------------------------------------
57. On the overhead panel 24VU:
-push the FLT CTL/SEC 2 pushbutton switch.
58. On the CAPT or F/O side:
-give the orders below one after the other:
-
full nose up
-
full nose down
-
full right turn
-
full left turn
-move the side stick back to the neutral position.
59. Close the circuit breakers 15CE1 and 15CE2.
R
R **ON A/C 151-199,
Subtask 27-96-00-710-081-AOn the overhead panel 24VU:
-
the OFF legend of the FLT CTL/SEC 2goes off.
On the lower ECAM display unit, on theF/CTL page:
-
the indexes which show the positionof the elevators and spoilers N. 2and 5 move in relation to the sidestick orders.
On the upper ECAM display unit:
-
the F/CTL ELAC 1 FAULT and F/CTL ELAC 2 FAULT messages go out of view.
A. Operational Test of the Logics that activates the ELAC 1 & 2 and SEC1 STBY PWR SPLY and Ability of the ELAC 1 and SEC 1 & 2 to Achieve Pitch Control
NOTE : During the test, ignore the MASTER CAUT legend and single shime.
____
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1. Open the circuit breakers 15CE1 On the overhead panel 23VU:
and 21CE1. - the FAULT legends of the FLT CTL/ELAC
1 and FLT CTL/SEC 1 pushbutton
switches are off.
2. On the panel 50VU: On the panel 50VU:
- release the BLUE PUMP OVRD - the ON legend of the BLUE PUMP OVRD
pushbutton switch. pushbutton switch goes off.
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ACTION RESULT -------------------------------------------------------------------------------
3. On the panel 50VU:
-push the BLUE PUMP OVRD
pushbutton switch.
4.
Close the circuit breakers 15CE1 and 21CE1.
5.
Open the circuit breakers 1GA, 52GA and 15CE2.
NOTE : Ignore the warning related
____
to the other systems
On the overhead panel 23VU:
-the FAULT legends of the FLT CTL/ELAC 1 and FLT CTL/SEC 1 pushbutton switches are off.
After approximately 30 seconds the FAULT legends come on.
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 OVRDpushbutton switch comes on.
The above mentioned warnings are still shown.
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本文链接地址：A320飞机维护手册 AMM FLIGHT CONTROLS 飞行操纵9(131)
