-------------------------------------------------------------------------------ACTION RESULT -------------------------------------------------------------------------------
R - move the side stick back to
R the neutral position.
R 53. Set the pitch-trim control wheel
R to the 10 UP position.
R 54. On the overhead panel 23VU:
R - release and push again the FLT
R CTL/SEC 1 pushbutton switch.
R
R
R
R
R 55. Set the pitch-trim control wheel
R to the 3 DN position.
R 56. On the overhead panel 23VU:
R - release and push again the FLT
R CTL/SEC 1 pushbutton switch.
R
R
R
R
R 57. Open the circuit breakers 15CE1
R and 15CE2.
R
R 58. On the CAPT or F/O side:
R - give the orders below one
R after the other:
R - full nose up
R - full nose down
R - full right turn
R - full left turn
R - move the side stick back to
R the neutral position.
R 59. On the overhead panel 23VU:
R - release the FLT CTL/SEC 1
R pushbutton switch.
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.
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.
R 1EFF : 106-149, 204-299, 1 27-96-00Page 594 1 1 Aug 01/05 1 1 1CES 1
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R 60. On the overhead panel 24VU:
R - push the FLT CTL/SEC 2
R pushbutton switch.
R 61. On the CAPT or F/O side:
R - give the orders below one
R after the other:
R - full nose up
R - full nose down
R - full right turn
R - full left turn
R - move the side stick back to
R the neutral position.
R 62. Close the circuit breakers 15CE1
R and 15CE2.
R
R **ON A/C 151-199, 301-399, 401-499,
R Post SB 27-1113 For A/C 151-199,
R Post SB 31-1115 For A/C 151-199,
R Subtask 27-96-00-710-081-D
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 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 1EFF : 106-149, 151-199, 204-299, 301-399, 1 27-96-00Page 595 1401-499, 1Aug 01/05 1 1 1CES 1
-------------------------------------------------------------------------------ACTION RESULT -------------------------------------------------------------------------------
R R R R
R R
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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(151)
