Slat System Interfaces - Data to Other Systems
 Figure 009

R 1EFF : 001-049, 051-099, 101-149, 151-199, 1 27-81-00Page 18 1201-299, 401-499, 1Aug 01/05 1 1 1CES 1R Slat System Interfaces - Data to Other Systems R Figure 009A

R 1EFF : 301-399, 1 27-81-00Page 19 1 1 May 01/04 1 1 1CES 1

 Slat System Interfaces - Data from Other Systems Figure 010
 1EFF : 1 1R 1CES  ALL  1 11 1 27-81-00 Page 20 May 01/04

 Valve Block Figure 011
 1EFF : 1 1R 1CES  ALL  1 11 1 27-81-00 Page 21 May 01/04

 Feedback Position Pick-off Unit Figure 012
 1EFF : 1 1R 1CES  ALL  1 11 1 27-81-00 Page 22 May 01/04

 Asymmetry Position Pick-Off Unit Figure 013
 1EFF : 1 1R 1CES  ALL  1 11 1 27-81-00 Page 23 May 01/04

 Adapter Plate Figure 014
 1EFF : 1 1R 1CES  ALL  1 11 1 27-81-00 Page 24 Aug 01/04

 F. Wing Tip Brake
 (Ref. Fig. 015)
 The slats WTB is the same as the flaps WTB. Refer to (Ref. 27-51-00) for data on the WTB.
 7. Operation/Control and Indicating
________________________________
 (Ref. Fig. 016)

 A. Normal Operation
 (1) System Requirements
 For the normal operation of the slats:
 -energize the aircraft electrical network
 -close the circuit breakers 5CV, 7CV, 9CV and 11CV
 -pressurize the Blue hydraulic system for the slat system 1 and the Green hydraulic system for the slat system 2.
 NOTE : For safety, the circuit breakers 9CV and 11CV have a red guard
____ installed to prevent incorrect operation during flight. To open the circuit breakers it is necessary to remove the applicable red guard first.
 (2) Manual Control
 The slat and flap control lever controls the position of the slats. When the lever is moved to a new position, the slats move to the indicated slat angle.
 NOTE : The slats will not move when the slat and flap control lever
____ moves from position 2 to 3 , or 3 to 2. As a function of the lever position, the flaps can move.

R **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 401-499,
 (3) Electrical Control
 The CSU sends discrete signals to the slat channel of each SFCC. At the same time, the CSU sends discrete signals for the flap position to the flap channel. The switch pattern of the CSU changes when the control lever moves. This causes the SFCC to get different signals (Ref. Table 2). Each slat channel receives signals from two sets of the 5-track switches in the CSU. For a correct signal, each channel must receive the same detent pattern from the two sets of switches.

 Wing Tip Brake Figure 015
 1EFF : 1 1R 1CES  ALL  1 11 1 27-81-00 Page 26 May 01/04

 Slats - Normal Operation Figure 016
 1EFF : 1 1R 1CES  ALL  1 11 1 27-81-00 Page 27 May 01/04

 For a permitted out-of-detent pattern, each channel must receive the same out-of-detent pattern from the two sets of switches. If a different configuration occurs, it is a CSU failure.
 **ON A/C 301-399,
 (3) Electrical Control
 The CSU sends discrete signals to the slat channel of each SFCC. At the same time, the CSU sends discrete signals for the flap position to the flap channel. The switch pattern of the CSU changes when the control lever moves. This causes the SFCC to get different signals (Ref. Table 2). Each slat channel receives signals from two sets of the 5-track switches in the CSU. For a correct signal, each channel must receive the same detent pattern from the two sets of switches.
 For a permitted out-of-detent pattern, each channel must receive the same out-of-detent pattern from the two sets of switches.
 A CSU failure is given as one of the two that follows:
 -a CSU pattern being other than a valid selection or out-of-detent
 -the CSU is seen to move directly from 0 to Full or from Full to 0 without going through positions 1, 2 or 3. This failure is called a CSU disadjust if it is confirmed by the other SFCC.

R **ON A/C 001-049, 051-099, 101-149, 201-299,
 -------------------------------------------------------------------------------LEVER POSITION 0 1 2 3 FULL -------------------------------------------------------------------------------TRACK 1 XXXXX XXXXX TRACK 2 XXXXXXXXXXX TRACK 3 XXXXXXXXXX TRACK 4 XXXXXXXXXXX TRACK 5 XXXXXXXXXXXXX -------------------------------------------------------------------------------SLAT ANGLE 0 18 22 22 27 -------------------------------------------------------------------------------FLAP ANGLE 0 10 15 20 35 -------------------------------------------------------------------------------
　
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7(52)