• 热门标签

当前位置: 主页 > 航空资料 > 机务资料 >

时间:2011-03-21 14:32来源:蓝天飞行翻译 作者:admin
曝光台 注意防骗 网曝天猫店富美金盛家居专营店坑蒙拐骗欺诈消费者

Lever Position and Switch Pattern Table 2R **ON A/C 151-199, 401-499,

 

 -------------------------------------------------------------------------------LEVER POSITION 0 1 2 3 FULL -------------------------------------------------------------------------------TRACK 1 XXXXX XXXX TRACK 2 XXXXXXXXXXX TRACK 3 XXXXXXXXXX TRACK 4 XXXXXXXXXXXX TRACK 5 XXXXXXXXXXXXX
 _______________________________________________________________________________ SLAT ANGLE 0 18 22 22 27 -------------------------------------------------------------------------------FLAP ANGLE 0 10 15 20 40
 Lever Position and Switch Pattern Table 2
 **ON A/C 301-399,
 -------------------------------------------------------------------------------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 14 21 25 -------------------------------------------------------------------------------TAB INB'D 0 5.4 8.4 13.6 16.1 -------------------------------------------------------------------------------TAB OUT'D 0 6.2 9.7 15.8 19.1 -------------------------------------------------------------------------------
Lever Position and Switch Pattern Table 2
R 1EFF : 151-199, 301-399, 401-499, 1 27-81-00Page 29 1 1 Aug 01/05 1 1 1CES 1 **ON A/C ALL


 The SFCC memory keeps the last correct signal, which controls the slat and flap position. The SFCCs compare a new CSU signal with the slat position signal which comes from the FPPU. If a change of slat angle is necessary, the PCU solenoids get electrical power. The slats move towards the new position (Ref. 27-54-00). When the position data from the FPPU is the same as the CSU signal, the slats stop.
 NOTE : Slat and flap movement always obeys the last correct control
____ lever movement. For example, when the lever moves from position 3 to FULL, the slats will extend in the direction of the FULL position. If the lever returns to position 3 before the slats reach position FULL, the direction of slat movement changes and the slats move back to position 3.

R **ON A/C 001-049, 051-099, 101-105, 151-199, 201-299,
 B. Slat Alpha Lock/Speed Baulk
 The Air Data/Inertial Reference Units (ADIRU) supply corrected angle-of-attack (alpha) and computed air speed (CAS) data to the SFCC. The SFCC use the data to prevent slat retraction at high alpha and/or low CAS. Slat retraction is not possible if:
 -
the alpha is more than 8.5 deg.

 -
the CAS is less than 148 knots.


 The function resets if alpha decreases below 7.6 deg. or CAS increases over 154 knots.
 Alpha lock/speed baulk is not possible if:
 -
the slat retraction is set before alpha is more than 8.5 deg. or CAS less than 148 knots

 -
the aircraft is on the ground with CAS below 60 knots.


 When the function is active, the ECAM shows the message A-Lock (cyan, pulsing) below the slat position indication (Ref. 27-85-00).

 

R **ON A/C 106-149, 401-499,
 B. Slat Alpha Lock/Speed Baulk
 The Air Data/Inertial Reference Units (ADIRU) supply corrected angle-of-attack (alpha) and computed air speed (CAS) data to the SFCC. The SFCC use the data to prevent slat retraction at high alpha and/or low CAS. Slat retraction is not possible if:
 -
the alpha is more than 8.5 deg.

 -
the CAS is less than 148 knots.


 The function resets if alpha decreases below 7.6 deg. or CAS increases over 154 knots.
 Alpha lock/speed baulk is not possible if:
 -
the slat retraction is set before alpha is more than 8.5 deg. or CAS less than 148 knots

 -
the aircraft is on the ground with CAS below 60 knots.


 When the function is active, the ECAM shows the message A LOCK (green, flashing) above the slat position indication (Ref. 27-85-00).
 **ON A/C 301-302,
 B. Slat Alpha Lock/Speed Baulk
 The Air Data/Inertial Reference Units (ADIRU) supply corrected angle-of-attack (alpha) and computed air speed (CAS) data to the SFCC. The SFCC use the data to prevent slat retraction at high alpha and/or low CAS. Slat retraction is not possible if:
 -
the alpha is more than 8.0 deg.

 -
the CAS is less than 165 knots.


 The function resets if alpha decreases below 7.1 deg. or CAS increases over 171 knots.
 Alpha lock/speed baulk is not possible if:
 -
the slat retraction is set before alpha is more than 8.0 deg. or CAS less than 165 knots
 
中国航空网 www.aero.cn
航空翻译 www.aviation.cn
本文链接地址:A320飞机维护手册 AMM FLIGHT CONTROLS 飞行操纵7(53)