• 热门标签

当前位置: 主页 > 航空资料 > 机务资料 >

时间:2011-03-28 13:44来源:蓝天飞行翻译 作者:航空
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

 (2) Do the BITE test of the EFCS (Ground Scanning) (Ref. AMM TASK 27-96-00-740-001).


 4. Fault Isolation
_______________
 A. If the BITE test gives the maintenance message:
 F/O ROLL CTL SSTU 4CE2

 - remove the F/O side stick assembly (Ref. AMM TASK 27-92-41-000-001).
 (1) Examine the control rods, bellcranks and input levers of the transducer unit and take the corrective actions if necessary.

 (2) If no mechanical problems:

 - replace the SSTU-ROLL CTL, F/O (4CE2), (Ref. AMM TASK 27-92-41-000-002) and (Ref. AMM TASK 27-92-41-400-002).

 (3) Install the F/O side stick assembly (Ref. AMM TASK 27-92-41-400-001).


 B. Do the operational test and the BITE test given in Para. 3.
 「一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一1 EFF : ALL ∞∞27-93-00∞∞∞∞∞∞∞∞∞∞Page 219
 Nov 01/01 CES Failure of the CAPT Pitch Control SSTU


 1. Possible Causes
_______________
 - SSTU-PITCH CTL, CAPT (4CE3)

 - control rods, bellcranks and input levers of the transducer unit


 2. Job Set-up Information
______________________
 A. Referenced Information
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
R AMM 27-92-41-000-001 Removal of the Side Stick Assembly 19VU (18VU) AMM 27-92-41-000-002 Removal of the Transducer Units (4CE1,4CE2,4CE3,4CE4) R AMM 27-92-41-400-001 Installation of the Side Stick Assembly 19VU (18VU) AMM 27-92-41-400-002 Installation of the Transducer Units (4CE1,4CE2,4CE3,4CE4) AMM 27-96-00-710-020 Operational Test of the Side Stick Assembly (Activation for the BITE Test) AMM 27-96-00-740-001 BITE Test of the EFCS (Ground Scanning)
 3. Fault Confirmation
__________________
 A. Test
 (1) Do the operational test of the side stick assembly (activation for the BITE test) (Ref. AMM TASK 27-96-00-710-020).

 (2) Do the BITE test of the EFCS (Ground Scanning) (Ref. AMM TASK 27-96-00-740-001).


 4. Fault Isolation
_______________
 A. If the BITE test gives the maintenance message:
 CAPT PITCH CTL SSTU 4CE3

 - remove the CAPT side stick assembly (Ref. AMM TASK 27-92-41-000-001).
 (1) Examine the control rods, bellcranks and input levers of the transducer unit and take the corrective actions if necessary.

 (2) If no mechanical problems:

 - replace the SSTU-PITCH CTL, CAPT (4CE3), (Ref. AMM TASK 27-92-41-000-002) and (Ref. AMM TASK 27-92-41-400-002).

 (3) Install the CAPT side stick assembly (Ref. AMM TASK 27-92-41-400-001).


 「一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一1 EFF : ALL ∞∞27-93-00∞∞∞∞∞∞∞∞∞∞Page 220
 Nov 01/01 CES


 B. Do the operational test and the BITE test given in Para. 3.

 

 Failure of the F/O Pitch Control SSTU
 1. Possible Causes
_______________
 - SSTU-PITCH CTL, F/O (4CE4)

 - control rods, bellcranks and input levers of the transducer unit


 2. Job Set-up Information
______________________
 A. Referenced Information
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
R AMM 27-92-41-000-001 Removal of the Side Stick Assembly 19VU (18VU) AMM 27-92-41-000-002 Removal of the Transducer Units (4CE1,4CE2,4CE3,4CE4) R AMM 27-92-41-400-001 Installation of the Side Stick Assembly 19VU (18VU) AMM 27-92-41-400-002 Installation of the Transducer Units (4CE1,4CE2,4CE3,4CE4) AMM 27-96-00-710-020 Operational Test of the Side Stick Assembly (Activation for the BITE Test) AMM 27-96-00-740-001 BITE Test of the EFCS (Ground Scanning)
 3. Fault Confirmation
__________________
 A. Test
 (1) Do the operational test of the side stick assembly (activation for the BITE test) (Ref. AMM TASK 27-96-00-710-020).

 (2) Do the BITE test of the EFCS (Ground Scanning) (Ref. AMM TASK 27-96-00-740-001).


 4. Fault Isolation
_______________
 A. If the BITE test gives the maintenance message:
 F/O PITCH CTL SSTU 4CE4

 - remove the F/O side stick assembly (Ref. AMM TASK 27-92-41-000-001).
 (1) Examine the control rods, bellcranks and input levers of the transducer unit and take the corrective actions if necessary.


 
中国航空网 www.aero.cn
航空翻译 www.aviation.cn
本文链接地址:A320 Trouble Shooting Manual 排故手册 飞行操纵 2(124)