A320飞机维护手册 AMM NAVIGATION 导航1(90)

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

 30-31-00-710-001 Operational Test of the Probe Ice Protection 34-10-00-710-007 Test of the Angle of Attack Warning 34-11-00-710-001 Test of the Monitoring of the ADR/AOA 26VAC Power Supply
R 34-11-19-991-002 Fig. 401
 3. Job Set-up
__________
 Subtask 34-11-19-860-051
 A. Aircraft Maintenance Configuration
 (1) Make sure that the access platform is in position in zone 231 for 3FP1 (232 for 3FP2) (127 for 3FP3).
 Subtask 34-11-19-865-051
 B. Make sure that this(these) circuit breaker(s) is(are) open, safetied and tagged
 -------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------FOR 3FP1
 49VU ANTI ICE/PROBES/AOA/1 4DA1 D04 49VU ANTI ICE/PROBES/PHC/1 2DA1 D03 49VU ANTI ICE/PROBES/PITOT/1 3DA1 D02 49VU NAV PROBES/ADIRU 1/AND AOA 1/26VAC 5FP1 F07 49VU NAV PROBES/ADIRU1/115VAC 4FP1 F06
 **ON A/C 001-049, 051-061, 101-105, 201-203,
 121VU ADIRS/ADIRU/3PWR/SWTG  9FP N10
 1EFF : ALL 1 34-11-19Page 406 1 1 Aug 01/05 1 1 1CES 1

 -------------------------------------------------------------------------------
PANEL DESIGNATION IDENT. LOCATION
 -------------------------------------------------------------------------------
R  **ON A/C 062-099, 106-149, 151-199, 204-299, 301-399, 401-499,
 121VU ADIRS/ADIRU/3PWR/SWTG  9FP  N09
 **ON A/C ALL
 122VU ANTI ICE/PROBES/1/STATIC 122VU ANTI ICE/PROBES/1/TAT FOR 3FP2 5DA1 1DA1  Z13Z12
 **ON A/C 001-049, 051-061, 101-105, 201-203,
 121VU ADIRS/ADIRU/2PWR/SHED 121VU ADIRS/ADIRU/2/26VAC AND AOA 121VU ADIRS/ADIRU/2/115VAC  10FP 5FP2 4FP2  N11N09N07 
R  **ON A/C 062-099, 106-149, 151-199, 204-299, 301-399, 401-499,
 121VU ADIRS/ADIRU/2PWR/SHED 121VU ADIRS/ADIRU/2/26VAC AND AOA 121VU ADIRS/ADIRU/2/115VAC  10FP 5FP2 4FP2  N10N08N06
 **ON A/C ALL
 122VU ANTI ICE/PROBES/2/TAT 122VU ANTI ICE/PROBES/2/PITOT 122VU ANTI ICE/PROBES/2/AOA 122VU ANTI ICE/PROBES/2/PHC 122VU ANTI ICE/PROBES/2/STATIC FOR 3FP3 1DA2 3DA2 4DA2 2DA2 5DA2  Y15Y14Y13Y12Y11
 **ON A/C 001-049, 051-061, 101-105, 201-203,
 121VU ADIRS/ADIRU/3PWR/SWTG 121VU ADIRS/ADIRU/3/26VAC AND AOA 121VU ADIRS/ADIRU/3/115VAC  9FP 5FP3 4FP3  N10N08N06

 1EFF : ALL 1 34-11-19Page 407 1 1 Aug 01/05 1 1 1CES 1 1EFF : ALL 1 34-11-19Page 408 1 1 Aug 01/05 1 1 1CES 1 1EFF : ALL 1 34-11-19Page 409 1 1 Aug 01/05 1 1 1CES 1 1EFF : ALL 1 34-11-19Page 410 1 1 Aug 01/05 1 1 1CES 1

R  -------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------**ON A/C 062-099, 106-149, 151-199, 204-299, 301-399, 401-499,
 121VU ADIRS/ADIRU/3PWR/SWTG 121VU ADIRS/ADIRU/3/26VAC AND AOA 121VU ADIRS/ADIRU/3/115VAC  9FP 5FP3 4FP3  N09N07N05
 **ON A/C ALL
 122VU ANTI ICE/PROBES/PHC/3 122VU ANTI ICE/PROBES/3/PITOT 122VU ANTI ICE/PROBES/3/AOA 122VU ANTI ICE/PROBES/3/STATIC  2DA3 3DA3 4DA3 5DA3  Y16Z16Z15Z14
 4. Procedure_________ 
R 
R  Subtask 34-11-19-420-050 
R  A. Installation of the Angle of Attack Sensor (3FP1, 3FP2, 3FP3) 
R  (1) Angle of Attack Sensor without drain hole. 
R R  NOTE : The procedure is the same for angle of attack sensors 3FP1,____ 3FP2 and 3FP3. 
R  (a) Clean the component interface and/or the adjacent area. 
R R  (b) Do an inspection of the component interface and/or the adjacent area. 
R  (c) Remove the blanking caps from the connectors (1) and (9). 
R R  (d) Make sure that the connectors (1) and (9) are clean and in the correct condition. 
R  (e) Put the seal (3) in its housing (2). 
R  (f) Connect the connector (1). 
R  (g) Push the connector (1) into the fuselage.

 

R  (h) Put the angle of attack sensor (5) in position with the stud (4) 
R  and hold it. 
R  (i) Tighten the screw (6). 
R  NOTE : During installation, the screw (6) must be inserted in the____ 
R  only c-sink hole of the AOA sensor (5).As the other holes 
R  have no c-sink, mounting the screw (6) in one of them may 
R  create non-flush surface. 
R  (j) Install and hold the blanking plate (7). 
R  NOTE : The AOA blanking plate (7) is manufactured with a radius____ 
R  that corresponds to the fuselage curve.The rotation of 
R  this plate around the AOA sensor may also create non-flush 
　
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 NAVIGATION 导航1(90)