• 热门标签

当前位置: 主页 > 航空资料 > 机务资料 >

时间:2011-03-28 22:55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

 B. Do the test given in para. 3.

 

 TASK 34-36-00-810-849
 Loss of the GPS Antenna 2 Signal

 1. Possible Causes
_______________
 - ANTENNA-GPS ACTIVE, 2 (43RT2)
 2. Job Set-up Information
______________________
 A. Referenced Information
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
R  AMM 20-28-00-912-003 Electrical Bonding of Electrical Connectors AMM 34-36-00-740-003 BITE Test of the MMR AMM 34-36-16-000-001 Removal of the GPS Active Antenna (43RT1, 43RT2) AMM 34-36-16-400-001 Installation of the GPS Active Antenna (43RT1, 43RT2)
 with Teflon Seal AMM 34-36-31-000-002 Removal of the Multi Mode Receiver (40RT1, 40RT2) AMM 34-36-31-400-002 Installation of the Multi Mode Receiver (40RT1,
 40RT2) R SRM 517400 P.Block001
 3. Fault Confirmation
__________________ **ON A/C ALL R Post SB 34-1147 For A/C 001-004,051-060,
 A. Test Do the BITE test of the MMR2 (Ref. AMM TASK 34-36-00-740-003).


 **ON A/C ALL
 4. Fault Isolation_______________
 **ON A/C ALL 
R  Post SB  34-1147 For A/C 001-004,051-060,
R R R R R R  A. If the test gives the maintenance message GPS ANTENNA2(43RT2)/COAX CABLE/MMR2(40RT2): - remove the MMR2 (Ref. AMM TASK 34-36-31-000-002) - remove the GPS antenna 2 (Ref. AMM TASK 34-36-16-000-001) - make sure that there is no moisture and/or corrosion on the coaxial cable of the GPS antenna 2 - if you find corrosion damage, refer to the Structural Repair Manual (Ref. SRM 517400 P.Block001) for types, inspection, removal, and corrosion protection - make sure that there is continuity on the coaxial cable of the GPS antenna 2 (Ref. AMM TASK 20-28-00-912-003) - replace the coaxial cable if necessary - make sure that there is discontinuity between the core and shield of the coaxial cable of the GPS antenna 2 - repair if necessary.
 (1) If the fault stops: - install the MMR2 (Ref. AMM TASK 34-36-31-400-002) - install the GPS antenna 2 (Ref. AMM TASK 34-36-16-400-001).
 (2) If the fault continues: - install a new ANTENNA-GPS ACTIVE, 2 (43RT2) (Ref. AMM TASK 34-36-16-400-001) - install the MMR2 (Ref. AMM TASK 34-36-31-400-002).
 B. Do the test given in para. 3.

 

 TASK 34-36-00-810-850
 Loss of the CFDIU INPUT Bus on the MMR1

 1. Possible Causes
_______________
 - MMR-1 (40RT1)

 - wiring of the CFDS DATA INPUT bus between the MMR1 (40RT1) and the first terminal block


 2. Job Set-up Information
______________________
 A. Referenced Information
 -------------------------------------------------------------------------------REFERENCE DESIGNATION
 -------------------------------------------------------------------------------
AMM 34-36-00-740-003 BITE Test of the MMR
 AMM 34-36-31-000-002 Removal of the Multi Mode Receiver (40RT1, 40RT2)
 AMM 34-36-31-400-002 Installation of the Multi Mode Receiver (40RT1,

 40RT2)
 ASM 34-36/01

 3. Fault Confirmation
__________________ **ON A/C ALL R Post SB 34-1147 For A/C 001-004,051-060,
 A. Test Do the BITE test of the MMR1 (Ref. AMM TASK 34-36-00-740-003).


 4. Fault Isolation
_______________ **ON A/C ALL R Post SB 34-1147 For A/C 001-004,051-060,
 A. If the test gives the maintenance message CFDIU(1TW)/MMR1(40RT1):
 - replace the MMR-1 (40RT1) (Ref. AMM TASK 34-36-31-000-002) and (Ref. AMM TASK 34-36-31-400-002).
 (1) If the fault continues:
 - do a check and repair the wiring of the CFDS DATA INPUT bus between the MMR1 (40RT1) and the first terminal block for pins AB/1E, 1F of the MMR1 (Ref. ASM 34-36/01).
 B. Do the test given in para. 3.


 TASK 34-36-00-810-851
 Loss of the CFDIU INPUT Bus on the MMR2

 1. Possible Causes
_______________
 - MMR-2 (40RT2)

 - wiring of the CFDS DATA INPUT bus between the MMR2 (40RT2) and the first terminal block


 2. Job Set-up Information
______________________
 A. Referenced Information
 -------------------------------------------------------------------------------REFERENCE DESIGNATION
 -------------------------------------------------------------------------------
AMM 34-36-00-740-003 BITE Test of the MMR
 AMM 34-36-31-000-002 Removal of the Multi Mode Receiver (40RT1, 40RT2)
 AMM 34-36-31-400-002 Installation of the Multi Mode Receiver (40RT1,

 40RT2)
 ASM 34-36/01

 3. Fault Confirmation
__________________ **ON A/C ALL R Post SB 34-1147 For A/C 001-004,051-060,
 
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 导航 NAVIGATION 2(130)