• 热门标签

当前位置: 主页 > 航空资料 > 机务资料 >

时间:2011-04-13 07:54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

 (v)  
Close the 6C34 AOA HEAT R circuit breaker on the P6 Main Power Distribution Panel.

 (w)  
Push the LSK that is adjacent to <PROBE HEAT R on the GROUND TESTS MENU. 1) Make sure bit 18 of label 270 is momentarily in the one

 state.

 (x)  
Open the 6C34 AOA HEAT R circuit breaker on the P6 Main Power Distribution Panel.

 (y)  
Close the 6D29 PROBE HEAT TAT R circuit breaker on the P6 Main Power Distribution Panel.

 (z)  
Push the LSK that is adjacent to <PROBE HEAT R on the GROUND TESTS MENU. 1) Make sure bit 16 of label 270 is momentarily in the one


 state.
 (aa) Open the 6D29 PROBE HEAT TAT R, 6D34 PROBE HEAT IND L, and 6D35 PROBE HEAT IND R circuit breakers on the P6 Main Power Distribution Panel.
 (ab) Set the AIR DATA switch on the captain's SOURCE SELECT module to the L position. (ac) Disconnect the ARINC 429 bus reader from the C ADC front panel TEST ONLY connecter.
 S 865-280
 (40) Remove the DO-NOT-CLOSE tags and close these circuit breakers:
 (a)  P6 Main Power Distribution Panel
 1) 6B17, WINDOW HEAT 1R

 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 34-12-00
 ALL  ú ú 09 Page 537 ú Oct 18/00
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400 MAINTENANCE MANUAL
 2) 6B34, WINDOW HEAT 1L 3) 6E28, WINDOW HEAT PWR 2L & 3R 4) 6E29, WINDOW HEAT IND 2L & 3R 5) 6E30, WINDOW HEAT PWR 2R & 3L 6) 6E31, WINDOW HEAT IND 2R & 3L
 M. Alternate SSEC Test
 (1)  S 485-829Connect an ARINC 429 bus reader to the L ADC front panel TEST ONLY connector.
 (2)  S 865-830Set the ARINC 429 bus reader to these parameters:
 Octal Label: 270 SDI: 1 (Bit 10=0, Bit 9=1) Display: Engineering Units
 (a)  Make sure bit 26 of label 270 is in the one state.
 (3)  S 085-831Disconnect the ARINC 429 bus reader from the L ADC front panel TEST ONLY connector.
 (4)  S 485-832Connect an ARINC 429 bus reader to the R ADC front panel TEST ONLY connector.
 (5)  S 865-833Set the ARINC 429 bus reader to these parameters:
 Octal Label: 270 SDI: 2 (Bit 10=1, Bit 9=0) Display: Engineering Units

 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 34-12-00
 ALL  ú ú 08 Page 538 ú Oct 18/00
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400 MAINTENANCE MANUAL
 (a)  Make sure bit 26 of label 270 is in the one state.
 S 085-834
 (6)  
Disconnect the ARINC 429 bus reader from the R ADC front panel TEST ONLY connector.

 S 725-835

 (7)  
Do these steps to do a test of the alternate SSEC for the
 center ADC:


 (a)  
Set the AIR DATA switch on the first officer's SOURCE SELECT module to the C position.

 (b)  
Connect an ARINC 429 bus reader to the C ADC front panel TEST ONLY connector.

 (c)  
Set the ARINC 429 bus reader to these parameters:

 


 Octal Label: 270 SDI: 2 (Bit 10=1, Bit 9=0) Display: Engineering Units
 1) Make sure bit 26 of label 270 is in the one state.
 (d)  
Disconnect the ARINC 429 bus reader from the C ADC front panel TEST ONLY connector.

 (e)  
Set the AIR DATA switch on the first officer's SOURCE SELECT module to the R position.


 N. Put the Airplane Back to Its Usual Condition
 S 085-281
 (1)  
Remove the test equipment.

 (2)
Remove electrical power if it is not necessary (Ref 24-22-00/201).


 S 865-306
 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 34-12-00
 ALL  ú ú 08 Page 539 ú Oct 10/94
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400
MAINTENANCE MANUAL
 
中国航空网 www.aero.cn
航空翻译 www.aviation.cn
本文链接地址:747-400 AMM 飞机维护手册 导航 NAVIGATION 1(111)