• 热门标签

当前位置: 主页 > 航空资料 > 机务资料 >

时间:2011-03-28 13:54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

_ 3 Trouble shoot the fuel probes on the related harness.
_ Start with the multi sensor (ULTRA COMP, DUAL COMP), if applicable, fuel probes first.
 4 Do the test given in Para. 3.B.
_

 「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 : 301-399, ∞∞28-42-00∞∞∞∞∞∞∞∞∞∞Page 215
 Feb 01/05R
 CES R **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 401-499,

 

 TASK 28-42-00-810-802
 Fuel Quantity - Cadensicon 19QT1(2), Left(Right) Wing
 WARNING : OBEY THE FUEL SAFETY PROCEDURES.
_______
 WARNING : WHEN YOU DO WORK ON THE FUEL SYSTEM WIRING, YOU MUST USE TEST
_______ EQUIPMENT THAT IS APPROVED (REFER TO INTERNATIONAL OR NATIONAL SPECIFICATIONS FOR INTRINSICALLY SAFE TEST EQUIPMENT, E.G. EN50-020, UL913 OR EQUIVALENT). TEST EQUIPMENT THAT IS NOT APPROVED CAN CAUSE FIRE OR AN EXPLOSION.
 1. Possible Causes
_______________
 - FQIC (3QT)

 - HARNESS-CHAN A, L WING TK INR (13QT1)

 - HARNESS-CHAN A, R WING TK INR (13QT2)

 - CADENSICON-RIB 2-3, L WNG TK INR GROUP A (19QT1)

 - CADENSICON-RIB 2-3, R WNG TK INR GROUP A (19QT2)

 - aircraft wiring

 - shorting plug 4041VC-A(4042VC-A)

 - fused connector 4041VC-A(4042VC-A)


 2. Job Set-up Information
______________________
 A. Fixtures, Tools, Test and Support Equipment
 -------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
No specific multimeter
 B. Referenced Information
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
ESPM 20-00-00 ESPM 20-52-21 ESPM 20-52-22 AMM 24-41-00-861-002 Energize the Aircraft Electrical Circuits from the
 External Power AMM 24-41-00-862-002 De-energize the Aircraft Electrical Circuits Supplied
 from the External Power AMM 28-10-00-910-001 Safety Procedures When You Do Work in a Fuel Tank AMM 28-10-00-910-002 Access to the Fuel Tanks and the Work Areas AMM 28-42-00-740-003 Interrogation of the FQIS Input Parameters Pages
 「一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一1R EFF : 001-049, 051-099, 101-149, 151-199, ∞∞28-42-00∞∞∞∞∞∞∞∞∞∞Page 216
 201-299, 401-499, Aug 01/05 CES -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------

 

R  AMM 28-42-00-740-007 Interrogation of the (SMITHS INDUSTRIES) FQIS Trouble
R Shooting Data AMM 28-42-16-000-001 Removal of the Cadensicon 19QT1 (19QT2) AMM 28-42-16-400-001 Installation of the Cadensicon 19QT1 (19QT2) AMM 28-42-34-000-001 Removal of the Fuel Quantity-Indicating Computer
 (FQIC) (3QT) AMM 28-42-34-400-001 Installation of the Fuel Quantity-Indicating Computer (FQIC) (3QT) AMM 28-42-43-000-006 Removal of the Wing-Tank Inner-Cell Group A Harness 13QT1(13QT2) AMM 28-42-43-000-008 Removal of the Wing Tank Fuel Quantity Indicating Probe Fused/Shorting Plug Connectors AMM 28-42-43-400-006 Installation of the Wing-Tank Inner-Cell Group A Harness 13QT1(13QT2) AMM 28-42-43-400-008 Installation of the Wing Tank Fuel Quantity Indicating Probe Fused/Shorting Plug Connectors AMM 31-32-00-860-001 Procedure to Get Access to the SYSTEM REPORT/TEST
 Menu Page
 AMM 31-60-00-860-001 EIS Start Procedure
 AMM 31-60-00-860-002 EIS Stop Procedure

R  AMM 28-42-00 P.Block 001 QUANTITY INDICATING ASM 28-42/05 ASM 28-42/06 AWM 28-42-04 AWM 28-42-05
 3. Fault Confirmation
__________________
 A. Table of the circuit breakers used in this procedure:
 -------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------49VU FUEL/FQI/CHAN/1 1QT A13 121VU FUEL/FQI/CHAN/2 2QT M27
 B. Test
 (1) To keep the number of computer replacements (with no fault found) to a minimum, do the power on BITE test of the FQIS as follows:
 NOTE : The L(R) wing inner cell must contain 1500kg (3300lb) of fuel
____
 to fully test the cadensicon.

 (a) If the FQIS is not energized:
 1  Close the C/Bs 1QT and 2QT.
_

 「一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一1R EFF : 001-049, 051-099, 101-149, 151-199, ∞∞28-42-00∞∞∞∞∞∞∞∞∞∞Page 217
 
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 FUEL 燃油2(113)