日期： 2011-03-28 22:58:18
B. Do the test given in para. 3. TASK 34-41-00-810-801 Loss of the Weather Radar Information on the ND 1. Possible Causes_______________ - DMC-1 (1WT1) - DMC-2 (1WT2) - XCVR-WEATHER RADAR, 1 (1SQ1) - CTL UNIT-WEATHER RADAR (3SQ) - MTG TRAY...
日期： 2011-03-28 22:55:56
1 If the fault continues: _ - replace the ADM-STBY STATIC PRESSURE (19FP8) (Ref. AMM TASK 34-11-17-000-001) and (Ref. AMM TASK 34-11-17-400-001). B. Do the 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...
日期： 2011-03-28 22:53:52
TASK 34-00-00-810-801 Display of a Warning Message on the Upper ECAM DU 1. Possible Causes _______________ - message on the Post Flight Report (PFR) 2. Job Set-up Information ______________________ A. Referenced Information ---------------...
日期： 2011-03-28 22:45:04
HIGHLIGHTS __________ REVISION NO. 30 Aug 01/05 Pages which have been revised are outlined below, together with the Highlights of the Revision CH/SE/SU C REASON FOR CHANGE EFFECTIVITY PAGES CHAPTER 33 L.E.P. 1- 4 REVISED TO REFLECT THIS RE...
日期： 2011-03-28 18:47:27
3. Fault Confirmation __________________ A. Test (1) Do the operational test of Alternate braking with/without anti skid (Ref. AMM TASK 32-43-00-710-001). Do a check to confirm that when you put a same force on the left and right brake ped...
日期： 2011-03-28 18:45:35
LANDING GEAR - GENERAL - FAULT ISOLATION PROCEDURES ___________________________________________________ TASK 32-00-00-810-801 1. Possible Causes Display of an Operational warning on the Upper ECAM DU _______________ - message on the Post F...
日期： 2011-03-28 18:37:10
4. Fault Isolation _______________ A. If the test gives the maintenance message DMC3 : PROGRAM PIN or DMC3 : POSITION PIN: R - do a check for ground signals at DMC3 (1WT3) connector AB (Ref. AWM 31-R 61-30). (1) If the wiring is incorrect:...
日期： 2011-03-28 18:34:59
TASK 31-54-00-810-899 Loss of the GCU 2/EGIU 2 Bus of the SDAC 1 1. Possible Causes _______________ - SDAC-1 (1WV1) - EGIU-2 (22XU2) - wiring from the SDAC 1 (1WV1) to the EGIU 2 (22XU2) 2. Job Set-up Information ______________________ A....
日期： 2011-03-28 18:30:41
ELECTRICAL CLOCK - FAULT ISOLATION PROCEDURES _____________________________________________ TASK 31-21-00-810-801 Failure of the Clock 1. Possible Causes _______________ - CLOCK (2FS) 2. Job Set-up Information ______________________ A. Ref...
日期： 2011-03-28 18:28:39
REVISION NO. 30 Aug 01/05 Pages which have been revised are outlined below, together with the Highlights of the Revision CH/SE/SU C REASON FOR CHANGE EFFECTIVITY PAGES CHAPTER 30 L.E.P. 1- 3 REVISED TO REFLECT THIS REVISION INDICATING NEW,...
日期： 2011-03-28 18:26:59
HIGHLIGHTS __________ REVISION NO. 30 Aug 01/05 Pages which have been revised are outlined below, together with the Highlights of the Revision CH/SE/SU C REASON FOR CHANGE EFFECTIVITY PAGES CHAPTER 29 L.E.P. 1- 2 REVISED TO REFLECT THIS RE...
日期： 2011-03-28 18:24:53
R **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 401-499, Post SB 28-1087 For A/C 001-049,051-061,101-105,201-203, A. Table of the circuit breakers referred to in this procedure: -----------------------------------------------------...
日期： 2011-03-28 14:17:49
NOTE : Each capacitive fuel probe is supplied with an alternating ____ current drive, of 30 volts at 30 kilo-hertz, from the FQIC. The fuel probes in a tank group (harness) share the drive and drive return (two aircraft wires) between the...
日期： 2011-03-28 13:54:33
(1) Not applicable. 4. Fault Isolation _______________ R **ON A/C 001-049, 051-099, 101-105, 151-154, 201-207, A. Procedure NOTE : This procedure is written for the C/B-FUEL/L WING TK/PUMP 2 SPLY ____ 7QA with the C/B-FUEL/R WING TK/PUMP 2...
日期： 2011-03-28 13:49:56
FUEL - GENERAL - FAULT ISOLATION PROCEDURES ___________________________________________ TASK 28-00-00-810-801 Fuel Smell In Cabin WARNING : OBEY THE FUEL SAFETY PROCEDURES. _______ 1. Possible Causes _______________ - a fuel leak found bel...
日期： 2011-03-28 13:46:32
B. Do the test given in Para. 3. 5. Close-up________ A. Depressurize the Blue hydraulic system (Ref. AMM TASK 29-10-00-864-003). Loss of the Blue Hydraulic Pressure Transducer Signal for the ELAC 1 1. Possible Causes _______________ - ELAC...
日期： 2011-03-28 13:44:42
(7) On the Valveblock, do a check for circuit isolation. (a) For the POB solenoid connect the pins L K together. (b) Connect one test lead of the 45Vdc Isolation Tester to the pins LK and the other test lead to pin G. (c) Supply a test sig...
日期： 2011-03-28 13:42:00
TASK 27-00-00-810-801 Display of an Operational Warning on the Upper ECAM DU 1. Possible Causes _______________ - Message on the Post Flight Report (PFR) 2. Job Set-up Information ______________________ Not Applicable 3. Fault Confirmation...
日期： 2011-03-28 13:28:37
HIGHLIGHTS __________ REVISION NO. 30 Aug 01/05 Pages which have been revised are outlined below, together with the Highlights of the Revision CH/SE/SU C REASON FOR CHANGE EFFECTIVITY PAGES CHAPTER 26 L.E.P. 1- 3 REVISED TO REFLECT THIS RE...
日期： 2011-03-28 13:22:42
R TASK 24-22-00-810-823 R Failure of the GLC 1 or Loss of its Status Indication R 1. Possible Causes _______________ R - GCU-1 (1XU1) R - RELAY (20XU) R - GLC-1 (9XU1) R - wiring R 2. Job Set-up Information ______________________ R A. Refe...
