日期： 2011-03-25 17:44:05
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 32 L.E.P. 1-35 REVISED TO REFLECT THIS RE...
日期： 2011-03-25 12:29:41
Subtask 31-63-22-020-052 B. Removal of the ND CAPT (3WT1) (1) Push in the two locking catches (4). (2) If necessary, push up the handle (3) to decrease the load applied to the locking catches (4): the handle falls to the level of the studs...
日期： 2011-03-25 12:26:34
5. Close-up ________ Subtask 31-55-34-410-050 A. Close Access (1) Make sure that the work area is clean and clear of tool(s) and other items. R (2) Close the access door 824 (Ref. TASK 52-41-00-410-002). (3) Remove the access platform(s)....
日期： 2011-03-25 12:22:57
R 1. On the panel 121VU : R - open the circuit breaker 2WV . - on the upper ECAM DU: R * the FWS SDAC2 FAULT warning message R comes into view. R - open the circuit breaker 44WV. * the ELEC DC BUS2 FAULT warning R message comes into view....
日期： 2011-03-25 12:19:27
+---------------------------------------------------------------------+ | Value | Content Description | |--------------|------------------------------------------------------| R |--------------|---------------------------------------------...
日期： 2011-03-25 12:16:53
3. Job Set-up __________ Subtask 31-36-00-860-061 A. Aircraft Maintenance Configuration (1) Energize the aircraft electrical circuits (Ref. TASK 24-41-00-861-002) (2) Energize the CFDS. R 1EFF : 001-049, 051-099, 101-105, 151-199, 1 31-36-...
日期： 2011-03-25 12:14:46
(4) Remove the QAR (1) from its rack (3). (5) Put blanking caps on the disconnected electrical connectors (2). R 1EFF : 001-049, 051-099, 101-105, 1 31-33-52Page 402 1 1 May 01/05 1 1 1CES 1 Quick Access Recorder (QAR) Figure 401/TASK 31-3...
日期： 2011-03-25 12:12:39
(e) Structure of the BITE system pages (example with TROUBLE SHOOTING DATA of SDAC 1) ------------------------------------------------------------------| Character | Content | ---------------------------------------------------------------...
日期： 2011-03-25 12:08:48
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 31 L.E.P. 1-34 REVISED TO REFLECT THIS RE...
日期： 2011-03-24 08:57:45
-------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------- 24-41-00-861-002 Energize the Aircraft Electrical Circuits...
日期： 2011-03-24 08:55:33
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 30 L.E.P. 1- 7 REVISED TO REFLECT THIS RE...
日期： 2011-03-24 08:43:41
BLUE AUXILIARY HYDRAULIC POWER (RAM AIR TURBINE) - REPAIRS __________________________________________________________ R **ON A/C 062-099, 106-149, 151-199, 204-299, 301-399, 401-499, TASK 29-22-00-300-001 Repair of the Blades of the Ram Ai...
日期： 2011-03-24 08:41:32
5. Close-up ________ Subtask 29-14-00-860-051 A. Put the aircraft back to the serviceable condition. (1) Close the ground connector and disconnect the ground air supply. (2) Install the blanking cap on the ground connector. (3) Remove the...
日期： 2011-03-24 08:39:35
B. Installation of the PTU Manifold CAUTION : USE A SECOND WRENCH TO APPLY COUNTERTORQUE TO THE UNION WHEN _______ YOU DISCONNECT/CONNECT HYDRAULIC LINES ON UNIONS. IF YOU USE THE SECOND WRENCH, YOU WILL NOT LOOSEN OR TIGHTEN THE UNION TOO...
日期： 2011-03-24 08:37:35
Subtask 29-11-52-865-050 C. Open, safety and tag this(these) circuit breaker(s): -------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION ---------------------------------------------...
日期： 2011-03-24 08:35:12
Subtask 29-10-00-210-060 B. Do a Check of the Filters in the Green Hydraulic System (1) For the low pressure (return) filter (1002GM): (a) Make sure that the red indicator button is not out. If the red indicator button is out, do these ste...
日期： 2011-03-24 08:31:30
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. 1-20 REVISED TO REFLECT THIS RE...
日期： 2011-03-22 07:05:47
- install 540AB, 540BB, 540CB, 540DB, 540EB, 540FB, 540GB, 540HB, 540JB, 574BB FOR 14QT2 - install 640AB, 640BB, 640CB, 640DB, 640EB, 640FB, 640GB, 640HB, 640JB, 674BB. (3) Remove the HOOK-COVER (RIB 2 SURGE DOORS) and carefully close the...
日期： 2011-03-22 07:03:53
R 1EFF : 301-399, 1 28-42-00Page 54 1 1 May 01/04 1 1 1CES 1 R ------------------------------------------------------------------------------- R | PARAMETER LIST PARAMETER CHARACTERISTICS (NUMERIC) | R -------------------------------------...
日期： 2011-03-22 06:55:48
B. Aircraft Maintenance Configuration (1) Energize the aircraft electrical circuits (Ref. TASK 24-41-00-861-002). (2) Do the EIS start procedure (ECAM only) (Ref. TASK 31-60-00-860-001). 4. Procedure _________ R **ON A/C 001-049, 051-099,...
