日期： 2011-03-27 00:08:25
R R R 1. On the ECAM control panel, push the DOOR key: 2. On the circuit breaker panel 121VU: - open the circuit breaker 2WV. - open the circuit breakers 15WN and 2WW. 3. On the circuit breaker panel 121VU: - close the circuit breakers 2WV...
日期： 2011-03-27 00:06:38
R 1EFF : 001-049, 051-099, 101-149, 151-199, 1 52-42-00Page 414 1201-299, 1May 01/05 1 1 1CES 1R **ON A/C 106-149, 151-199, 201-299, 301-399, 401-499, Subtask 52-42-00-860-051 B. Put the aircraft back to its initial configuration. (1) Set...
日期： 2011-03-27 00:00:11
R **ON A/C 401-499, R 52-32-21-991-019-C Fig. 403C **ON A/C 001-049, 053-099, 101-105, 201-220, 52-32-21-991-017 Fig. 417 **ON A/C 106-149, 221-299, 301-399, 52-32-21-991-017-B **ON A/C 151-199, Fig. 417A R 52-32-21-991-017-A **ON A/C 401-...
日期： 2011-03-26 23:57:46
1EFF : ALL 1 52-32-00Page 71 1 1 Aug 01/05 1 1 1CES 1 The sequence shaft operates the link assy at the same time so that the target lever moves to the door sill. The related target operates the proximity switch 32WV (Ref. 52-71-00). When t...
日期： 2011-03-26 23:54:35
3. Job Set-up __________ Subtask 52-30-00-860-050 A. Aircraft Maintenance Configuration (1) Make sure that the Yellow hydraulic system reservoir is pressurized (Ref. TASK 29-14-00-614-002). (2) Make sure that the level of the hydraulic flu...
日期： 2011-03-26 23:52:04
4. Procedure _________ Subtask 52-13-31-020-051 A. Removal of the Stop Fittings (Ref. Fig. 402/TASK 52-13-31-991-002) (1) Remove the old sealant with CLEANING AGENTS (Material No. 11-004), MISCELLANEOUS (Material No. 19-003) and a non meta...
日期： 2011-03-26 23:42:34
(b) With the door in the down position (door closed and locked): -make sure that the clearance J11 between the frame structure and the safety pin is 4 -1 +1 mm (0.1574 -0.0393 +0.0393 in.). (c) If the clearances J10 and J11 are not in the...
日期： 2011-03-26 23:38:56
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 52 L.E.P. 1-33 REVISED TO REFLECT THIS RE...
日期： 2011-03-26 14:51:29
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 51 L.E.P. 1- 2 REVISED TO REFLECT THIS RE...
日期： 2011-03-26 14:47:34
| high | | ----+----------------------------------------+-------------------------+------- ------------------------------------------------------------------------------- FCN | Fault Description | CFDS Message | Class ----+----------------...
日期： 2011-03-26 14:43:57
______________________ A. Fixtures, Tools, Test and Support Equipment -------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ----------------------------------------------------------------...
日期： 2011-03-26 14:41:53
Subtask 49-23-51-865-059 B. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): 1KD, 2KD. Subtask 49-23-51-710-051 C. Do the operational test of the APU (Ref. TASK 49-00-00-710-008). (1) Do a check for leaks...
日期： 2011-03-26 14:39:37
R EFF : 001-049, 101-105, 107-107, 151-199, 49-16-41Page 408 201-210, Config-2 Aug 01/05 CES DIVERTER - REMOVAL/INSTALLATION _______________________________ TASK 49-16-41-000-004 Removal of the fixed APU Diverter (APS 3200) 1. Reason for t...
日期： 2011-03-26 14:35:49
5. Close-up ________ Subtask 49-11-00-410-051 A. Close Access (1) Make sure that the work area is clean and clear of tool(s) and other items. (2) Set the LIGHT control switch 11LJ to the off position. (3) Close the APU access doors 315AL,...
日期： 2011-03-26 14:32:10
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 49 L.E.P. 1-24 REVISED TO REFLECT THIS RE...
日期： 2011-03-26 09:26:44
F E E C F M 『EE E E 56-5B EE 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 80 L.E.P. 1...
日期： 2011-03-26 09:24:29
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 46 L.E.P. 1- 4 REVISED TO REFLECT THIS RE...
日期： 2011-03-26 09:21:43
B. Vacuum Generator 37MG (1) The vacuum generator is connected to the aircraft power circuit through the motor starting relay (36MG). The generator operates: -At ground level and up to an altitude of 5487 m (18000 ft.) (the altitude pressu...
日期： 2011-03-26 09:18:42
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 38 L.E.P. 1- 8 REVISED TO REFLECT THIS RE...
日期： 2011-03-26 09:15:36
1EFF : ALL 1 36-11-49Page A413 1 1 Nov 01/04R 1 1 1CES 1 (7) Tighten the bolts (20) sufficiently to hold the duct in position. Do not torque the bolts at this time. (8) Make sure that the fifth stage elbow duct (25) is in the correct posit...
