日期： 2011-03-20 21:18:19
On the FWD AIP 320RH: - the CNCL AFT L message goes off. On the AFT LH AIP 320RH: - the OVER CAPTAIN message goes off. On the AFT RH AIP 320RH: - the CALL CAPTAIN message goes off.On the Capt audio selector panel: - the CAB rotary-knob int...
日期： 2011-03-20 21:14:47
(3) On the maintenance panel 50VU, make sure that the SVCE INT OVRD pushbutton switch is not pushed. (4) On the overhead control and indicating panel 48VU, make sure that the AUDIO SWITCHING selector switch is in the NORM position. R 1EFF...
日期： 2011-03-20 21:11:50
- the cursor moves to the MEMO 2 display. -after not many seconds the READY light comes on. In the cabin: - the prerecorded announcement 1 is heard from all the passenger and the lavatory loudspeakers. At the selected PCU's: - the prerecor...
日期： 2011-03-20 21:06:50
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 23 L.E.P. 1-19 REVISED TO REFLECT THIS RE...
日期： 2011-03-20 21:03:35
(c) Optimum altitude The optimum altitude is displayed on the PROG page. It is computed by taking into account the active strategic mode (including the cost index if it is ECON), the predicted aircraft and atmospheric conditions. The optim...
日期： 2011-03-20 20:57:22
On the portable data loader: - the MDDU READY indication is shown. - the power-up test of the FMGC 1 starts. -at the end of this test, the triple click aural warning sounds. On the portable data loader: -the TRANS IN PROG indication is sho...
日期： 2011-03-20 20:51:20
(c) Aural warning (single chime). (d) THR LK message flashing on the two PFDs if, upon disengagement, the thrust is frozen on at least one engine (THR LK = thrust lock). In addition, the A/THR engage pushbutton switch goes off on the FCU a...
日期： 2011-03-20 20:47:27
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 22 L.E.P. 1-13 REVISED TO REFLECT THIS RE...
日期： 2011-03-20 12:25:58
EFFECTIVITY AF 160,162-171,183,184 799 Page 409 34-43-03 Sep 25/94 (4) Put dust caps on the waveguide flanges. 6. AF 160, 162-171, 183, 184; Weather Radar Antenna Flat Plate Removal (Fig. 404) ________________________________________ A. En...
日期： 2011-03-20 12:20:14
EFFECTIVITY AIRPLANES WITH DELCO INS CONFIG 1 03 A Page 101 Apr 25/8634-41-00 E. On airplanes with PMS, when the INS is in the PMS waypoint control mode, the INS responds to all data received from the PMS and rejects all data inserted at...
日期： 2011-03-20 12:17:43
1 B XFR RLY VOR/ILS Power Block Diagram Figure 3 (Sheet 3) EFFECTIVITY CONFIG 1 AF 152-154,172-173,191-194; 799 Page 20 GN ALL; MD ALL 34-31-00 Dec 25/85 F/O VOR/ILS RECEIVER 2 1B XFR RLY VOR/ILS Power Block Diagram Figure 3 (Sheet 4) EFFE...
日期： 2011-03-20 12:12:31
CHAPTER 34 - NAVIGATION TABLE OF CONTENTS _________________ Chapter Section Subject_______ Subject ____ Effectivity _______ Page ___________ NAVIGATION 34-00-00 __________ Description and Operation 1 CONFIG 1 [*] General 1 [*] AZ ALL LH AL...
日期： 2011-02-24 09:55:35
up to 180 DEG.C (385 DEG.F) | normal operation | |--------------------------------------|-------------------------------------| | 180 DEG.C (385 DEG.F) to | tempearture range in case of ram | | 215 DEG.C (419 DEG.F) | air inlet is fully op...
日期： 2011-02-24 09:51:27
AIR COOLING SYSTEM - REMOVAL/INSTALLATION _________________________________________ TASK 21-52-00-920-001 R Removal and Replacement of the Combo and Periseals in the Air Conditioning Pack R Ducts 1. Reason for the Job __________________ Re...
日期： 2011-02-24 09:47:21
OUTFLOW VALVE 21-31-51 OFV electronic box 1 fault ELECTRONIC 1 (XX) OUTFLOW VALVE 21-31-51 OFV electronic box 2 fault ELECTRONIC 2 (XX) OUTFLOW VALVE FEEDBACK 21-31-51 OFV feedback module fault ASSY (XX) OUTFLOW VALVE 21-31-51 OFV fault (m...
日期： 2011-02-24 09:37:45
R 1EFF : 001-049, 051-058, 101-101, 1 21-26-00Page 203 1 1 May 01/05 1 1 1CES 1 R R Deactivation of the Valves Figure 201/TASK 21-26-00-991-007- 14 (SHEET 1) 1EFF : 1 1 1CES ALL 1 111 21-26-00 Page 204 Nov 01/02 R R Deactivation of the Val...
日期： 2011-02-24 09:22:28
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 21 L.E.P. 1-21 REVISED TO REFLECT THIS RE...
日期： 2011-02-24 09:14:44
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 20 L.E.P. 1- 5 REVISED TO REFLECT THIS RE...
日期： 2011-02-12 09:19:48
LUBRICATION - DESCRIPTION AND OPERATION _______________________________________ 1. General _______ The lubrication instructions define: -Specification of the lubricant to be used -Points to be lubricated - Special precautions to be observe...
日期： 2011-02-12 09:03:14
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 11 L.E.P. 1- 5 REVISED TO REFLECT THIS RE...
