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...
日期： 2011-03-26 09:12:31
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 36 L.E.P. 1- 9 REVISED TO REFLECT THIS RE...
日期： 2011-03-26 09:06:11
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 35 L.E.P. 1- 6 REVISED TO REFLECT THIS RE...
日期： 2011-03-26 00:27:37
ISO: data word coded in ISO5 code DIS: discrete data word HEX: hexadecimal coded HYB: mixed code -ALPHA CODE: indicates the parameter mnemonic code, -SOURCE ORIGIN: parameter source computer or system. -------------------------------------...
日期： 2011-03-26 00:16:56
(c) GPS/FMS position disagreement When GPS Primary is active and either FMGC 1 or FMGC 2 latitude (longitude) deviates from either MMR 1 or MMR 2 latitude (longitude) by more than 0.5 Nm, the NAV FMS/GPS POS DISAGREE and A/C POS..............
日期： 2011-03-26 00:13:34
R (2) ADIRU 3 R (a) Aircraft with Trim = 0ft R -------------------------------------------------------- R | | CAPT PFD and F/O PFD | R | Pressure generator | AIR DATA switch | R | | at CAPT/3 or F/O/3 | R |------------------------------|--...
日期： 2011-03-26 00:09:57
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 34 L.E.P. 1-18 REVISED TO REFLECT THIS RE...
日期： 2011-03-26 00:07:23
Subtask 33-41-15-941-051 B. Put the ACCESS PLATFORM 3M (10 FT)- ADJUSTABLE in position at the APU tail-cone-exhaust area, Zone 317. 4. Procedure_________ (Ref. Fig. 402/TASK 33-41-15-991-002) Subtask 33-41-15-020-052 A. Removal of the Lamp...
日期： 2011-03-26 00:04:47
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. 1-10 REVISED TO REFLECT THIS RE...
日期： 2011-03-26 00:00:43
1EFF : 001-004, 051-054, 1 32-51-00Page 563 1 1 Aug 01/05R 1 1 1CES 1 (6) Install the RVDT 4GC (16) (Ref. TASK 32-51-19-400-001) -engage the spigot (20) in the hole (21) on the ADJUSTING TOOL - NWS GEARBOX (13), -make sure that it is flush...
日期： 2011-03-25 23:58:18
4. Procedure _________ (Ref. Fig. 401/TASK 32-45-52-991-002) Subtask 32-45-52-020-050 A. Removal of the Rotary Switch (1) Remove the screw (5), the pin (4), and the knob (3). (2) Loosen the four Dzus fasteners (2) from the panel 110VU (1)...
日期： 2011-03-25 18:04:55
R **ON A/C 002-049, 053-099, 101-149, 151-199, 201-299, 301-399, Subtask 32-42-13-560-050-A D. Preparation of the Replacement Component (1) Remove the unions (3). Remove and discard the packings (4) from the unions (3). (2) Remove the rest...
日期： 2011-03-25 18:01:25
B. Installation of the Control Handle (1) Remove the cotter pin (30) and discard it, then remove the nut (29) and the washer (28). (2) Remove the bolt (22) and disconnect the rod (25). (3) Cut and remove the lockwire and loosen the check n...
日期： 2011-03-25 17:58:35
1EFF : ALL 1 32-31-44Page 412 1 1 May 01/04R 1 1 1CES 1 (c) Turn the eye end IN or OUT until the Dimension X is reached. (d) Tighten the eye end-lock nut and Torque to 14.6 m.daN (107.66 lbf.ft). (e) Safety the eye end with MISCELLANEOUS (...
日期： 2011-03-25 17:55:29
4. Procedure _________ **ON A/C 001-049, 051-061, 101-105, 201-203, (Ref. Fig. 602/TASK 32-22-00-991-003) 1EFF : ALL 1 32-22-00Page 607 1 1 Aug 01/05 1 1 1CES 1 NLG Doors - Gaps Figure 602/TASK 32-22-00-991-003- 12 (SHEET 1) R 1EFF : 001-0...
日期： 2011-03-25 17:53:04
Door and Fairings Figure 001 1EFF : ALL 1 32-12-00 Page 2 1 1 Feb 01/98 1 1 1CES 1 MLG Fairings Figure 002 1EFF : ALL 1 32-12-00 Page 3 1 1 Feb 01/98 1 1 1CES 1 MLG Main Door - Fittings Figure 003 1EFF : ALL 1 32-12-00 Page 4 1 1 Feb 01/98...
日期： 2011-03-25 17:50:24
Subtask 32-11-12-860-053 B. Aircraft Maintenance Configuration (1) Disconnect the isolation coupling of the PTU (Ref. TASK 29-23-00-860-001). (2) Make sure that the Yellow and Green hydraulic systems are depressurized (Ref. TASK 29-00-00-8...
