日期： 2011-03-22 06:52:35
-------------------------------------------------------------------------------ACTION RESULT ------------------------------------------------------------------------------- -release (out) the X FEED - the X FEED P/BSW ON and OPEN lights P/...
日期： 2011-03-22 06:49:13
15. R **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 401-499, 5. Close-up ________ Subtask 28-12-41-410-055 A. Close Access (1) Make sure that the work area is clean and clear of tool(s) and other items. (2) Install the applicable a...
日期： 2011-03-22 06:45:17
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 28 L.E.P. 1-23 REVISED TO REFLECT THIS RE...
日期： 2011-03-22 06:40:26
the RAT extension command is generated - the AC and DC essential busbars are immediately supplied by the batteries. -after 7s the AC and DC essential busbars are supplied by the standby generator. The RAT extension can be manually controll...
日期： 2011-03-21 14:35:05
1EFF : ALL 1 27-84-45Page 459 1 1 Feb 01/00R 1 1 1CES 1 INTENTIONALLY BLANK R 1 1 27-84-45Page 460 1 1 Feb 01/00 1 1 1CES 1 TASK 27-84-45-000-007 Removal of the Torque Shafts 6016CM(6066CM)/6020CM(6070CM)/6026CM(6076CM)/ 6030CM(6080CM) WAR...
日期： 2011-03-21 14:32:13
DO NOT CAUSE DAMAGE TO THE ELECTRICAL CABLE RACEWAYS. - DO NOT CAUSE DAMAGE TO THE ELECTRICAL CABLE INSTALLATIONS. -MAKE SURE THAT THE ELECTRICAL CABLES ARE INSTALLED CORRECTLY. INCORRECT INSTALLATION CAN CAUSE DAMAGE. 1. Reason for the Jo...
日期： 2011-03-21 14:21:32
R 1EFF : 159-199, 211-212, 1 27-54-55Page 451 1 1 Aug 01/05 1 1 1CES 1 R (k) If necessary, drill a 2.5 mm (0.10 in.) hole for the cotter pin R (37) in an applicable position on the bearing housing (34). R Remove all unwanted material from...
日期： 2011-03-21 14:18:04
F. Connect the Flap Drive Arms (1) At the track 3 position: (a) Connect the flap drive arm to the rotary actuator drive-lever with the bolt (226), the washer (229) and the nut (230). (b) TORQUE the nut (230) to between 10.0 and 12.0 m.daN...
日期： 2011-03-21 14:12:39
1_ For the flap track No.1 torque limiter: - 193AB, 193BB - 573BB (Ref. TASK 57-51-37-400-002). 2_ For the flap track No.2 torque limiter: - 573AB, 573BB (Ref. TASK 57-51-37-400-002). 3_ For the flap track No.3 torque limiter: - 575BB, 575...
日期： 2011-03-21 13:53:58
B. Consumable Materials ------------------------------------------------------------------------------- REFERENCE DESIGNATION ------------------------------------------------------------------------------- R Material No. 02-003 F NSA 30711...
日期： 2011-03-21 13:47:25
R **ON A/C 106-149, 159-199, 211-299, 301-399, 401-499, Subtask 27-21-41-010-050-B F. Get Access (1) Put the access platform in position. (2) Open the access panels 325BL, 325BR, 325CL, 325CR, 325DL and remove the access panels 325EL, 325E...
日期： 2011-03-21 13:44:15
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 27 L.E.P. 1-38 REVISED TO REFLECT THIS RE...
日期： 2011-03-21 08:43:02
Engine 1(2) Fire Extinguishing Circuit - Schematic Figure 006 1EFF : ALL 1 26-21-00 Page 20 1 1 Nov 01/03 1 1 1CES 1 When you press the TEST pushbutton switch, the FIRE warning indications are triggered and you check the condition of the f...
日期： 2011-03-21 08:41:02
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- 7 REVISED TO REFLECT THIS RE...
日期： 2011-03-21 08:32:10
5. Close-up ________ Subtask 25-54-11-410-050 A. Put the aircraft back to the serviceable condition. (1) Make sure that the work area is clean and clear of tool(s) and other items. Subtask 25-54-11-865-052 B. Remove the safety clip(s) and...
日期： 2011-03-21 08:27:50
Upper Attachment of the Galley 6475MM at Location 1 Figure 403/TASK 25-31-41-991-018 R EFF : 001-049, 101-105, 25-31-41 Page 422 May 01/05 CES DAMAGED OR INJURE PERSONNEL. THE UNIT/ASSEMBLY IS HEAVY. 1_ Carefully lift the galley off the bl...
日期： 2011-03-21 08:24:35
R E. Do the Test of the Restraint System. NOTE : Do this test if no inertia reel is installed.____ (1) Make sure that the buckle locks/unlocks correctly. R R (2) Make sure that you can adjust the length of the belt assy correctly. 5. Close...
日期： 2011-03-21 08:20:02
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 25 L.E.P. 1-20 REVISED TO REFLECT THIS RE...
日期： 2011-03-21 08:16:53
__________ Subtask 24-24-34-860-052 A. Aircraft Maintenance Configuration (1) Make sure that the ground service network is energized (Ref. TASK 24-42-00-861-001). (2) Make sure that the warning notice is in the cockpit, on the EMER ELEC PW...
日期： 2011-03-21 08:13:14
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 24 L.E.P. 1-12 REVISED TO REFLECT THIS RE...
