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...
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...
