• 热门标签

当前位置: 主页 > 航空资料 > 机务资料 >

时间:2011-03-21 13:44来源:蓝天飞行翻译 作者:admin
曝光台 注意防骗 网曝天猫店富美金盛家居专营店坑蒙拐骗欺诈消费者

 27-CONTENTS Page 25 Aug 01/05 R CES


 CHAPTER 27
__________
 FLIGHT CONTROLS
 TABLE OF CONTENTS
_________________
 SUBJECT_______ CH/SE/SU _ PAGE EFFECTIVITY
________ C ____ ___________ Bearings Actuator Track 1 6205CM(6255CM) 38 ALL Actuator Track 2 6211CM(6261CM) 54 ALL Actuator Track 3 6221CM(6271CM) 61 ALL Actuator Track 4 6233CM(6283CM) 68 ALL Flap Carriages 73 ALL Flap and Track Fairing Operating 77 301-399, Mechanism Inboard and Outboard Tab 77 301-399, Operating Mechanism
 Operation/Control and Indicating 78 ALL Hydraulic Actuation 78 ALL Power Transmission 79 001-049, 051-099
 101-149, 151-199 201-299, 401-499 Power Transmission 80 301-399, BITE 81 ALL
 FLAPS HYDRAULIC ACTUATION AND POWER 27-54-00
 TRANSMISSION

 ADJUSTMENT/TEST 501 ALL Operational Test of the Flap 501 ALL System Operational Test of the Flap and 506 ALL Slat Systems Adjustment of the LH (RH) Flap 512 051-052, 062-099 Drive System 106-149, 151-199
 204-299, 401-499
 FLAPS HYDRAULIC ACTUATION AND POWER 27-54-00
 TRANSMISSION

 INSPECTION/CHECK 601 ALL
 Detailed Visual Inspection of the 601 ALL
 Transmission Assembly (Including
 Part of the Transmission in Zone
 140)
 Check of the Integrity of the Flap 617 ALL
 Transmission System and Inspection
 of the Seal Witness Drains of the
 Wing Tip Brakes
 Check Flap Attachment Bearing No 1 624 051-051,
 for Liner Migration
 Detailed Dimensional Check - Free 630 ALL
 Movement at the Trailing Edge of

 27-CONTENTS Page 26 Aug 01/05 R CES


 CHAPTER 27
__________
 FLIGHT CONTROLS
 TABLE OF CONTENTS
_________________
 SUBJECT_______ CH/SE/SU _ PAGE EFFECTIVITY
________ C ____ ___________ the Flaps Detailed Inspection of Inboard A609 001-001, 051-052 Flap Trunnions for Evidence of Wear Marks Detailed Inspection of Inboard A615 ALL Flap Drive Trunnions in the Sliding Panel Hook Area For Wear.
 GEARBOX - RIGHT ANGLE 27-54-41
 REMOVAL/INSTALLATION 401 ALL
 Removal of the Right Angle Gearbox 401 ALL
 6203CM, (6253CM)
 Installation of the Right Angle 407 ALL
 Gearbox 6203CM, (6253CM)

 STEADY BEARING ASSY 27-54-44
 REMOVAL/INSTALLATION 401 ALL
 Removal of the Steady Bearings FIN 401 ALL
 6207CM(6257CM)/6213CM(6263CM)
 Installation of the Steady 405 ALL
 Bearings FIN
 6207CM(6257CM)/6213CM(6263CM)
 Removal of the Steady Bearings FIN 411 ALL
 6215CM(6265CM)/6219CM(6269CM)/6223
 (6273CM)/6225CM(6275CM)/6229CM(627
 Installation of the Steady 415 ALL
 Bearings FIN
 6215CM(6265CM)/6219CM(6269CM)/6223
 (6273CM)/6225CM(6275CM)/6229CM(627

 TORQUE SHAFT ASSY - TRANSMISSION 27-54-45
 REMOVAL/INSTALLATION 401 ALL
 Removal of the Torque Shaft 401 ALL
 6202CM(6252CM)
 Installation of the Torque Shaft 409 ALL
 6202CM(6252CM)
 Removal of the Torque Shaft 416 ALL
 6204CM(6254CM)
 Installation of the Torque Shaft 420 ALL
 6204CM(6254CM)
 Removal of the Torque Shaft 427 ALL
 6206CM(6256CM)
 Installation of the Torque Shaft 432 ALL
 6206CM(6256CM)
 Removal of the Torque Shaft 440 ALL
 6208CM(6258CM)
 Installation of the Torque Shaft 448 ALL
 6208CM(6258CM)
 Removal of the Torque Shaft 455 ALL

 27-CONTENTS Page 27 Aug 01/05 R CES


 CHAPTER 27
__________
 FLIGHT CONTROLS
 TABLE OF CONTENTS
_________________
 SUBJECT_______ CH/SE/SU _ PAGE EFFECTIVITY
________ C ____ ___________ 6210CM(6260CM) Installation of the Torque Shaft 459 ALL 6210CM(6260CM) Removal of the Torque Shaft 466 ALL 6212CM(6262CM) Installation of the Torque Shaft 471 ALL 6212CM(6262CM) Removal of the Torque Shafts 479 ALL 6214CM(6264CM)/6220CM(6270CM) Installation of the Torque Shafts 484 ALL 6214CM(6264CM)/6220CM(6270CM) Removal of the Torque Shafts 491 ALL 6216CM(6266CM)/6226CM(6276CM) Installation of the Torque Shafts 497 ALL 6216CM(6266CM)/6226CM(6276CM) Removal of Torque Shaft A406 ALL 6218CM(6268CM) Installation of the Torque Shaft A411 ALL 6218CM(6268CM) Removal of the Torque Shaft A419 ALL 6222CM(6272CM) Installation of the Torque Shaft A423 ALL 6222CM(6272CM) Removal of the Torque Shafts A431 ALL 6224CM(6274CM)/6230CM(6280CM) Installation of the Torque Shafts A436 ALL 6224CM(6274CM)/6230CM(6280CM) Removal of the Torque Shaft A443 ALL 6228CM(6278CM) Installation of the Torque Shaft A447 ALL 6228CM(6278CM) Removal of the Torque Shaft A455 ALL 6232CM(6282CM) Installation of the Torque Shaft A460 ALL 6232CM(6282CM)
 
中国航空网 www.aero.cn
航空翻译 www.aviation.cn
本文链接地址:A320飞机维护手册 AMM FLIGHT CONTROLS 飞行操纵1(59)