A320飞机维护手册 AMM FLIGHT CONTROLS 飞行操纵1(64)

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 SUBJECT_______  CH/SE/SU _ PAGE EFFECTIVITY
________ C ____ ___________ Detailed Visual Inspection of the 611 ALL Slat Track Rollers, the Pinions and the Curved Rack Gears (As Far As Visible) Check of Slat Transmission 620 ALL Shafting Integrity Including Inspection of Seal Witness Drains Operational Test of Wingtip 629 ALL Brakes/Pressure-Off Brakes, Followed by Check of Transmission Shafting Integrity and Inspection of Seal Witness Drains
 GEARBOX - BEVEL 19 DEG  27-84-41
 REMOVAL/INSTALLATION 401 ALL Removal of the Bevel Gearbox 401 ALL 6003CM Installation of the Bevel Gearbox 406 ALL 6003CM
 GEARBOX - TEE  27-84-42
 REMOVAL/INSTALLATION 401 ALL Removal of the Tee Gearbox 6005CM 401 ALL Installation of the Tee Gearbox 407 ALL 6005CM
 GEARBOX - BEVEL 63.5 DEG  27-84-43
 REMOVAL/INSTALLATION 401 ALL Removal of the Bevel Gearbox 63.5 401 ALL 6009CM, 6011CM (6059CM, 6061CM) Installation of the Bevel Gearbox 406 ALL
 63.5 6009CM, 6011CM (6059CM,
 6061CM)
 STEADY BEARING ASSY - TRANSMISSION 27-84-44

 REMOVAL/INSTALLATION  401 ALL Removal of the Steady Bearing FIN 401 ALL 6007CM(6057CM) Installation of the Steady Bearing 405 ALL FIN 6007CM(6057CM) Removal of the Steady Bearings FIN 410 ALL 6017CM(6067CM)/6019CM(6069CM) Installation of the Steady 414 ALL Bearings FIN 6017CM(6067CM)/6019CM(6069CM) Removal of the Steady Bearing FIN 419 ALL 6021CM(6071CM) Installation of the Steady Bearing 422 ALL FIN 6021CM(6071CM) Removal of the Steady Bearing FIN 427 ALL
 27-CONTENTS Page 40 Aug 01/05 R CES

 CHAPTER 27
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 FLIGHT CONTROLS
 TABLE OF CONTENTS
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 SUBJECT_______ CH/SE/SU _ PAGE EFFECTIVITY
________ C ____ ___________ 6023CM(6073CM) Installation of the Steady Bearing 430 ALL FIN 6023CM(6073CM) Removal of the Steady Bearing FIN 435 ALL 6025CM(6075CM) Installation of the Steady Bearing 438 ALL FIN 6025CM(6075CM) Removal of the Steady Bearing FIN 443 ALL 6031CM(6081CM) Installation of the Steady Bearing 446 ALL FIN 6031CM(6081CM)
 TORQUE SHAFT ASSY - TRANSMISSION 27-84-45
 REMOVAL/INSTALLATION 401 ALL Removal of the Torque Shaft 401 ALL 6002CM(6004CM) Installation of the Torque Shaft 406 ALL 6002CM(6004CM) Removal of the Torque Shaft 412 ALL 6006CM(6056CM) Installation of the Torque Shaft 415 ALL 6006CM(6056CM) Removal of the Torque Shaft 420 ALL 6008CM(6058CM) Installation of the Torque Shaft 423 ALL 6008CM(6058CM) Removal of the Torque Shaft 428 ALL 6010CM(6060CM) Installation of the Torque Shaft 433 ALL 6010CM(6060CM) Removal of the Torque Shaft 439 ALL 6012CM(6062CM) Installation of the Torque Shaft 443 ALL 6012CM(6062CM) Removal of the Torque Shafts 450 ALL 6014CM(6064CM)/6028CM(6078CM)/6036 6038CM(6088CM)/6040CM(6090CM)/6042 Installation of the Torque Shafts 453 ALL 6014CM(6064CM)/6028CM(6078CM)/6036 (6086CM)/6038CM(6088CM)/6040CM(609 M(6094CM) Removal of the Torque Shafts 461 ALL 6016CM(6066CM)/6020CM(6070CM)/6026 6030CM(6080CM) Installation of the Torque Shafts 464 ALL 6016CM(6066CM)/6020CM(6070CM)/6026 (6076CM)/6030CM(6080CM)
 27-CONTENTS Page 41 Aug 01/05 R CES

 CHAPTER 27
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 FLIGHT CONTROLS
 TABLE OF CONTENTS
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 SUBJECT_______ CH/SE/SU _ PAGE EFFECTIVITY
________ C ____ ___________ Removal of the Torque Shaft 470 ALL 6018CM(6068CM) Installation of the Torque Shaft 473 ALL 6018CM(6068CM) Removal of the Torque Shaft 478 ALL 6022CM(6072CM) Installation of the Torque Shaft 481 ALL 6022CM(6072CM) Removal of the Torque Shaft 487 ALL 6024CM(6074CM) Installation of the Torque Shaft 490 ALL 6024CM(6074CM) Removal of the Torque Shaft 497 ALL 6032CM(6082CM) Installation of the Torque Shaft A400 ALL 6032CM(6082CM) Removal of the Torque Shaft A406 ALL 6034CM(6084CM) Installation of the Torque Shaft A409 ALL 6034CM(6084CM) Removal of the Torque Shaft A415 ALL 6046CM(6096CM) Installation of the Torque Shaft A419 ALL 6046CM(6096CM)
 ACTUATOR ASSY - TYPE A 27-84-48
 REMOVAL/INSTALLATION 401 ALL Removal of the Type A Actuators 401 ALL 6013CM(6063CM)/6015CM(6065CM) Installation of the Type A 409 ALL Actuators 6013CM(6063CM)/6015CM(6065CM)
 ACTUATOR ASSY - TYPE B 27-84-49
 REMOVAL/INSTALLATION 401 ALL Removal of the Type B Actuators 401 ALL 6027CM(6077CM)/6029CM(6079CM)/6035 (6085CM)/6039CM(6089CM)/6045CM(609 Installation of the Type B 409 ALL Actuators 6027CM(6077CM)/6029CM(6079CM)/6035 (6085CM)/6039CM(6089CM)/6045CM(609 Removal of the Type B Actuators 419 ALL 6033CM(6083CM)/6037CM(6087CM)/6041 (6091CM) Installation of the Type B 425 ALL Actuators 6033CM(6083CM)/6037CM(6087CM)/
 27-CONTENTS Page 42 Aug 01/05 R CES

 CHAPTER 27
__________
 FLIGHT CONTROLS
 TABLE OF CONTENTS
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 SUBJECT_______ CH/SE/SU _ PAGE EFFECTIVITY
　
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