CHAPTER 27
__________
FLIGHT CONTROLS
TABLE OF CONTENTS
_________________
SUBJECT_______ CH/SE/SU _ PAGE EFFECTIVITY
________ C ____ ___________ WTB Solenoids
Refer to the MMEL TASK: 27-51-02 422 ALL
Reactivation of the SFCC 2 Flap 426 ALL
WTB Solenoids
Refer to the MMEL TASK: 27-51-02 426 ALL
FLAPS ELECTRICAL CONTROL AND 27-51-00
MONITORING
ADJUSTMENT/TEST 501 ALL Read-out of Class 3 Faults in the 501 ALL Flap System Bite Test of the Slat and Flap 503 ALL Control Computers (Flap System) Operational Test of the Wing Tip 508 ALL Brake and the Pressure Off Brake Operational Test of the Wing Tip 514 ALL Brake and the Pressure Off Brake with the Ground Power Cart Operational Test of the Wing Tip 523 ALL Brake and the Pressure Off Brake with the Engine Driven Pumps Manual Adjustment of the Position 532 ALL Pick-Off Units Operational Test of the Flap 537 ALL Interconnecting Strut and the Flap-Attachment Failure-Detection Sensors Automatic Integrity Test of the 547 ALL Slat and Flap Control Computers To Do a Check of the Flap Rigged 551 ALL Position (With the Sharks Fin) Adjustment of the Forward 595 ALL Eccentrics to the Datum Position Adjustment of the Flap Rigged A501 001-049, 051-099 Position With the Sharks Fin Tool 101-149, 151-199 (A318/319/320) 201-299, 401-499 Adjustment of the Flap Rigged A584 301-399, Position With the Sharks Fin Tool (A321)
SENSOR FLAP ATTACHMENT FAILURE 27-51-15
DETECTION
REMOVAL/INSTALLATION 401 ALL
Removal of the Proximity-Sensors 401 ALL
of the Interconnecting Strut
Installation of the 403 ALL
27-CONTENTS Page 23 Aug 01/05 R CES
CHAPTER 27
__________
FLIGHT CONTROLS
TABLE OF CONTENTS
_________________
SUBJECT_______ CH/SE/SU _ PAGE EFFECTIVITY
________ C ____ ___________ Proximity-Sensors of the Interconnecting Strut
COMMAND SENSOR UNIT (CSU) 27-51-17
REMOVAL/INSTALLATION 401 ALL Removal of the Command Sensor Unit 401 ALL (CSU) (51CV) Installation of the Command Sensor 404 ALL Unit (CSU) (51CV)
COMMAND SENSOR UNIT (CSU) 27-51-17
INSPECTION/CHECK 601 ALL Removal and Workshop Check of the 601 ALL Friction Brake of the Flap/Slat Command Sensor Unit (CSU)
POSITION PICK OFF UNIT - ASYMMETRY 27-51-18
(APPU)
REMOVAL/INSTALLATION 401 ALL Removal of the Asymmetry-Position 401 ALL Pick-Off Unit 29CV (30CV) Installation of the 407 ALL Asymmetry-Position Pick-Off Unit 29CV (30CV)
POSITION PICK - OFF UNIT - FEED BACK 27-51-19
(FPPU)
REMOVAL/INSTALLATION 401 ALL Removal the Feed Back Position 401 ALL Pick-Off Unit Installation of the Feed Back 404 ALL Position Pick-Off Unit
COMPUTER - SLAT AND FLAP CONTROL 27-51-34
(SFCC)
REMOVAL/INSTALLATION 401 ALL Removal of the SFCC (21CV, 22CV) 401 ALL Installation of the SFCC (21CV, 404 ALL 22CV)
LEVER - FLAP AND SLAT CONTROL 27-51-43
REMOVAL/INSTALLATION 401 ALL Removal of the Flap and Slat 401 ALL Control Lever Installation of the Flap and Slat 405 ALL Control Lever Removal of the Lighted Plate 408 ALL Installation of the Lighted Plate 411 ALL
STRUT - INTERCONNECTING 27-51-44
REMOVAL/INSTALLATION 401 ALL Removal of the Interconnecting 401 ALL Strut
27-CONTENTS Page 24 Aug 01/05 R CES
CHAPTER 27
__________
FLIGHT CONTROLS
TABLE OF CONTENTS
_________________
SUBJECT_______ CH/SE/SU _ PAGE EFFECTIVITY
________ C ____ ___________ Installation of the 408 ALL Interconnecting Strut Removal of the Proximity-Sensor of 423 ALL the Interconnecting Strut Installation of the 430 ALL Proximity-Sensor of the Interconnecting Strut
STRUT - INTERCONNECTING 27-51-44
ADJUSTMENT/TEST 501 ALL Adjustment of the Interconnecting 501 ALL Strut
STRUT - INTERCONNECTING 27-51-44
INSPECTION/CHECK 601 ALL Detailed Visual Inspection of the 601 ALL Flap Interconnecting Strut and Attachments Replacement of the Flap 616 ALL Interconnecting Strut Rod-End
BRAKE - WING TIP (WTB) 27-51-51
REMOVAL/INSTALLATION 401 ALL Removal of the Flap Wing-Tip Brake 401 ALL Installation of the Flap Wing-Tip 407 ALL Brake Removal of the Solenoid Valves of 421 ALL the Flap Wing-Tip Brake (WTB) Installation of the Solenoid 426 ALL Valves of the Flap Wing-Tip Brake (WTB)
FLAPS HYDRAULIC ACTUATION AND POWER 27-54-00 TRANSMISSION
DESCRIPTION AND OPERATION 1 ALL General 1 ALL Component Location 1 ALL System Description 7 ALL
Hydraulic Actuation 7 ALL
Power Transmission 9 ALL Power Supply 17 ALL Interface 17 ALL Component Description 17 ALL
Power Control Unit 17 ALL Right Angle Gearbox 30 ALL 6203CM(6253CM) Line Gearbox 6209CM(6259CM) 30 ALL Bevel Gearbox 6217CM(6267CM) 30 ALL Torque Shafts and Steady 34 ALL
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(58)
