A320飞机维护手册 AMM FLIGHT CONTROLS 飞行操纵1(56)

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 CABLES - THS CONTROL 27-41-44
 REMOVAL/INSTALLATION 401 ALL Removal of the THS Control Cables 401 ALL Installation of the THS Control 425 ALL Cables
 DRIVE SHAFT - MECHANICAL INPUT 27-41-45
 REMOVAL/INSTALLATION 401 ALL Removal of the Mechanical Input 401 ALL Drive Shaft Assy Installation of the Mechanical 410 ALL Input Drive Shaft Assy
 THS HYDRAULIC ACTUATION 27-44-00
 DESCRIPTION AND OPERATION 1 ALL General 1 ALL Component Location 1 ALL System Description 1 ALL Power Supply 6 ALL Component Description 6 ALL Hydraulic Motors 6 ALL Fail-Safe Ball Screw-Jack 6 ALL Control Valve Blocks 7 ALL Gearbox 7 ALL Pressure-Off Brakes 8 ALL Pitch Trim Actuator 8 ALL Position Transducer 8 ALL Structural Components 8 ALL Line Replaceable Units (LRU) 9 ALL Technical Data 9 ALL
 Operation 10 ALL Normal Operation 10 ALL Mechanical Control Operation 14 ALL Ground Operation from the 14 ALL Electric Pumps Operation in Failure Conditions 14 ALL
 Test 15 ALL Ground Test 15 ALL
 THS HYDRAULIC ACTUATION 27-44-00
 ADJUSTMENT/TEST 501 ALL

 27-CONTENTS Page 17 Aug 01/05 R CES

 CHAPTER 27
__________
 FLIGHT CONTROLS
 TABLE OF CONTENTS
_________________
 SUBJECT_______ CH/SE/SU _ PAGE EFFECTIVITY
________ C ____ ___________ Operational Test of the Jamming 501 ALL Protection Device of the Trimmable Horizontal Stabilizer Actuator Operational Test of the Trimmable 522 ALL Horizontal Stabilizer Actuator with the Individual Hydraulic Systems Operational Test of the Trimmable 526 ALL Horizontal Stabilizer Actuator with both (Green and Yellow) and Individual Hydraulic Systems
 ACTUATOR - THS 27-44-51
 REMOVAL/INSTALLATION 401 ALL Removal of the Trimmable 401 ALL Horizontal Stabilizer (THS) Actuator (9CE) Installation of the Trimmable 417 ALL Horizontal Stabilizer (THS) Actuator (9CE) Removal of the Oil Filler Plug 434 ALL and/or the Oil Drain Plug from the THS Actuator (9CE) Installation of the Oil Filler 438 ALL Plug and/or the Oil Drain Plug in the THS Actuator (9CE) Removal of the Lower Claw Stop 443 ALL Installation of the Lower Claw 448 ALL Stop
 ACTUATOR - THS 27-44-51
 ADJUSTMENT/TEST 501 ALL Operational Test of the No-Back 501 ALL Device (No-Back Pawls)
 ACTUATOR - THS 27-44-51
 INSPECTION/CHECK 601 ALL Visual Inspection of the 601 ALL THS-Actuator Detailed Visual Inspection of the 605 ALL the Ball-Screw Nut Body, the Screw and the Claw Stops of the THS-Actuator Visual Check of the Threaded 610 ALL (Fail-Safe) Nut Check the Indicator of the No-Back 612 ALL Wear Detection-Device of the THS-Actuator Check the Integrity of the Ball 616 ALL
 27-CONTENTS Page 18 Aug 01/05 R CES

 CHAPTER 27
__________
 FLIGHT CONTROLS
 TABLE OF CONTENTS
_________________
 SUBJECT_______ CH/SE/SU _ PAGE EFFECTIVITY
________ C ____ ___________ Screw Shaft (Primary and Secondary Load Paths) of the THS-Actuator Detailed Visual Inspection of the 620 ALL Upper and the Lower Attachments (Primary and Secondary) of the THS-Actuator Check the Oil Level of the Gearbox 623 ALL of the THS-Actuator Check the Backlash between the 630 ALL Ball Screw Nut and Screw of the THS-Actuator Inspection of the Magnetic Chip 635 ALL Detector and Boroscope Inspection of the Power Gear of the THS-Actuator Drain and Refill the Trimable 641 ALL Horizontal Stabilizer Actuator Gearbox Inspection of the THS Actuator 646 001-049, 051-099 Lower Attachment for the Integrity 101-105, 151-199 of the Secondary Load Path and 201-228, 301-302 Check the Gap at the Secondary Nut Trunnion
 MOTOR - THS ACTUATOR 27-44-53
 REMOVAL/INSTALLATION 401 ALL
 Removal of the THS Actuator Motor 401 ALL
 Installation of the THS Actuator 406 ALL
 Motor

 BRAKE - PRESSURE OFF, THS ACTUATOR 27-44-54
 ADJUSTMENT/TEST 501 ALL
 Functional Test of the 501 ALL
 Pressure-Off Brakes

 TRANSDUCER - THS ACTUATOR POSITION 27-44-56
 REMOVAL/INSTALLATION 401 ALL
 Removal of the Position Transducer 401 ALL
 from the THS Actuator 9CE
 Installation of the Position 405 ALL
 Transducer to the THS Actuator 9CE

 ACTUATOR - PITCH TRIM, THS 27-44-57
 REMOVAL/INSTALLATION 401 ALL
 Removal of the Pitch Trim Actuator 401 ALL
 from the THS Actuator 9CE
 Installation of the Pitch Trim 405 ALL
 Actuator to the THS Actuator 9CE
 Removal of the Electronic Modules 409 ALL
 of the Pitch Trim Actuator

 27-CONTENTS Page 19 Aug 01/05 R CES

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