REMOVAL/INSTALLATION 401 051-051, Removal of the Pressure Transducer 401 051-051, Installation of the Pressure 407 051-051, Transducer
FTU (FORCE TRANSDUCER UNIT) - RUDDER 27-92-27
PEDAL
REMOVAL/INSTALLATION 401 301-399, Removal of the Rudder Pedal Force 401 301-399, Transducer (74CE) Installation of the Rudder Pedal 405 301-399, Force Transducer (74CE)
27-CONTENTS Page 48 Aug 01/05 R CES
CHAPTER 27
__________
FLIGHT CONTROLS
TABLE OF CONTENTS
_________________
SUBJECT_______ CH/SE/SU _ PAGE EFFECTIVITY
________ C ____ ___________ SIDE STICK ASSEMBLY 27-92-41
REMOVAL/INSTALLATION 401 ALL Removal of the Side Stick Assembly 401 ALL 19VU (18VU) Installation of the Side Stick 408 ALL Assembly 19VU (18VU) Removal of the Transducer Units 415 ALL (4CE1, 4CE2, 4CE3, 4CE4) Installation of the Transducer 418 ALL Units (4CE1, 4CE2, 4CE3, 4CE4) Removal of the Dampers 423 ALL Installation of the Dampers 426 ALL Removal of the Solenoid (12CA1, 429 ALL 12CA2) Installation of the Solenoid 432 ALL (12CA1, 12CA2) Removal of the Control Handle 438 ALL Installation of the Control Handle 441 ALL Removal of the Radio PTT Switch 445 ALL (11RN, 12RN) Installation of the Radio PTT 450 ALL Switch (11RN, 12RN) Removal of the Pushbutton 453 ALL Switch-Takeover and Priority (8CE1, 8CE2) Installation of the Pushbutton 456 ALL Switch-Takeover and Priority (8CE1, 8CE2) Removal of the Side Stick Bellows 459 ALL Installation of the Side Stick 464 ALL Bellows Removal of the Side Stick Spring 470 ALL Rods Installation of the Side Stick 475 ALL Spring Rods
SIDE STICK ASSEMBLY 27-92-41
ADJUSTMENT/TEST 501 ALL Operational Test of the Side Stick 501 ALL Assembly
ELAC SYSTEM (ELEVATOR AILERON COMPUTER) 27-93-00
DESCRIPTION AND OPERATION 1 ALL General 1 ALL Component Location 1 ALL Power Supply 3 ALL Component Description 3 ALL
27-CONTENTS Page 49 Aug 01/05 R CES
CHAPTER 27
__________
FLIGHT CONTROLS
TABLE OF CONTENTS
_________________
SUBJECT_______ CH/SE/SU _ PAGE EFFECTIVITY
________ C ____ ___________ General 3 ALL Description of Boards 14 ALL
Operation 32 ALL Monitoring of Peripherals (IMP 32 ALL VAL) Computation of Laws 51 ALL Control Surface Slaving 51 ALL Self-Monitoring of the Computer 59 ALL Behavior upon Power Rise and 60 ALL Cutoff Behavior upon Action on the 60 ALL OFF/R Pushbutton Switch Power-up Tests Initialization 63 001-049, 051-060 and Cockpit Repercussions 101-101,
ELAC SYSTEM (ELEVATOR AILERON 27-93-00
COMPUTER)
DEACTIVATION/REACTIVATION 401 ALL
Deactivation of the Elevator 401 ALL
Aileron Computer
Refer to the MMEL TASK: 27-93-01 401 ALL
Reactivation of the Elevator 408 ALL
Aileron Computer
Refer to the MMEL TASK: 27-93-01 408 ALL
ELAC SYSTEM (ELEVATOR AILERON 27-93-00
COMPUTER)
ADJUSTMENT/TEST 501 ALL
Operational Test of the Elevator 501 ALL
and Aileron Computers (ELACs)
Operational Test of the ELAC 2 507 ALL
STBY PWR SPLY Availability in case
of loss of Blue Hydraulic Pressure
(To be done before revenue flight
landing gear down)
COMPUTER - ELEVATOR AILERON (ELAC) 27-93-34
REMOVAL/INSTALLATION 401 ALL
Removal of the ELAC (2CE1, 2CE2) 401 ALL
Installation of the ELAC (2CE1, 404 ALL
2CE2)
SEC SYSTEM (SPOILER AND ELEVATOR 27-94-00 COMPUTER) DESCRIPTION AND OPERATION 1 ALL
27-CONTENTS Page 50 Aug 01/05 R CES
CHAPTER 27
__________
FLIGHT CONTROLS
TABLE OF CONTENTS
_________________
SUBJECT_______ CH/SE/SU _ PAGE EFFECTIVITY________ C ____ ___________ General 1 ALL Component Location 1 ALL Power Supply 1 ALL Interface 7 ALL Analog Interface 7 ALL Discrete Interface 14 ALL ARINC Interface 14 ALL Component Description 28 ALL General 28 ALL Description of the Boards 31 ALL Operation 32 ALL General 32 ALL Functions 35 ALL
Test 68 001-049, 051-060
101-101, Power-up Tests Initialization 68 001-049, 051-060 and Cockpit Repercutions 101-101,
SEC SYSTEM (SPOILER AND ELEVATOR 27-94-00
COMPUTER)
DEACTIVATION/REACTIVATION 401 ALL
Deactivation of the Spoiler 401 ALL
Elevator Computer (SEC)
Refer to the MMEL TASK: 27-94-01 401 ALL
Reactivation of the Spoiler 406 ALL
Elevator Computer (SEC)
SEC SYSTEM (SPOILER AND ELEVATOR 27-94-00
COMPUTER)
ADJUSTMENT/TEST 501 ALL
Operational Test of the Spoiler 501 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(67)
