CHAPTER 27
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FLIGHT CONTROLS
TABLE OF CONTENTS
_________________
SUBJECT_______ CH/SE/SU _ PAGE EFFECTIVITY________ C ____ ___________
201-299, 401-499 Installation of the Pendulum of 448 001-049, 051-099 the No. 1 Flap Track Carriage 101-149, 151-199
201-299, 401-499 CARRIAGE 27-54-46
INSPECTION/CHECK 601 ALL
Detailed Visual Inspection of the 601 ALL
Flap Tracks and Rollers (as far as
is possible)
Detailed Inspection of the Flap 611 ALL
Carriage Rollers for In-Service
Wear
LINE GEARBOX 27-54-47
REMOVAL/INSTALLATION 401 ALL
Removal of the Line Gearbox 401 ALL
6209CM(6259CM)
Installation of the Line Gearbox 405 ALL
6209CM(6259CM)
BEVEL GEAR BOX 27-54-48
REMOVAL/INSTALLATION 401 ALL
Removal of the Bevel Gear Box 401 ALL
6217CM(6267CM)
Installation of the Bevel Gear Box 406 ALL
6217CM(6267CM)
ACTUATOR ASSY 27-54-49
REMOVAL/INSTALLATION 401 ALL
Removal of the Flap Track 1 to 4 401 ALL
Actuators
6205CM(6255CM)/6211CM(6261CM)/
6221CM(6271CM)/6233CM(6283CM)
Installation of the Flap Track 1 407 ALL
to 4 Actuators
6205CM(6255CM)/6211CM(6261CM)/
6221CM(6271CM)/6233CM(6283CM)
Removal of the Flap Track 1 418 ALL
Actuator 6205CM(6255CM)
Installation of the Flap Track 1 434 ALL
Actuator 6205CM(6255CM)
Removal of the Flap Track 2 453 ALL
Actuator 6211CM(6261CM)
Installation of the Flap Track 2 463 ALL
Actuator 6211CM(6261CM)
Removal of the Flap Track 3 478 ALL
Actuator 6221CM(6271CM)
Installation of the Flap Track 3 488 ALL
Actuator 6221CM(6271CM)
27-CONTENTS Page 29 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 Flap Track 4 A404 ALL Actuator 6233CM(6283CM) Installation of the Flap Track 4 A414 ALL Actuator 6233CM(6283CM)
CONTROL UNIT - POWER (PCU) (FLAPS) 27-54-51
REMOVAL/INSTALLATION 401 ALL Removal of the Power Control Unit 401 ALL 6201CM of the Flap System Installation of the Power Control 410 ALL Unit 6201CM of the Flap System
BRAKE - PRESSURE OFF, FLAPS PCU 27-54-52
REMOVAL/INSTALLATION 401 ALL Removal of the Pressure-Off Brake 401 ALL of the Flap Power Control Unit Installation of the Pressure-Off 407 ALL Brake of the Flap Power Control Unit
VALVE BLOCK - FLAP PCU 27-54-53
REMOVAL/INSTALLATION 401 ALL Removal of the Valve Blocks 23CV, 401 ALL 24CV of the Power Control Unit (Flap) Installation of the Valve Blocks 407 ALL 23CV, 24CV of the Power Control Unit (Flap) Removal of the Solenoid Valves of 416 ALL the Power Control Unit (Flap) Installation of the Solenoid 420 ALL Valves of the Power Control Unit (Flap) Removal of the Filters of the 425 ALL Valve Blocks Installation of the Filters of the 429 ALL Valve Blocks
MOTOR - HYDRAULIC, FLAPS PCU 27-54-54
REMOVAL/INSTALLATION 401 ALL Removal of the Hydraulic Motor of 401 ALL the Flap Power Control-Unit (6201CM) with the Pressure-Off Brake and the Valve Block Assembly Installation of the Hydraulic 407 ALL Motor of the Flap Power Control-Unit (6201CM) with the Pressure-Off Brake and the Valve Block Assembly Removal of the Hydraulic Motor of 416 ALL
27-CONTENTS Page 30 Aug 01/05 R CES
CHAPTER 27
__________
FLIGHT CONTROLS
TABLE OF CONTENTS
_________________
SUBJECT_______ CH/SE/SU _ PAGE EFFECTIVITY
________ C ____ ___________ the Flap Power Control-Unit (6201CM) without the Pressure-Off Brake and the Valve Block Assembly Installation of the Hydraulic 421 ALL Motor of the Flap Power Control-Unit (6201CM) without the Pressure-Off Brake and the Valve Block Assembly
LEVER ASSY - FLAP ACTUATOR 27-54-55
REMOVAL/INSTALLATION 401 ALL
Removal of the Flap-Actuator Lever 401 ALL
Assembly - Tracks 1 and 2
Installation of the Flap-Actuator 428 ALL
Lever Assembly - Tracks 1 and 2
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