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UF94200
EFFECTIVITY Page 354
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FLAP TRANSMISSION COMPONENTS - ACTUATORS - BEVEL GEARBOX - 19°
TMUFCTN01-P03 LEVEL 3
EFFECTIVITY 27-54-00 Page 7
Oct 31/97
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 27 FLIGHT CONTROLS
UF94200
EFFECTIVITY Page 355
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FLAP TRANSMISSION COMPONENTS
TORQUE LIMITERS
COMPONENT DESCRIPTION
A bi-directional torque limiter is incorporated in the
transmission input of each actuator.
A latching mechanical indicator shows if a lock out
torque has occurred.
FLAP TRACK FAIRING
COMPONENT DESCRIPTION
A flap link arm is attached to the bottom flap surface
outboard of each track and transmits the drive from
the actuator directly to the flap.
Attached to the flap bottom, at tracks 2,3 and 4, is
an arm which operates the moveable track fairing during
flap movement.
TMUFCTN01-T04 LEVEL 3
EFFECTIVITY 27-54-00 Page 8
Oct 31/97
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 27 FLIGHT CONTROLS
UF94200
EFFECTIVITY Page 356
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TMUFCTN01-P04 LEVEL 3
FLAP TRANSMISSION COMPONENTS - TORQUE LIMITERS - FLAP TRACK FAIRING
EFFECTIVITY 27-54-00 Page 9
Oct 31/97
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 27 FLIGHT CONTROLS
UF94200
EFFECTIVITY Page 357
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FLAP TRANSMISSION COMPONENTS
WING TIP BRAKE
IDENTIFICATION
FIN: 33CV, 34CV
LOCATION
ZONE: 575, 675
COMPONENT DESCRIPTION
If pressure is not available to one piston, the other
piston provides sufficient torque to stop and hold the
torque shaft.
Access: 575EB/675EB between T3 and T4.
FLAP ASYMMETRY POSITION PICK OFF UNIT
IDENTIFICATION
FIN: 29CV, 30CV
LOCATION
ZONE: 575, 675
COMPONENT DESCRIPTION
One Asymmetry Position Pick off Unit (APPU) is located
at the end of the transmission system in each wing.
They are identical to and interchangeable with the
Feedback Position Pick off Unit (FPPU) and the
Instrument Position Pick off Unit (IPPU).
Access: 575FB/675FB.
TMUFCTN01-T05 LEVEL 3
EFFECTIVITY 27-54-00 Page 10
Oct 31/97
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 27 FLIGHT CONTROLS
UF94200
EFFECTIVITY Page 358
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FLAP TRANSMISSION COMPONENTS - WING TIP BRAKE - FLAP APPU
TMUFCTN01-P05 LEVEL 3
EFFECTIVITY 27-54-00 Page 11
Oct 31/97
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 27 FLIGHT CONTROLS
UF94200
EFFECTIVITY Page 359
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TMUFCTN01 LEVEL 3
EFFECTIVITY 27-54-00 Page 12
Oct 31/97
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 27 FLIGHT CONTROLS
UF94200
EFFECTIVITY Page 360
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27 - FLIGHT CONTROLS
27-84-00 SLAT TRANSMISSION COMPONENTS
CONTENTS:
Bevel Gearbox - 19°
T Gearbox
Universal Joints
Steady Bearing Assembly
Torque Shafts
Bevel Gearbox - 63.5°
Actuators
Torque Limiters
Slat Track Installation
Wing Tip Brakes
Asymmetry Position Pick Off Units
TMUFCTP01 LEVEL 3
EFFECTIVITY 27-84-00 Page 1
Oct 31/97
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 27 FLIGHT CONTROLS
UF94200
EFFECTIVITY Page 361
ALL
SLAT TRANSMISSION COMPONENTS
BEVEL GEARBOX - 19°
IDENTIFICATION
FIN: 6003CM
LOCATION
ZONE: 191
COMPONENT DESCRIPTION
The bevel gearbox has a 1:1 ratio.
It is pre-packed with grease and incorporates unsealed
stainless bearings.
Inspection plugs are provided for on condition
maintenance.
T GEARBOX
IDENTIFICATION
FIN: 6005CM
LOCATION
ZONE: 191
COMPONENT DESCRIPTION
The gearbox has a 1:1 ratio.
Bearings, seals, and methods of lubrication and
inspection are similar to those used on the 19° bevel
gearbox.
UNIVERSAL JOINTS
COMPONENT DESCRIPTION
Universal joints are bolted to the ends of the torque
shafts.
This permits small angular changes of alignment and
wing flexing.
TMUFCTP01-T01 LEVEL 3
EFFECTIVITY 27-84-00 Page 2
Oct 31/97
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 27 FLIGHT CONTROLS
UF94200
EFFECTIVITY Page 362
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SLAT TRANSMISSION COMPONENTS - 19° BEVEL GEARBOX - T GEARBOX - UNIVERSAL JOINTS
　
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