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TMUFCTP01-P01 LEVEL 3
EFFECTIVITY 27-84-00 Page 3
Oct 31/97
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 27 FLIGHT CONTROLS
UF94200
EFFECTIVITY Page 363
ALL
SLAT TRANSMISSION COMPONENTS
STEADY BEARING ASSEMBLY
COMPONENT DESCRIPTION
Steady bearings, attached to the structure, hold the
shafts where small angular changes of alignment are
present.
TORQUE SHAFTS
COMPONENT DESCRIPTION
The torque shaft made from stainless steel are
connected through universal joints and supported in
steady bearings.
6012CM, 6062CM, 6024CM, 6074CM, 6034CM, 6084CM have
an additional flanged joint at the middle point of the
shaft.
BEVEL GEARBOX 63.5°
IDENTIFICATION
FIN: 6009CM, 6059CM, 6011CM, 6061CM
LOCATION
ZONE: 191, 192
COMPONENT DESCRIPTION
There are four 63.5 degree bevel gearboxes.
Bearings, seals and methods of lubrication and
inspection are the same as those used on the 19 degrees
bevel gearbox.
TMUFCTP01-T02 LEVEL 3
EFFECTIVITY 27-84-00 Page 4
Oct 31/97
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 27 FLIGHT CONTROLS
UF94200
EFFECTIVITY Page 364
ALL
SLAT TRANSMISSION COMPONENTS - STEADY BEARING ASSEMBLY - TORQUE SHAFTS -
63.5º BEVEL GEARBOX
TMUFCTP01-P02 LEVEL 3
EFFECTIVITY 27-84-00 Page 5
Oct 31/97
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 27 FLIGHT CONTROLS
UF94200
EFFECTIVITY Page 365
ALL
SLAT TRANSMISSION COMPONENTS
ACTUATORS
IDENTIFICATION
FIN: 6013CM, 6063CM
LOCATION
ZONE: 521, 621
COMPONENT DESCRIPTION
Two sizes of actuators are used.
The large diameter ones at T2 and T3 incorporate
additional gearing but construction and operation is
similar for all actuators.
They are pre-packed with grease for "life time"
lubrication.
Vent holes are provided in the casing for drainage of
any accumulated moisture.
TORQUE LIMITERS
IDENTIFICATION
FIN: 6013CM, 6063CM
LOCATION
ZONE: 521, 621
COMPONENT DESCRIPTION
Each actuator incorporates a bi-directional torque
limiter which prevents excessive torque being
transmitted to the output.
A latching mechanical indicator is provided to show
when lock-out torque has occurred.
The mechanism may be reset by reverse operation but
the indicator remains extended until cancelled
manually.
TMUFCTP01-T03 LEVEL 3
EFFECTIVITY 27-84-00 Page 6
Oct 31/97
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 27 FLIGHT CONTROLS
UF94200
EFFECTIVITY Page 366
ALL
SLAT TRANSMISSION COMPONENTS - ACTUATORS - TORQUE LIMITERS
TMUFCTP01-P03 LEVEL 3
EFFECTIVITY 27-84-00 Page 7
Oct 31/97
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 27 FLIGHT CONTROLS
UF94200
EFFECTIVITY Page 367
ALL
SLAT TRANSMISSION COMPONENTS
SLAT TRACK INSTALLATION
IDENTIFICATION
FIN: 6013CM, 6063CM
LOCATION
ZONE: 521, 621
COMPONENT DESCRIPTION
Each track runs in grease-lubricated vertical and side
load-rollers.
A fixed stop is provided at each end of the driven
tracks.
A gear track engages a pinion driven by the actuator
output shaft.
TMUFCTP01-T04 LEVEL 3
EFFECTIVITY 27-84-00 Page 8
Oct 31/97
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 27 FLIGHT CONTROLS
UF94200
EFFECTIVITY Page 368
ALL
SLAT TRANSMISSION COMPONENTS - SLAT TRACK INSTALLATION
TMUFCTP01-P04 LEVEL 3
EFFECTIVITY 27-84-00 Page 9
Oct 31/97
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 27 FLIGHT CONTROLS
UF94200
EFFECTIVITY Page 369
ALL
SLAT TRANSMISSION COMPONENTS
WING TIP BRAKES
IDENTIFICATION
FIN: 35CV, 36CV
LOCATION
ZONE: 522, 622
COMPONENT DESCRIPTION
If the pressure is not available to one piston, the
other piston provides sufficient torque to stop and
hold the torque shaft.
ACCESS: 522SB / 622SB
ASYMMETRY PPUs
IDENTIFICATION
FIN: 31CV, 32CV
LOCATION
ZONE: 522, 622
COMPONENT DESCRIPTION
One Asymmetry Position Pick off Unit (APPU) is located
outboard of track 12 on each wing. APPUs are identical
to and interchangeable with the Feedback Position Pick
off Unit (FPPU) and the Instrument Position Pick off
　
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