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60kt.
- AOA exceeds 8°5 or CAS drops below 148kt
while retraction from 18° to 0° has already
started.
TMUFC1602-T07 LEVEL 1
EFFECTIVITY 27-00-00 Page 14
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MECHANICS / ELECTRICS & AVIONICS COURSE 27 FLIGHT CONTROLS
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SLATS AND FLAPS CONTROL AND POSITION INDICATION - SLATS ALPHA-LOCK PROTECTION
TMUFC1602-P07 LEVEL 1
EFFECTIVITY 27-00-00 Page 15
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SELF EXAMINATION
What happens when Slats/Flaps configuration is 1+F
and the CAS reaches 210 knots?
A - Flaps retract automatically to 0 and the
new Slats/Flaps configuration is 1.
B - Flaps extend automatically because the
speed is too high.
C - The alpha lock function is engaged
because the CAS is too high.
TMUFC1602 LEVEL 1
EFFECTIVITY 27-00-00 Page 16
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27 - FLIGHT CONTROLS
27-00-00 SLATS AND FLAPS CONTROL AND
POSITION INDICATION
CONTENTS:
Slats / Flaps Control Lever
Slats / Flaps Extension On Ground
Slats / Flaps Retraction On Ground
Slats / Flaps Extension In Flight
Slats / Flaps Retraction In Flight
Automatic Retraction In Flight
Slats Alpha-Lock Protection
Self Examination
TMUFC1603 LEVEL 1
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SLATS AND FLAPS CONTROL AND POSITION INDICATION
SLATS / FLAPS CONTROL LEVER
The Slats / Flaps control lever is located in the
cockpit on the center pedestal.
It is connected to the Command Sensor Unit which
transforms the mechanical demand into electrical
signals for the Slat / Flap Control Computers (SFCCs).
The lever selects simultaneous operation of the slats
and flaps and the collar must be lifted before
selection of any position.
The relationship between the lever position, flight
phase and slat flap angles is shown here.
TMUFC1603-T01 LEVEL 1
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SLATS AND FLAPS CONTROL AND POSITION INDICATION - CONTROL LEVER
TMUFC1603-P01 LEVEL 1
EFFECTIVITY 27-00-00 Page 3
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MECHANICS / ELECTRICS & AVIONICS COURSE 27 FLIGHT CONTROLS
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SLATS AND FLAPS CONTROL AND POSITION INDICATION
SLATS / FLAPS EXTENSION ON GROUND
The white points on the ECAM display are the selectable
Slat / Flap positions. These white points are not
displayed in clean configuration.
A word "FLAP" appears on the ECAM display when the
slats and flaps are not fully retracted.
When a new position is selected, the position number,
the word "FLAP" and the selected position triangles
are displayed in cyan.
When the selected position is reached, the position
number, and triangles become green. The word "FLAP"
becomes white. A green line is added to the display.
When the flaps are set to full, the word FULL replaces
the flap position number.
TMUFC1603-T02 LEVEL 1
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UF94200
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SLATS AND FLAPS CONTROL AND POSITION INDICATION - EXTENSION ON GROUND
TMUFC1603-P02 LEVEL 1
EFFECTIVITY 27-00-00 Page 5
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SLATS AND FLAPS CONTROL AND POSITION INDICATION
SLATS / FLAPS RETRACTION ON GROUND
With the aircraft on ground, the configuration is 1+F.
Once the surfaces have reached the fully retracted
position, the clean configuration is displayed on the
ECAM display.
TMUFC1603-T03 LEVEL 1
EFFECTIVITY 27-00-00 Page 6
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_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 27 FLIGHT CONTROLS
　
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