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Then, dashes will replace the heading or track.
During the arming and active phases, the light is on.
TMUFM2004-T03 LEVEL 3
EFFECTIVITY 22-81-00 Page 6
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_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 22 AUTO FLIGHT SYSTEM
UF94200
EFFECTIVITY Page 130
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FLIGHT CONTROL UNIT DESCRIPTION/OPERATION - HEADING/TRACK LATERAL CONTROL KNOB
TMUFM2004-P03 LEVEL 3
EFFECTIVITY 22-81-00 Page 7
Jul 31/00
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 22 AUTO FLIGHT SYSTEM
UF94200
EFFECTIVITY Page 131
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FLIGHT CONTROL UNIT DESCRIPTION/OPERATION
ALTITUDE SELECTOR KNOB
The outer knob has 2 selectable positions, 100 feet
and 1000 feet.
The inner knob sets the altitude in the FCU altitude
window with increments depending on the outer knob
position (100 or 1000).
The inner knob can be pushed or pulled and is
spring-loaded to neutral. It can also be turned.
PULLED:
When pulled, open climb or open descent mode engages
if the displayed altitude is different from the present
aircraft altitude. The level change light is off.
Aircraft immediately climbs (or descends) towards the
selected altitude.
TURNED:
When turned, the displayed altitude changes by
thousands or hundreds feet, depending on the outer
knob selection.
The selected altitude changes.
PUSHED:
When pushed, climb or descent mode engages if the
displayed altitude (in the FCU) is different from the
present aircraft altitude. The level change is managed
and the level change light is on.
NOTE: The ALT window always displays a target value
selected by the crew. The window is never dashed.
METRIC ALTITUDE PUSHBUTTON
This METRIC ALT pushbutton is used to display the FCU
altitude target in meters on the lower ECAM display
unit.
Note that the altitude target, on the FCU, is always
in feet.
TMUFM2004-T04 LEVEL 3
EFFECTIVITY 22-81-00 Page 8
Jul 31/00
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 22 AUTO FLIGHT SYSTEM
UF94200
EFFECTIVITY Page 132
ALL
TMUFM2004-P04 LEVEL 3
FLIGHT CONTROL UNIT DESCRIPTION/OPERATION -
ALTITUDE SELECTOR KNOB / METRIC ALTITUDE PUSHBUTTON
EFFECTIVITY 22-81-00 Page 9
Jul 31/00
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 22 AUTO FLIGHT SYSTEM
UF94200
EFFECTIVITY Page 133
ALL
FLIGHT CONTROL UNIT DESCRIPTION/OPERATION
VERTICAL SPEED/FLIGHT PATH ANGLE CONTROL KNOB
The Vertical Speed/Flight Path Angle control knob
can be pushed or pulled. It is spring-loaded to
neutral. It can also be turned.
PULLED:
When pulled, Vertical Speed or Flight Path Angle mode
engages with a reference displayed on the FCU. The
level change light is off.
If the associated window was previously dashed, the
value which appears is the present Vertical Speed or
Flight Path Angle.
The range are:
- between -9.9° and +9.9° for FPA,
- between -6000 and +6000 feet per minute for
V/S.
TURNED:
When turned, it changes the displayed Vertical
Speed (or FLight Path Angle).
If the associated window was previously dashed, the
first click changes the dashes into the present A/C
V/S or FPA. When turned more, the value changes.
If the knob is not pulled within 45 seconds, the
display reverts to dashes.
PUSHED:
Pushing the V/S/FPA rotary knob will command an
immediate level off by engaging the V/S/FPA mode with
a zero target as diplayed in the FCU window. FMA
annunciation will turn to ALT green when levelled off.
Any new setting of a V/S or FPA (selector turned) will
lead to A/C movement accordingly.
HEADING-V/S/TRACK-FPA SWITCHING PUSHBUTTON
This pushbutton allows selection of heading and
Vertical Speed or track and Flight Path Angle modes.
If any of the modes (HDG, V/S, TRK, FPA) are active,
pressing the pushbutton changes the mode(s) into the
corresponding one(s) (HDG TRK and V/S FPA).
Pressing the pushbutton, changes the HDG V/S into TRK
FPA on the center of the FCU and vice versa.
Note that the flight director symbology on the PFD
changes and the flight path vector and the flight path
director appears.
TMUFM2004-T05 LEVEL 3
EFFECTIVITY 22-81-00 Page 10
Jul 31/00
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 22 AUTO FLIGHT SYSTEM
UF94200
EFFECTIVITY Page 134
ALL
FLIGHT CONTROL UNIT DESCRIPTION/OPERATION -
　
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