mode reversionsmode reversions - smartcockpit · mode reversions are inherent to the integration of...
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![Page 1: MODE REVERSIONSMODE REVERSIONS - SmartCockpit · Mode reversions are inherent to the integration of theintegration of the AutopilotAutopilot and Auto thrustAuto thrust. ... A320 without](https://reader030.vdocuments.site/reader030/viewer/2022040513/5e661616787988671a0d3bb6/html5/thumbnails/1.jpg)
MODE REVERSIONSMODE REVERSIONSMODE REVERSIONSMODE REVERSIONSMODE REVERSIONSMODE REVERSIONSMODE REVERSIONSMODE REVERSIONS
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WHY MODE REVERSIONS ?
Mode reversions are inherent to the integration of the AutopilotAutopilot and Auto thrustAuto thrustintegration of the AutopilotAutopilot and Auto thrustAuto thrust.
The necessary design of automation behaviorautomation behaviori vario s ar i al circ sta cesar i al circ sta cesn u m g n um nm g n um n .
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MODES
LATERALLATERAL
VERTICALVERTICALVERTICALVERTICAL
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CCC
LATERAL
NAV to HDG discontinuityCCC
BBB
ClickClickCli k
AAA
Click
FROM UTC SPD/ALT
AAA 1210 280/FL130
BBB 1215 280/FL130BBB 1215 280/FL130
- - - - - - F-PLN DISCONTINUITY - - - - - - -
CCC 1219 280/FL130
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LAT - DISCONT AHEAD
![Page 5: MODE REVERSIONSMODE REVERSIONS - SmartCockpit · Mode reversions are inherent to the integration of theintegration of the AutopilotAutopilot and Auto thrustAuto thrust. ... A320 without](https://reader030.vdocuments.site/reader030/viewer/2022040513/5e661616787988671a0d3bb6/html5/thumbnails/5.jpg)
CCC
LATERAL
NAV to HDG discontinuityCCC
BBB
ClickClickCli k
FROM UTC SPD/ALTAAA
ClickPPOS 1215 280/FL130
- - - - - - F-PLN DISCONTINUITY - - - - - - -
CCC 1219 280/FL130FROM UTC SPD/ALT
AAA 1210 280/FL130
BBB 1215 280/FL130BBB 1215 280/FL130
- - - - - - F-PLN DISCONTINUITY - - - - - - -
CCC 1219 280/FL130
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LAT - DISCONT AHEAD
![Page 6: MODE REVERSIONSMODE REVERSIONS - SmartCockpit · Mode reversions are inherent to the integration of theintegration of the AutopilotAutopilot and Auto thrustAuto thrust. ... A320 without](https://reader030.vdocuments.site/reader030/viewer/2022040513/5e661616787988671a0d3bb6/html5/thumbnails/6.jpg)
VERTICAL
*ALT* Altitude Target ChangeAltitude Target Change Auto Disengagement of VerticalV/S excessiveFD orders not followedFD orders not followed
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ClickClick
Triple clicks come 5’’ later
if no pilot ti ALT
VERTICAL
- ALT*ClickClick
action on ALT or V/S Knobs
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ClickClick
Triple clicks come 5’’ later
if no pilot ti ALT
VERTICAL
- ALT*ClickClick
action on ALT or V/S Knobs
V/S boxed white for 10 V/S boxed white for 10 more seconds
V/S engaged on current A/C V/S
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VERTICAL
- ALT set below current altitude
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VERTICAL
- ALT set below current altitude
ClickClickClick
Triple clicks come 5’’ later if no pilot action on ALT or V/S Knobs
V/S boxed white for 10 more seconds
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VERTICAL
- Auto disengagement of vertical
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VERTICAL
- Auto disengagement of vertical
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VERTICAL
- Auto disengagement of vertical
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VERTICAL
- Excessive V/S in climb
Reaching VLSReaching VLS (or VLS-5)
ClickClickClickClick
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VERTICAL
- Excessive V/S in climb
Reaching VLS
Note: This does not apply to A320 without GSP
Reaching VLS (or VLS-5)
ClickClickClickClick
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VERTICAL
- Excessive V/S in descent
Reaching Vmax VFE VLE ( , ,
VMO)
ClickClickClick
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VERTICAL
- Excessive V/S in descent
Note: This does not apply to A320 without GSP
Reaching Vmax VFE VLE ( , ,
VMO)
ClickClickClick
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If Speed
VERTICAL
- FD orders not followed
ClickClickClick
protection activated,
pitch up will occur
Note: This does not apply to A320 ith t GSP
Reaching VMAX + 4 VMO VLE VFE
A320 without GSP
( , , )
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VERTICAL
- FD orders not followed
ClickClickClick
Reaching Vls-2(or Vls-17)( )
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Note: This does not apply to A320 without GSP
VERTICAL
- FD orders not followed
ClickClickClick
If Alpha protection is
reached, Alpha Fl illFloor will engage
Reaching Vls-2(or Vls-17)( )
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