Podcast
Questions and Answers
What action should the flight crew take to exit alpha protection (αPROT)?
What action should the flight crew take to exit alpha protection (αPROT)?
- Keep the sidestick neutral while descending
- Pull back on the sidestick quickly
- Maintain a constant hold on the throttle
- Ease forward on the sidestick and add power (correct)
Under what condition does αfloor protection activate?
Under what condition does αfloor protection activate?
- When a manual override is initiated
- When the aircraft is above αMAX
- When the sidestick is held back for 2 seconds
- Just after entering αPROT (correct)
What happens if the sidestick is held aft while in αPROT?
What happens if the sidestick is held aft while in αPROT?
- The aircraft will dive rapidly
- The aircraft will start to climb at a low airspeed (correct)
- The aircraft will stall immediately
- The aircraft will maintain a constant altitude
What must be done to cancel the αfloor protection?
What must be done to cancel the αfloor protection?
Which of the following conditions will cause the aircraft to leave angle-of-attack protection?
Which of the following conditions will cause the aircraft to leave angle-of-attack protection?
What happens when the angle-of-attack exceeds αPROT?
What happens when the angle-of-attack exceeds αPROT?
How can the flight crew further increase the angle-of-attack after reaching αPROT?
How can the flight crew further increase the angle-of-attack after reaching αPROT?
What does the side stick input represent during High AOA protection?
What does the side stick input represent during High AOA protection?
What is the consequence of releasing the sidestick during High AOA conditions?
What is the consequence of releasing the sidestick during High AOA conditions?
What is true about the aircraft's trim during High AOA conditions?
What is true about the aircraft's trim during High AOA conditions?
When is αPROT equal to αMAX?
When is αPROT equal to αMAX?
How does the angle-of-attack return to αPROT after reaching αMAX?
How does the angle-of-attack return to αPROT after reaching αMAX?
What condition does the High AOA protection prioritize?
What condition does the High AOA protection prioritize?
What factors primarily influence Vα PROT, Vα MAX, and the αfloor condition?
What factors primarily influence Vα PROT, Vα MAX, and the αfloor condition?
Who computes the Vα PROT and Vα MAX values shown on the PFD?
Who computes the Vα PROT and Vα MAX values shown on the PFD?
How is αPROT affected as Mach increases?
How is αPROT affected as Mach increases?
What condition will allow the aircraft to exit angle-of-attack protection using the sidestick input?
What condition will allow the aircraft to exit angle-of-attack protection using the sidestick input?
Under which scenario does the sidestick input NOT contribute to exiting angle-of-attack protection?
Under which scenario does the sidestick input NOT contribute to exiting angle-of-attack protection?
Flashcards
αPROT Angle of Attack
αPROT Angle of Attack
A critical angle of attack where the aircraft activates a protection system.
αMAX Angle of Attack
αMAX Angle of Attack
The maximum safe angle of attack for the aircraft.
αFloor Activation
αFloor Activation
Automatic go-around thrust deployment when entering αPROT.
Exiting αPROT
Exiting αPROT
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Cancelling αFloor
Cancelling αFloor
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High Angle-of-Attack (AOA) Protection
High Angle-of-Attack (AOA) Protection
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αPROT
αPROT
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αMAX
αMAX
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Vα PROT
Vα PROT
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Vα MAX
Vα MAX
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PRIM
PRIM
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High AOA Protection Priority
High AOA Protection Priority
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αfloor
αfloor
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How are Vα PROT, Vα MAX, and αfloor connected?
How are Vα PROT, Vα MAX, and αfloor connected?
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Why do Vα PROT, Vα MAX, and αfloor vary?
Why do Vα PROT, Vα MAX, and αfloor vary?
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What does PRIM calculate?
What does PRIM calculate?
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What is Vα PROT?
What is Vα PROT?
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What is Vα MAX?
What is Vα MAX?
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What is Alpha Floor?
What is Alpha Floor?
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What is High Angle of Attack (AOA) protection?
What is High Angle of Attack (AOA) protection?
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Alpha (α) in αPROT
Alpha (α) in αPROT
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Sidestick in αPROT
Sidestick in αPROT
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Mach Effects on αPROT
Mach Effects on αPROT
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Climbing with Sidestick Fee
Climbing with Sidestick Fee
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αPROT and Turns
αPROT and Turns
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Leaving αPROT
Leaving αPROT
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Angle of Attack (α) Protection
Angle of Attack (α) Protection
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αPROT Activation
αPROT Activation
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αPROT and αMAX
αPROT and αMAX
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Study Notes
High Angle-of-Attack (AOA) Protection System
- Activation: High AOA protection activates when the current angle-of-attack exceeds αPROT.
- Automatic Control: F/CTL computers maintain the angle-of-attack at αPROT without flight crew input.
- Manual Override: Flight crew can increase AOA up to a maximum value of αMAX.
- Input Change: With high AOA protection active, side stick input becomes an AOA demand instead of a load factor demand.
- Operational Restrictions: Deliberate operation in high AOA is limited except for brief periods when maximum maneuvering speed is needed.
- Variable Speeds (Vα): Vα PROT and Vα MAX, displayed on the PFD, are computed by the PRIM and vary based on AOA, configuration, weight, and load factor.
- αfloor: αfloor activation logic is handled by the PRIM and influences speed and thrust based on AOA, configuration, weight, and load factor. Refer to specific document for further details. (DSC-22_10-50-20)
- Angle-of-Attack Limits: αMAX is the maximum allowable angle-of-attack, even with full back stick.
- Trim Restrictions: Nose-up trim is inhibited beyond the point reached when entering the protection (amber/black trip). Nose-down trim remains available.
- Takeoff Specifics: αPROT equals αMAX for the first 8 seconds of takeoff.
- Priority: High AOA protection has higher priority than other protection systems.
- High-Level Protection: Protection also works at high altitudes, safeguarding against buffet boundary.
Protection System Recovery
- Exiting Protection: To exit protection, push the sidestick forward—by more than 8 degrees, or more than 0 degrees for at least 1 second when α < αMAX, or held at neutral or forward for at least 0.5 second when α < αPROT—then simultaneously adding power if necessary (or if the αfloor is not active or has been cancelled) to reduce alpha below αPROT's threshold.
- Alpha Floor Trigger: Between αPROT and αMAX, αfloor protection may automatically activate go-around thrust, usually immediately after entering αPROT.
- Holding Aft Stick: If the sidestick is held aft and the aircraft enters the protection state, it will climb at a relatively constant low airspeed.
Exit Procedures
- Recovery Method: Ease forward on the sidestick to exit Alpha protection and deactivate Alpha floor protection (if activated) by using the disconnect pushbutton on either thrust lever. Wait until safe speeds are achieved.
- Side Stick Input Conditions: Specific side stick input thresholds, for at least 1 and .5 second, are provided for exiting the protections.
- Disconnection: Disconnecting the thrust is required to exit the α floor protection.
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