Stalling Flashcards

1
Q

Why does an aerofoil stall?

A

The critical angle has been exceeded and the wing can no longer produce enough lift to balance the weight

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2
Q

Vs0

A

Stall speed with flaps - 41 KTS

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3
Q

Vs1

A

Stall speed without flaps - 47 KTS

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4
Q

How does increased weight affect stall speed?

A

Stall speed increase

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5
Q

How does CoG moving aft affect stall speed?

A

Stall speed decrease

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6
Q

How does decreased power affect stall speed?

A

Stall speed increase

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7
Q

How do retracted flaps affect stall speed?

A

Stall speed increase

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8
Q

HASELL (HELL)

A

-Height sufficient to recover by 3000’ AGL
-Airframe configured as required
-Security, no loose articles, hatches/harnesses
-Engine T’s and P’s in green
-Location, clear of high traffic areas
-Lookout, 180/2x 90 degree turns

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9
Q

Symptoms of incipient stall

A
  • Reduced cockpit noise
  • Low and decreasing airspeed
  • Stall horn
  • Reduced control effectiveness
  • Unusually high nose attitude
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10
Q

Recovery from incipient stall

A
  • Lower nose
  • Apply power
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11
Q

Fully developed stall symptoms

A
  • Nose drop
  • High rate of descent
  • Aircraft highly unstable, possible wing drop
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12
Q

Recovery from full stall

A

Stall horn activates - carby heat off
Pitch nose down to S&L
Full power, ailerons neutral
Rudder to prevent yaw
Once 65 retract 1st stage flaps
Raise nose to climb attitude
Positive rate of climb
Retract the rest of flap

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13
Q

Incipient spin effect

A
  • Both wings are stalled
  • Aircraft yawing at the point of stall, called autorotation
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14
Q

Incipient spin recovery

A

Power - idle
Aileron - neutral
Rudder - full opposite
Elevator - through neutral
Once rotation stopped
Centralise rudder
Positive dive recovery
Power above horizon

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