AVIT 414 - Stage 25
Study online at
https://quizlet.com/_eefrvv
1. Vso 45 KIAS
2. Vs 50 KIAS
3. Vx 64 KIAS
4. Vy 76 KIAS
5. Best Glide 76 KIAS
6. Cruise Cimb 87 KIAS
7. Vfe 102 KIAS
8. Vo 113 KIAS @ 2550
98 KIAS @ 1917
9. Vno 125 KIAS
10. Vne 154 KIAS
11. What factors will -Weight
affect stall speed? -CG Location
-Load Factor
-Wing Contamination
-Configuration (flaps)
12. Vs vs Vo Vs = Stalling speed or minimum steady flight speed at which
the a/c is controllable
Vso = Stalling speed or the minimum steady flight speed at
which the a/c is controllable in landing configuration
13. Vo vs Vno Vo = The speed in which full and abrupt control input will stall th
aircraft
(or cause structural damage if above Vo for given weight.
1/
44
, AVIT 414 - Stage 25
Study online at
https://quizlet.com/_eefrvv
Vno = The maximum structural cruising speed or better known
as normal operating speed. It should not be exceeded except
in smooth air and only then with caution.
14. How does Vo -It has to do with flying closer to the critical AoA. Heavier a/c
chnage with requires more lift to maintain altitude. More lift requires
weight? increasing AoA which consequently is closer to the critical AoA.
The closer an airfoil is to the critical AoA, the sooner it will
stall hence increasing the Vo speed.
-Lighter aircraft requires less lift to maintain altitude and
therefore flies at a smaller AoA and is futher away from the critical
AoA and will stall later/at a slower speed
15. Engine Failure Below Vr Throttle --- Idle
Brakes --- As Required
Engine --- Shutdown if Necessary
16. Engine Failure Above Vr Airspeed --- Maintain Safe
Landing --- Straight Ahead
Engine --- Shutdown if
Necessary
17. Electrical Fire in FlightEmergency Battery Switch --- Verify ARM
Battery Master Switch --- Ott
Alternator Switch --- Ott
Vents --- Open
Heat & Defrost Controls --- Ott
Fire --- Extinguish
18. Engine Fire In Flight Fuel Selector --- Ott
Throttle --- Closed
Mixture --- Idle/Cut-Ott
2/
44
, AVIT 414 - Stage 25
Study online at
https://quizlet.com/_eefrvv
Fuel Pump Switch --- Ott
Heat & Defrost Controls --- Ott
19. Engine Fire During Start Starter --- Continue Cranking
Mixture --- Idle/Cut-Ott
Throttle --- Full Open
Fuel Pump Switch --- Ott
Fuel Selector --- Ott
20. Emergency Descent Throttle --- Idle
Mixture --- Rich
Bank --- 45°
Fuel Pump Switch --- On
Airspeed --- Do not exceed 125
KIAS Rollout --- Pilot Option
21. Spin Recovery Rudder --- Full Opposite to Direction of Rotation
Control Wheel --- Full Forward & Ailerons
Neutral Throttle --- Idle
Rudder --- Neutral (when rotation
stops) Control Wheel --- Smooth
Back Pressure Throttle --- As
Required
22. Power-Off Landing Airspeed --- Maintain 76 KIAS
Place to Land --- Pilot Option
Cabin & Passengers ---
Prepare
23. Engine Failure Airspeed --- Maintain 76
During Flight KIAS Fuel Selector --- Switch
Tanks Fuel Pump Switch ---
On Mixture --- Rich
Alternate Air --- Open
3/
44
, AVIT 414 - Stage 25
Study online at
Engine https://quizlet.com/_eefrvv
Instruments --- Check
4/
44
Study online at
https://quizlet.com/_eefrvv
1. Vso 45 KIAS
2. Vs 50 KIAS
3. Vx 64 KIAS
4. Vy 76 KIAS
5. Best Glide 76 KIAS
6. Cruise Cimb 87 KIAS
7. Vfe 102 KIAS
8. Vo 113 KIAS @ 2550
98 KIAS @ 1917
9. Vno 125 KIAS
10. Vne 154 KIAS
11. What factors will -Weight
affect stall speed? -CG Location
-Load Factor
-Wing Contamination
-Configuration (flaps)
12. Vs vs Vo Vs = Stalling speed or minimum steady flight speed at which
the a/c is controllable
Vso = Stalling speed or the minimum steady flight speed at
which the a/c is controllable in landing configuration
13. Vo vs Vno Vo = The speed in which full and abrupt control input will stall th
aircraft
(or cause structural damage if above Vo for given weight.
1/
44
, AVIT 414 - Stage 25
Study online at
https://quizlet.com/_eefrvv
Vno = The maximum structural cruising speed or better known
as normal operating speed. It should not be exceeded except
in smooth air and only then with caution.
14. How does Vo -It has to do with flying closer to the critical AoA. Heavier a/c
chnage with requires more lift to maintain altitude. More lift requires
weight? increasing AoA which consequently is closer to the critical AoA.
The closer an airfoil is to the critical AoA, the sooner it will
stall hence increasing the Vo speed.
-Lighter aircraft requires less lift to maintain altitude and
therefore flies at a smaller AoA and is futher away from the critical
AoA and will stall later/at a slower speed
15. Engine Failure Below Vr Throttle --- Idle
Brakes --- As Required
Engine --- Shutdown if Necessary
16. Engine Failure Above Vr Airspeed --- Maintain Safe
Landing --- Straight Ahead
Engine --- Shutdown if
Necessary
17. Electrical Fire in FlightEmergency Battery Switch --- Verify ARM
Battery Master Switch --- Ott
Alternator Switch --- Ott
Vents --- Open
Heat & Defrost Controls --- Ott
Fire --- Extinguish
18. Engine Fire In Flight Fuel Selector --- Ott
Throttle --- Closed
Mixture --- Idle/Cut-Ott
2/
44
, AVIT 414 - Stage 25
Study online at
https://quizlet.com/_eefrvv
Fuel Pump Switch --- Ott
Heat & Defrost Controls --- Ott
19. Engine Fire During Start Starter --- Continue Cranking
Mixture --- Idle/Cut-Ott
Throttle --- Full Open
Fuel Pump Switch --- Ott
Fuel Selector --- Ott
20. Emergency Descent Throttle --- Idle
Mixture --- Rich
Bank --- 45°
Fuel Pump Switch --- On
Airspeed --- Do not exceed 125
KIAS Rollout --- Pilot Option
21. Spin Recovery Rudder --- Full Opposite to Direction of Rotation
Control Wheel --- Full Forward & Ailerons
Neutral Throttle --- Idle
Rudder --- Neutral (when rotation
stops) Control Wheel --- Smooth
Back Pressure Throttle --- As
Required
22. Power-Off Landing Airspeed --- Maintain 76 KIAS
Place to Land --- Pilot Option
Cabin & Passengers ---
Prepare
23. Engine Failure Airspeed --- Maintain 76
During Flight KIAS Fuel Selector --- Switch
Tanks Fuel Pump Switch ---
On Mixture --- Rich
Alternate Air --- Open
3/
44
, AVIT 414 - Stage 25
Study online at
Engine https://quizlet.com/_eefrvv
Instruments --- Check
4/
44
