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5 Cards in this Set
- Front
- Back
Elements of aircraft performance
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- Take off and landing distance
- Rate of climb - Fuel economy - Cruising speed |
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Factors that affect the performance
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- Air density
- Surface wind - Runway surface - Upslope/downslope runway - Weight |
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Effect of increased density altitude?
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Higher density altitude => air is less dense
- increased take off/landing distances - Reduced rate of climb - Increased true airspeed |
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Cessna 172 speeds - airspeed limitations
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Vne = 163 IAS (never exceed)
Vno = 129 IAS (normal operations) Va ( maneuvering speed) - 2550 = 105 IAS - 2200 = 98 IAS - 1900 = 90 IAS Vfe = 110 IAS Vso = 40 IAS (stalling speed in landing config) |
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Cessna 172 speeds - airspeed
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Vy = 74 IAS
Vx = 56 IAS with 10 flaps |