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5 Cards in this Set

  • Front
  • Back
Elements of aircraft performance
- Take off and landing distance
- Rate of climb
- Fuel economy
- Cruising speed
Factors that affect the performance
- Air density
- Surface wind
- Runway surface
- Upslope/downslope runway
- Weight
Effect of increased density altitude?
Higher density altitude => air is less dense
- increased take off/landing distances
- Reduced rate of climb
- Increased true airspeed
Cessna 172 speeds - airspeed limitations
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)
Cessna 172 speeds - airspeed
Vy = 74 IAS
Vx = 56 IAS with 10 flaps