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Aircraft Performance. Flying Further Than Any Other Aircraft in History. 26,389.3 miles. Written for the Notre Dame Pilot Initiative By the Pilots of the University of Notre Dame. Roadmap. POH Density Altitude Takeoff Distance Cruise Performance, Power & Fuel Burn Landing Distance - PowerPoint PPT Presentation
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“Teaching the Science, Inspiring the Art, Producing Aviation Candidates!”
Aircraft PerformanceAircraft PerformanceFlying Further Than Any Other
Aircraft in History
Written for the Notre Dame Pilot Initiative By the Pilots of the University of Notre Dame
26,389.3 miles
RoadmapRoadmapPOHDensity AltitudeTakeoff DistanceCruise Performance, Power & Fuel
BurnLanding DistanceCrosswinds
Pilot’s Operating Handbook Pilot’s Operating Handbook (POH)(POH)
Also known as Approved Flight Manual (AFM) Organized into Sections
General Limitations Emergency Procedures Normal Procedures Performance Weight & Balance Airplane & Systems Description Handling, Service, & Maintenance Supplements
Frequent TermsFrequent TermsMaximum Takeoff Weight (MTOW)
Maximum gross weight at which the airplane is permitted to takeoff
Maneuvering SpeedMaximum speed for maneuvers at which
full application of the primary flight controls cannot overstress the airframe
Maneuvering SpeedManeuvering Speed
VA = 113 kts
Density Altitude RevisitedDensity Altitude RevisitedDensity Altitude is pressure altitude
corrected for nonstandard temperatureVaries directly with temperature and
humidityVaries indirectly with pressure
It is a number which tells you what the airplane (wings and engine) feels
Density AltitudeDensity Altitude
Density Altitude ChartDensity Altitude Chart
Takeoff DistanceTakeoff DistanceTwo Varieties
Ground Roll Distance to Clear 50 ft obstacle
Also known as Takeoff Distance Distance for aircraft to clear a 50-foot obstacle after a
standing start at maximum takeoff powerFactors
↑ Weight = ↑ Distance (and speed) ↑ Air Density = ↓ Distance ↑ Headwind = ↓ Distance ↑ Slope = ↑ Ground Roll ↑ Flaps = ↓ Ground Roll ↑ Friction = ↑ Ground Roll
Takeoff Distance
Cessna 172R
0 deg Takeoff Perf0 deg Takeoff Perf
25 deg Takeoff Perf25 deg Takeoff Perf
Climb PerformanceClimb Performance
Vx=Best Angle of ClimbGain maximum altitude in shortest
distanceVY=Best Rate of Climb
Gain maximum altitude in shortest timeCruise Climb
Clim
b Perform
anceC
essna 172R
Cruise FlightCruise FlightAn airplane is more efficient at altitude
Wings Engines
Weather is generally confined to the troposphere so you can fly over it
Higher gives more options in case of emergencies
Reserves Day VFR: 30 minutes at normal cruising speed Night VFR: 45 minutes at normal cruising
speed
Cruise
Performance
Cessna 172R
Cruise
Performance
Cessna 172R
Engine PerformanceEngine Performance
Performance CruisePerformance Cruise
VG = VL/D = 65 kts
Economy CruiseEconomy Cruise
VS = 55 kts
Endurance GraphEndurance Graph
Landing DistancesLanding Distances Two Varieties
Ground Roll Distance over a 50 foot obstacle
Also known as Takeoff Distance Distance for aircraft to clear a 50-foot obstacle after a standing
start at maximum takeoff power Factors
↑ Weight = ↑ Distance (and speed) ↑ Air Density = ↓ Distance ↑ Headwind = ↓ Distance ↑ Slope = ↓ Ground Roll ↑ Flaps = ↓ Distance ↑ Friction = ↓ Ground Roll
Maximum performance landings are always accomplished with full flaps Stiff crosswinds sometimes dictate the use of partial flaps
Landing Distance
Cessna 172R
40 deg Landing Perf40 deg Landing Perf
Landing Distance
Boeing 727
CrosswindsCrosswindsMaximum Demonstrated Crosswind
Component is the maximum crosswind that existed during FAA certificationOften is not close to real maximum
capability of aircraftWeak link is generally lack of rudder
authority (not enough deflection)Often VX-Wind = 0.3 VS0
Crosswind ChartCrosswind Chart
30 knot wind,30 knot wind,
30 deg off of 30 deg off of the nose the nose
= 26 knot = 26 knot headwind headwind
= 15 knot = 15 knot crosswindcrosswind