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“Teaching the Science, Inspiring the Art, Producing Aviation Candidates!” Aircraft Performance Aircraft Performance Flying 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

Aircraft Performance

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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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Page 1: Aircraft Performance

“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

Page 2: Aircraft Performance

RoadmapRoadmapPOHDensity AltitudeTakeoff DistanceCruise Performance, Power & Fuel

BurnLanding DistanceCrosswinds

Page 3: Aircraft Performance

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

Page 4: Aircraft Performance

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

Page 5: Aircraft Performance

Maneuvering SpeedManeuvering Speed

VA = 113 kts

Page 6: Aircraft Performance

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

Page 7: Aircraft Performance

Density AltitudeDensity Altitude

Page 8: Aircraft Performance

Density Altitude ChartDensity Altitude Chart

Page 9: Aircraft Performance

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

Page 10: Aircraft Performance

Takeoff Distance

Cessna 172R

Page 11: Aircraft Performance

0 deg Takeoff Perf0 deg Takeoff Perf

Page 12: Aircraft Performance

25 deg Takeoff Perf25 deg Takeoff Perf

Page 13: Aircraft Performance

Climb PerformanceClimb Performance

Vx=Best Angle of ClimbGain maximum altitude in shortest

distanceVY=Best Rate of Climb

Gain maximum altitude in shortest timeCruise Climb

Page 14: Aircraft Performance

Clim

b Perform

anceC

essna 172R

Page 15: Aircraft Performance

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

Page 16: Aircraft Performance

Cruise

Performance

Cessna 172R

Page 17: Aircraft Performance

Cruise

Performance

Cessna 172R

Page 18: Aircraft Performance

Engine PerformanceEngine Performance

Page 19: Aircraft Performance

Performance CruisePerformance Cruise

VG = VL/D = 65 kts

Page 20: Aircraft Performance

Economy CruiseEconomy Cruise

VS = 55 kts

Page 21: Aircraft Performance

Endurance GraphEndurance Graph

Page 22: Aircraft Performance

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

Page 23: Aircraft Performance

Landing Distance

Cessna 172R

Page 24: Aircraft Performance

40 deg Landing Perf40 deg Landing Perf

Page 25: Aircraft Performance

Landing Distance

Boeing 727

Page 26: Aircraft Performance

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

Page 27: Aircraft Performance

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