Projects:EASA PPL/Flight Performance and Planning

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Revision as of 14:35, 20 January 2023 by Marcluer (talk | contribs) (Created page with "* Units: ** 1 NM = 1.852 km ** 1m = 3,28 ft ** 1 US gal = 3.785 L ** 1 kg = 2.205 pounds * Terminologie: ** Neutrally stable: center of gravity towards rear limit ** Datum: on longitudinal axis, not necessarily between nose and tail ** backside of power curve: speed unstable ** rate of climb: climb gradient (%) * TAS / 100 ** climb gradient: *** (thrust - drag) / weigth * 100 *** Rate of climb / True airspeed **climb angle: tan-1 (gradient (rise/run) e.g. 5,2% -> 5.2/1...")
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  • Units:
    • 1 NM = 1.852 km
    • 1m = 3,28 ft
    • 1 US gal = 3.785 L
    • 1 kg = 2.205 pounds
  • Terminologie:
    • Neutrally stable: center of gravity towards rear limit
    • Datum: on longitudinal axis, not necessarily between nose and tail
    • backside of power curve: speed unstable
    • rate of climb: climb gradient (%) * TAS / 100
    • climb gradient:
      • (thrust - drag) / weigth * 100
      • Rate of climb / True airspeed
    • climb angle: tan-1 (gradient (rise/run) e.g. 5,2% -> 5.2/100 -> tan-1 (0.052)
    • glide for max time (endurance) :
      • at minimum rate of descent, TAS for max time will increase with altitude
      • ~max rate of climb speed (Vmindrag = VY?)
    • glide for max range (distance):
      • Lift / Drag ratio at maximum, TAS for max range will increase with altitude
    • VS0: stalling speed in landing configuration
    • VS1: stalling speed in specific configuration (e.g. cruise)
    • VX: Best angle of climb (obstacle avoidance), max excess of thrust over drag
    • VY: Best rate of climb speed, max excess power (diff between drag curve and power curve), flaps reduce VY


  • Weight & Mass:
    • BEM: Basic empty mass
    • DOM: Dry operating mass (BEM + variable load (Crew+special equipment)
    • ZFM: Zero fuel mass (DOM + TL)
    • TL / TF: Traffic Load / Payload
    • Max permissible take-off mass - wake turbulence category: L 7000kg
  • Fuel:
    • Block / Ramp Fuel: In the tank before the trip
    • Start
    • Taxi
    • Trip: take off, climb, cruise, descent, approach, landing
    • Reserve:
      • Contingency: 5% of trip or 5min at cruise comsumption
      • Alternate: missed approach, climb, cruise, descent, approach, landing
      • Final reserve: 45min
      • Additional: choice by PIC
    • Avgas: 0,72 density / specific gravity
  • Flight Plan:
    • Required when: IFR, cross-border
    • Total estimated time: from take-off to arrive over destination
    • Elapsed time format: 1h55min -> 0155
    • Item 7, Identifier for Radio equipped aircraft: RTF callsign
    • Item 9, Number and Type of Aircraft / Aircraft designator:
      • Number of Aircraft: in group
      • No designator: ZZZZ + entry in item 18
    • Item 10, Equipment: Carriage of a Mode A+C (altitude) Transponder -> Letter C
    • Item 15, Speed: TAS
    • Item 16, Destination estimated time to: EDDM0215 (2h 15min flight time)
    • Item 19,
      • Number of passangers: TBN (to be notified) if not known when filing
      • Emergency and survival equipment: cross out the relevant boxes of equipment NOT carried


  • Memorize questions:
    • What is minimum headwind to land at Helgoland?
      • 1300ft Runway, MSL, ISA, 3200lbs -> 10kt
    • Landing distance?
      • OAT: 27°C, 3000ft alt, 2900lbs, tailwind 5kt, -> Landing distance: 1850ft
      • OAT: ISA+15°C, 0ft alt, 2940lbs, headwind 10kt, grass factor 1.38 -> Landing distance: 1794ft
    • Ground distance to reach height:
      • OAT: 25°C, 1000ft alt, 3600lbs, 100KIAS, 15kt headwind -> Ground distance: 15596ft
    • Wind correction angle:
      • True course 017° / TAS 420kt - Wind 340°/30kt -> WCA -2°; 396kt GS
      • True cource 42°, Variantion 6°, Deviation card for 045=-4 -> 052° Compass heading
    • Map
      • Villingen to Freudenstadt: 24NM distance
      • Villingen to Freundenstadt: min altitude 4500ft
      • Peiting to Immenstadt: 32NM distance
      • Saulgau to Altenstadt: Magnetic 091°, 54NM
      • Erbach to Poltringen: Magnetic 289°, 76km
      • Sigmaringen to Biberach: Magnetic 084°, 22NM
      • Zurich VOLMET: 127.20 MHz
      • Nav aid @ 48°23N 008°39E -> VOR
    • Fuel consumption:
      • FL 75, OAT 10°, 2300rpm, -> 11.6gph / 160kt
      • 3500lbs, 2500ft alt, OAT 10°C, FL140 (OAT -5°C) -> 23,5min / 7.1gal / 48.5 NM
      • 3663lbs, AVGAS (6lbs/gal), 74gal, Take off MSL, Headwind 40kt, Cruise 8000ft, 2300RPM -> 633NM
      • Tripfuel: 136kg , 2h45min flight time, -> 3h34min
      • 10lbs startup + taxi,
        • 64 pounds per hour
        • Total block 283 lbs = 205lbs cruise + 10lbs startup + 6lbs (1gal) + 62 lbs reserve (205*30%)
    • Weather:
      • EGLL forecast 0600 -> 1500m min vis