Projects:EASA PPL/Flight Performance and Planning: Difference between revisions
(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 | |||
== Terminology == | |||
* 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 | |||
== Power curve == | |||
== V-Speeds == | |||
* | *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 when off the blocks | |||
* Start: start engine | |||
* Taxi: taxi to runway | |||
* 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 | |||
* Memorize questions: | * 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? | ** What is minimum headwind to land at Helgoland? | ||
*** 1300ft Runway, MSL, ISA, 3200lbs -> 10kt | *** 1300ft Runway, MSL, ISA, 3200lbs -> 10kt |
Revision as of 17:22, 22 January 2023
Units
- 1 NM = 1.852 km
- 1m = 3,28 ft
- 1 US gal = 3.785 L
- 1 kg = 2.205 pounds
Terminology
- 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
Power curve
V-Speeds
- 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 when off the blocks
- Start: start engine
- Taxi: taxi to runway
- 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
- What is minimum headwind to land at Helgoland?