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GENERAL DISCLAIMERS
This site is for educational purposes in nature and is not designed to assist pilots and aircrews for flight planning or familiarization. It may be not used in conjunction with pre-flight or flight information needed to satisfy any requirements of the Federal Aviation Administration (FAA) and is not to be considered as any source of information to meet pre-flight or flight action. If you are in an actual airplane or planning for an actual flight, you are to de-install this app or navigate away from this website immediately.
Takeoff performance data. The calcualtor is copied from the following website: Thomas Arsenault Takeoff Performance Calculator. The numbers shown here are changed for the Vans RV-6A aircraft.
The following table gives takeoff distances (in feet) for RV-6A aircraft, showing the effects of aircraft weight, head-wind, altitude and ambient temperature, with flaps up on a hard runway. The figures include an extra 10% allowance required by a FAA change sheet inserted into the POH.
Density altitude | ||||||||||
---|---|---|---|---|---|---|---|---|---|---|
Sea level @ 59°F 15°C | 2500ft @ 50°F 10°C | 5000ft @ 41°F 5°C | 7500ft @ 32°F 0°C | |||||||
Gross weight (lb) |
IAS at 50ft |
Head wind (mph) |
Ground run |
To clear 50ft obstacle |
Ground run |
To clear 50ft obstacle |
Ground run |
To clear 50ft obstacle |
Ground run |
To clear 50ft obstacle |
985 | 55 | 0 | 283 | 507 | 338 | 598 | 406 | 712 | 497 | 891 |
10 | 189 | 371 | 231 | 442 | 280 | 533 | 348 | 676 | ||
20 | 114 | 250 | 140 | 306 | 176 | 374 | 224 | 484 | ||
1200 | 60 | 0 | 410 | 712 | 491 | 861 | 588 | 1056 | 728 | 1401 |
10 | 283 | 533 | 345 | 653 | 419 | 812 | 527 | 1095 | ||
20 | 179 | 377 | 221 | 468 | 276 | 592 | 387 | 816 | ||
1650 | 65 | 0 | 562 | 991 | 676 | 1241 | 816 | 1612 | 1017 | 2506 |
10 | 400 | 761 | 488 | 965 | 598 | 1271 | 754 | 2022 | ||
20 | 263 | 553 | 328 | 715 | 410 | 962 | 527 | 1576 |
Takeoff distance calculator
The calculator below performs takeoff distance calculations using the data from the table above. It works by calculating the density altitude (using the pressure, temperature, dew-point and airfield elevation), then interpolating between the data points in the table. The answer it gives is the Takeoff Distance Required (TODR) - i.e. the distance needed to reach a height of 50 feet.
Important safety note:This calculator is for use doing takeoff performance calculations before flying RV-6A aircraft, but you should be aware that this calculator is specific to that particular aircraft. The answers it gives are not applicable to any other aircraft. You must use the data taken from the POH of your particular aircraft.