de Havilland Dragon Rapide
de Havilland. A light piston aircraft for small operators.
- Seats
- Standard 8
- Range
- 900 km
- Cruise
- 190 km/h
- Payload
- 850 kg
- Take off run
- 350 m
- Fuel burn
- 85 kg per block hour
- Reference price
- $28,000 in 1958 dollars
- Production ends
- 1946-01-01
- Confidence
- estimated (to be verified)
Source: Checked field by field against published sources, see evidence. Fields not listed under verifiedFields are estimates.
Evidence
Figures below were checked against published sources. The game value can differ from the checked value where sources used another definition, for example a range at maximum fuel against a range with a full load. Agreement describes the game value at the time of checking. Checked figures that agree: rangeKm, mtowT, seats.
| Field | Checked value | Agreement | Source |
|---|---|---|---|
| cruiseKmh | 212 km/h | close | en.wikipedia.org |
| rangeKm | 895 km | confirmed | en.wikipedia.org |
| mtowT | 2.5 tonnes | confirmed | en.wikipedia.org |
| takeoffRunM | 265 m | differs | en.wikipedia.org |
| introDate | 1934 year | differs | en.wikipedia.org |
| seats | 8 seats | confirmed | en.wikipedia.org |
Caveats are kept in the repository file docs/research/aircraft-verification.json. The web pages cited were read through a summarising fetch tool, so figures should be rechecked against the originals before any release.