gptkbp:instanceOf
|
aircraft
|
gptkbp:aircraft
|
general aviation
cantilever wing
|
gptkbp:cockpit
|
open cockpit
|
gptkbp:constructionMaterial
|
metal construction
|
gptkbp:controls
|
dual control
|
gptkbp:countryOfOrigin
|
gptkb:United_Kingdom
|
gptkbp:crew
|
1
|
gptkbp:design
|
gptkb:Miles_Aircraft_Ltd.
low-wing monoplane
|
gptkbp:engine
|
Gipsy Major engine
|
gptkbp:engineType
|
inline engine
|
gptkbp:firstFlight
|
1946
1946-07-01
|
gptkbp:fuelCapacity
|
150 liters
|
gptkbp:headlights
|
conventional tail
|
gptkbp:historicalSignificance
|
post-war light aircraft development
|
https://www.w3.org/2000/01/rdf-schema#label
|
Miles M.39 Messenger
|
gptkbp:introduced
|
1946
|
gptkbp:landingGear
|
tailwheel
|
gptkbp:length
|
8.23 m
|
gptkbp:manufacturer
|
gptkb:Miles_Aircraft
|
gptkbp:marketedAs
|
M.39_Messenger
|
gptkbp:maxSpeed
|
200 km/h
|
gptkbp:maxTakeoffWeight
|
1,600 kg
|
gptkbp:notableFeature
|
good short-field performance
|
gptkbp:numberBuilt
|
50
|
gptkbp:passengerCapacity
|
2
|
gptkbp:primaryUser
|
gptkb:Royal_Air_Force
|
gptkbp:productionYears
|
1946-1950
|
gptkbp:propulsion
|
two-bladed propeller
|
gptkbp:range
|
800 km
|
gptkbp:retired
|
1960s
|
gptkbp:role
|
light aircraft
training aircraft
|
gptkbp:services
|
4,500 m
1946-1960s
|
gptkbp:successor
|
Miles M.65 Gemini
|
gptkbp:type
|
civil aircraft
|
gptkbp:usedBy
|
civil aviation
|
gptkbp:variant
|
Miles_M.39A_Messenger
Miles_M.39B_Messenger
|
gptkbp:weight
|
1,200 kg
|
gptkbp:wingArea
|
15.5 m²
|
gptkbp:wingspan
|
10.67 m
|