Grumman G-730 Mallard II

GPTKB entity

Properties (49)
Predicate Object
gptkbp:instanceOf aircraft
gptkbp:aircraft 3,175 kg
civil aviation
conventional tail
high-wing
amphibious aircraft
gptkbp:capacity up to 10 passengers
gptkbp:cockpit enclosed cockpit
gptkbp:constructionMaterial aluminum
gptkbp:crew 1 to 2 pilots
gptkbp:decommissioned 1970s
gptkbp:design 1940s
floatation gear
Grumman_design_team
gptkbp:engine 2
gptkbp:engineType radial engine
gptkbp:firstFlight 1946
gptkbp:fuelCapacity 1,500 liters
gptkbp:headlights T-tail
gptkbp:height 4.57 meters
gptkbp:historicalSignificance first post-war amphibious aircraft
https://www.w3.org/2000/01/rdf-schema#label Grumman G-730 Mallard II
gptkbp:influencedBy gptkb:Grumman_G-21_Goose
gptkbp:landingGear retractable landing gear
gptkbp:length 12.80 meters
gptkbp:manufacturer gptkb:Grumman_Aircraft_Engineering_Corporation
gptkbp:maxSpeed 200 knots
gptkbp:maxTakeoffWeight 4,536 kg
gptkbp:nickname gptkb:Mallard
gptkbp:notableOperations gptkb:United_States_Navy
gptkbp:numberBuilt 59
gptkbp:operationalHistory used in commercial and military roles
gptkbp:passengerCapacity 1,000 kg
gptkbp:productionLocation gptkb:United_States
gptkbp:productionYears 1946-1951
gptkbp:propulsion variable-pitch propellers
gptkbp:range 1,200 nautical miles
gptkbp:relatedAircraft gptkb:Grumman_G-21_Goose
gptkbp:retirementYear 1980s
gptkbp:role transport aircraft
gptkbp:services 15,000 feet
gptkbp:speed 160 knots
gptkbp:successor gptkb:Grumman_G-21_Goose
gptkbp:takeoffDistance 1,000 feet
1,200 feet
gptkbp:type amphibious aircraft
gptkbp:variant G-73 Mallard
gptkbp:wingArea 40.5 square meters
gptkbp:wingspan 15.24 meters