| Název: Name: | General Aviation C-14A | General Aviation C-14A |
| Originální název: Original Name: | General Aviation C-14A | |
| Kategorie: Category: | dopravní letoun | passenger aeroplane |
| Výrobce: Producer: | DD.MM.1932-DD.MM.1932 General Aviation Corp., Hasbrouck Heights, New Jersey | |
| Období výroby: Production Period: | DD.MM.1932-DD.MM.1932 | |
| Vyrobeno kusů: Number of Produced: | 1 konverze C-14 | |
| První vzlet: Maiden Flight: | DD.MM.RRRR | |
| Osádka: Crew: | 1 + 6 | |
| Základní charakteristika: Basic Characteristics: | ||
| Vzlet a přistání: Take-off and Landing: | CTOL - konvenční vzlet a přistání | CTOL - conventional take-off and landing |
| Uspořádání křídla: Arrangement of Wing: | jednoplošník | monoplane |
| Uspořádání letounu: Aircraft Concept: | klasické | conventional |
| Podvozek: Undercarriage: | pevný | fixed |
| Přistávací zařízení: Landing Gear: | kola | wheels |
| Technické údaje: Technical Data: | ||
| Hmotnost prázdného letounu: Empty Weight: | ? kg | ? lb |
| Vzletová hmotnost: Take-off Weight: | ? kg | ? lb |
| Maximální vzletová hmotnost: Maximum Take-off Weight: | 3268 kg | 7204 lb |
| Rozpětí: Wingspan: | 18.11 1) m | 59ft 5in1) |
| Délka: Length: | 13.18 m | 43ft 3in |
| Výška: Height: | 3.91 m | 12ft 10in |
| Plocha křídla: Wing Area: | 51.19 m2 | 551 ft2 |
| Plošné zatížení: Wing Loading: | ? kg/m2 | ? lb/ft2 |
| Pohon: Propulsion: | ||
| Kategorie: Category: | pístový | piston |
| Počet motorů: Number of Engines: | 1 | |
| Typ: Type: | Wright G1R-1820-7 Cyclone o výkonu 429 kW třílistá kovová vrtule | Wright G1R-1820-7 Cyclone, power 575 hp three-bladed metal propeler |
| Objem palivových nádrží: Fuel Tank Capacity: | ? | ? |
| Výkony: Performance: | ||
| Maximální rychlost: Maximum Speed: | 231.7 km/h v ? m | 144 mph in ? ft |
| Cestovní rychlost: Cruise Speed: | ? km/h v ? m | ? mph in ? ft |
| Rychlost stoupání: Climb Rate: | ? m/s | ? ft/min |
| Čas výstupu na výšku: Time to Climb to: | ? min do ? m | ? min to ? ft |
| Operační dostup: Service Ceiling: | ? m | ? ft |
| Dolet: Range: | 1086.3 km | 675 mi |
| Maximální dolet: Maximum Range: | ? km | ? mi |
| Výzbroj: Armament: | - | - |
| Uživatelské státy: User States: | | |
| Poznámka: Note: | - C-14 s novým motorem a třílistou vrtulí | - C-14 with new engine and three-bladed propeller |
| Zdroje: Sources: | Hegener, Henri. Fokker - The Man and his Aircraft. Harleyford Publications, Letchford 1961. Johnson, E. R. American Military Transport Aircraft Since 1925. McFarland & Company, Inc., Jefferson 2013. ISBN 978-0-7864-6269-8. Fahey, James C. U.S. Army Aircraft 1908-1946. Ships and Aircraft, Falls Church, 1964. www.nationalmuseum.af.mil | |
General Aviation C-14A
www.nationalmuseum.af.mil
www.nationalmuseum.af.mil
www.nationalmuseum.af.mil].
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| Date (DD.MM.RRRR) | DD.MM.RRRR |
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| Type | General Aviation C-14A |
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Ve služebním zbarvení.
| Period | - |
| Producer | - |
| Type | General Aviation C-14A |
| Camouflage | - |
| Country | - |
| Pilot | - |
| Production No. | - |
| Serial No. / Evidence No. | - |
| Tactical Marking / Imatriculation | - |
| Name | - |
| Unit | - |
| Base | - |
| Date (DD.MM.RRRR) | DD.MM.RRRR |
| Author | - |
| Print size / 300 DPI | - |
| Published with authors permit | - |
| Author Website | - |
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