| 词条 | Tecnam P92 | ||||||||||||||||
| 释义 |
The Tecnam P92 Echo and Tecnam P92 Eaglet are Italian high-winged, light aircraft, designed by Luigi Pascale and built by Tecnam of Naples.[1][2] Design and developmentThe P92 design dates to 1960, but versions comply with the Fédération Aéronautique Internationale microlight rules and US light-sport aircraft rules. It features a strut-braced high-wing, an enclosed cabin with two-seats-in-side-by-side configuration accessed by doors, fixed tricycle landing gear or conventional landing gear and a single engine in tractor configuration.[2] The aircraft is made sheet aluminum tubing. Standard engines available are the {{convert|100|hp|kW|0|abbr=on}} Rotax 912ULS, {{convert|115|hp|kW|0|abbr=on}} Rotax 914 and the {{convert|100|hp|kW|0|abbr=on}} Lycoming O-233 four-stroke powerplants.[2] The P92 Eaglet was introduced in 2008. It employs a cockpit section made of steel tubing covering in sheet aluminum and a monocoque tail cone. It also features a new wing design, a rear window and a cabin that is {{convert|117|cm|in|0|abbr=on}} wide.[2] The design is an accepted Federal Aviation Administration special light-sport aircraft.[3] Variants
OperatorsCivilThe P92 is popular with flight training schools and is also operated by private individuals and companies. Military
Specifications (P92 Echo Super){{aircraft specifications|plane or copter?=plane |jet or prop?=prop |ref=manufacturer[5] |crew=one, pilot |capacity=one passenger |payload main= |payload alt= |length main= 6.40 m |length alt= 20 ft 11 in |span main= 8.70 m |span alt= 28 ft 6 in |height main= 2.50 m |height alt= 8 ft 3 in |area main= 12 m2 |area alt= 129 sq ft |airfoil= |empty weight main= 670 lb |empty weight alt= 304 kg |loaded weight main= |loaded weight alt= |useful load main= 650 lb |useful load alt= 295 kg |max takeoff weight main= 1,212 lb |max takeoff weight alt= 550 kg |more general= |engine (prop)= Rotax 912ULS |type of prop= |number of props=1 |power main= 100 hp |power alt= 73.5 kW |power original= |max speed main= 235 km/h at sea-level |max speed alt= 124 kn |cruise speed main= 215 km/h |cruise speed alt= 105 kn |stall speed main= 63 km/h |stall speed alt= 33 kn |never exceed speed main= 270 km/h |never exceed speed alt= 168 mph |range main= 800 km |range alt= 500 mi |ceiling main= 4500 m |ceiling alt= 14,760 ft |climb rate main= 354 m/min |climb rate alt= 1,161 ft/min |loading main= |loading alt= |thrust/weight= |power/mass main= |power/mass alt= |more performance=
|armament= |avionics= }} See also{{aircontent||related= |similar aircraft=
|lists= |see also= }} References1. ^Bayerl, Robby; Martin Berkemeier; et al: World Directory of Leisure Aviation 2011-12, page 80. WDLA UK, Lancaster UK, 2011. {{ISSN|1368-485X}} 2. ^1 2 3 4 5 6 7 8 Tacke, Willi; Marino Boric; et al: World Directory of Light Aviation 2015-16, pages 82-83. Flying Pages Europe SARL, 2015. {{ISSN|1368-485X}} 3. ^{{cite web|url = https://www.faa.gov/aircraft/gen_av/light_sport/media/SLSA_Directory.xlsx|title = SLSA Make/Model Directory|accessdate = 21 March 2017|last = Federal Aviation Administration|date = 26 September 2016}} 4. ^{{cite web|title=Tecnam to Produce P92 Tail Dragger |url=http://www.flyingmag.com/aircraft/lsasport/tecnam-produce-p92-tail-dragger |accessdate=6 August 2012}} 5. ^{{cite web|url = http://www.tecnam.com/ing/echosuper.cfm|title = Technical Features|accessdate = 21 March 2017|author= Costruzioni Aeronautiche Tecnam|work = tecnam.com|year = 1999|archiveurl = https://web.archive.org/web/20070601202554/http://www.tecnam.com/ing/echoSuper.cfm|archivedate = 1 June 2007}} External links{{commons category|Tecnam P92}}
5 : Tecnam aircraft|Italian civil utility aircraft 1990–1999|Single-engined tractor aircraft|High-wing aircraft|Aircraft first flown in 1993 |
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