- Development
- Operational history
- Specifications (variant)
- Notes
- References
- External links
name=Wilson Global Explorer | image=Wilson Global Explorer N376LC (1) Santa Fe NM 25.06.95R edited-2.jpg | caption=The second Global Explorer undergoing maintenance at Santa Fe Airport, New Mexico, in 1995. }}{{Infobox Aircraft Type | type=amphibian | national origin=United States | manufacturer=Dean W. Wilson | designer=Dean W. Wilson | first flight=April 1991 | introduced=1994 | retired= | status=currently airworthy | primary user=international explorers | more users= | produced= | number built=2 | program cost= | unit cost= | developed from= | variants with their own articles= }} |
The Wilson Global Explorer is an American-built amphibious aircraft of the early 1990s which has been utilised to assist the exploration of remote areas. DevelopmentThe high-wing twin-engine Global Explorer was designed and constructed by Dean W. Wilson to the order of the explorer Hubert de Chevigny and the aircraft first flew in April 1991.[1] A second aircraft was constructed later. The Global Explorer has an unusually deep and wide fuselage design with many glazed areas, and accommodation at the rear for sleeping and other purposes. For added strength, the high-set wings are each supported by brace structures from the side fuselage and from the lower sponsons. The nose gear retracts forward of the hull and acts as a bumper for water operations.[2] The mainwheels can be removed and the fixed side sponsons assist flotation and manoeuvering on water. Various Lycoming engines of between 200 hp and 300 hp have been fitted, depending on the expected altitude to be reached during planned operations. Operational historyThe Explorer 1 was used by Hubert de Chevigny and Nicolas Hulot. It crashed near Paris. The Explorer 2 has been used by Canal + for the French show "dans la nature" with Stephane Perron, with the name "L'Avion", in the exploration and filming of a wide variety of locations including Australia's Great Barrier Reef, Argentina's Tierra del Fuego and Bolivia. It can be readily stripped down and shipped by sea to required locations and can carry and accommodate seven persons overnight.[3] The plane flew finally from Australia to France in 1998 and it was then withdrawn from use and the project was abandoned due to the unique aircraft's high cost of maintenance. Specifications (variant) {{Aircraft specs |ref= coastcomp.com |prime units?=imp |genhide= |crew=1 |capacity=6 passengers and crew |length m= |length ft=39 |length in=10 |length note= |span m= |span ft=67 |span in=0 |span note= |upper span m= |upper span ft= |upper span in= |upper span note= |mid span m= |mid span ft= |mid span in= |mid span note= |lower span m= |lower span ft= |lower span in= |lower span note= |swept m= |swept ft= |swept in= |swept note= |dia m= |dia ft= |dia in= |dia note= |width m= |width ft= |width in= |width note= |height m= |height ft=22 |height in=0 |height note= |wing area sqm= |wing area sqft= |wing area note= |swept area sqm= |swept area sqft= |swept area note= |volume m3= |volume ft3= |volume note= |aspect ratio= |airfoil= |empty weight kg= |empty weight lb=4995 |empty weight note= |gross weight kg= |gross weight lb=8000 |gross weight note= |max takeoff weight kg= |max takeoff weight lb= |max takeoff weight note= |fuel capacity= |lift kg= |lift lb= |lift note= |more general=
|eng1 number=2 |eng1 name=Lycoming IO-540 |eng1 type= |eng1 kw= |eng1 hp=300 |eng1 kn= |eng1 lbf= |eng1 note= |power original= |thrust original= |eng1 kn-ab= |eng1 lbf-ab= |eng2 number= |eng2 name= |eng2 type= |eng2 kw= |eng2 hp= |eng2 kn= |eng2 lbf= |eng2 note= |eng2 kn-ab= |eng2 lbf-ab= |eng3 number= |eng3 name= |eng3 type= |eng3 kw= |eng3 hp= |eng3 kn= |eng3 lbf= |eng3 note= |eng3 kn-ab= |eng3 lbf-ab= |more power=
|perfhide= |max speed kmh= |max speed mph=120 |max speed kts= |max speed note= |max speed mach= |cruise speed kmh= |cruise speed mph=110 |cruise speed kts= |cruise speed note= |stall speed kmh= |stall speed mph=60 |stall speed kts= |stall speed note= |never exceed speed kmh= |never exceed speed mph= |never exceed speed kts= |never exceed speed note= |minimum control speed kmh= |minimum control speed mph= |minimum control speed kts= |minimum control speed note= |range km= |range miles= |range nmi= |range note= |combat range km= |combat range miles= |combat range nmi= |combat range note= |ferry range km= |ferry range miles= |ferry range nmi= |ferry range note= |endurance= |ceiling m= |ceiling ft= |ceiling note= |g limits= |roll rate= |glide ratio= |climb rate ms= |climb rate ftmin= |climb rate note= |time to altitude= |sink rate ms= |sink rate ftmin= |sink rate note= |lift to drag= |wing loading kg/m2 |wing loading lb/sqft= |wing loading note= |disk loading kg/m2= |disk loading lb/sqft= |disk loading note= |power/mass= |thrust/weight= |more performance= }}{{aircontent |see also= |related= |similar aircraft= |lists= }}
Notes1. ^Simpson, 2001, p.583 2. ^coastcomp.com 3. ^coastcomp.com
References{{refbegin}}- {{cite book|last=Simpson|first=Rod|title=Airlife's World Aircraft|year=2001|publisher=Airlife Publishing Ltd|isbn=1-84037-115-3}}
{{refend}}External links{{commons category|Wilson Global Explorer}}- Website with photographs and data on the Global Explorer
3 : United States civil utility aircraft 1990–1999|Homebuilt aircraft|Amphibious aircraft |