Mainair Blade
{{Short description|British ultralight trike}}
{{Use dmy dates|date=March 2018}}
{{Use British English|date=March 2018}}
| {{Infobox Aircraft Begin
| name=Blade | image=Mainair blade ultralight g-mzbl kemble arp.jpg | caption=Mainair Blade 582 }}{{Infobox Aircraft Type | type=Ultralight trike | national origin=United Kingdom | manufacturer=Mainair Sports | designer= | first flight= | introduced= | retired= | status=Production completed | primary user= | more users= | produced= | number built=60 (February 2000) | developed from= | variants with their own articles=Mainair Rapier }} |
The Mainair Blade is a British ultralight trike that was designed and produced by Mainair Sports and later P&M Aviation. The aircraft was supplied as a completed aircraft.Cliche, Andre: Ultralight Aircraft Shopper's Guide 8th Edition, page C-14. Cybair Limited Publishing, 2001. {{ISBN|0-9680628-1-4}}Bertrand, Noel; Rene Coulon; et al: World Directory of Leisure Aviation 2003-04, page 104. Pagefast Ltd, Lancaster OK, 2003. {{ISSN|1368-485X}}Downey, Julia: 2000 Trike and 'Chute Directory, Kitplanes, Volume 17, Number 2, February 2000, page 46 and 47. Kitplanes Acquisition Company. {{ISSN|0891-1851}}
In the early 2000s Mainair was merged with rival Pegasus Aviation into P&M Aviation, but production of the Blade continued. As the company rationalized the two aircraft lines, Blade production ended. By 2012 the manufacturer indicated, "This aircraft is no longer in production...Full spares and support are still available and will remain so for the foreseeable future. Complete aircraft can still be manufactured but by special request only."{{Cite web|url = http://www.pmaviation.co.uk/mainair-blade.html|title = The Mainair Blade |accessdate = 18 January 2012|last = P&M Aviation |year = n.d.}}
Design and development
The aircraft was designed as a high-end touring trike, to comply with the Fédération Aéronautique Internationale microlight category, including the category's maximum gross weight of {{convert|450|kg|lb|0|abbr=on}} and is also certified to comply with UK BCAR Section "S". The aircraft has a maximum gross weight of {{convert|390|kg|lb|0|abbr=on}}. It features a cable-braced hang glider-style high-wing, weight-shift controls, a two-seats-in-tandem, open cockpit, tricycle landing gear and a single engine in pusher configuration.
The aircraft is made from bolted-together aluminium tubing, with its double-surface wing covered in Dacron sailcloth. Its {{convert|10.6|m|ft|1|abbr=on}} span wing is supported by a single tube-type kingpost and uses an "A" frame control bar. The occupants are accommodated in tandem seating, with a fibreglass cockpit fairing that includes a small windshield. Engines factory supplied include the {{convert|37|kW|hp|0|abbr=on}} Rotax 503 twin cylinder, two-stroke, air cooled powerplant as well as the twin cylinder, two-stroke, liquid cooled {{convert|48|kW|hp|0|abbr=on}} Rotax 582 and the four cylinder, four-stroke {{convert|60|kW|hp|0|abbr=on}} Rotax 912UL and {{convert|74.5|kW|hp|0|abbr=on}} Rotax 912ULS.
Operational history
Blades have been used for a number of microlight record distance flights, including a flight to Australia by Colin Bodill and Simon Reeve and a flight around the world by Bodill.
The Blade 912 set the record for London to Sydney by microlight of 49 days (175 hours of flying) at an average speed of {{convert|124|km/h|mph|0|abbr=on}}.
Variants
;Blade 582
:Version powered by a {{convert|48|kW|hp|0|abbr=on}} Rotax 582 engine. Price in 2003 was £16,450.
;Blade 912
:Version powered by a {{convert|60|kW|hp|0|abbr=on}} Rotax 912UL or the {{convert|74.5|kW|hp|0|abbr=on}} Rotax 912ULS. In 2003 it was reported that the Blade 912 accounted for the majority of customer orders. Price in 2003 was £21,800.
Specifications (Blade 912)
{{Aircraft specs
|prime units?=met
|genhide=
|crew=one
|capacity=one passenger
|length m=
|length ft=
|length in=
|length note=
|span m=10.6
|span ft=
|span in=
|span note=
|height m=
|height ft=
|height in=
|height note=
|wing area sqm=15.6
|wing area sqft=
|wing area note=
|aspect ratio=
|airfoil=
|empty weight kg=190
|empty weight lb=
|empty weight note=
|gross weight kg=390
|gross weight lb=
|gross weight note=
|fuel capacity={{convert|65|L}}
|more general=
|eng1 number=1
|eng1 name=Rotax 912
|eng1 type=four cylinder, four-stroke aircraft engine
|eng1 kw=60
|eng1 hp=
|prop blade number=
|prop name=
|prop dia m=
|prop dia ft=
|prop dia in=
|prop note=
|perfhide=
|max speed kmh=145
|max speed mph=
|max speed kts=
|max speed note=
|cruise speed kmh=106
|cruise speed mph=
|cruise speed kts=
|cruise speed note=
|stall speed kmh=48
|stall speed mph=
|stall speed kts=
|stall speed note=
|never exceed speed kmh=
|never exceed speed mph=
|never exceed speed kts=
|never exceed speed note=
|range km=
|range miles=
|range nmi=220
|range note=
|endurance=
|ceiling m=
|ceiling ft=10000
|ceiling note=
|g limits=
|roll rate=
|glide ratio=
|climb rate ms=6.35
|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=25.0
|wing loading lb/sqft=
|wing loading note=
|power/mass=
|thrust/weight=
|more performance=
|avionics=
}}
{{aircontent
|see also=
|related=
|similar aircraft=
|lists=
}}
References
{{reflist}}
External links
{{commons category|Mainair Blade}}
- {{Official website|http://www.pmaviation.co.uk/mainair-blade.html}}
{{P&M Aviation aircraft}}
Category:1990s British ultralight aircraft