{{Short description|British ultralight trike}} {{Use dmy dates|date=March 2018}} {{Use British English|date=March 2018}} <!-- This article is a part of [[Wikipedia:WikiProject Aircraft]]. Please see [[Wikipedia:WikiProject Aircraft/page content]] for recommended layout. --> {{Infobox aircraft | name = Blade | logo = | logo_size = | image = Mainair blade ultralight g-mzbl kemble arp.jpg | alt = | caption = Mainair Blade 582 | long_caption = | other_names = | aircraft_type = [[Ultralight trike]] | aim = | outcome = | related = | national_origin = United Kingdom | manufacturer = [[Mainair Sports]]<br />[[P&M Aviation]] | design_group = | designer = | builder = | issuer = | status = Production completed | owners = | primary_user = | more_users = | service = | major_applications = | proposals = | prototypes = | number_built = 60 (February 2000) | construction_number = | civil_registration = | military_serial = | radio_code = | requirement = | aircraft_carried = | flights = | total_hours = | total_distance = | construction_date = | introduction = | retired = | first_flight = | initiated = | in_service = | last_flight = | expected = | developed_from = | variants = [[Mainair Rapier]] | developed_into = | preservation = | fate = | predecessors = | successors = | concluded = }} 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.<ref name="Cliche">Cliche, Andre: ''Ultralight Aircraft Shopper's Guide'' 8th Edition, page C-14. Cybair Limited Publishing, 2001. {{ISBN|0-9680628-1-4}}</ref><ref name="WDLA04">Bertrand, Noel; Rene Coulon; et al: ''World Directory of Leisure Aviation 2003-04'', page 104. Pagefast Ltd, Lancaster OK, 2003. {{ISSN|1368-485X}}</ref><ref name="KitplanesFeb2000">Downey, Julia: ''2000 Trike and 'Chute Directory'', Kitplanes, Volume 17, Number 2, February 2000, page 46 and 47. Kitplanes Acquisition Company. {{ISSN|0891-1851}}</ref>
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."<ref name="WDLA04" /><ref name="Blade">{{Cite web|url = http://www.pmaviation.co.uk/mainair-blade.html|title = The Mainair Blade |accessdate = 18 January 2012|last = P&M Aviation |date = n.d.}}</ref>
==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 [[Flying wires|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]].<ref name="Cliche" />
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]] [[Aircraft fairing|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]].<ref name="Cliche" /><ref name="WDLA04" />
==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.<ref name="WDLA04" />
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}}.<ref name="KitplanesFeb2000" />
==Variants== ;Blade 582 :Version powered by a {{convert|48|kW|hp|0|abbr=on}} [[Rotax 582]] engine. Price in 2003 was [[Pound sterling|£]]16,450.<ref name="WDLA04" /> ;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.<ref name="WDLA04" /> <!-- ==Aircraft on display== -->
==Specifications (Blade 912) == {{Aircraft specs |ref=Bertrand and Kitplanes<ref name="WDLA04" /><ref name="KitplanesFeb2000" /> |prime units?=met<!-- imp or kts first for US aircraft, and UK aircraft pre-metrification, met(ric) first for all others. You MUST choose a format, or no specifications will show --> <!-- General characteristics --> |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= <!-- Powerplant --> |eng1 number=1 |eng1 name=[[Rotax 912]] |eng1 type=four cylinder, [[four-stroke]] [[aircraft engine]] |eng1 kw=60<!-- prop engines --> |eng1 hp=<!-- prop engines -->
|prop blade number=<!-- propeller aircraft --> |prop name= |prop dia m=<!-- propeller aircraft --> |prop dia ft=<!-- propeller aircraft --> |prop dia in=<!-- propeller aircraft --> |prop note=
<!-- Performance --> |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=<!-- if range unknown --> |ceiling m= |ceiling ft=10000 |ceiling note= |g limits= |roll rate=<!-- aerobatic --> |glide ratio=<!-- sailplanes --> |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= }}
<!-- ==See also== --> {{aircontent <!-- include as many lines are appropriate. additional lines/entries with carriage return. --> |see also= |related=<!-- related developments --> |similar aircraft=<!-- similar or comparable aircraft --> |lists=<!-- related lists --> }}
==References== {{reflist}}
==External links== {{commons category|Mainair Blade}} *{{Official website|http://www.pmaviation.co.uk/mainair-blade.html}} {{P&M Aviation aircraft}}
[[Category:P&M Aviation aircraft|Mainair Blade]] [[Category:1990s British ultralight aircraft]] [[Category:Single-engined pusher aircraft]] [[Category:Ultralight trikes]]