# Mainair Blade

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British ultralight trike

Blade Mainair Blade 582 General information Type Ultralight trike National origin United Kingdom Manufacturer Mainair Sports P&M Aviation Status Production completed Number built 60 (February 2000) History Variant Mainair Rapier

The **Mainair Blade** is a British [ultralight trike](/source/Ultralight_trike) that was designed and produced by [Mainair Sports](/source/Mainair_Sports) and later [P&M Aviation](/source/P%26M_Aviation). The aircraft was supplied as a completed aircraft.[1][2][3]

In the early 2000s Mainair was merged with rival [Pegasus Aviation](/source/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."[2][4]

## Design and development

The aircraft was designed as a high-end touring trike, to comply with the [Fédération Aéronautique Internationale](/source/F%C3%A9d%C3%A9ration_A%C3%A9ronautique_Internationale) [microlight](/source/Microlight) category, including the category's maximum gross weight of 450 kg (992 lb) and is also certified to comply with UK BCAR Section "S". The aircraft has a maximum gross weight of 390 kg (860 lb). It features a [cable-braced](/source/Flying_wires) [hang glider](/source/Hang_glider)-style [high-wing](/source/High-wing), weight-shift controls, a two-seats-in-[tandem](/source/Tandem), open cockpit, [tricycle landing gear](/source/Tricycle_landing_gear) and a single engine in [pusher configuration](/source/Pusher_configuration).[1]

The aircraft is made from bolted-together [aluminium](/source/Aluminium) tubing, with its double-surface wing covered in [Dacron](/source/Dacron) sailcloth. Its 10.6 m (34.8 ft) span wing is supported by a single tube-type [kingpost](/source/Kingpost) and uses an "A" frame control bar. The occupants are accommodated in tandem seating, with a [fibreglass](/source/Fibreglass) [cockpit fairing](/source/Aircraft_fairing) that includes a small windshield. Engines factory supplied include the 37 kW (50 hp) [Rotax 503](/source/Rotax_503) twin cylinder, [two-stroke](/source/Two-stroke), air cooled powerplant as well as the twin cylinder, two-stroke, liquid cooled 48 kW (64 hp) [Rotax 582](/source/Rotax_582) and the four cylinder, [four-stroke](/source/Four-stroke) 60 kW (80 hp) [Rotax 912UL](/source/Rotax_912UL) and 74.5 kW (100 hp) [Rotax 912ULS](/source/Rotax_912ULS).[1][2]

## Operational history

Blades have been used for a number of microlight record distance flights, including a flight to [Australia](/source/Australia) by [Colin Bodill](/source/Colin_Bodill) and Simon Reeve and a flight around the world by Bodill.[2]

The Blade 912 set the record for London to Sydney by microlight of 49 days (175 hours of flying) at an average speed of 124 km/h (77 mph).[3]

## Variants

**Blade 582**
- Version powered by a 48 kW (64 hp) [Rotax 582](/source/Rotax_582) engine. Price in 2003 was [£](/source/Pound_sterling)16,450.[2]

**Blade 912**
- Version powered by a 60 kW (80 hp) [Rotax 912UL](/source/Rotax_912UL) or the 74.5 kW (100 hp) [Rotax 912ULS](/source/Rotax_912ULS). In 2003 it was reported that the Blade 912 accounted for the majority of customer orders. Price in 2003 was £21,800.[2]

## Specifications (Blade 912)

*Data from* Bertrand and Kitplanes[2][3]

**General characteristics**

- **Crew:** one

- **Capacity:** one passenger

- **Wingspan:** 10.6 m (34 ft 9 in)

- **Wing area:** 15.6 m2 (168 sq ft)

- **Empty weight:** 190 kg (419 lb)

- **Gross weight:** 390 kg (860 lb)

- **Fuel capacity:** 65 litres (14 imp gal; 17 US gal)

- **Powerplant:** 1 × [Rotax 912](/source/Rotax_912) four cylinder, [four-stroke](/source/Four-stroke) [aircraft engine](/source/Aircraft_engine), 60 kW (80 hp)

**Performance**

- **Maximum speed:** 145 km/h (90 mph, 78 kn)

- **Cruise speed:** 106 km/h (66 mph, 57 kn)

- **Stall speed:** 48 km/h (30 mph, 26 kn)

- **Range:** 410 km (250 mi, 220 nmi)

- **Service ceiling:** 3,000 m (10,000 ft)

- **Rate of climb:** 6.35 m/s (1,250 ft/min)

- **Wing loading:** 25.0 kg/m2 (5.1 lb/sq ft)

## References

1. ^ [***a***](#cite_ref-Cliche_1-0) [***b***](#cite_ref-Cliche_1-1) [***c***](#cite_ref-Cliche_1-2) Cliche, Andre: *Ultralight Aircraft Shopper's Guide* 8th Edition, page C-14. Cybair Limited Publishing, 2001. [ISBN](/source/ISBN_(identifier)) [0-9680628-1-4](https://en.wikipedia.org/wiki/Special:BookSources/0-9680628-1-4)

1. ^ [***a***](#cite_ref-WDLA04_2-0) [***b***](#cite_ref-WDLA04_2-1) [***c***](#cite_ref-WDLA04_2-2) [***d***](#cite_ref-WDLA04_2-3) [***e***](#cite_ref-WDLA04_2-4) [***f***](#cite_ref-WDLA04_2-5) [***g***](#cite_ref-WDLA04_2-6) Bertrand, Noel; Rene Coulon; et al: *World Directory of Leisure Aviation 2003-04*, page 104. Pagefast Ltd, Lancaster OK, 2003. [ISSN](/source/ISSN_(identifier)) [1368-485X](https://search.worldcat.org/issn/1368-485X)

1. ^ [***a***](#cite_ref-KitplanesFeb2000_3-0) [***b***](#cite_ref-KitplanesFeb2000_3-1) [***c***](#cite_ref-KitplanesFeb2000_3-2) Downey, Julia: *2000 Trike and 'Chute Directory*, Kitplanes, Volume 17, Number 2, February 2000, page 46 and 47. Kitplanes Acquisition Company. [ISSN](/source/ISSN_(identifier)) [0891-1851](https://search.worldcat.org/issn/0891-1851)

1. **[^](#cite_ref-Blade_4-0)** P&M Aviation (n.d.). ["The Mainair Blade"](http://www.pmaviation.co.uk/mainair-blade.html). Retrieved 18 January 2012.

## External links

Wikimedia Commons has media related to [Mainair Blade](https://commons.wikimedia.org/wiki/Category:Mainair_Blade).

- [Official website](http://www.pmaviation.co.uk/mainair-blade.html)

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Adapted from the Wikipedia article [Mainair Blade](https://en.wikipedia.org/wiki/Mainair_Blade) by Wikipedia contributors ([contributor history](https://en.wikipedia.org/wiki/Mainair_Blade?action=history)). Available under [Creative Commons Attribution-ShareAlike 4.0 International](https://creativecommons.org/licenses/by-sa/4.0/). Changes may have been made.