Mainair Blade 582 Manual
The Rotax 582 is a 48kW (64hp)two-stroke, two-cylinder, rotary intake valve, oil-in-fuel or oil injection pump, liquid-cooled, gear reduction-drive aircraft engine manufactured by BRP-Rotax GmbH & Co. KG. It is for use in non-certified aircraft operating in day visual flight rules.
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Development
Is it time to fly yet? Yes, let's go fly! Skip to content. Mainair Blade 582 For Sale. Post by BuzzLight » Fri Oct 03, 2014 5:43 am Tx Nico. Incident: Mainair Blade 582, Microlight, EI-DRH, Rathcoole Airfield, 5 Nov 2006: Report No 2007-005 SYNOPSIS The microlight was taking off from the grass runway at Rathcoole Airfield, Mallow, Co. Mainair Blade 582 £3750. Mainair Blade 582 G-MYYY 720 hours Permit till 12 March 2018 4 Blade warp drive 2 owners from new Flys beautifully, not being flown enough Wing and batten bag Based at Strathaven £3750 for quick sale. Contact the advertiser Contact Details 8. The BLADE is a two-seat flexwing in the traditional Mainair style. First built in 1994, with over 350 flying around the world today. First solo around the world with champion pilot Colin Bodill, the Mainair Blade is a true thoroughbred with an impeccable pedigree.
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. 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. Help us improve GOV.UK. To help us improve GOV.UK, we’d like to know more about your visit today. We’ll send you a link to a feedback form. It will take only 2 minutes to fill in. CIVIL AVIATION AUTHORITY – SAFETY REGULATION GROUP MICROLIGHT TYPE APPROVAL DATA SHEET (TADS) NO: BM47 ISSUE: 11 TADS BM47 Issue 11 Page 2 of 10 (6) POWER PLANTS Designation Blade 582 Blade 582 Blade 462 Blade 462 Blade 462 Blade 503 Blade 503 Blade 503 Engine Type Rotax 582-2v.
The Rotax 582 is based upon the earlier Rotax 532 engine design and was designed for ultralight aircraft.[1][2] The 582 increased the bore from the 532 engine's 72 to 76mm (2.8 to 3.0in) and increased the stroke from 61 to 64mm (2.4 to 2.5in). This increased the displacement from 521.2cc (31.81cuin) to 580.7cc (35.44cuin), an increase of 11%. The increased displacement had the effect of flattening out the 532's torque curve and allowed the 582 to produce useful power over a wider rpm range. Reliability over the 532 was also improved.[2]
The 582 features liquid-cooled cylinder heads and cylinders with a Rotary Intake Valve. Cooling is via an externally mounted radiator. Lubrication is either by use of pre-mixed fuel and oil or oil injection from an externally mounted oil tank. The 582 has dual independent breakerless, magneto capacitor discharge ignition (CDI) systems and is equipped with two piston-type carburetors. It uses a manifold-driven pneumatic fuel pump to provide fuel pressure. An optional High Altitude Compensation kit is available.[1][2]
The engine's propeller drive is via a Rotax type B, C or E style gearbox. The standard engine includes a muffler exhaust system with an extra after-muffler as optional. The standard starter is a recoil start type, with an electric starter optional. An integral alternating current generator producing 170watts at 12volts with external rectifier-regulator is optional. The engine includes an intake air filter and can be fitted with an intake silencer system.[1][2]
Limitations
The manufacturer acknowledges the design limitations of this engine, warning pilots:[1]
'This engine, by its design, is subject to sudden stoppage. Engine stoppage can result in crash landings, forced landings or no power landings. Such crash landings can lead to serious bodily injury or death..This is not a certificated aircraft engine. It has not received any safety or durability testing, and conforms to no aircraft standards. It is for use in experimental, uncertificated aircraft and vehicles only in which an engine failure will not compromise safety. User assumes all risk of use, and acknowledges by his use that he knows this engine is subject to sudden stoppage..Never fly the aircraft equipped with this engine at locations, airspeeds, altitudes, or other circumstances from which a successful no-power landing cannot be made, after sudden engine stoppage. Aircraft equipped with this engine must only fly in DAYLIGHT VFR conditions.'[1]
Applications
- Revolution Mini-500 helicopter
Mainair Blade 582 Manual Transmission
Specifications (Rotax 582)
General characteristics
- Type: two-cylinder, two-stroke, rotary valve, oil-in-fuel or oil-injected lubrication, dual carburetors, electronic dual ignition
- Bore: 76 mm (2.99 in)
- Stroke: 64 mm (2.52 in)
- Displacement: 580.7 cm³ (35.44 cu in)
- Dry weight: 50 kg (110 lb) with electric starter, carburetors, fuel pump, air filters and reduction gear
Components
- Fuel type: premium unleaded: RON 90 octane or higher leaded or unleaded or AVGAS 100 LL
- Oil system: oil-in-fuel (pre-mix) or oil injection
- Cooling system: liquid cooled

Performance
- Power output: 48 kW (64.4 hp) at 6,500RPM
- Compression ratio: 11.5 (theoretical) - 5.75 effective
Mainair Blade 582 Manual Pdf
See also
References
- BRP-Rotax GmbH & Co. KG (2006). 'OPERATORS MANUAL FOR ENGINE TYPES 447, 503 & 582'(PDF). Retrieved 2009-03-09.
- Raisner, William: LEAF catlog, pages 6-105. Leading Edge Airfoils, 1995.
External links
| Wikimedia Commons has media related to Rotax 582. |
| Two-stroke piston engines |
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| Four-stroke piston engines |
