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Dyn'Aéro MCR4S

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(Redirected fromDyn'Aéro Four seat)
Dyn'Aéro MCR4S
General information
Type2/4 seatkitbuiltultralight
National originFrance
ManufacturerDyn'Aéro
StatusIn production (2015)
History
First flight14 June 2000
Developed fromDyn'Aéro MCR01
VariantDyn'Aéro Twin-R

TheDyn'Aéro MCR4S is a four-seat development of theFrench two seat, single engineDyn'Aéro MCR01. It first flew in early 2000 and is sold as a kit forhomebuilding in several versions by SE Aviation ofPontarlier.[1]

Design and development

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A Dyn'Aéro MCR4S under construction

The MCR4S is a four-seat development of theDyn'Aéro MCR01 and retains many similarities. Both types arelow wing, single engine monoplanes withT-tails. The major changes are an increase infuselage length to accommodate an extra row of seats with generous windows and the replacement of theflaperons seen on the long span variants of the MCR01, which have wings of about the same span as those of the MCR4S, with slotted flaps.[2]

The wing and all control surfaces of the MCR4S havecarbon fibre spars and ribs, to which preformed aluminium skins are glued. The wings have constant chord and carry 3° ofdihedral. Theailerons are short, leaving the rest of the trailing edge of each wing divided between twodouble slotted, three position flaps.Winglets were introduced in 2001 and modified to have straight (in plan) trailing edges from 2002. The MCR4S has a T-tail with anall-moving tailplane. Thefin is an integral part of the carbon fibremonocoque fuselage shell which also features a smallventral fin.[2]

The cabin seats up to four, depending on the variant, in two side-by-side rows. Entry is via the large, forward hinged, two piececanopy. Two large windows light the rear seats, the port side one doubling as an emergency exit. A variety ofRotaxflat four engines may be fitted, driving a two or three blade propeller, which may have fixed orvariable pitch. The MCRS4 has atricycle undercarriage. The main wheels are mounted on short, vertical legs beneath the wings, as on the Club and ULC variants of the MCR01, with a track of 2.33 m (7 ft 8 in). All undercarriage wheels and legs arefaired.[2]

The Dyn'Aéro MCR4S flew for the first time on 14 June 2000.[2]

The MCR4S structure has been used byEADS Defence & Security for its EADS Surveyor 2500drone.[3]

Operational history

[edit]

The first public appearance of the MCR4S was at the International Air Rally held atCranfield just nine days after the first flight. French certification was gained in June 2001 (DGAC) and the first customer, aircraft designer Pierre Robin, flew his aircraft shortly afterwards.UK certification (LAA), though sought, had not been achieved by 2009.[2]

In mid-2010, 90 MCR4Ss appeared on the civil aircraft registers of European countries excluding Russia.[4]

Variants

[edit]

Data from Jane's All the World's Aircraft 2011/12[2]

Current (2010) versions are based on the MCRS4S-2002 specification.
MCR4S evolution
Powered by the newRotax 915 iS engine and developed by SE Aviation in Pontarlier, France.
MCR2S Ibis
Two seat configuration with large baggage volume.Rotax 912 engine.
Pickup
Two seat, lightened to 290 kg (639 lb) empty, to produce a microlight aircraft with two seats, maximum internal capacity and performance.Rotax 912UL or ULS engines of 80 to 100 hp (60 to 75 kW).[1]
Three seat
Three seat, powered by a 60 kW (80 hp)Rotax 912 UL orJPX 4TX75 engine.
Four seat
Four seat, powered by a 74 kW (99 hp)Rotax 912 UL-S engine.
Four seat Performance
Four seat, powered by an 85 kW (113 hp)Rotax 914 UL engine.
CITEC
Powered by aWilksch-120 90 kW (120 hp) two stroke, three cylinder diesel engine.[5]
Dyn'Aéro Twin-R
Twin engine version, first flown March 2011.[1]
MRC ULC
Version lightened to 230 kg (507 lb) empty weight, withtricycle landing gear and powered by an 80 hp (60 kW)Rotax 912 UL or 100 hp (75 kW)Rotax 912 ULS powerplant. The aircraft has a cruise speed of 250 km/h (155 mph) with the 80 hp (60 kW) engine.[1]
MRC M
Version of the MRC ULC withconventional landing gear and powered by an 80 hp (60 kW)Rotax 912 UL or 100 hp (75 kW)Rotax 912 ULS powerplant.[1]

Specifications (Four seat Performance)

[edit]

Data from Jane's All the World's Aircraft 2011/12[2]

General characteristics

  • Capacity: 4
  • Length: 6.72 m (22 ft 1 in)
  • Wingspan: 8.66 m (28 ft 5 in)
  • Height: 1.95 m (6 ft 5 in)
  • Wing area: 8.15 m2 (87.7 sq ft)
  • Empty weight: 370 kg (816 lb) unequipped
  • Max takeoff weight: 750 kg (1,653 lb) ; will be as high as 820 kg with Rotax 914 or 915
  • Fuel capacity: 120 L (200L with long range fuel tanks
  • Powerplant: 1 ×Rotax 914 ULflat four piston engine, turbocharged, air and water cooled, driving constant speed propeller and optimised for cruise at 3,048 m (10,000 ft), 84.6 kW (113.5 hp) can also be fitted with 912S or 915iS

Performance

  • Maximum speed: 250 km/h (160 mph, 130 kn)
  • Cruise speed: 230 km/h (140 mph, 120 kn) 5000rpm, 30 inHg (1.0 bar)
  • Stall speed: 83 km/h (52 mph, 45 kn) flaps down
  • Never exceed speed: 305 km/h (190 mph, 165 kn)
  • Range: 2,000 km (1,200 mi, 1,100 nmi) @ economic cruise speed, with long range fuel tanks (200L), with reserves
  • g limits: +3.8/-1.5
  • Rate of climb: 4.6 m/s (910 ft/min)

References

[edit]
Wikimedia Commons has media related toDyn'Aéro MCR4S.
  1. ^abcdeTacke, Willi; Marino Boric; et al:World Directory of Light Aviation 2015–16, pages 25 & 96. Flying Pages Europe SARL, 2015.ISSN 1368-485X
  2. ^abcdefgJackson, Paul (2011).Jane's All the World's Aircraft 2011–12. Redhill, UK: IHS Jane's. pp. 200–1.ISBN 978-0-7106-2955-5.
  3. ^"Surveyor 2500 – Unmanned Vehicle (UAV) Specifications & Data Sheet". Archived fromthe original on 2014-03-25. Retrieved2014-04-01.
  4. ^Partington, Dave (2010).European registers handbook 2010. Air Britain (Historians) Ltd.ISBN 978-0-85130-425-0.
  5. ^"WAM engines". Retrieved2011-07-20.

External links

[edit]
Dyn'Aéro aircraft
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