Dyn'Aero · 1996+
Dyn'Aero MCR-01 Ban-Bi
Specifications
Cruise
162KTAS
Range
567nm
Seats
2
Useful Load
717lbs
Full-fuel payload
573lbs
Fuel Burn
4.5gph
Fuel Cap.
24gal
MPG
41.4mpg
Stall (Vs0)
45KIAS
T/O roll
620ft
Ldg roll
560ft
Power
100hp
Engine
piston single
Gear
Fixed
IFR
No
Category
experimental
Pricing
Typical
$55k
Range
$35k – $90k
Annual all-in
~$6k/yr
All-in estimate at ~100 flying hours a year — fuel, annual inspection, engine reserve, insurance, and hangar. It scales with your actual hours, and insurance and hangar vary most by region and pilot.
Cost to own — estimate
Set your yearly hours and local fuel price. Fixed costs (insurance, hangar, annual inspection) don't change with hours; fuel and the engine reserve do.
- Fuel (4.5 gph)
- $2,925
- Engine reserve (toward overhaul)
- $1,100
- Fixed (insurance, hangar, annual, subscriptions)
- $1,475
- Total per year
- $5,500
- Per flight hour
- $55
- Miles flown / year (at cruise)
- 18,643 mi
- Cost per mile
- $0.30/mi
Estimate, not a quote — insurance and hangar (the fixed bucket) vary most by region and pilot. Anchored to our model figure at 100 hrs and $6.50/gal.
Strengths
- Exceptional fuel economy: 160+ KTAS on ~4.5 GPH rivals certified aircraft with 3× the power
- Responsive, efficient cross-country performer: 560 NM range, true pilot's airplane
- Excellent climb and density-altitude performance for a 100 HP airframe
- Clean all-composite construction: airframe life effectively unlimited if inspections remain clean
Weaknesses
- Extremely slippery on descent—requires active flap/prop management; unforgiving energy state on approach
- European kit with orphan-status in US: parts lead times multi-month, support limited outside Rotax shops
- VFR-only, two-seat, minimal baggage: poor for any mission requiring IFR or payload flexibility
- Composite airframe repairs expensive and specialized; requires builder or composite-capable A&P
Overview
The Dyn'Aero MCR-01 is a French two-seat, low-wing, all-composite carbon fiber light aircraft designed by Michel Colomban (of Cri-Cri fame) and originally produced by Dyn'Aero in Darois, France beginning in 1996. Marketed under the nickname "Ban-Bi" (Breton for "two-seater"), the MCR-01 is famous in the European kit community for extracting remarkable cruise speeds from a tiny 80-100 HP Rotax 912 engine — a clean Sportster/VLA variant will true out at 160+ KTAS on roughly 4.5 GPH, rivaling aircraft with three times the horsepower. Production has since transferred to SE Aviation (branded "MCR Evolution"), which continues to sell kits and ready-to-fly examples. Several hundred have been built worldwide, with strong concentrations in France, Germany, the UK, New Zealand, and Australia. In the US it appears almost exclusively as amateur-built Experimental. The aircraft is a darling of efficiency-minded cross-country pilots but is uncommon, demands careful energy management on approach, and carries the usual orphan-kit concerns of any low-volume European composite.
Variants & History
| Variant | Years | Engine | HP | MTOW | Wing Span | Key Differences |
|---|---|---|---|---|---|---|
| MCR-01 ULC (Ban-Bi) | 1996– | Rotax 912UL | 80 | 450–472.5 kg (ULM) | 8.64 m | Long wings, microlight/ultralight category, higher MTOW in later rule updates |
| MCR-01 Club | 1998– | Rotax 912S/ULS | 100 | 560 kg | ~7.0 m | Slightly bigger wing than VLA, intended for clubs/schools, lower stall |
| MCR-01 VLA "Sportster" | 2000– | Rotax 912ULS | 100 | 560 kg | 6.63 m | Short-wing VLA certification, fastest variant, T-tail |
| MCR-01 Banbi "Sport" | 2001– | Rotax 912ULS / 914 | 100–115 | 560 kg | 6.63 m | Turbocharged option, export/kit |
| MCR Pick-Up | 2008– | Rotax 912S / 914 | 100–115 | 560 kg | 6.63 m | High-wing derivative (separate airframe) — not covered here |
| dynaero-mcr-4s | 2004– | Rotax 914/915 | 115–141 | 750–820 kg | 8.72 m | Four-seat stretched development, see dedicated page |
Note: ULC is the ultralight/microlight variant with the larger wing; Sportster/VLA is the short-wing hotrod; Club sits in between. All share the carbon-fiber fuselage and wing spar architecture.
Performance
The MCR-01 Sportster's book cruise of 300 km/h (162 KTAS) at 75% power is achievable in the real world — owners consistently report 155–165 KTAS on 18–20 L/hr (4.8–5.3 GPH) of mogas. Climb rate on the Rotax 912ULS is a genuine 1,500–1,750 FPM at light weights, falling toward 1,000 FPM at MTOW. Service ceiling is practical to 13,000 ft and absolute to 17,000 ft. The ULC with its longer wing gives up about 15 KTAS cruise for materially better short-field and stall behavior (stall ~39 KIAS vs ~47 KIAS for the VLA). The aircraft is slippery — flaps and prop pitch management are essential on descent, and owners warn that "point the nose down and you accelerate to Vne in seconds." Density altitude performance is excellent for a 100 HP airplane thanks to the very low empty weight (~235 kg / 518 lb).
Payload & Range
With a ~518 lb empty weight and ~1,235 lb MTOW (Sportster/VLA), useful load is an impressive ~717 lb for a 100 HP airplane:
- Full fuel (24 gal = 144 lb) + 2 pax (340 lb) + 233 lb baggage: Achievable within the limited baggage volume (~40 lb real-world), yielding ~560 NM range at 162 KTAS with VFR reserves.
- Full seats (400 lb pax) + reduced fuel: Not typically necessary — the airplane can fly full fuel and two adults with room to spare on paper. The binding constraint is usually baggage volume, not weight.
- Long-range tanks (36 gal / 216 lb): Push range toward 700+ NM at economy cruise (140 KTAS on ~3.5 GPH), turning the MCR-01 into a genuine European-style touring airplane.
- Real-world limitation: The cabin is narrow (~42" width) and baggage volume is small; two adults plus overnight bags fills the airplane before weight becomes the issue.
For cross-country mission scoring see cross-country; for the fun-flying mission that this airplane genuinely excels at see local-fun-flying.
Mission Suitability
- Local fun flying (9): Responsive, fast, efficient, visually striking — a pilot's airplane in the truest sense.
- Cross-country (8): 160+ KTAS on 4.5 GPH is genuinely transformative economics; range ~560 NM with reserves. Penalized only by small cabin, limited baggage, and no IFR certification.
- Business travel (5): Speed is there, but VFR-only, two seats, minimal baggage, and unfamiliar-to-FBO composite airframe limit practicality.
- Surveying (4): Efficient, but visibility from low-wing and limited loiter endurance penalize it vs high-wing options.
- Flight training (3): Not a trainer — fast, slippery, unforgiving on approach speed management, and rare/expensive to insure for students.
- Aerobatics (2): Not stressed or approved for aerobatics; +4/-2 G structural envelope.
- Backcountry (2): Low wing, small wheels, fragile composite belly, and need for smooth surfaces.
- Cargo hauling (2): 717 lb useful load sounds generous but the cabin is tiny and baggage area minimal.
Avionics Ecosystem
Almost all MCR-01s are experimental and wear experimental avionics. Typical panels:
- Entry tier ($8–15k): Single Dynon SkyView HDX or Garmin G3X Touch 7", basic ADS-B out via uAvionix tailBeacon, handheld COM backup. See avionics-pricing.
- Mid tier ($15–30k): Dual Dynon/Garmin PFD+MFD, Garmin GTR 200 COM, GTX 45R transponder, Dynon or TruTrak autopilot (2-axis).
- Top tier ($30–50k): Dual G3X Touch 10", GTN 650Xi navigator (for VFR GPS approaches in owner workflow), GFC 500 autopilot (where supported), engine monitoring via Dynon EMS.
IFR-certified installations are rare and not supported by the airframe's certification basis in most countries; treat the MCR-01 as a VFR airplane.
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STCs & Modifications
As an experimental/kit, there are no STCs in the traditional sense. Common owner modifications:
- E-Props or DUC Hélices carbon propellers — 2–4 KTAS cruise gain, smoother idle, ~€2,500–3,500
- Long-range fuel tanks — wing tank extensions boosting total fuel from 60 L to 91 L (16 to 24 gal); extends range toward 650+ NM
- Rotax 914 turbo upgrade — adds ~15 HP and maintains sea-level power to altitude, ~€15,000 engine swap
- Retractable gear kit (historical Dyn'Aero option on some variants) — adds 5–8 KTAS but significantly complicates insurance and maintenance
- Glass panel upgrades — retrofit from analog-era panels to Dynon/Garmin EFIS is a very common refresh
Maintenance & Support
See maintenance-ecosystem. Parts and support are a genuine concern:
- Parts availability: Fair. SE Aviation in France supplies kit parts, but US shipping, euros, and customs add time and cost. Some items (carbon panels, canopies) have multi-month lead times.
- Mechanic familiarity: Specialist. Rotax 912 service is widely available at any Light Sport/Rotax-capable shop; the airframe itself requires an A&P comfortable with composites or the builder themselves as the repairman (for amateur-built).
- Annual condition inspection: $800–1,500 typical if no discrepancies
- Typical annual operating cost: ~$5,000–6,500 including fuel (100 hrs), insurance, hangar, reserves, and annual
- Expensive items: Rotax gearbox rubber coupling replacement (~$1,500), prop overhaul (~$1,800), canopy replacement (~$4,000+), carbon structural repair (wildly variable)
- Reserves: Budget $8–10/hr for engine reserve, $2–3/hr for airframe reserve
Valuation Factors
See valuation-methodology for the general framework. MCR-01-specific notes:
- Price tiers: Project/unfinished kits $15–30k; older flying Sportster with steam panel $35–55k; well-equipped glass-panel VLA $60–90k; recent SE Aviation "MCR Evolution" ready-to-fly €120–160k+ (USD equivalent $130–175k)
- Engine time: Rotax 912ULS overhaul is ~$18–22k; a mid-time engine (1,000+ hr remaining) adds $8–12k vs a run-out
- Avionics: A full Dynon/Garmin glass panel adds $15–25k vs a basic analog/single-screen setup
- Long-range tanks: $3–5k value add
- Airframe hours: Lower sensitivity than certified aircraft because TBO is engine-driven; airframe life is effectively unlimited on composite if inspections are clean
- Builder reputation: Well-known European or commercial builders command a 10–20% premium over unknown amateur builders
- Country of origin: European-registered examples imported to the US can require significant paperwork and DAR inspection — discount accordingly
ADs & Common Problems
Experimental aircraft do not receive FAA Airworthiness Directives, but Dyn'Aero and SE Aviation have issued service bulletins owners must track:
- Carbon spar inspection bulletins — periodic bond-line inspection at wing root; look for any delamination history in logs
- Rotax 912 gearbox overhaul — 1,000-hour rubber coupling and slipper-clutch inspection, mandatory regardless of airframe
- Elevator trim servo wear — reported issue on T-tail Sportster variants; check for slop
- Canopy latch reliability — multiple reports of in-flight unlatches; many owners have fitted secondary pins
- Fuel tank vent icing — in cold climates, owners have added heated vents
- Landing gear leg fatigue cracks — composite main gear legs have shown hairline cracks after hard landings; inspect at annual
- Nosewheel shimmy — common, often from worn bungees or incorrect toe-in
Pre-buy red flags: any history of hard landing, delamination repair, non-factory structural modification, or builder who deviated from the kit manual. Always demand the full build log and photographic evidence of critical bond joints.
Insurance Profile
See insurance-underwriting. The MCR-01 is a tough insurance target:
- Hull insurance: ~$2,000–2,800/year on a $70k hull, reflecting fast approach speeds, rare type, and composite repair cost
- Liability: $800–1,200/year for $1M smooth
- Underwriting quirks: Underwriters often require 25+ hours dual in type (difficult to obtain in the US), 200+ hours total time, and a tailored checkout. First-year premiums for low-time pilots can exceed $4,000 or coverage may be declined outright.
- Rare-type penalty: Few US adjusters have seen a damaged MCR-01; claims tend toward total-loss outcomes on otherwise minor incidents
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