DynAero MCR-01 Sportster Model Guide
DynAero MCR-01 Sportster · Model Guide
Overview
The DynAero MCR-01 Sportster is a two-seat, low-wing kit aircraft with a carbon structure. The flight manual covered here describes the 100 HP Rotax 912 S version. It flies under a restricted airworthiness certificate, VFR day only, and may not be used for hire or reward. Buyers should confirm the mandatory flap-system bulletin was done and check the propeller bolt tightening history.
- Two seats, 490 kg maximum take-off weight, 80 l fuel (79 l usable), and a 15 kg luggage limit.
- Restricted-category kit aircraft: VFR day only, no icing, no aerobatics, no spins, no hire or reward use.
- Flap control retrofit BS 12 F 0043 was made mandatory by an AD and applies to all serial numbers. Confirm it was done.
- Rotax 912 S gives 100 HP for take-off and 92 HP continuous. Several fixed and variable-pitch propellers are approved.
Summary written by AI from the source document. Check the original before relying on it. See which parts of Sprinkle are written by AI.
Reference only, not for flight. Use the current approved manual for your aircraft. See terms, section 5.
Document
Source
Copy found at sprinkle.com. Sprinkle hosts a reference copy with an added summary, specifications and searchable full text.
Document details
- Type ·
- Model Guide
- Year ·
- 2026
- File size ·
- 49 KB
- Copy found at ·
- sprinkle.com
Specifications & performance
Extracted from this document.
Specifications
- Height m ·
- 1.43
- Length m ·
- 5.48
- Wing span m ·
- 6.63
- Wing area m2 ·
- 5.2
- Usable fuel l ·
- 79
- Fuel capacity l ·
- 80
- Engine takeoff power (hp) ·
- 100
- Engine continuous power (hp) ·
- 92
V-speeds
- VA_KTS ·
- 127
- VFE_KTS ·
- 92
- VNE_KTS ·
- 173
- VNO_KTS ·
- 143
- GREEN_ARC_START_KTS ·
- 65
- WHITE_ARC_START_KTS ·
- 50
Weight & balance
- Mac mm ·
- 800
- Max luggage kg ·
- 15
- Max landing weight kg ·
- 490
- Max takeoff weight kg ·
- 490
- Cg aft limit percent mac ·
- 45
- Max weight without fuel kg ·
- 432
- Cg forward limit percent mac ·
- 15
- Max instrument panel weight kg ·
- 15
How many people can the DynAero MCR-01 Sportster carry?
The DynAero MCR-01 Sportster has two seats. The minimum crew is one pilot and two people is the maximum on board. Maximum take-off weight is 490 kg and the luggage limit is 15 kg.
Can the DynAero MCR-01 Sportster be used for hire or reward?
No. The DynAero MCR-01 Sportster was built from a kit and flies under a restricted airworthiness certificate. The manual prohibits hire or reward use, aerobatics and spins, and limits flights to VFR day without icing.
What fuel and oil does the DynAero MCR-01 Sportster use?
For the DynAero MCR-01 Sportster, the fuel filler placard shows an 80 l tank and a minimum grade of RON 90. The oil tank placard shows 3.5 l of 10 W 40. For other grades the manual refers to the Rotax manual.
Is the flap bulletin mandatory on the DynAero MCR-01 Sportster?
Yes. BS 12 F 0043 was made mandatory by a French DGAC airworthiness directive and applies to all serial numbers of the DynAero MCR-01 Sportster. It covers the flap control retrofit, electric end stops and dust seals, with compliance due by 01/01/2013.
What is the DynAero MCR-01 Sportster Model Guide?
The DynAero MCR-01 Sportster Model Guide is a model guide for the DynAero MCR-01 Sportster, dated 2026.
What year was the DynAero MCR-01 Sportster Model Guide published?
The DynAero MCR-01 Sportster Model Guide — the DynAero MCR-01 Sportster model guide on file — is dated 2026.
Uncommon. Rarer than 57% of the aircraft models we track.
Most owners only have the POH. Here's the essential set for the DynAero MCR-01 Sportster.
- Pilot's Operating Handbook / AFM
- Checklist
- Maintenance Manual
- Parts Catalog (IPC)
- Systems & Wiring
- Service Bulletins on file
- Type Certificate (TCDS)
Free — save the MCR-01 Sportster to your watchlist and track it in one place.
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In this document
Limits and loading
Never-exceed speed is 173 kts, maximum structural cruising speed 143 kts, manoeuvring speed 127 kts, and the flaps-extended limit 92 kts. Weight limits are 490 kg at take-off and at landing, and 432 kg without fuel. The CG range is 15 to 45% of the 800 mm mean aerodynamic chord. Manoeuvring load factor is +3.8 / -1.5 g.
Engine and propeller
The Rotax 912 S is limited to 5800 RPM at take-off and 5500 RPM continuous. Do not run continuously above 5500 rpm for more than 5 minutes. The manual gives different cylinder head figures in different tables (135 °C maximum in one, a 150 °C red line in another), so check them against your instruments. Tighten propeller bolts before first flight, after 1 and 5 flight hours, then every 50 hours and after any ground period over 1 month.
Maintenance and what to check
The maintenance manual (edition 25/09/19) sets 50H, 100H/annual, 1000H and 5-year inspections. SE Aviation allows no lightening or shortening of the programme. Service bulletin BS 12 F 0043 requires a reinforced flap control, electric end-stop switches and dust seals, with compliance by 01/01/2013. It also calls for a wear check of the frame 5 lead-screw bushings.
Summary written by AI from the source document. Check the original before relying on it. See which parts of Sprinkle are written by AI.
Safety notes
- Spins and aerobatics are prohibited. Operation is VFR day only, in conditions without icing.
- Do not switch off the main switch before the engine is stopped.
- After any flap work, check the electric stops: the front one stops 1 mm before the mechanical stop, the rear one at 25° (+/-1°) flap deflection.
Summary written by AI from the source document. Check the original before relying on it. See which parts of Sprinkle are written by AI.
Full document text
DynAero MCR-01 Sportster Model Guide The DynAero MCR-01 Sportster is a two-seat, low-wing kit aircraft with a carbon structure. The flight manual covered here describes the 100 HP Rotax 912 S version. It flies under a restricted airworthiness certificate, VFR day only, and may not be used for hire or reward. Buyers should confirm the mandatory flap-system bulletin was done and check the propeller bolt tightening history. • Two seats, 490 kg maximum take-off weight, 80 l fuel (79 l usable), and a 15 kg luggage limit. • Restricted-category kit aircraft: VFR day only, no icing, no aerobatics, no spins, no hire or reward use. • Flap control retrofit BS 12 F 0043 was made mandatory by an AD and applies to all serial numbers. Confirm it was done. • Rotax 912 S gives 100 HP for take-off and 92 HP continuous. Several fixed and variable-pitch propellers are approved. Limits and loading Never-exceed speed is 173 kts, maximum structural cruising speed 143 kts, manoeuvring speed 127 kts, and the flaps-extended limit 92 kts. Weight limits are 490 kg at take-off and at landing, and 432 kg without fuel. The CG range is 15 to 45% of the 800 mm mean aerodynamic chord. Manoeuvring load factor is +3.8 / -1.5 g. Engine and propeller The Rotax 912 S is limited to 5800 RPM at take-off and 5500 RPM continuous. Do not run continuously above 5500 rpm for more than 5 minutes. The manual gives different cylinder head figures in different tables (135 °C maximum in one, a 150 °C red line in another), so check them against your instruments. Tighten propeller bolts before first flight, after 1 and 5 flight hours, then every 50 hours and after any ground period over 1 month. Maintenance and what to check The maintenance manual (edition 25/09/19) sets 50H, 100H/annual, 1000H and 5-year inspections. SE Aviation allows no lightening or shortening of the programme. Service bulletin BS 12 F 0043 requires a reinforced flap control, electric end-stop switches and dust seals, with compliance by 01/01/2013. It also calls for a wear check of the frame 5 lead-screw bushings. Safety notes: • Spins and aerobatics are prohibited. Operation is VFR day only, in conditions without icing. • Do not switch off the main switch before the engine is stopped. • After any flap work, check the electric stops: the front one stops 1 mm before the mechanical stop, the rear one at 25° (+/-1°) flap deflection.