Aircraft › Bernd Hager / Anatoli Stobbe › R90 Series › R 90-230RG
The Ruschmeyer R 90-230RG is a model in the R90 Series family. It is described here as a Four-seat retractable-gear piston single.
Bernd Hager / Anatoli Stobbe R 90-230RG specifications
| Manufacturer | Bernd Hager / Anatoli Stobbe |
|---|---|
| Model | R 90-230RG |
| Aircraft type | Four-seat retractable-gear piston single |
| Seats | 4 |
| Landing gear | Retractable tricycle |
| Certification | EASA |
Bernd Hager / Anatoli Stobbe R 90-230RG weights and capacities
| Maximum takeoff weight | 2,976 lb |
|---|---|
| Standard fuel capacity | 62.3 gal total |
| Maximum baggage | 110 lb combined |
Bernd Hager / Anatoli Stobbe R 90-230RG engine and configuration
| Engine | Lycoming · IO-540-C4D5 · 230 hp |
|---|
Bernd Hager / Anatoli Stobbe R 90-230RG history and development
The Ruschmeyer R 90-230RG is a four-seat German retractable-gear touring aircraft. Production aircraft use the Lycoming IO-540-C4D5 de-rated to about 230 hp with a constant-speed propeller. Published aircraft data identify a 1,350 kg maximum takeoff mass, approximately 236 L (62.3 U.S. gal) fuel capacity and a 50 kg baggage limit. Type-certificate responsibility has changed over time, so current continued-airworthiness records should be checked for the individual aircraft.
Bernd Hager / Anatoli Stobbe R 90-230RG fuel capacity
Standard total fuel: 62.3 U.S. gallons. Published R90-230RG aircraft data identify approximately 236 L / 62.3 U.S. gallons fuel capacity.
Bernd Hager / Anatoli Stobbe R 90-230RG model applicability and configuration
Use the current type-holder documentation and aircraft AFM. Engine/propeller modifications and later support changes can affect applicability.
Bernd Hager / Anatoli Stobbe R 90-230RG weight and balance
Maximum takeoff weight: 2,976 lb. Maximum combined baggage: 110 lb. Maximum takeoff mass is 1,350 kg (2,976 lb), published fuel capacity is about 62.3 U.S. gallons and baggage is limited to about 50 kg in the represented configuration. Use the approved aircraft-specific documentation and current weight-and-balance record for operational calculations. WBcalc does not currently provide a model-specific Ruschmeyer R 90-230RG calculator.
Bernd Hager / Anatoli Stobbe R 90-230RG frequently asked questions
What engine does the Ruschmeyer R 90-230RG use?
The engine listed for this model is Lycoming IO-540-C4D5.
What is the maximum takeoff weight of the Ruschmeyer R 90-230RG?
The represented maximum takeoff weight is 2,976 lb.
Reference sources
EASA / continued-airworthiness records: Ruschmeyer R 90-230RG
Published R90-230RG aircraft/POH data: R90-230RG specifications