Aircraft › CEAPR › DR200 / DR220 / DR250 / DR253 Series › DR 250-160
The DR 250-160 is a model in the DR200 / DR220 / DR250 / DR253 Series family. It is described here as a Single-engine low-wing piston aircraft.
CEAPR DR 250-160 specifications
| Manufacturer | CEAPR |
|---|---|
| Model | DR 250-160 |
| Aircraft type | Single-engine low-wing piston aircraft |
| Landing gear | Fixed tricycle |
| Certification | EASA EASA.A.367 |
CEAPR DR 250-160 weights and capacities
CEAPR DR 250-160 engine and configuration
| Engine | Lycoming · O-320-D2A · 162 hp · @ 2,700 rpm |
|---|
Certified weight limits and applicability
| Certified limits | Takeoff 960 kg · Landing 920 kg · normal category |
|---|
Fuel capacity and configuration
| wing tank LH | 40 L total |
|---|---|
| wing tank RH | 40 L total |
| main fuselage tank | 70 L total · 63 L usable |
| supplementary tank | 50 L total · 50 L usable · approved supplementary installation |
Baggage and loading applicability
| Baggage | 40 kg maximum · arm 1.9 m |
|---|
CEAPR DR 250-160 history and development
DR 250-160 is a certificated member of the CEAPR/Robin DR200 / DR220 / DR250 / DR253 family. Certification for this model is listed under EASA Type Certificate Data Sheet EASA.A.367 - DR200 / DR220 / DR250 / DR253 series. These French light-aircraft families include numerous engine, maximum-weight, fuel, propeller and equipment variations. Model-specific values that have not been verified are left unspecified rather than copied from related variants.
CEAPR DR 250-160 fuel capacity
exact model-specific fuel capacity / usable fuel has not yet been verified from the applicable EASA type-certificate section, approved flight manual, or manufacturer data. Do not infer it from a neighboring CEAPR/Robin model or suffix.
CEAPR DR 250-160 model applicability and configuration
Verify exact model designation, serial number, installed engine, propeller, fuel system and approved configuration against the applicable EASA TCDS/AFM and individual aircraft documentation.
CEAPR DR 250-160 weight and balance
Use the exact model/serial-number loading data and the individual aircraft's approved weight-and-balance record. No baggage limit is inferred from a related CEAPR/Robin model. The exact model-specific maximum takeoff weight / gross weight remains unverified until the applicable EASA approval section is verified. Operational loading must use the aircraft-specific empty weight, CG, station arms and limitations. Use the approved aircraft-specific documentation and current weight-and-balance record for operational calculations. WBcalc does not currently provide a model-specific DR 250-160 calculator.
Reference sources
EASA: EASA Type Certificate Data Sheet EASA.A.367, Issue 05, 16 October 2023