Aircraft › CEAPR › DR300 Series › DR 380
The DR 380 is a model in the DR300 Series family. It is described here as a Single-engine low-wing piston aircraft.
CEAPR DR 380 specifications
| Manufacturer | CEAPR |
|---|---|
| Model | DR 380 |
| Aircraft type | Single-engine low-wing piston aircraft |
| Landing gear | Fixed tricycle |
| Certification | EASA EASA.A.367 |
CEAPR DR 380 weights and capacities
CEAPR DR 380 engine and configuration
| Engine | Lycoming · O-360-A3A · @ 2,700 rpm |
|---|
Certified weight limits and applicability
| Certified limits | Takeoff 1,070 kg · Landing 1,020 kg · normal category |
|---|
Fuel capacity and configuration
| main tank | 75 L total · 65 L usable |
|---|---|
| wing tank RH | 40 L total · 40 L usable |
| wing tank LH | 40 L total · 40 L usable |
| supplementary tank | 50 L total · 50 L usable · approved supplementary installation |
Baggage and loading applicability
| Baggage | 60 kg maximum |
|---|
CEAPR DR 380 history and development
DR 380 is a certificated member of the CEAPR/Robin DR300 family. Certification for this model is listed under EASA Type Certificate Data Sheet EASA.A.367 - DR300 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 380 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 380 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 380 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 380 calculator.
Reference sources
EASA: EASA Type Certificate Data Sheet EASA.A.367, Issue 05, 16 October 2023