Aircraft › CEAPR › DR400 Series › DR 400/120
The DR 400/120 is a model in the DR400 Series family. It is described here as a Single-engine low-wing piston aircraft.
CEAPR DR 400/120 specifications
| Manufacturer | CEAPR |
|---|---|
| Model | DR 400/120 |
| Aircraft type | Single-engine low-wing piston aircraft |
| Landing gear | Fixed tricycle |
| Certification | EASA EASA.A.367 |
CEAPR DR 400/120 weights and capacities
CEAPR DR 400/120 engine and configuration
| Configuration 1 | Lycoming · O-235-L2A · @ 2,800 rpm |
|---|---|
| Configuration 2 | Lycoming · O-235-K2A · @ 2,800 rpm |
| Configuration 3 | Lycoming · O-235-K2B · @ 2,800 rpm |
Certified weight limits and applicability
| normal category | Takeoff 900 kg · Landing 900 kg · normal category |
|---|---|
| utility category | Takeoff 900 kg · Landing 900 kg · utility category |
Fuel capacity and configuration
| main tank | 110 L total · 100 L usable · Standard 88 configuration |
|---|---|
| main tank | 110 L total · 109 L usable · Standard 92 configuration where approved |
| supplementary tank | 50 L total · 50 L usable · approved supplementary installation |
Baggage and loading applicability
| Baggage | 40 kg maximum |
|---|
CEAPR DR 400/120 history and development
DR 400/120 is a certificated member of the CEAPR/Robin DR400 family. Certification for this model is listed under EASA Type Certificate Data Sheet EASA.A.367 - DR400 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 400/120 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 400/120 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 400/120 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 400/120 calculator.
Reference sources
EASA: EASA Type Certificate Data Sheet EASA.A.367, Issue 05, 16 October 2023
Related DR400 Series models
- CEAPR DR 400/100
- CEAPR DR 400/120 A
- CEAPR DR 400/120 D
- CEAPR DR 400/125
- CEAPR DR 400/125 i
- CEAPR DR 400/140
- CEAPR DR 400/140 B
- CEAPR DR 400/160
- CEAPR DR 400/160 D
- CEAPR DR 400/180
- CEAPR DR 400/180 R
- CEAPR DR 400/180 S
- CEAPR DR 400/2+2
- CEAPR DR 400/200 I
- CEAPR DR 400/200 R
- CEAPR DR 400/500
- CEAPR DR 400/NGL
- CEAPR DR 400/RP