Robin DR400-180
TCDS: EASA.A.367 Max Weight: 1,100 lbs
Robin Aircraft
Aircraft Overview
Official TCDS specifications for Robin DR400-180 per Type Certificate EASA.A.367
Critical weight and balance data per Type Certificate EASA.A.367. Verify against current aircraft records before flight operations.
Weight Limits
Loading Stations & Arms
| Station | Arm | Description |
|---|---|---|
| Fuel Tanks | 85.8 in | Main fuel tanks (standard configuration) |
| Rear Seats | 118.1 in | Rear passenger positions |
| Baggage Area | 141.7 in | Primary baggage compartment |
| Pilot Front Seats | 85.4 in | Pilot and front passenger positions |
Center of Gravity Envelope
CG must remain within these limits throughout all phases of flight.
Technical Details
The Robin DR400-180 Regent is the flagship model with maximum cruise speed of 278 km/h, service ceiling of 4,715m, and range of 1,450 km. Excellent for touring and advanced training.
⚠️ Important Disclaimers
Verification Required
Always verify against current aircraft records and equipment list before flight operations.
TCDS Reference
This summarizes TCDS EASA.A.367 but does not replace the official document.
Regulatory Compliance
Calculations must comply with 14 CFR Part 23 and applicable airworthiness directives.
Data Accuracy
Specifications may vary by serial number and modifications. Verify with aircraft documentation.