Britten-Norman BN-2A Mk III Trislander
Regional Airliner
The Britten-Norman BN-2A Mk III Trislander is a three-engine eighteen-seat regional airliner aircraft produced by the British manufacturer Britten-Norman.
The Trislander is a enlarged three-engine development of the
BN-2 Islander.
| Propulsion | 3 Piston Engines |
| Engine Model | Lycoming O-540-E4C5 |
| Engine Power (each) | 194 kW | 260 hp |
| Speed | 309 km/h | 167 kts
192 mph |
| Service Ceiling | 4.450 m | 14.600 ft |
| Range | 1.609 km | 869 NM
1.000 mi. |
| Empty Weight | 2.650 kg | 5.842 lbs |
| max. Takeoff Weight | 4.536 kg | 10.000 lbs |
| Wing Span | 16,15 m | 52 ft 12 in |
| Wing Area | 31,3 m² | 337 ft² |
| Length | 15,01 m | 49 ft 3 in |
| Height | 4,32 m | 14 ft 2 in |
| First Flight | 11.09.1970 |
| Production Status | out of production |
| Total Production | 72 |
| Developed from | Britten-Norman BN-2 |
| ICAO Code | TRIS |
| IATA Code | BNT |
| FAA TCDS | A17EU |
| Data for (Version) | Britten-Norman BN-2A Mk III Trislander |
