De Havilland Canada DHC-6 Twin Otter
| Entry into service | 1966 |
| Dimensions | Length : 15.77 m |
| Wing span : 19.81 m | |
| Height : 5.66 m | |
| Weights | Maximum take off weight : 5,670 kg |
| Maximum landing weight : 5,579 kg | |
| Operating empty weight : 3,320 kg | |
| Maximum payload : 2,004 kg | |
| Powerplant | 2 x 652 hp (489 kW) Pratt & Whitney (UACL) PT6A-27. |
| Fuel capacity | 2,273 l |
| Performance | Maximum cruise speed : 182 kt - 228 km/h |
| Maximum cruising altitude : 26,700 ft - 8,140 m | |
| T-O distance : 262 m | |
| Landing field length : 290 m | |
| Design range :1,775. | |
| Accommodations | 1-class : 20 |
| 2-class : - | |
| 3-class : - |