| A/C | Manufacturer | Viking Air | Sources: | ||||||||
| Aircraft type | Twin Otter | [1] | https://www.flightglobal.com/download?ac=73559 | ||||||||
| Total number of operating A/C | 315 | [1] | [2] | https://www.vikingair.com/sites/default/files/Viking-Twin-Otter-Series-400-Technical-Specifications-R-01-2018.pdf | |||||||
| Option/Variant | DHC-6 400 | [4] | [3] | https://www.vikingair.com/twin-otter-series-400/technical-description | |||||||
| Engine | No. of Engines | 2 | [4] | [4] | TAYLOR, John W.R., 1974. Jane's All The World's Aircraft 1974–75. New York, USA. | ||||||
| Model | PT6A-34 | [4] | [5] | https://www.easa.europa.eu/downloads/7070/en | |||||||
| Max. Rated Takeoff Thrust, T_TO [kN] | - | Comments: | |||||||||
| Equivalent Power, P [kW] | 462 | [4] | ¹ Fuel reserve for 45 minutes, LRC | ||||||||
| Propeller | HC-B3TN-3D/T10282N | [4] | |||||||||
| Cabin | Length, l_CABIN [m] | 5,64 | [4] | ||||||||
| Max. Height, h_CABIN [m] | 1,5 | [4] | |||||||||
| Max. Width, d_F,I [m] | 1,61 | [4] | |||||||||
| Passenger Compartment Volume, V_CABIN [m³] | 10,9 | [2] | |||||||||
| Fuselage | Height, h_F [m] | N/A | |||||||||
| Width, w_F [m] | N/A | ||||||||||
| Total | Length, l_A/C [m] | 15,77 | [2] | ||||||||
| Span, b_W [m] | 19,81 | [2] | |||||||||
| Height, h_A/C [m] | 5,94 | [2] | |||||||||
| Landing Gear | Track, l_T [m] | 3,7 | [2] | ||||||||
| Wheelbase, l_WB [m] | 4,53 | [2] | |||||||||
| Wing | Area, S_W [m²] | 39,02 | [4] | ||||||||
| Taper ratio, λ_W | 1,00 | [2] | |||||||||
| 1/4 Chord Sweep, φ_25,W [°] | 0 | [2] | |||||||||
| Vertical Tail | Area, S_V [m²] | 4,46 | [4] | ||||||||
| Height, b_V [m] | 3,9 | [2] | |||||||||
| Taper ratio, λ_V | 0,51 | [2] | |||||||||
| 1/4 Chord Sweep, φ_25,V [°] | 24 | [2] | |||||||||
| Horizontal Tail | Area, S_H [m²] | 9,29 | [4] | ||||||||
| Span, b_H [m] | 6,29 | [2] | |||||||||
| Taper Ratio, λ_H | 0 | [2] | |||||||||
| 1/4 Chord Sweep, φ_25,H [°] | 1 | [2] | |||||||||
| Cruise | V_MO [kt] | 187 | [5] | ||||||||
| M_MO [Mach] | 0,29 | [5] | |||||||||
| Cruise Speed, M_CR [Mach] | N/A | ||||||||||
| Max. Certified Flight Level, h_MCR [FL] | 250 | [5] | |||||||||
| Cruise Altitude, h_CR [FL] | 100 | [2] | |||||||||
| Fuel | Unusable Fuel [l] | 14 | [5] | ||||||||
| Optional Fuel [l] | 337 | [2] | |||||||||
| Max usable fuel [l] | 1446 | [4] | |||||||||
| Range | Max. Payload, R_MPL [nm] | N/A | |||||||||
| Max. Pax, R_M,pax [nm] | N/A | ||||||||||
| Max. Range, R_PLMR [nm] | 702 | ¹[2] | |||||||||
| Mass | Max. Ramp, m_MR (MRM) [kg] | 5670 | [5] | ||||||||
| Max. Take-Off, m_MTO (MTOM) [kg] | 5670 | [5] | |||||||||
| Max. Landing, m_ML (MLM) [kg] | 5579 | [5] | |||||||||
| Max. Zero Fuel, m_MZF (MZFM) [kg] | N/A | ||||||||||
| Operating Empty, m_OE (OEM) (MZFM-MPL) [kg] | 3377 | [2] | |||||||||
| Max. Payload, m_MPL (MPL) [kg] | N/A | ||||||||||
| Payload at Max. Range, m_PLMR [kg] | 1030 | [2] | |||||||||
| Cargo | Volume, V_CARGO [m³] | 3,57 | [4] | ||||||||
| Cargo Capacity | - | ||||||||||
| Max. Pallet Underfloor | - | ||||||||||
| Seats | Max. Seats, n_M,SEAT | 19 | [5] | ||||||||
| Std. Layout, n_SEAT | 19 | [4] | |||||||||