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