[AIRCRAFT]DORNIER 228NG
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[AIRCRAFT]DORNIER 228NG
DORNIER 228 NG, a twin turbo-prop utility plane. is it.
Please Download it from my website.↓
https://sites.google.com/view/k2wysf/modern -----------------------------------
DORNIER 228-212(NG) New Central Airservice(JA34CA) Introduction
Dornier 228 series aircrafts are a twin turbo-prop STOL aircraft, desined by Dornier Flugzeugwerke.
They were developed in 1981, and were used as local airliners and other multi purpose utility aircrafts.
Dornier ended their productions in 1998, but, RUAG Aerospace restarted Do228 project, with new technology such as glass cockpit, since 2009. Those new products are called Dornier 228NG.
the other hand, Hindustan Aeronautics Limited (HAL), a Indian Industry, bought a production licence from Dornier in 1983. They supplied 228 series for Indian Air force and other public air service. They also supply the airframe parts for RUAG's 228NG product.
In JAPAN, New Central Airservice, which has local airline between Chofu airport in the suburbs of Tokyo and Izu Islands, is using some passenger type 228 aircrafts since 1998. In 2011, they introduced their first Do228NG aircraft (tail number JA34CA). it is first builted passengertype NG aircraft in the world.
Specification(NG)
Length 16.56m
Wing Span 16.97m
Max. Take-Off Weight 6400kg
Max. Landing Weight 6100kg
Max. Fuel 1885kg
Max. Payload 1960kg
Max, Passengers 19 persons
Max. Range 1312nm in ferry 214nm with Max payload
Speeds min. control(Vmc) 74KIAS
landing(Vref) 80-85KIAS
take-off(Vr) 88-95KIAS
flap extension(Vfe) 130KIAS(Flap 2 / DN)/160KIAS(Flap 1)
gear extension(Vle) 135KIAS
cruise normal(Vc) 170-180KIAS
max(Vmo) 223KIAS (up to 15000ft)
max operating(Mmo) 265KTAS(490km/h) (at 25000ft)
never exceed(Vne) 280KIAS
engines Honneywell TPE331-10GP-511 776SHP x2
Propeller RPM Idle 1100 (70%rpm)
Take-off/decent 1591 (101%rpm)
cruise/climb 1510 (96%rpm)
※Weight balance of payload and fuel
This addon treat an additional Flare pod (with 20 add.FLR 139kg) as two passengers. If you set max 160 add.FLR and 100% fuel, you get the 7114 kg gross-weight which is 814kg larger than Max.take-off Weight and 1014kg larger than Max. landing weight.
I show a figure of balance between add.FLR and fuel setting for weight limmit below.
Add.FLR | Fuel (for Land) | Fuel (for Take-off)
20 | 95%(97.8%) | 100%(113.7%)
40 | 90%(90.5%) | 100%(106.4%)
60 | 80%(83.1%) | 95%(99.0%)
80 | 75%(75.7%)←Default | 90%(91.6%)
100 | 65%(68.3%) | 80%(84.2%)
120 | 60%(61.0%) | 75%(76.9%)
140 | 50%(53.6%) | 65%(69.5%)
160 | 45%(46.2%) | 60%(62.1%)
※un-expected operation
Thrust Vector as Boarding door.
Bomb Bay as sun-shades
Air Brake as cockpit door connected to cabin
This is free for any repaint and remodelings.
- u2fly
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Re: [AIRCRAFT]DORNIER 228NG
Does it mean that users may use it under terms of CreativeCommons license?
If yes, which one should be applied: "CC-BY" or "CC-BY-SA"?
- CC-BY 4.0 - https://creativecommons.org/licenses/by/4.0/
- CC-BY-SA 4.0 - https://creativecommons.org/licenses/by-sa/4.0/
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(31 DEC 2016)
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Re: [AIRCRAFT]DORNIER 228NG
I want not to do any claim for my add-ons.u2fly wrote: ↑Wed Mar 10, 2021 8:59 pm
Does it mean that users may use it under terms of CreativeCommons license?
If yes, which one should be applied: "CC-BY" or "CC-BY-SA"?
- CC-BY 4.0 - https://creativecommons.org/licenses/by/4.0/
- CC-BY-SA 4.0 - https://creativecommons.org/licenses/by-sa/4.0/
it means like CC0 https://creativecommons.org/choose/zero/
But, as an intention, I want you to use only for non-commercial use. Because I want to aboid any kind of troubles.
Of course, we should consider about Industrial design rights of real companies such Dornier, NCA for real world .
- Gunny
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Re: [AIRCRAFT]DORNIER 228NG
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