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DA118-208 AIR CHINA

9,267 Deandash  2.0 years ago
3,756 downloads
Auto Credit Based on Deandash's DA118-201X

I'm very happy to lanuch my new plane!
Thanks to @kaqiusha123's help about FunkyTree ,provided beautiful cover.
And thank @Elizabethovo provide the delicate main landing gear.
I also thank @TYUI3120 for his suggestion about the start program.
The Air China's LOGO is made by@DEC12.
I have been helped by many people. Thank you very much.

Basic introduction

DA118,Twin engine regional airliner,The passenger capacity is about 100 people.It adopts the layout of engine top and canard wing,More powerful performance at low speed.At the same time, it can better adapt to the harsh environment.It in order to replace DA116 and complete with other airliner.

Infor of DA118

Type:DA118-209
MAX Speed(altitude 10000m):1030km/h
Cruising altitude :10000m
Cruising speed :867km/h(70%Throttle)
Max passenger capacity :110 people.

Nav light&Becon light &rain brush need open in cockpit
Activate
1:Taxi Light
2:Strobe Light
3:Take off Light
4:Landing Light
5:Landing roll back to center mode
6:Reverse await.move Trim to 10% to start reverse.
7:Cabin light
Trim:Manual Trim
VTOL0~1:Flap

Other instructions

Engine start program

The progress I wrote in the roof of cockpit,and I made a switch to skip the startup process, but it will cause the loss of some experiences, such as the sound of the engine and the light on the cockpit roof

Coordinate guide system

This system was used in DA117,and continue to use in DA118.
It can according a coordinate you input ,then indicate the direction and distance between you and the destination.The use way I wrote in plane instruction.

AUTO TRIM

This system in order to solve the cumbersome problem of manual trim and manual trim at high speed is very difficult to make the plane balance.
It is according to setting climb & descent rate or pitch angle to control the plane's pitch at the corresponding angle.
The use way&note I wrote in plane instruction.

Due to the radical layout, DA118 encountered various difficulties during the test flight. Fortunately, these problems were basically solved?
I personally like to make strange airliners based on certain rationality. I hope you can like it and have a pleasant flight.

Have a nice flight!



This photo by@GhostTeam

Spotlights

General Characteristics

  • Predecessor DA118-201X
  • Successors 2 airplane(s)
  • Created On Windows
  • Wingspan 119.6ft (36.4m)
  • Length 108.3ft (33.0m)
  • Height 27.3ft (8.3m)
  • Empty Weight N/A
  • Loaded Weight 20,337lbs (9,225kg)

Performance

  • Power/Weight Ratio 1.591
  • Horse Power/Weight Ratio 0.024
  • Wing Loading 8.0lbs/ft2 (38.9kg/m2)
  • Wing Area 2,555.4ft2 (237.4m2)
  • Drag Points 7422

Parts

  • Number of Parts 936
  • Control Surfaces 5
  • Performance Cost 4,281
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  • Profile image
    9,267 Deandash

    @togethersimpleKMG 因为有顺序,没有按照顺序的话就启动不了

    9 months ago
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    问一问up主为什么有些按钮点不动

    10 months ago
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    9,267 Deandash

    @bliblijianfeiplayer 😁

    1.5 years ago
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    飞都飞不来

    +4 1.5 years ago
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    9,267 Deandash

    @BigAeroplane 我尽量零件数不超过1000个

    1.6 years ago
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    3,140 BigAeroplane

    936个零件,极致压缩啊!

    1.7 years ago
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    9,267 Deandash

    @WinsWings Thanks

    1.7 years ago
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    254k WinsWings

    I love this concept. Great work

    1.7 years ago
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    9,267 Deandash

    @IMULAerospaceIndustries hhh,you can experiment overload by an airliner .jpg

    +1 1.9 years ago
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    I love pulling 80G turns and turning everyone inside the aircraft to paste, you don’t?

    +1 1.9 years ago
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    9,267 Deandash

    @TKT541 Thanks

    2.0 years ago
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    0 TKT541

    Cool

    2.0 years ago
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    9,267 Deandash

    @UltraLight SP's physical properties are really strange, but that's what makes some strange aircraft. It is true that the upper engine will cause maintenance difficulties, but this is also to make use of the boundary effect to supplement the air flow on the upper wing. Thank you for enjoying my plane

    +4 2.0 years ago
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    9,267 Deandash

    @MrCOPTY Thanks

    2.0 years ago
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    38.2k UltraLight

    @Deandash yeah, the 4 or 5 degrees you see here is not exactly realistic to real life haha. SP physics makes air behave more like water, very hard to squeeze and shape. Essentially the wing just goes whatever direction it's pointing, which means higher AoAs are really difficult to hit without a super unstable plane like GuyFolk makes. So IRL it would be landing at much higher AoA than here.

    Also landing at low AoA is super dangerous because the speed is way higher than it needs to be. So yeah sorry to poop on your design so much but in all honesty, it's cool and I like it, but it just probably wouldn't be a thing. Also because like engine maintenance and stuff it would be better below the wing.

    +1 2.0 years ago
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    68.8k MrCOPTY

    @Deandash Bro Good Job, It's Your Best Aircraft Ever

    2.0 years ago
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    9,267 Deandash

    @acdgTCAS 谢谢

    2.0 years ago
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    9,267 Deandash

    @chenyz13351 问题不大,之后不会再难了

    2.0 years ago
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    up太牛了,大爱大爱

    2.0 years ago
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    好家伙,这起飞是一次比一次难

    +1 2.0 years ago
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    9,267 Deandash

    @UltraLight Yes, At high angles of attack, the canard wing will block the engine and affect the intake. Therefore, we can limit the angle of attack. For example, when landing, the angle of attack will be basically small or even negative. When I test the stall speed of 89km / h, the angle of attack will be about 4 or 5 degrees. It cannot be avoided during take-off, but will the duck wing cover be stronger or weaker when the speed is faster? I'm not sure. This time I mainly want to try the plane with canard wing layout. The upper engine is to further enhance the lift. Thank you for liking this design

    2.0 years ago
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    9,267 Deandash

    @Faqa There have a switch can enable you control engine directly

    +1 2.0 years ago
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    0 Faqa

    I just want to fly not trying to a pilot with the engine start

    2.0 years ago
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    38.2k UltraLight

    Cool concept though.

    2.0 years ago
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    38.2k UltraLight

    Lol the front canards' wake would probably create a massive vacuum in front of the jets when at a high angle of attack(takeoff and landing), so one would stall out, you would lose power, causing a huge drop in airspeed. The pilots would be putting in quite a bit of yaw to counter the asymmetrical thrust, meaning they might try to use aileron in the final approach. Unfortunately, this will stall the wing and send them into a spin.

    Everybody dies

    2.0 years ago
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