Development milestones
First flight: 5 November 1997
Developed from: Diamond DA20
机型库Diamond DA40
bomberpilot · CC BY-SA 2.0 · Diamond DA40 Diamond Star picturedDiamond DA40
Mechanical stick controls with aerodynamic pitch trim and separately tuned pitch and roll resistance.
General aviationDA40配置文件选项：10 个
了解飞机
The DA40 took the DA20's general concept into a larger cabin. Its low wing, fixed tricycle undercarriage and extensive canopy glazing give it a distinctive appearance. Production has taken place in Austria and Canada, with several engine and equipment developments.
Petrol-engined and diesel-family DA40s differ in engine management and cockpit equipment. The simulator products identify their represented model.
Diamond DA40 NG
- Powerplant
- Austro AE 300 turbodiesel, 168 hp↗
- Seats
- 4↗
- Max takeoff weight
- 2,888 lb (1,310 kg)↗
- Wingspan
- 38 ft 2 in (11.63 m)↗
- Length
- 26 ft 5 in (8.06 m)↗
- Never exceed (Vne)
- 178 KIAS↗
- Maneuvering (Va)
- 108 KIAS at MTOW↗
- Stall, landing config (Vs0)
- ≈49 KCAS↗
- Max cruise
- ≈154 KTAS↗
- Service ceiling
- 16,400 ft↗
- Range
- ≈940 nm at economy cruise↗
- Usable fuel
- ≈39 US gal Jet A↗
Familiar fine handling, with a qualified verdict on the diesel
Whiteman approached the Austro-powered DA40 NG with experience of the original prototype and earlier production versions. Flying G-SUEO with its regular demonstration pilot, Mark, he appreciated the simple power control and comfortable seating, although mastering the Garmin displays would require more study. Initial acceleration was strong, but the departure did not deliver the improvement he had hoped for. Retracting the flaps brought a noticeable reduction in the modest early climb.
Once established, the familiar appeal returned: light, well-coordinated controls, a useful mechanical trimwheel and excellent visibility made formation flying and general manoeuvring a pleasure. The aeroplane required continuing right-pedal pressure, which Mark suspected might reflect that particular aircraft's rigging; Whiteman did not establish it as a fleet characteristic. His final assessment remained mixed. He admired the DA40's handling and recognised the diesel's potential economy, while wishing its takeoff and initial climb felt more convincing.
A trainer that rewards coordination and planning
Turner evaluated the DA40 as a prospective training aircraft and found plenty to keep a student engaged. Its low seating position and broad view made the runway feel close, while the initial takeoff required deliberate directional control. In the air, he found the stick easy to adopt and the controls light without becoming vague. Once properly trimmed, the aircraft held its attitude well, but its clean airframe demanded anticipation when levelling off or preparing to descend.
An overcast formed beneath the demonstration flight, so the return included an IFR clearance and vectors to an ILS. That gave Turner a practical opportunity to explore the workload of an instrument approach before breaking into visual conditions for landing. He finished the flight smiling and considered the Diamond a promising trainer for future professional pilots. His praise included the demands it placed on rudder coordination and energy management, alongside reservations about ground ventilation, storage space and the attention required during transition.
Dinner at Santa Paula changes a traditional pilot’s mind
Lee wanted to experience the DA40 XLS on an ordinary outing, so he joined distributor demonstration pilot Robert Stewart for a trip from Long Beach to Santa Paula. The wraparound view immediately impressed him, and he welcomed the manual trimwheel after initially fumbling with electric trim. Climbing out toward the coast, he began to appreciate how much of the surrounding landscape was visible from ahead of the wing.
The journey combined low-speed handling demonstrations, music through the headsets and a look at the Garmin synthetic-vision display before an arrival among Santa Paula's classic aircraft. Lee had expected to dislike a modern composite aeroplane, but found that the technology left plenty of opportunity to enjoy hand-flying. Returning to Long Beach, he was reluctant to walk away.
公开来源 16
- Diamond DA40 Diamond StarResearch background · Wikipedia revision 1373674831 · retrieved 2026-09-12
- Microsoft Flight Simulator aircraft manuals
- MSFS 2024 FAQ and edition aircraft inventory
- MSFS 2020 FAQ and edition aircraft inventory
- Flight test: Diamond DA40 NGPhilip Whiteman · 12 June 2015
- Diamond DA40: Airline Pilot Trainer, Part IIThomas Turner · 27 November 2004
- DA 40 XLS: The Innovator Keeps Getting BetterMarc C. Lee · 24 February 2009
- ICAO Doc 8643 — aircraft type designatorsPublic search data retrieved 2026-09-14; authority update 2026-09-03
- COWS | DA40 SeriesProduct listing captured 2026-09-30; edition scope from the reviewed catalogue
- DA40 Expansion PackProduct listing captured 2026-09-24; edition scope from the reviewed catalogue
- Take Command!: RealSimGear DA40NG, X-AviationProduct listing captured 2026-09-23; edition scope from the reviewed catalogue
- Diamond DA40NG-SimSolutions-DA40Product listing captured 2026-09-23; edition scope from the reviewed catalogue
- Diamond DA40-180 Diamond StarProduct listing captured 2026-09-24; edition scope from the reviewed catalogue
- Diamond DA40 NG AFM纸质或存档参考资料；无公开链接
- EASA TCDS A.022纸质或存档参考资料；无公开链接
- Diamond published data纸质或存档参考资料；无公开链接
配置文件如何建模
Diamond DA40 NG
Free + ProMSFS 2024MSFS 2020
The DA40 took the DA20's general concept into a larger cabin. Its low wing, fixed tricycle undercarriage and extensive canopy glazing give it a distinctive appearance. Production has taken place in Austria and Canada, with several engine and equipment developments.
The factory starting point selects Diamond DA40 NG across MSFS 2024, MSFS 2020.
Mechanical linkage motivates airspeed-sensitive stick resistance. Spring resistance builds with the selected airspeed response. A separate aerodynamic term adds speed-dependent control load.
The DA40 elevator tab supplies pitch pressure relief, unlike the DA20’s spring-preload system. Valid trim provides the configured pressure relief. Autopilot following is enabled for supported control references.
此确切修订版尚未开放公开安装。
Controls and trim
The DA40’s elevator and ailerons use pushrods, with cables operating the rudder. A Bowden cable drives the elevator trim tab, and electric flaps select their named positions. Lycoming XLS and diesel NG versions retain different propulsion and cockpit equipment.
About the values
The gains are normalized profile settings. They describe the chosen effect balance; hand force depends on the device and its output limits. IAS references are tuning values rather than operating limits. Physical acceptance of this revision remains pending.
Master gain & control system
Master gain85%
施加于模型产出的一切、在设备上限之前的最终整体输出缩放。
调高: 一切(弹簧、载荷、效果)一同增强。
调低: 一切一同变柔。
设定理由: Scales overall profile strength while preserving effect balance, subject to device and output limits.
Forces
Spring strength80%
把摇杆拉回中央的基础回中力。其他所有力都叠加在它之上。太低,正常飞行中摇杆会发软;太高,它会与你的手较劲,并掩盖叠加其上的细微提示。
调高: 更硬的回中,更抗手。
调低: 更软的杆,只靠气动载荷。
设定理由: Mechanical linkage motivates airspeed-sensitive stick resistance. The baseline spring is 0.8. Its low-speed blend reaches baseline strength at 67 KIAS.
Exact product and documentation researchDA40 Expansion PackDiamond-authored DA40NG AFM archived copyDiamond official DA40NG G1000 legacy checklist 21.0Publisher DA40NG v1.2.0 current compatibility and trim changesRealSimGear separate NXi option and aircraft compatibilityDiamond DA40NG-SimSolutions-DA40Diamond DA40-180 Diamond StarDiamond DA40 technical specificationsDA40-180 Diamond StarFlight test: Diamond DA40 NGDA 40 XLS: The Innovator Keeps Getting BetterBuying a Used Aircraft: Diamond DA40 StarSpring deadband4%
中央附近弹簧保持安静的小中立区,让静止时的微小移动不会咔嗒作响。更宽更安稳但更松,更窄更精确但可能在中央附近抖动。
调高: 更安静但更松的中央,旷量更大。
调低: 更紧的中央,静止时可能抖动。
设定理由: Sets travel around the centre before the baseline spring resists. Smaller values engage it sooner.
Overall aerodynamic load70%
作用于两条持续轴载荷的主缩放,在它们各自的独立平衡之前施加。配置文件通常不动它,而是调校两条轴载荷。
调高: 两轴载荷一同加重。
调低: 两轴一同减轻。
设定理由: The aerodynamic-load gain is 0.7 with an indicated-speed reference of 125 KIAS. This supplies speed-dependent loading alongside the spring.
Spring engagement full67 kt
弹簧达到全强度的空速。从起点到这里,随着气流在操纵面上增强,回中逐渐变硬。
设定理由: Sets the IAS where the low-speed blend reaches baseline strength; high-speed stiffening also uses it.
Centre firmness vs speed15%
在偏转载荷之外,回中本身随速度变硬的程度。零则中央手感恒定;越大,巡航时回中越硬,起落航线上越松。
调高: 中央随速度明显变硬。
调低: 任何速度下中央手感恒定。
设定理由: The high-speed spring-stiffening gain is 0.15. It strengthens the permitted spring response above 67 KIAS, with the squared-speed ratio capped at 5.
Centre stiffening cap5
速度驱动的中央变硬上限,防止高速飞行把弹簧无限上紧。
调高: 高速允许更多总硬化。
调低: 硬化更早封顶。
设定理由: Limits the squared airspeed ratio used for high-speed spring stiffening; it is not a device-force cap.
Aileron load85%
由副翼偏转和空速产生的持续横滚载荷,独立于俯仰调校。与升降舵载荷一起,决定评测中常说的操纵协调比。
调高: 横滚力更重。
调低: 副翼更轻更灵。
设定理由: Roll and pitch aerodynamic scales are 0.85 and 1, respectively. They set the aerodynamic axis balance. No custom spring-travel curve is enabled.
Elevator load100%
由升降舵偏转和空速产生的持续俯仰载荷,独立于横滚调校。这是决定机型俯仰重量的主杠杆。它不影响副翼、弹簧、配平或抖振力。
调高: 速度下持续俯仰力更重。
调低: 升降舵更轻,握持更省力。
设定理由: Scales pitch aerodynamic loading; pitch spring travel and trim responses are separate settings.
Max output force55%
每个稳态俯仰或横滚力到达设备前的上限,防止猛烈机动中砸击或饱和硬件。
调高: 削波前更高的稳态力峰值。
调低: 更柔的上限;猛烈机动更早被抹平。
设定理由: Caps directed-force output. Native spring effects and device limits remain separate.
Airspeed blendingTrue
启用低速弹簧介入窗口(上面的起始/全强度节数)。关闭时弹簧在所有速度下恒定。
设定理由: Allows baseline spring strength to rise with indicated airspeed where the control law permits it.
Low-speed spring floor50%
在静止、空速尚未产生气动力之前,弹簧还剩多少。下限高,停机时摇杆结实;下限低,则是停放轻型飞机那种钢索松弛的感觉。
调高: 停机和滑行时杆更结实。
调低: 停机时杆发软,只随速度苏醒。
设定理由: Sets low-speed spring strength as a fraction of baseline when blending is enabled. One keeps full strength.
Spring engagement start15 kt
弹簧从低速下限开始向全强度攀升的空速:起飞滑跑中操纵面"苏醒"的那一刻。
设定理由: Sets the IAS where the low-speed spring blend starts rising. This is a feel threshold, not a flight limit.
力反馈调校速度125
气动载荷达到设计满值的指示空速。它把整条载荷曲线锚定在飞机真实的速度范围:172在110节就载满,喷气机要晚得多。
调高: 载荷来得更晚;杆轻到更高速度。
调低: 载荷来得更早,巡航更沉。
设定理由: Sets the IAS reference for aerodynamic loading. It is an estimate, not published cruise TAS or a flight limit.
Trim
Trim relief (elevator)30%
升降舵配平缓解持续俯仰力、移动杆的安定位置的强度。在100 %时,配平得当的飞机不需要保持压力——正是真实飞行中"用配平消掉载荷"的流程。
调高: 配平消掉更多持续力;100 %时满配平可完全抵消。
调低: 即使配平也仍要持续用力。
设定理由: The DA40 elevator tab supplies pitch pressure relief, unlike the DA20’s spring-preload system. Pitch authority 0.3 provides load relief and permitted centre movement; roll authority is 0.
Exact product and documentation researchDA40 Expansion PackDiamond-authored DA40NG AFM archived copyDiamond official DA40NG G1000 legacy checklist 21.0Publisher DA40NG v1.2.0 current compatibility and trim changesRealSimGear separate NXi option and aircraft compatibilityDiamond DA40NG-SimSolutions-DA40Diamond DA40-180 Diamond StarDiamond DA40 technical specificationsDA40-180 Diamond StarFlight test: Diamond DA40 NGDA 40 XLS: The Innovator Keeps Getting BetterBuying a Used Aircraft: Diamond DA40 StarTrim relief (aileron)0%
横滚配平的同类缓解。多数通航机型没有真正的副翼配平,所以保持为零;有横滚配平的机型获得相应的值。
调高: 横滚配平消掉更多持续力。
调低: 横滚配平作用更小。
设定理由: Scales supported roll-trim relief and permitted centre movement. Zero removes roll response.
Effect gains · Ground
Runway rumble38%
由轮速和地面类型(铺装、草地、砾石)产生的滚动振动。
调高: 杆上更强的地面质感。
调低: 更平滑的滑行。
设定理由: Sets rolling texture strength, modified by speed, surface and undercarriage configuration.
Gear bumps25%
来自伸缩缝、车辙和粗糙地面的短促离散颠簸,为持续隆隆声打上标点。
调高: 接缝与车辙的冲击更清晰。
调低: 更柔的地面细节。
设定理由: Sets gear-bump texture during ground motion, separate from touchdown impact.
Effect gains · Airframe
Stick shaker50%
由飞机自身失速警告系统触发的专用抖杆器振动。只有真有抖杆器的机型才有值;其余全靠气动抖振和喇叭。
调高: 更硬的抖杆器。
调低: 更含蓄的抖杆器。
设定理由: Sets triggered shaker strength; inactive while the shaker feature is disabled.
Stall buffet50%
接近失速及失速警告响起时的机体抖动:这副机翼宣告不满的音量。断失干脆的机型抖振收敛,让喇叭承担警告。
调高: 更强的失速前颤抖。
调低: 更含蓄的机翼;警告交给喇叭。
设定理由: Sets stall-buffet strength. Zero removes the cue without changing simulator stalls or warnings.
Mach buffet0%
接近马赫极限的跨音速抖振。对接近MMO的喷气机有意义,对到不了那里的活塞机和涡桨机为零。
调高: 接近马赫极限时更强的跨音速抖振。
调低: 高马赫下更平滑的飞行。
设定理由: Sets high-Mach buffet strength; onset and full-strength thresholds are separate.
Flap buffet28%
襟翼伸入气流后机体的低频振动,发生在它们真正做功的速度窗口内。
调高: 襟翼做功时更粗糙的飞行。
调低: 更柔的进近襟翼。
设定理由: Sets flap buffet at the configured position and speed gates. Flap movement texture is separate.
Gear buffet0%
可收放起落架悬在气流中引起的机体鼓振。固定起落架机型为零,它们的机体外形从不改变。
调高: 放起落架时更多鼓振。
调低: 放起落架飞行更干净。
设定理由: Sets gear aerodynamic buffet; movement and ground-contact cues are separate.
Effect gains · Engine, mechanical & drag
Touchdown thump65%
机轮触及跑道那一下的单次冲击,按下沉率缩放:轻柔着陆是耳语,结实到达是一记闷响。
调高: 触地时更硬的一击。
调低: 更柔的到达。
设定理由: Sets landing-impact strength; landing telemetry and response shape determine the pulse.
Reverse rumble0%
反推或桨叶beta区工作时的滑跑振动。无反推机型为零。
调高: 反推下更粗糙的滑跑。
调低: 更含蓄的反推。
设定理由: Sets reverse-thrust vibration with valid reverser and engine conditions. Zero removes the cue.
Engine rumble16%
从慢车到全功率跟随转速的持续动力装置振动——前方有东西在烧油的永恒提醒。
调高: 杆里更多发动机。
调低: 更含蓄的发动机。
设定理由: Sets estimated engine vibration using configured telemetry and response, not measured cockpit vibration.
Flap motion12%
仅在模拟器报告襟翼舵面确实移动时的持续振动。它跟随真实作动器的运动和故障,而非估算的计时器。
调高: 襟翼移动中更多振动。
调低: 更含蓄的襟翼行程。
设定理由: Sets texture from observed flap movement; a command without movement does not establish the cue.
Autopilot follow
AP follow authority10%
自动驾驶指令可以让杆实际移动多远。在MSFS中保持极小,因为移动的轴可能被读回为飞行员输入;零则完全禁用跟随。
调高: 自动驾驶让你的杆移动得明显更多。
调低: 几乎察觉不到的跟随。
设定理由: Sets admitted AP-follow gain, not a percentage of travel. Runtime ownership and input limits still apply.
Autopilot
Autopilot · Follow enabledTrue
Whether this feature is active in this profile.
设定理由: Following is on at 0.1 authority when a supported, valid autopilot control reference is available.
Autopilot · Neutral hold enabledFalse
Whether this feature is active in this profile.
设定理由: Permits centering hold during a supported AP state, separate from following a moving target.
Autopilot · Neutral hold strength0.6
设定理由: Sets admitted AP neutral-hold strength; inactive while neutral hold is disabled.
Stick feel
StickFeel · Trim feel enabledTrue
Whether this feature is active in this profile.
设定理由: Retained for compatibility and group membership. Trim relief, rather than this flag, controls centre movement.
StickFeel · Trim relief enabledTrue
Whether this feature is active in this profile.
设定理由: Allows trim relief with supported control law and valid telemetry. Axis authorities set its amount.
StickFeel · Force trim enabledFalse
Whether this feature is active in this profile.
设定理由: Enables local force trim, separate from aircraft-owned trim and add-on integration qualification.
StickFeel · G load enabledTrue
Whether this feature is active in this profile.
设定理由: Allows load-factor changes to modify permitted spring laws. Passive fly-by-wire feel can suppress it.
StickFeel · Rate damping enabledTrue
Whether this feature is active in this profile.
设定理由: Enables rate damping with the configured coefficients and control law.
Aero
Aero · Max flap index2
Where this effect reaches full strength (or has fully faded, for washouts).
调高: a more gradual build to a later peak.
调低: a quicker build.
设定理由: Sets the final flap index for detent normalization. UP plus three detents uses maximum index3.
Aero · Min flap index1
Where this effect begins fading in.
调高: the effect begins later.
调低: it begins earlier.
设定理由: Sets the first flap detent that admits buffet; this is a handle index, not degrees.
Aero · EnabledTrue
Whether this feature is active in this profile.
设定理由: Enables aerodynamic cues; each still needs nonzero strength and its simulator conditions.
Aero · Shaker enabledFalse
Whether this feature is active in this profile.
设定理由: Permits shaker at supported warning conditions; the switch does not establish aircraft equipment.
Ground
Ground · EnabledTrue
Whether this feature is active in this profile.
设定理由: Enables ground effects; each still needs its own strength and contact or motion telemetry.
Engine
Engine · EnabledTrue
Whether this feature is active in this profile.
设定理由: Enables engine cues with nonzero settings and valid running-engine telemetry.
Mechanical
Mechanical · EnabledTrue
Whether this feature is active in this profile.
设定理由: Enables accessory cues with configured strengths and observed accessory movement.
Mechanical · Gain0
The strength of this effect.
调高: a stronger effect.
调低: a weaker one.
设定理由: Sets texture from observed gear movement, separate from aerodynamic and touchdown effects.
全部配置文件设置
| 参数 | 数值 | 控制作用及原因 |
|---|---|---|
| Spring strength | 0.8 | Mechanical linkage motivates airspeed-sensitive stick resistance. The baseline spring is 0.8. Its low-speed blend reaches baseline strength at 67 KIAS. |
| Spring deadband | 0.04 | Sets travel around the centre before the baseline spring resists. Smaller values engage it sooner. |
| Force gain | 0.7 | The aerodynamic-load gain is 0.7 with an indicated-speed reference of 125 KIAS. This supplies speed-dependent loading alongside the spring. |
| Master gain | 0.85 | Scales overall profile strength while preserving effect balance, subject to device and output limits. |
| Spring full-strength speed | 67 kt | Sets the IAS where the low-speed blend reaches baseline strength; high-speed stiffening also uses it. |
| Airspeed spring stiffening | 0.15 | The high-speed spring-stiffening gain is 0.15. It strengthens the permitted spring response above 67 KIAS, with the squared-speed ratio capped at 5. |
| Airspeed stiffening cap | 5 | Limits the squared airspeed ratio used for high-speed spring stiffening; it is not a device-force cap. |
| Aileron force scale | 0.85 | Roll and pitch aerodynamic scales are 0.85 and 1, respectively. They set the aerodynamic axis balance. No custom spring-travel curve is enabled. |
| Elevator force scale | 1 | Scales pitch aerodynamic loading; pitch spring travel and trim responses are separate settings. |
| Maximum output force | 0.55 | Caps directed-force output. Native spring effects and device limits remain separate. |
| Autopilot · Follow enabled | True | Following is on at 0.1 authority when a supported, valid autopilot control reference is available. |
| Autopilot · Follow authority | 0.1 | Sets admitted AP-follow gain, not a percentage of travel. Runtime ownership and input limits still apply. |
| Autopilot · Neutral hold enabled | False | Permits centering hold during a supported AP state, separate from following a moving target. |
| Autopilot · Neutral hold strength | 0.6 | Sets admitted AP neutral-hold strength; inactive while neutral hold is disabled. |
| StickFeel · Trim feel enabled | True | Retained for compatibility and group membership. Trim relief, rather than this flag, controls centre movement. |
| StickFeel · Trim relief enabled | True | Allows trim relief with supported control law and valid telemetry. Axis authorities set its amount. |
| Aero · Max flap index | 2 | Sets the final flap index for detent normalization. UP plus three detents uses maximum index3. |
| Aero · Min flap index | 1 | Sets the first flap detent that admits buffet; this is a handle index, not degrees. |
| Aero · Amplitude | 0.5 | Sets triggered shaker strength; inactive while the shaker feature is disabled. |
| Dynamic-pressure blend | True | Allows baseline spring strength to rise with indicated airspeed where the control law permits it. |
| Minimum spring factor | 0.5 | Sets low-speed spring strength as a fraction of baseline when blending is enabled. One keeps full strength. |
| Spring wake-up speed | 15 kt | Sets the IAS where the low-speed spring blend starts rising. This is a feel threshold, not a flight limit. |
| 力反馈调校速度 | 125 kt | Sets the IAS reference for aerodynamic loading. It is an estimate, not published cruise TAS or a flight limit. |
| StickFeel · Elevator authority | 0.3 | The DA40 elevator tab supplies pitch pressure relief, unlike the DA20’s spring-preload system. Pitch authority 0.3 provides load relief and permitted centre movement; roll authority is 0. |
| StickFeel · Aileron authority | 0 | Scales supported roll-trim relief and permitted centre movement. Zero removes roll response. |
| StickFeel · Force trim enabled | False | Enables local force trim, separate from aircraft-owned trim and add-on integration qualification. |
| StickFeel · G load enabled | True | Allows load-factor changes to modify permitted spring laws. Passive fly-by-wire feel can suppress it. |
| StickFeel · Rate damping enabled | True | Enables rate damping with the configured coefficients and control law. |
| Aero · Enabled | True | Enables aerodynamic cues; each still needs nonzero strength and its simulator conditions. |
| Aero · Gain | 0.5 | Sets stall-buffet strength. Zero removes the cue without changing simulator stalls or warnings. |
| Aero · Gain | 0 | Sets high-Mach buffet strength; onset and full-strength thresholds are separate. |
| Aero · Gain | 0.28 | Sets flap buffet at the configured position and speed gates. Flap movement texture is separate. |
| Aero · Gain | 0 | Sets gear aerodynamic buffet; movement and ground-contact cues are separate. |
| Aero · Shaker enabled | False | Permits shaker at supported warning conditions; the switch does not establish aircraft equipment. |
| Ground · Enabled | True | Enables ground effects; each still needs its own strength and contact or motion telemetry. |
| Ground · Gain | 0.38 | Sets rolling texture strength, modified by speed, surface and undercarriage configuration. |
| Ground · Gain | 0.25 | Sets gear-bump texture during ground motion, separate from touchdown impact. |
| Ground · Gain | 0.65 | Sets landing-impact strength; landing telemetry and response shape determine the pulse. |
| Ground · Gain | 0 | Sets reverse-thrust vibration with valid reverser and engine conditions. Zero removes the cue. |
| Engine · Enabled | True | Enables engine cues with nonzero settings and valid running-engine telemetry. |
| Engine · Gain | 0.16 | Sets estimated engine vibration using configured telemetry and response, not measured cockpit vibration. |
| Mechanical · Enabled | True | Enables accessory cues with configured strengths and observed accessory movement. |
| Mechanical · Gain | 0.12 | Sets texture from observed flap movement; a command without movement does not establish the cue. |
| Mechanical · Gain | 0 | Sets texture from observed gear movement, separate from aerodynamic and touchdown effects. |
公开来源 23
- Diamond DA40 Diamond StarResearch background · Wikipedia revision 1373674831 · retrieved 2026-09-12
- Exact product and documentation researchExact COWS product: configurations, AFCS/trim, systems and platformsProduct listing captured 2026-09-30; edition scope from the reviewed catalogue
- DA40 Expansion PackExact product and reviewed configuration passagesProduct listing captured 2026-09-24; edition scope from the reviewed catalogue
- Diamond-authored DA40NG AFM archived copyDA40NG AFM PDF pp263-267, section7-3 to7-7; PDF263-265/printed7-3 to7-5, revision3; image reviewed
- Diamond official DA40NG G1000 legacy checklist 21.0ZIP DA40_NG_Checklist_Legacy_rev21.pdf p10,
- Publisher DA40NG v1.2.0 current compatibility and trim changesPublisher opening post; Bug Fixes and Improvements
- RealSimGear separate NXi option and aircraft compatibilityProduct compatibility list
- Diamond DA40NG-SimSolutions-DA40XP12version1.3.0 January25,2025 and1.2.x changesProduct listing captured 2026-09-23; edition scope from the reviewed catalogue
- Diamond DA40-180 Diamond StarExact product and reviewed configuration passagesProduct listing captured 2026-09-24; edition scope from the reviewed catalogue
- Diamond DA40 technical specificationsDiamond DA40
- DA40-180 Diamond StarDiamond DA40
- Flight test: Diamond DA40 NGPhilip Whiteman · 12 June 2015
- DA 40 XLS: The Innovator Keeps Getting BetterMarc C. Lee · 24 February 2009
- Buying a Used Aircraft: Diamond DA40 StarDiamond DA40
- Microsoft Flight Simulator aircraft manuals
- MSFS 2024 FAQ and edition aircraft inventory
- MSFS 2020 FAQ and edition aircraft inventory
- Diamond DA40: Airline Pilot Trainer, Part IIThomas Turner · 27 November 2004
- ICAO Doc 8643 — aircraft type designatorsPublic search data retrieved 2026-09-14; authority update 2026-09-03
- Take Command!: RealSimGear DA40NG, X-AviationProduct listing captured 2026-09-23; edition scope from the reviewed catalogue
- Diamond DA40 NG AFM纸质或存档参考资料；无公开链接
- EASA TCDS A.022纸质或存档参考资料；无公开链接
- Diamond published data纸质或存档参考资料；无公开链接
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机库闲谈
关于 Diamond DA40 的飞行与调校的公开讨论(社区论坛)。上方的纠错将私下送达维护者;机库闲谈是公开的。
Hangar talk for the Diamond DA40 NG. How does the real one feel, and how close does the built-in profile get? Compare cockpit time, tuning tweaks, and community profiles here. Research page: Diamond DA40 NG in the aircra…
社区
该机型的社区配置
| 飞机 | 个人资料 | 模拟器 | 硬件 | Added | Reviews | Discussion | 下载 | Open profile |
|---|---|---|---|---|---|---|---|---|
| DA40-NG AsoboDA40 | DA40-NG Asobo by TheMomiX | MSFS | PicoWinder SideWinder Force Feedback Pro | 1 reply7月 27 | 508 |