Development milestones
First flight: 5 November 1997
Developed from: Diamond DA20
機体ライブラリ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プロファイル候補：10
機体を知る
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.
公開資料 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印刷物またはアーカイブ資料（公開リンクなし）
- EASA TCDS A.022印刷物またはアーカイブ資料（公開リンクなし）
- Diamond published data印刷物またはアーカイブ資料（公開リンクなし）
プロファイルによるモデル化
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.
この正確なリビジョンは、まだ公開インストールに対応していません。
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%
モデルが生み出すすべてに適用される最終的な全体出力スケール。デバイス上限の前に適用されます。
上げると: すべて(バネ、荷重、効果)が一緒に強まります。
下げると: すべてが一緒に和らぎます。
この値の理由: Scales overall profile strength while preserving effect balance, subject to device and output limits.
Forces
Spring strength80%
スティックを中央へ引き戻す基本のセンタリング力。他のすべての力はこの上に積み重なります。低すぎると通常飛行でスティックが頼りなく、高すぎると手に逆らい、上に重なる細かな手がかりを覆い隠します。
上げると: 手により強く抵抗する、固いセンタリング。
下げると: 空力荷重だけに頼る、柔らかいスティック。
この値の理由: 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%
中央付近でバネが沈黙する小さなニュートラルゾーン。静止時の微小な動きがガタつかないようにします。広いほど落ち着きますが緩くなり、狭いほど精密ですが中央で震えることがあります。
上げると: より静かだが緩い、遊びの多い中央。
下げると: 静止時に震えうる、締まった中央。
この値の理由: Sets travel around the centre before the baseline spring resists. Smaller values engage it sooner.
Overall aerodynamic load70%
両軸の持続荷重にかかるマスタースケールで、各軸の独立バランスの前に適用されます。プロファイルは通常これに触れず、二つの軸荷重を調整します。
上げると: 両軸がより強く荷重します。
下げると: 両軸が一緒に軽くなります。
この値の理由: 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
バネが全強度に達する速度。開始点からここまでの間、舵面上の気流が増すにつれセンタリングは徐々に固まります。
この値の理由: Sets the IAS where the low-speed blend reaches baseline strength; high-speed stiffening also uses it.
Centre firmness vs speed15%
舵角荷重に加えて、センタリング自体が速度でどれだけ固くなるか。ゼロなら中央の感触は一定、大きくすると巡航で固く、場周で緩くなります。
上げると: 速度とともに明確に固くなる中央。
下げると: どの速度でも一定の中央感覚。
この値の理由: 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
速度によるセンター硬化の上限。超高速飛行でバネが際限なく巻き上がるのを防ぎます。
上げると: 高速でより多くの総硬化を許容。
下げると: 硬化がより早く頭打ちに。
この値の理由: Limits the squared airspeed ratio used for high-speed spring stiffening; it is not a device-force cap.
Aileron load85%
エルロン舵角と速度による持続的なロール荷重で、ピッチとは独立に調整されます。エレベーター荷重と合わせて、レビューで語られる操縦調和の比率を決めます。
上げると: より重いロール力。
下げると: より軽く機敏なエルロン。
この値の理由: 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%
エレベーター舵角と速度による持続的なピッチ荷重で、ロールとは独立に調整されます。機種ごとのピッチの重さを決める主レバーです。エルロン、バネ、トリム、バフェットの力には触れません。
上げると: 速度での持続ピッチ力がより重く。
下げると: 保持する力の軽い、より軽やかなエレベーター。
この値の理由: Scales pitch aerodynamic loading; pitch spring travel and trim responses are separate settings.
Max output force55%
各定常ピッチ・ロール力がデバイスへ届く前の上限。強い機動でハードウェアを叩いたり飽和させたりしないための保護です。
上げると: クリップ前の定常力ピークがより高く。
下げると: より柔らかい天井。激しい機動が早く平らに。
この値の理由: Caps directed-force output. Native spring effects and device limits remain separate.
Airspeed blendingTrue
低速のバネ立ち上げ窓(上記の開始/全強度ノット)を有効にします。オフではバネは全速度で一定です。
この値の理由: Allows baseline spring strength to rise with indicated airspeed where the control law permits it.
Low-speed spring floor50%
停止状態で、速度が空力を生む前にバネがどれだけ残るか。床が高いと駐機中のスティックはしっかりし、低いと駐機した軽飛行機のケーブルが緩んだような感触になります。
上げると: 駐機・タキシー時により固いスティック。
下げると: 速度でしか目覚めない、駐機時の柔らかいスティック。
この値の理由: Sets low-speed spring strength as a fraction of baseline when blending is enabled. One keeps full strength.
Spring engagement start15 kt
バネが低速の床から全強度へ立ち上がり始める速度。離陸滑走で操縦系統が「目を覚ます」ポイントです。
この値の理由: Sets the IAS where the low-speed spring blend starts rising. This is a feel threshold, not a flight limit.
フォース調整速度125
空力荷重が設計上の満量に達する指示対気速度。荷重カーブ全体を機体の実際の速度域に固定します。172は110ノットで荷重が乗り、ジェットはずっと後です。
上げると: 荷重の到来が遅くなり、より速くまでスティックが軽いまま。
下げると: 荷重が早く到来し、巡航がより重く。
この値の理由: Sets the IAS reference for aerodynamic loading. It is an estimate, not published cruise TAS or a flight limit.
Trim
Trim relief (elevator)30%
エレベータートリムが保持ピッチ力をどれだけ和らげ、スティックの落ち着き位置をずらすか。100 %では正しくトリムされた機体は保持圧が不要になり、実機の「荷重をトリムで消す」手順そのものです。
上げると: トリムがより多くの保持力を除去。100 %ではフルトリムで打ち消し。
下げると: トリムしても力を保持し続けます。
この値の理由: 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%
ロールトリムの同じ軽減。多くのGA機には本物のエルロントリムがないためゼロのまま。ロールトリムを持つ機種には相応の値が入ります。
上げると: ロールトリムがより多くの保持力を除去。
下げると: ロールトリムの効きが弱く。
この値の理由: Scales supported roll-trim relief and permitted centre movement. Zero removes roll response.
Effect gains · Ground
Runway rumble38%
車輪速度と路面種別(舗装、草、砂利)による転がりの振動。
上げると: スティックの路面テクスチャがより強く。
下げると: より滑らかなタキシー。
この値の理由: Sets rolling texture strength, modified by speed, surface and undercarriage configuration.
Gear bumps25%
伸縮継ぎ目や轍、荒れた路面からの短い個別の衝撃で、連続的なゴロゴロに句読点を打ちます。
上げると: 継ぎ目と轍の衝撃がより鋭く。
下げると: より柔らかな地面のディテール。
この値の理由: Sets gear-bump texture during ground motion, separate from touchdown impact.
Effect gains · Airframe
Stick shaker50%
機体自身の失速警報システムが発火させる専用のスティックシェーカーの振動。本物のシェーカーを持つ機種だけに値が入り、他はすべて空力バフェットと警報音に頼ります。
上げると: より固いシェーカー。
下げると: より控えめなシェーカー。
この値の理由: Sets triggered shaker strength; inactive while the shaker feature is disabled.
Stall buffet50%
失速接近時と失速警報作動中の機体の震え。この翼が不満をどれだけ大声で告げるかです。切れ味よく落ちる機種は控えめなバフェットになり、警報音に警告を任せます。
上げると: より強い失速前の震え。
下げると: より控えめな翼。警報音が警告を担います。
この値の理由: Sets stall-buffet strength. Zero removes the cue without changing simulator stalls or warnings.
Mach buffet0%
マッハ限界接近時の遷音速バフェット。MMO付近のジェットには意味があり、そこへ到達しないレシプロやターボプロップではゼロです。
上げると: マッハ限界近くのより強い遷音速バフェット。
下げると: 高マッハでより滑らかな飛行。
この値の理由: Sets high-Mach buffet strength; onset and full-strength thresholds are separate.
Flap buffet28%
フラップが実際に空気を掴む速度窓で、気流に展開されたフラップによる機体の低周波振動。
上げると: フラップ作動中のより荒い飛行。
下げると: より柔らかな進入フラップ。
この値の理由: Sets flap buffet at the configured position and speed gates. Flap movement texture is separate.
Gear buffet0%
気流中に垂れた引込脚による機体のドラミング。機体形状が変わらない固定脚の機種ではゼロです。
上げると: 脚下げ時のドラミングが増加。
下げると: 脚下げ飛行がより綺麗に。
この値の理由: Sets gear aerodynamic buffet; movement and ground-contact cues are separate.
Effect gains · Engine, mechanical & drag
Touchdown thump65%
車輪が滑走路に触れる瞬間の単発のキック。沈下率でスケールされ、グリーサーはささやき、固い接地はドンと響きます。
上げると: 接地のより固い衝撃。
下げると: より柔らかな到着。
この値の理由: Sets landing-impact strength; landing telemetry and response shape determine the pulse.
Reverse rumble0%
逆推力やベータ域のプロペラが働いている間の滑走振動。リバースのない機種ではゼロです。
上げると: リバース中のより荒い滑走。
下げると: より控えめなリバース。
この値の理由: Sets reverse-thrust vibration with valid reverser and engine conditions. Zero removes the cue.
Engine rumble16%
アイドルから全出力まで回転数に従う連続的な動力装置の振動。前方で何かが燃料を燃やしている、常に存在する注意喚起です。
上げると: スティックのエンジンが増加。
下げると: より控えめなエンジン。
この値の理由: Sets estimated engine vibration using configured telemetry and response, not measured cockpit vibration.
Flap motion12%
シミュレーターがフラップ舵面の実際の移動を報告している間だけの連続振動。推定タイマーではなく、実際のアクチュエーター動作と故障に従います。
上げると: フラップ移動中の振動が増加。
下げると: より控えめなフラップ走行。
この値の理由: Sets texture from observed flap movement; a command without movement does not establish the cue.
Autopilot follow
AP follow authority10%
オートパイロットの指令がスティックを物理的にどこまで動かせるか。動いた軸がパイロット入力として読み返されうるMSFSでは極小に保ちます。ゼロで追従は完全に無効です。
上げると: オートパイロットがスティックを目に見えて多く動かします。
下げると: ほぼ気づかない追従。
この値の理由: 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.
この値の理由: 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.
この値の理由: Permits centering hold during a supported AP state, separate from following a moving target.
Autopilot · Neutral hold strength0.6
この値の理由: 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.
この値の理由: 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.
この値の理由: 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.
この値の理由: 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.
この値の理由: 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.
この値の理由: 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).
上げると: a more gradual build to a later peak.
下げると: a quicker build.
この値の理由: 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.
上げると: the effect begins later.
下げると: it begins earlier.
この値の理由: 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.
この値の理由: Enables aerodynamic cues; each still needs nonzero strength and its simulator conditions.
Aero · Shaker enabledFalse
Whether this feature is active in this profile.
この値の理由: Permits shaker at supported warning conditions; the switch does not establish aircraft equipment.
Ground
Ground · EnabledTrue
Whether this feature is active in this profile.
この値の理由: 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.
この値の理由: Enables engine cues with nonzero settings and valid running-engine telemetry.
Mechanical
Mechanical · EnabledTrue
Whether this feature is active in this profile.
この値の理由: Enables accessory cues with configured strengths and observed accessory movement.
Mechanical · Gain0
The strength of this effect.
上げると: a stronger effect.
下げると: a weaker one.
この値の理由: Sets texture from observed gear movement, separate from aerodynamic and touchdown effects.
すべてのプロファイル設定
| パラメーター | 値 | 何を制御するのかとその理由 |
|---|---|---|
| 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. |
| フォース調整速度 | 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. |
公開資料 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印刷物またはアーカイブ資料（公開リンクなし）
- EASA TCDS A.022印刷物またはアーカイブ資料（公開リンクなし）
- Diamond published data印刷物またはアーカイブ資料（公開リンクなし）
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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…
コミュニティ
この機体のコミュニティプロファイル
| 航空機 | プロファイル | シミュレーター | ハードウェア | Added | Reviews | Discussion | ダウンロード | Open profile |
|---|---|---|---|---|---|---|---|---|
| DA40-NG AsoboDA40 | DA40-NG Asobo by TheMomiX | MSFS | PicoWinder SideWinder Force Feedback Pro | 1 reply7月 27 | 506 |