Development milestones
First flight: 14 July 1988
Developed from: Mooney 301
機体ライブラリDaher TBM family
Michael Mainiero · CC BY-SA 3.0 · Daher-SOCATA TBM 900 in flightDaher TBM family
Manual yoke loading and aerodynamic pitch-trim relief, with separate propeller, gear and flap cues.
TurbopropTBM9プロファイル候補：5
機体を知る
The TBM programme began as a collaboration between SOCATA and Mooney and continued under Daher. The low-wing airframe carries one nose-mounted turboprop and a pressurised cabin. Successive versions developed the engines, aerodynamics, avionics and pilot interface.
The analogue-panel TBM 850, glass-cockpit TBM 900 and TBM 930 occupy different points in that progression. Simulator developers model these panel generations and different levels of persistent system behaviour, documented for each product.
Daher TBM 930
- Powerplant
- Pratt & Whitney PT6A-66D, 850 shp↗
- Seats
- 6↗
- Max takeoff weight
- 7,394 lb (3,354 kg)↗
- Wingspan
- 42 ft 1 in (12.83 m)↗
- Length
- 35 ft 2 in (10.72 m)↗
- Max operating (Vmo)
- 266 KIAS↗
- Stall, landing config (Vs0)
- ≈65 KCAS↗
- Max cruise
- 330 KTAS↗
- Service ceiling
- 31,000 ft↗
- Range
- 1,730 nm↗
- Usable fuel
- 291 US gal↗
- Pressurization
- 6.2 psi differential↗
Demonstrating the 930’s emergency descent and learning its menus
Horne flew the TBM 930 at Tarbes with chief test pilot Stéphane Jacques in March 2016. Their demonstration deliberately explored the aircraft's response to a depressurisation scenario: at 20,000 feet they put on oxygen masks and shut off the bleed-air supply. Horne watched the emergency-descent function turn the aircraft and bring it down to a selected safe level, with terrain affecting the altitude used for the exercise. It was a planned demonstration with a test pilot, rather than an account of an in-service emergency.
He also explored the electronic stability protection and the new G3000 interface. The protective servo forces became noticeable as he pushed toward the system's limits. Meanwhile, the touchscreen menus introduced a learning task even for a pilot familiar with earlier TBMs: finding the right page and returning through layers of selections required practice.
A 960 on a real trip through busy airspace
Boatman joined owner-pilot Malte Lorenz on flights between Hagerstown and Republic Airport in his 2024 TBM 960. The trip put the aircraft into the congested Northeast airspace in which Lorenz regularly used it. A complicated initial clearance and relatively low assigned altitudes reinforced his preference for a turboprop on shorter journeys. At Republic, they made an instrument approach beneath a coastal cloud layer. Another practical moment came when extra passengers wanted to join: the on-board loading calculation showed the proposed load exceeded limits, and they declined the request.
Returning to Hagerstown brought strong southerly winds and a choice of the shorter runway with a more favourable alignment. Lorenz disconnected the autopilot early and controlled the approach speed carefully. Boatman describes a gentle touchdown and ample room remaining, while acknowledging how short the runway looked from the approaching aircraft.
Crisp handling, a coupled go-around and a simulated engine failure
Gerzanics evaluated TBM 940 F-HGDA with Daher demonstration pilot Wayman Luy at Pompano Beach. He found the ground steering precise and the yoke forces light during takeoff. In a fast descent the aircraft responded crisply in all three axes. His stall demonstrations were more varied: the clean stall produced a wings-level pitch break, while flap-extended stalls included a left wing drop that he arrested during recovery. Luy suggested the left-wing radar installation as a possible explanation for that asymmetry.
The flight also contrasted automation with hands-on flying. Gerzanics watched the autopilot and autothrottle manage an instrument approach and coupled go-around, then handled a simulated engine failure toward Belle Glade. They arrived a little high and touched down long, using braking and reverse to slow. He particularly enjoyed manoeuvring the aircraft through tight turns on the narrow runway afterward. The engine remained available during the simulated failure.
公開資料 16
- SOCATA TBMResearch background · Wikipedia revision 1363498428 · retrieved 2026-09-12
- Microsoft Flight Simulator aircraft manuals
- MSFS 2024 FAQ and edition aircraft inventory
- MSFS 2020 FAQ and edition aircraft inventory
- TBM 850 manual
- X-Plane aircraft and avionics manuals
- TBM 900 product
- Pilot Report: Daher’s New TBM 930A 2016 real-aircraft pilot report. Publisher access restrictions may apply.
- TBM 850Official developer / designated store catalogue · checked 2026-09-12
- TBM’s 930 joins the flockThomas A. Horne · June 2016 · Tarbes demonstration
- Moment of ZenJulie Boatman · November 2024 · 2024 TBM 960
- Power of one: TBM 940 flight testMichael Gerzanics · 15–21 October 2019 · pages 26–29
- ICAO Doc 8643 — aircraft type designatorsPublic search data retrieved 2026-09-14; authority update 2026-09-03
- Daher TBM 930 POH印刷物またはアーカイブ資料（公開リンクなし）
- EASA TCDS A.010印刷物またはアーカイブ資料（公開リンクなし）
- Daher 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
Black Square TBM 850
Free + ProMSFS 2020MSFS 2024Black Square
The TBM programme began as a collaboration between SOCATA and Mooney and continued under Daher. The low-wing airframe carries one nose-mounted turboprop and a pressurised cabin. Successive versions developed the engines, aerodynamics, avionics and pilot interface.
This profile selects Black Square TBM 850 for MSFS 2020, MSFS 2024.
The powered-control profile provides its selected yoke centering. Spring resistance builds with the selected airspeed response. A separate aerodynamic term adds speed-dependent control load.
Trim changes aircraft balance; the selected profile determines the amount of hardware relief. Valid trim provides the configured pressure relief. Autopilot following is off.
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 selected TBM documentation distinguishes elevator anti-tabs from other trim tabs. Automatic-flight disengagement can leave flight-director modes displayed, so the flight director, autopilot and manual trim are separate cockpit states. TBM model and avionics generations remain named in the individual product.
The selected implementation
Black Square’s TBM 850 models elevator anti-tabs and separate trim tabs. Disconnecting the autopilot can leave flight-director modes selected.
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 strength74%
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: The powered-control profile provides its selected yoke centering. The baseline spring is 0.74. Its low-speed blend reaches baseline strength at 65 KIAS.
operating manualTBM 850 manualTBM 900: Daher Builds a Near-JetDaher’s TBM 930: MAX Upset ProtectionTBM 900 — AOPA Pilot, April 2014Spring deadband5%
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 load68%
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 0.68 with an indicated-speed reference of 190 KIAS. This supplies speed-dependent loading alongside the spring.
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 floor55%
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 start8 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.
Spring engagement full65 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.
フォース調整速度190
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.
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 65 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 load72%
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 0.72 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.
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: Trim changes aircraft balance; the selected profile determines the amount of hardware relief. Pitch authority 0.3 provides load relief and permitted centre movement; roll authority is 0.14.
operating manualTBM 850 manualTBM 900: Daher Builds a Near-JetDaher’s TBM 930: MAX Upset ProtectionTBM 900 — AOPA Pilot, April 2014Trim relief (aileron)14%
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 rumble42%
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 bumps32%
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
Stall buffet28%
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 buffet0%
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.
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.
Effect gains · Engine, mechanical & drag
Touchdown thump82%
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 rumble6%
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.
Stick feel
StickFeel · Trim feel enabledFalse
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.
Autopilot
Autopilot · Follow enabledFalse
Whether this feature is active in this profile.
この値の理由: Autopilot following is off; the configured spring and load retain the hardware feel.
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.
Aero
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 · 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 index2
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 · 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 · Gain0.12
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 | 0.74 | The powered-control profile provides its selected yoke centering. The baseline spring is 0.74. Its low-speed blend reaches baseline strength at 65 KIAS. |
| Spring deadband | 0.05 | Sets travel around the centre before the baseline spring resists. Smaller values engage it sooner. |
| Force gain | 0.68 | The aerodynamic-load gain is 0.68 with an indicated-speed reference of 190 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. |
| Dynamic-pressure blend | True | Allows baseline spring strength to rise with indicated airspeed where the control law permits it. |
| Minimum spring factor | 0.55 | Sets low-speed spring strength as a fraction of baseline when blending is enabled. One keeps full strength. |
| Spring wake-up speed | 8 kt | Sets the IAS where the low-speed spring blend starts rising. This is a feel threshold, not a flight limit. |
| Spring full-strength speed | 65 kt | Sets the IAS where the low-speed blend reaches baseline strength; high-speed stiffening also uses it. |
| フォース調整速度 | 190 kt | Sets the IAS reference for aerodynamic loading. It is an estimate, not published cruise TAS or a flight limit. |
| Airspeed spring stiffening | 0.15 | The high-speed spring-stiffening gain is 0.15. It strengthens the permitted spring response above 65 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 | 0.72 | Roll and pitch aerodynamic scales are 0.72 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. |
| StickFeel · Trim feel enabled | False | 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. |
| StickFeel · Elevator authority | 0.3 | Trim changes aircraft balance; the selected profile determines the amount of hardware relief. Pitch authority 0.3 provides load relief and permitted centre movement; roll authority is 0.14. |
| StickFeel · Aileron authority | 0.14 | 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. |
| Autopilot · Follow enabled | False | Autopilot following is off; the configured spring and load retain the hardware feel. |
| 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. |
| Aero · Enabled | True | Enables aerodynamic cues; each still needs nonzero strength and its simulator conditions. |
| Aero · Gain | 0.28 | 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 | Sets flap buffet at the configured position and speed gates. Flap movement texture is separate. |
| Aero · Max flap index | 2 | Sets the final flap index for detent normalization. UP plus three detents uses maximum index3. |
| Aero · Min flap index | 2 | Sets the first flap detent that admits buffet; this is a handle index, not degrees. |
| 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. |
| Aero · Amplitude | 0.5 | Sets triggered shaker strength; inactive while the shaker feature is disabled. |
| Ground · Enabled | True | Enables ground effects; each still needs its own strength and contact or motion telemetry. |
| Ground · Gain | 0.42 | Sets rolling texture strength, modified by speed, surface and undercarriage configuration. |
| Ground · Gain | 0.32 | Sets gear-bump texture during ground motion, separate from touchdown impact. |
| Ground · Gain | 0.82 | 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 | 0.06 | 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 | 0.12 | Sets texture from observed gear movement, separate from aerodynamic and touchdown effects. |
公開資料 20
- SOCATA TBMResearch background · Wikipedia revision 1363498428 · retrieved 2026-09-12
- operating manualTBM850 manual controls, autopilot and change log: trim animation correction
- TBM 850 manualDaher TBM family
- TBM 900: Daher Builds a Near-JetDaher TBM family
- Daher’s TBM 930: MAX Upset ProtectionDaher TBM family
- TBM 900 — AOPA Pilot, April 2014Daher TBM family
- Microsoft Flight Simulator aircraft manuals
- MSFS 2024 FAQ and edition aircraft inventory
- MSFS 2020 FAQ and edition aircraft inventory
- X-Plane aircraft and avionics manuals
- TBM 900 product
- Pilot Report: Daher’s New TBM 930A 2016 real-aircraft pilot report. Publisher access restrictions may apply.
- TBM 850Official developer / designated store catalogue · checked 2026-09-12
- TBM’s 930 joins the flockThomas A. Horne · June 2016 · Tarbes demonstration
- Moment of ZenJulie Boatman · November 2024 · 2024 TBM 960
- Power of one: TBM 940 flight testMichael Gerzanics · 15–21 October 2019 · pages 26–29
- ICAO Doc 8643 — aircraft type designatorsPublic search data retrieved 2026-09-14; authority update 2026-09-03
- Daher TBM 930 POH印刷物またはアーカイブ資料（公開リンクなし）
- EASA TCDS A.010印刷物またはアーカイブ資料（公開リンクなし）
- Daher published data印刷物またはアーカイブ資料（公開リンクなし）
コミュニティと訂正
実機経験からこのページに誤りがあると思ったら、ここで訂正してください。
パイロットによる訂正
この機体に乗っていますか?このページを訂正。
このページは引用文献に基づいていますが、実機での経験は引用に勝ります。 誤っている主張を引用し、実機が実際にどうかを教えてください。訂正は メンテナーが確認し、この調査の次の改訂に反映されます。
訂正の送信にはサインインしてください。パスワード不要、ワンタイムのメールリンクだけです。
サインイン
ハンガートーク
Daher TBM familyの操縦や調整についてのオープンな会話です(コミュニティフォーラム)。上の訂正はメンテナーに非公開で届きます。ハンガートークは公開です。
開始するにはサインインしてください。パスワード不要、ワンタイムのメールリンクだけです。
サインイン
コミュニティ
この機体のコミュニティプロファイル
この機体のコミュニティプロファイルはまだありません。
自分好みに調整しましたか? プロファイルを共有 するとここに表示されます。