Development milestones
First flight: 14 July 1988
Developed from: Mooney 301
机型库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配置文件选项：5 个
了解飞机
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.
公开来源 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纸质或存档参考资料；无公开链接
- EASA TCDS A.010纸质或存档参考资料；无公开链接
- Daher published data纸质或存档参考资料；无公开链接
配置文件如何建模
Daher TBM 930
Free + ProMSFS 2024MSFS 2020X-Plane 11
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 factory starting point selects Daher TBM 930 across MSFS 2024, MSFS 2020, X-Plane 11.
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 enabled for supported control references.
此确切修订版尚未开放公开安装。
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.
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 strength86%
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: The powered-control profile provides its selected yoke centering. The baseline spring is 0.86. Its low-speed blend reaches baseline strength at 90 KIAS.
operating manualTBM 850 manualTBM 900: Daher Builds a Near-JetDaher’s TBM 930: MAX Upset ProtectionTBM 900 — AOPA Pilot, April 2014Spring 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 205 KIAS. This supplies speed-dependent loading alongside the spring.
Spring engagement full90 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 speed12%
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 0.12. It strengthens the permitted spring response above 90 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 force60%
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 floor55%
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 start20 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205
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: 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 0.12.
operating manualTBM 850 manualTBM 900: Daher Builds a Near-JetDaher’s TBM 930: MAX Upset ProtectionTBM 900 — AOPA Pilot, April 2014Trim relief (aileron)12%
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 rumble36%
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 bumps26%
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 shaker70%
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 buffet30%
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 buffet20%
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 buffet32%
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 buffet22%
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 thump72%
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 rumble36%
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 rumble14%
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 motion16%
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 enabledTrue
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 · Gain0.18
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 | 0.86 | The powered-control profile provides its selected yoke centering. The baseline spring is 0.86. Its low-speed blend reaches baseline strength at 90 KIAS. |
| Spring deadband | 0.045 | 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 205 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 | 90 kt | Sets the IAS where the low-speed blend reaches baseline strength; high-speed stiffening also uses it. |
| Airspeed spring stiffening | 0.12 | The high-speed spring-stiffening gain is 0.12. It strengthens the permitted spring response above 90 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 | 0.6 | 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 | 0.7 | 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 | 0.55 | Sets low-speed spring strength as a fraction of baseline when blending is enabled. One keeps full strength. |
| Spring wake-up speed | 20 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 | 205 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 | 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 0.12. |
| StickFeel · Aileron authority | 0.12 | 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 | 0.3 | Sets stall-buffet strength. Zero removes the cue without changing simulator stalls or warnings. |
| Aero · Gain | 0.2 | Sets high-Mach buffet strength; onset and full-strength thresholds are separate. |
| Aero · Gain | 0.32 | Sets flap buffet at the configured position and speed gates. Flap movement texture is separate. |
| Aero · Gain | 0.22 | Sets gear aerodynamic buffet; movement and ground-contact cues are separate. |
| Aero · Shaker enabled | True | 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 | 0.36 | Sets rolling texture strength, modified by speed, surface and undercarriage configuration. |
| Ground · Gain | 0.26 | Sets gear-bump texture during ground motion, separate from touchdown impact. |
| Ground · Gain | 0.72 | Sets landing-impact strength; landing telemetry and response shape determine the pulse. |
| Ground · Gain | 0.36 | 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 | 0.14 | 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 | 0.16 | Sets texture from observed flap movement; a command without movement does not establish the cue. |
| Mechanical · Gain | 0.18 | Sets texture from observed gear movement, separate from aerodynamic and touchdown effects. |
公开来源 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纸质或存档参考资料；无公开链接
- EASA TCDS A.010纸质或存档参考资料；无公开链接
- Daher published data纸质或存档参考资料；无公开链接
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