Development milestones
First flight: May 24, 1956
機型庫Piper Comanche
Alan Radecki Akradecki · CC BY-SA 4.0 · Piper PA-24 Comanche picturedPiper Comanche
Piper's retractable-gear, all-metal touring single, developed through several engine and seating versions.
General aviation設定檔選項：2 個
瞭解飛機
Piper's Comanche first flew in 1956 with an all-metal low-wing airframe, enclosed cabin and retractable tricycle gear. Later versions changed engine power and seating, alongside the separate Twin Comanche line.
Production ended after the 1972 flood at Piper's Lock Haven plant. A2A models a particular Comanche with persistent engine and airframe condition; its manual describes the loading, maintenance and mechanical systems included in the simulation.
Piper PA-24 Comanche · Specifications (PA-24-260C) · real aircraft; source units retained
- Length
- 25 ft 0 in (7.62 m)↗
- Wingspan
- 36 ft 0 in (10.97 m)↗
- Height
- 7 ft 6 in (2.29 m)↗
- Wing area
- 178 sq ft (16.5 m² )↗
- Empty weight
- 1,773 lb (804 kg)↗
- Max takeoff weight
- 3,200 lb (1,451 kg)↗
- Powerplant
- 1 × Lycoming IO-540 air-cooled six-cylinder horizontally-opposed engine, 260 hp (190 kW)↗
- Propellers
- 2-bladed Hartzell HC82XK1D metal constant-speed propeller , 6 ft 5 in (1.96 m) diameter↗
- Maximum speed
- 195 mph (314 km/h, 169 kn) at sea level↗
- Cruise speed
- 185 mph (298 km/h, 161 kn) at 6,300 ft (1,900 m) (max. cruise, 75% power)↗
A moving tailplane and hand-operated flaps
The Comanche 250’s pitch control uses a stabilator: the horizontal tail moves as a unit instead of carrying a separate hinged elevator. Its anti-servo tab also provides longitudinal trim. A2A’s aircraft description pairs that arrangement with manually operated flaps and conventional yoke-and-pedal controls. This combination gives the cockpit several distinct mechanical controls, even before the separate engine and propeller levers are considered.
Landing gear connected by cables and a gear train
An electric motor and reduction mechanism beneath the floor move the three landing-gear units through push-pull cables. The nosewheel steering disconnects as the gear retracts, reducing the steering mechanism’s contribution to airborne rudder-pedal loads. The manual also describes a ground anti-retraction switch and separate indications for gear position. The selector operates the documented electrical and mechanical landing-gear system.
Documented detail
The list supplies trim-required lights and AP controls, and identifies the elevator trim handle with a standard SimVar requested in percent.
A restored 250 on a short grass runway
Unwin flew Mark Bonsall's refurbished 1963 Comanche 250 from Netherthorpe with instructor Nick Riddin. This particular aircraft had fuel injection and a three-blade propeller, so it was not an untouched factory example. With two aboard and partial fuel, it accelerated briskly from the grass strip. Unwin liked the harmonisation of the primary controls and their low initial resistance, although he found the older instrument and engine-control layout less intuitive than a modern cockpit. In airwork, his stalls gave clear warning and little inclination to drop a wing.
The landing and photo flights exposed different demands. He could feel the aircraft entering ground effect and thought excess approach speed would produce a long float; careful speed control rewarded him with successive satisfactory landings. Flying close formation for the photographer required more work, partly because the view from his chosen seat was restrictive. His overall appreciation was for a capable touring aircraft, with handling observations tied to the loading and modifications of the example he actually flew.
Why an experienced owner kept his 1958 Comanche
Wall's attachment to the Comanche began with a flying-club comparison in 1958. Interviewed by Bill Cox, he recalled flying a loaded Comanche 250 and a contemporary Bonanza between Burbank and Phoenix. He considered the Comanche the stronger performer in that particular comparison, while acknowledging the appeal of the Beechcraft's handling. Decades later, after a professional flying career, that experience helped draw him back to a 1958 Comanche of his own.
By the 2005 article, Wall had accumulated more than a thousand hours in the type and restored his aircraft extensively. He distinguished brochure claims from his experience: the advertised climb figure seemed optimistic to him, while maximum cruise was closer to what he observed. His usual choice was an economical high-altitude cruise rather than maximum speed. As an owner and mechanic, he also valued access for maintenance and familiarity with the systems he had rebuilt. These are the preferences and reported results of one experienced owner, rather than a controlled comparison of all Comanches and Bonanzas.
An unannounced Comanche with considerably more power
Looking back on his test-flying years, Kershner remembered the Comanche 400 as one of the aircraft that stood out. He identified the two final test aircraft and explained Pug Piper's interest in obtaining high-altitude performance without turbocharging. The extra power gave him an impression reminiscent of a fighter, but he also recalled substantial fuel consumption and troublesome hot starts during the flight-test period. His account concerns the eight-cylinder 400, a different proposition from the familiar 180 and 250.
One flight supplied the story's human detail. Over Lock Haven, he overtook a conventional Comanche and made further passes that prompted its pilot to ask what version he was flying. Kershner gave an evasive answer over the radio, then returned to a reprimand for drawing attention to an aircraft Piper had not yet announced. He also remembered watching the fuel indication move towards empty.
The owner whose Comanche became the simulation
In the manual's developer notes, Gentile explains why A2A chose his own Comanche 250, N6229P, for its new Accu-Sim system. He had owned and operated the aeroplane for more than a decade. That familiarity gave the team continuing access to an aircraft they could examine and fly while investigating questions raised during development. His account describes the connection between an owner's long experience and the choice of a simulation subject.
Gentile's affection is equally explicit. He values the Comanche's combination of speed, load-carrying ability, cabin room and manageable handling, and says the aircraft has become part of the family. The appeal began with its appearance and deepened over years of operation. This is an enthusiastic owner's introduction, written by the developer selling the simulation, rather than an independent comparison flight.
公開來源 10
- Piper PA-24 ComancheResearch background · Wikipedia revision 1371634258 · retrieved 2026-09-12
- Comanche Pilot Manual
- Comanche variables list
- Microsoft Flight Simulator aircraft manuals
- Accu-Sim Comanche · native MSFS 2024Official developer / designated store catalogue · checked 2026-09-12
- Accu-Sim Comanche · MSFS 2020Official developer / designated store catalogue · checked 2026-09-12
- Flight Test: Piper’s Classic Cruiser – The ComancheDave Unwin · 30 March 2017. Modified PA-24-250 N61970, Netherthorpe, United Kingdom.
- Piper’s First Retractable SingleRobert Wall, interviewed by Bill Cox · 1 March 2005. Owner account of a 1958 Comanche 250, including a recalled 1958 comparison.
- Practice Area: Inimitable Airplanes, within New PilotWilliam K. Kershner · May 1997. Retrospective by Piper test pilot William K. Kershner; PA-24-400 subsection.
- ICAO Doc 8643 — aircraft type designatorsPublic search data retrieved 2026-09-14; authority update 2026-09-03
設定檔如何建模
A2A Comanche 250
Free + ProMSFS 2020MSFS 2024A2A
Piper's Comanche first flew in 1956 with an all-metal low-wing airframe, enclosed cabin and retractable tricycle gear. Later versions changed engine power and seating, alongside the separate Twin Comanche line.
This profile selects A2A Comanche 250 for MSFS 2020, MSFS 2024.
The stabilator/anti-servo arrangement motivates reversible yoke loading. Spring resistance builds with the selected airspeed response. A separate aerodynamic term adds speed-dependent control load.
The anti-servo tab supplies pitch relief; ALT-mode trim lamps request manual action. Valid trim provides the configured pressure relief. Autopilot following is enabled for supported control references.
此確切修訂版尚未開放公開安裝。
Controls and trim
The Comanche’s manually controlled stabilator uses an anti-servo tab for longitudinal trim. A2A’s S-TEC30 altitude hold has an elevator servo and lamps requesting pilot trim, without automatic pitch trim. Native 2024 GPSS supplies lateral steering as a separate addition.
The selected implementation
A2A’s native 2024 Comanche removes the earlier Elevator Force tablet input option and adds ST901 GPSS lateral guidance; S-TEC30 ALT still requests manual trimming.
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%
施加於模型產出的一切、在裝置上限之前的最終整體輸出縮放。
調高: 一切(彈簧、載荷、效果)一同增強。
調低: 一切一同變柔。
設定理由: Scales overall profile strength while preserving effect balance, subject to device and output limits.
Forces
Spring strength74%
把搖桿拉回中央的基礎回中力。其他所有力都疊加在它之上。太低,正常飛行中搖桿會發軟;太高,它會與你的手較勁,並掩蓋疊加其上的細微提示。
調高: 更硬的回中,更抗手。
調低: 更軟的桿,只靠氣動載荷。
設定理由: The stabilator/anti-servo arrangement motivates reversible yoke loading. The baseline spring is 0.74. Its low-speed blend reaches baseline strength at 75 KIAS.
Comanche Pilot ManualComanche variables listExact product and documentation researchNative ComancheSpring deadband4%
中央附近彈簧保持安靜的小中立區,讓靜止時的微小移動不會咔嗒作響。更寬更安穩但更松,更窄更精確但可能在中央附近抖動。
調高: 更安靜但更松的中央,曠量更大。
調低: 更緊的中央,靜止時可能抖動。
設定理由: Sets travel around the centre before the baseline spring resists. Smaller values engage it sooner.
Overall aerodynamic load80%
作用於兩條持續軸載荷的主縮放,在它們各自的獨立平衡之前施加。設定檔通常不動它,而是調校兩條軸載荷。
調高: 兩軸載荷一同加重。
調低: 兩軸一同減輕。
設定理由: The aerodynamic-load gain is 0.8 with an indicated-speed reference of 150 KIAS. This supplies speed-dependent loading alongside the spring.
Airspeed blendingTrue
啟用低速彈簧介入視窗(上面的起始/全強度節數)。關閉時彈簧在所有速度下恆定。
設定理由: Allows baseline spring strength to rise with indicated airspeed where the control law permits it.
Low-speed spring floor50%
在靜止、空速尚未產生氣動力之前,彈簧還剩多少。下限高,停機時搖桿結實;下限低,則是停放輕型飛機那種鋼索鬆弛的感覺。
調高: 停機和滑行時桿更結實。
調低: 停機時桿發軟,只隨速度甦醒。
設定理由: Sets low-speed spring strength as a fraction of baseline when blending is enabled. One keeps full strength.
Spring engagement start20 kt
彈簧從低速下限開始向全強度攀升的空速:起飛滑跑中操縱面"甦醒"的那一刻。
設定理由: Sets the IAS where the low-speed spring blend starts rising. This is a feel threshold, not a flight limit.
Spring engagement full75.0 kt
彈簧達到全強度的空速。從起點到這裡,隨著氣流在操縱面上增強,回中逐漸變硬。
設定理由: Sets the IAS where the low-speed blend reaches baseline strength; high-speed stiffening also uses it.
力回饋調校速度150
氣動載荷達到設計滿值的指示空速。它把整條載荷曲線錨定在飛機真實的速度範圍:172在110節就載滿,噴氣機要晚得多。
調高: 載荷來得更晚;桿輕到更高速度。
調低: 載荷來得更早,巡航更沉。
設定理由: Sets the IAS reference for aerodynamic loading. It is an estimate, not published cruise TAS or a flight limit.
Centre firmness vs speed15%
在偏轉載荷之外,回中本身隨速度變硬的程度。零則中央手感恆定;越大,巡航時回中越硬,起落航線上越松。
調高: 中央隨速度明顯變硬。
調低: 任何速度下中央手感恆定。
設定理由: The high-speed spring-stiffening gain is 0.15. It strengthens the permitted spring response above 75 KIAS, with the squared-speed ratio capped at 5.
Centre stiffening cap5
速度驅動的中央變硬上限,防止高速飛行把彈簧無限上緊。
調高: 高速允許更多總硬化。
調低: 硬化更早封頂。
設定理由: Limits the squared airspeed ratio used for high-speed spring stiffening; it is not a device-force cap.
Aileron load72%
由副翼偏轉和空速產生的持續橫滾載荷,獨立於俯仰調校。與升降舵載荷一起,決定評測中常說的操縱協調比。
調高: 橫滾力更重。
調低: 副翼更輕更靈。
設定理由: 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%
由升降舵偏轉和空速產生的持續俯仰載荷,獨立於橫滾調校。這是決定機型俯仰重量的主槓桿。它不影響副翼、彈簧、配平或抖振力。
調高: 速度下持續俯仰力更重。
調低: 升降舵更輕,握持更省力。
設定理由: Scales pitch aerodynamic loading; pitch spring travel and trim responses are separate settings.
Max output force55%
每個穩態俯仰或橫滾力到達裝置前的上限,防止猛烈機動中砸擊或飽和硬體。
調高: 削波前更高的穩態力峰值。
調低: 更柔的上限;猛烈機動更早被抹平。
設定理由: Caps directed-force output. Native spring effects and device limits remain separate.
Trim
Trim relief (elevator)30%
升降舵配平緩解持續俯仰力、移動桿的安定位置的強度。在100 %時,配平得當的飛機不需要保持壓力——正是真實飛行中"用配平消掉載荷"的流程。
調高: 配平消掉更多持續力;100 %時滿配平可完全抵消。
調低: 即使配平也仍要持續用力。
設定理由: The anti-servo tab supplies pitch relief; ALT-mode trim lamps request manual action. Pitch authority 0.3 provides load relief and permitted centre movement; roll authority is 0.
Comanche Pilot ManualComanche variables listExact product and documentation researchNative ComancheTrim relief (aileron)0%
橫滾配平的同類緩解。多數通航機型沒有真正的副翼配平,所以保持為零;有橫滾配平的機型獲得相應的值。
調高: 橫滾配平消掉更多持續力。
調低: 橫滾配平作用更小。
設定理由: Scales supported roll-trim relief and permitted centre movement. Zero removes roll response.
Effect gains · Ground
Runway rumble40%
由輪速和地面型別(鋪裝、草地、礫石)產生的滾動振動。
調高: 桿上更強的地面質感。
調低: 更平滑的滑行。
設定理由: Sets rolling texture strength, modified by speed, surface and undercarriage configuration.
Gear bumps25%
來自伸縮縫、車轍和粗糙地面的短促離散顛簸,為持續隆隆聲打上標點。
調高: 接縫與車轍的衝擊更清晰。
調低: 更柔的地面細節。
設定理由: Sets gear-bump texture during ground motion, separate from touchdown impact.
Effect gains · Airframe
Stall buffet35%
接近失速及失速警告響起時的機體抖動:這副機翼宣告不滿的音量。斷失乾脆的機型抖振收斂,讓喇叭承擔警告。
調高: 更強的失速前顫抖。
調低: 更含蓄的機翼;警告交給喇叭。
設定理由: Sets stall-buffet strength. Zero removes the cue without changing simulator stalls or warnings.
Mach buffet0%
接近馬赫極限的跨音速抖振。對接近MMO的噴氣機有意義,對到不了那裡的活塞機和渦槳機為零。
調高: 接近馬赫極限時更強的跨音速抖振。
調低: 高馬赫下更平滑的飛行。
設定理由: Sets high-Mach buffet strength; onset and full-strength thresholds are separate.
Flap buffet14%
襟翼伸入氣流後機體的低頻振動,發生在它們真正做功的速度視窗內。
調高: 襟翼做功時更粗糙的飛行。
調低: 更柔的進近襟翼。
設定理由: Sets flap buffet at the configured position and speed gates. Flap movement texture is separate.
Gear buffet10%
可收放起落架懸在氣流中引起的機體鼓振。固定起落架機型為零,它們的機體外形從不改變。
調高: 放起落架時更多鼓振。
調低: 放起落架飛行更乾淨。
設定理由: Sets gear aerodynamic buffet; movement and ground-contact cues are separate.
Stick shaker50%
由飛機自身失速警告系統觸發的專用抖桿器振動。只有真有抖桿器的機型才有值;其餘全靠氣動抖振和喇叭。
調高: 更硬的抖桿器。
調低: 更含蓄的抖桿器。
設定理由: Sets triggered shaker strength; inactive while the shaker feature is disabled.
Effect gains · Engine, mechanical & drag
Touchdown thump65%
機輪觸及跑道那一下的單次衝擊,按下沉率縮放:輕柔著陸是耳語,結實到達是一記悶響。
調高: 觸地時更硬的一擊。
調低: 更柔的到達。
設定理由: Sets landing-impact strength; landing telemetry and response shape determine the pulse.
Reverse rumble0%
反推或槳葉beta區工作時的滑跑振動。無反推機型為零。
調高: 反推下更粗糙的滑跑。
調低: 更含蓄的反推。
設定理由: Sets reverse-thrust vibration with valid reverser and engine conditions. Zero removes the cue.
Engine rumble12%
從慢車到全功率跟隨轉速的持續動力裝置振動——前方有東西在燒油的永恆提醒。
調高: 桿裡更多引擎。
調低: 更含蓄的引擎。
設定理由: Sets estimated engine vibration using configured telemetry and response, not measured cockpit vibration.
Flap motion12%
僅在模擬器報告襟翼舵面確實移動時的持續振動。它跟隨真實作動器的運動和故障,而非估算的計時器。
調高: 襟翼移動中更多振動。
調低: 更含蓄的襟翼行程。
設定理由: Sets texture from observed flap movement; a command without movement does not establish the cue.
Autopilot follow
AP follow authority100%
自動駕駛指令可以讓桿實際移動多遠。在MSFS中保持極小,因為移動的軸可能被讀回為飛行員輸入;零則完全停用跟隨。
調高: 自動駕駛讓你的桿移動得明顯更多。
調低: 幾乎察覺不到的跟隨。
設定理由: Sets admitted AP-follow gain, not a percentage of travel. Runtime ownership and input limits still apply.
Stick feel
StickFeel · Trim feel enabledTrue
Whether this feature is active in this profile.
設定理由: 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.
設定理由: 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.
設定理由: 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.
設定理由: 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.
設定理由: Enables rate damping with the configured coefficients and control law.
Autopilot
Autopilot · Follow enabledTrue
Whether this feature is active in this profile.
設定理由: Following is on at 1 authority when a supported, valid autopilot control reference is available.
Autopilot · Neutral hold enabledFalse
Whether this feature is active in this profile.
設定理由: Permits centering hold during a supported AP state, separate from following a moving target.
Autopilot · Neutral hold strength0.6
設定理由: Sets admitted AP neutral-hold strength; inactive while neutral hold is disabled.
Aero
Aero · EnabledTrue
Whether this feature is active in this profile.
設定理由: Enables aerodynamic cues; each still needs nonzero strength and its simulator conditions.
Aero · Max flap index3
Where this effect reaches full strength (or has fully faded, for washouts).
調高: a more gradual build to a later peak.
調低: a quicker build.
設定理由: 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.
調高: the effect begins later.
調低: it begins earlier.
設定理由: 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.
設定理由: Permits shaker at supported warning conditions; the switch does not establish aircraft equipment.
Ground
Ground · EnabledTrue
Whether this feature is active in this profile.
設定理由: 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.
設定理由: Enables engine cues with nonzero settings and valid running-engine telemetry.
Mechanical
Mechanical · EnabledTrue
Whether this feature is active in this profile.
設定理由: Enables accessory cues with configured strengths and observed accessory movement.
Mechanical · Gain0.12
The strength of this effect.
調高: a stronger effect.
調低: a weaker one.
設定理由: Sets texture from observed gear movement, separate from aerodynamic and touchdown effects.
全部設定檔設定
| 引數 | 數值 | 控制作用及原因 |
|---|---|---|
| Spring strength | 0.74 | The stabilator/anti-servo arrangement motivates reversible yoke loading. The baseline spring is 0.74. Its low-speed blend reaches baseline strength at 75 KIAS. |
| Spring deadband | 0.045 | Sets travel around the centre before the baseline spring resists. Smaller values engage it sooner. |
| Force gain | 0.8 | The aerodynamic-load gain is 0.8 with an indicated-speed reference of 150 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 | 0.5 | 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. |
| Spring full-strength speed | 75.0 kt | Sets the IAS where the low-speed blend reaches baseline strength; high-speed stiffening also uses it. |
| 力回饋調校速度 | 150.0 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 75 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 | 1.0 | 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 | 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. |
| StickFeel · Elevator authority | 0.3 | The anti-servo tab supplies pitch relief; ALT-mode trim lamps request manual action. 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. |
| Autopilot · Follow enabled | True | Following is on at 1 authority when a supported, valid autopilot control reference is available. |
| Autopilot · Follow authority | 1.0 | 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 | 0.35 | 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 | 0.14 | Sets flap buffet at the configured position and speed gates. Flap movement texture is separate. |
| Aero · Max flap index | 3 | 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 | 0.1 | 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 | 0.4 | 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 | 0.12 | 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. |
公開來源 11
- Piper PA-24 ComancheResearch background · Wikipedia revision 1371634258 · retrieved 2026-09-12
- Comanche Pilot ManualComanche Pilot Manual PDF pp.24, 27-29 and 49
- Comanche variables listVariables list p.8, trim and autopilot indicators
- Exact product and documentation researchNative2024 addendum PDF pp.5 and 17-20
- Native ComancheNative2024 product introduction and upgrade explanationOfficial developer / designated store catalogue · checked 2026-09-12
- Microsoft Flight Simulator aircraft manuals
- Accu-Sim Comanche · MSFS 2020Official developer / designated store catalogue · checked 2026-09-12
- Flight Test: Piper’s Classic Cruiser – The ComancheDave Unwin · 30 March 2017. Modified PA-24-250 N61970, Netherthorpe, United Kingdom.
- Piper’s First Retractable SingleRobert Wall, interviewed by Bill Cox · 1 March 2005. Owner account of a 1958 Comanche 250, including a recalled 1958 comparison.
- Practice Area: Inimitable Airplanes, within New PilotWilliam K. Kershner · May 1997. Retrospective by Piper test pilot William K. Kershner; PA-24-400 subsection.
- ICAO Doc 8643 — aircraft type designatorsPublic search data retrieved 2026-09-14; authority update 2026-09-03
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