NAMC YS-11航空自衛隊 · CC BY 4.0 · JASDF YS-11P 52-1152 in flight.

NAMC YS-11

Japan’s postwar regional turboprop, with Rolls-Royce Dart power and a career spanning passenger, freight and specialist government flying.
Airliner1 choix de profil

Connaître l'avion

NAMC developed the YS-11 as a pressurised, low-wing regional airliner with Rolls-Royce Dart turboprops. It brought Japan's postwar aircraft industry into the market connecting smaller cities as airlines moved from piston engines to turbine power.

Airlines used the YS-11 for passengers and freight. Military operators in Japan and Greece also employed the family in transport, surveillance and electronic-warfare roles.

Aircraft family

Propulsion
Twin Rolls-Royce Dart turboprops↗
Configuration
Pressurised low-wing regional airliner↗

En savoir plus sur cet aéronef sur AirframeDB

Learning to certify a new airliner

Former Civil Aviation Bureau inspector 藤原 洋 recalls that the YS-11 demanded a new level of certification work from Japan’s postwar civil aviation authorities. He worked on fundamental measurements such as airspeed-system errors, stall speeds and takeoff and landing distances. His account describes the team studying foreign test methods and adapting them to the equipment and experience available locally.

The prototype programme also led to substantial changes. He reports enlarged ailerons and increased wing dihedral after early handling problems, along with a revised rudder-tab arrangement. Later airline service exposed practical difficulties that development flying had missed, including moisture problems during Japan’s rainy season. The recollection connects the finished aircraft to the testing, modification and operating experience that shaped it.

Across the Atlantic in a newly acquired airliner

Zeglin remembers the YS-11 as part of a varied early airline career at Provincetown Boston Airline. She began with sightseeing flying in 1982 and subsequently worked as first officer on several commuter types, including the YS-11, before also becoming a captain on it. One unusually memorable assignment took her to Malta in May 1984, where PBA pilots collected four aircraft for the American fleet. On that journey she occupied the right seat of N219P.

Her recollection follows the delivery route through Italy, Switzerland, Britain and Scotland, then across Iceland and Greenland to Canada and down the eastern United States. They left Malta on 26 May and reached Miami on 31 May, with 33.4 flying hours recorded for the trip. Her photographs and correspondence preserve the people and stops behind an aircraft acquisition, including airliners still wearing the previous operator’s colours.

A steady instrument platform remembered from Piedmont

Writing on PPRuNe, TomConard recalls a short period in Piedmont’s YS-11 before moving to the Boeing 727. He is candid about the limits of his memory: his experience amounted to roughly 75 hours in the right seat, and he was looking back nearly three decades. What remained vivid was the contrast between modest hot-weather climb performance and an aircraft he particularly liked as a stable platform for instrument approaches.

He remembers frequent use of water-assisted takeoffs and says the crew’s cruising altitude depended strongly on temperature, loading and stage length. Once configured and settled on an ILS, however, he found the aircraft unusually steady. These are a former crew member’s impressions from one operator and period. His remembered performance figures and system explanations have not been adopted here as aircraft specifications.

Heavy controls and affection on the final flight

After the final flight of YS-11FC 52-1151, captain 渡邉 潤一 told Aviation Wire that the aircraft’s manual controls had made it demanding to master. He had flown the type for about eleven years and accumulated roughly 1,900 hours in it. Of the flight-inspection aircraft he knew, he remembered 151 as the heaviest on the controls; the other two were more straightforward. That challenge had strengthened his determination to fly it well and his attachment to the machine.

The connection reached back to childhood, when a visit to Chitose as a schoolboy gave him his first YS-11 ride and encouraged his ambition to become a pilot. Later service took him as far as Minamitorishima via Iwo Jima, a journey he remembered particularly clearly. At retirement he also credited the maintenance and support personnel whose work had kept the aircraft flying for more than half a century.

Sources publiques 7
  1. Local Legend 22: NAMC YS-11Release announcement · 25 September 2025
  2. YS-11 MSFS manual v1.0.7Manual v1.0.7 · 14 September 2025
  3. Half a century ago: certifying the YS-11藤原 洋, former Civil Aviation Bureau aircraft inspector · Aviation and Culture No.107, summer 2013; online 25 December 2013
  4. PBA YS-11 ferry flight from Malta to MiamiNancy Zeglin recollection, published by David P. Henderson · May 1984 ferry flight
  5. YS-11 data: TomConard’s Piedmont recollectionTomConard · 4 May 2006, post 3 · self-reported former Piedmont first officer
  6. The last Dart-powered YS-11FC flightTadayuki Yoshikawa reporting · captain 渡邉 潤一 interviewed after the 17 March 2021 final flight
  7. ICAO Doc 8643 — aircraft type designatorsPublic search data retrieved 2026-09-14; authority update 2026-09-03

Comment le profil le modélise

NAMC YS-11

Free + Pro
MSFS 2024MSFS 2020

NAMC developed the YS-11 as a pressurised, low-wing regional airliner with Rolls-Royce Dart turboprops. It brought Japan's postwar aircraft industry into the market connecting smaller cities as airlines moved from piston engines to turbine power.

This starting point selects NAMC YS-11. Its aircraft-level settings do not select a particular developer’s custom systems.

The profile supplies selected regional-transport resistance. Spring resistance builds with the selected airspeed response. A separate aerodynamic term adds speed-dependent control load.

Pitch relief is independent of cabin pressure and mission fit. Valid trim provides the configured pressure relief. Autopilot following is enabled for supported control references.

Controls and trim

The YS-11 brought Rolls-Royce Dart turboprops and a pressurized cabin to Japan’s post-war regional-airliner programme. Passenger, cargo and military variants carried the family into different operator roles.

YS-11 MSFS manual v1.0.7Local Legend 22: NAMC YS-11

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%

L'échelle globale finale appliquée à tout ce que produit le modèle, avant la limite du périphérique.

Plus : tout (ressort, charges, effets) se renforce ensemble.

Moins : tout s'adoucit ensemble.

Pourquoi ici : Scales overall profile strength while preserving effect balance, subject to device and output limits.

Forces

Spring strength74%

La force de rappel de base qui ramène le manche au neutre. Toutes les autres forces s'empilent dessus. Trop faible, le manche paraît mou en vol normal ; trop forte, elle lutte contre la main et masque les signaux plus fins.

Plus : un centrage plus ferme qui résiste davantage à la main.

Moins : un manche plus mou qui ne compte que sur la charge aérodynamique.

Pourquoi ici : The profile supplies selected regional-transport resistance. The baseline spring is 0.74. Its low-speed blend reaches baseline strength at 90 KIAS.

YS-11 MSFS manual v1.0.7Local Legend 22: NAMC YS-11
Spring deadband5%

Une petite zone neutre autour du centre où le ressort reste muet, pour que les micro-mouvements à l'arrêt ne vibrent pas. Plus large, c'est plus calme mais plus lâche ; plus étroite, plus précis mais parfois nerveux au neutre.

Plus : un centre plus calme mais plus lâche, avec plus de jeu.

Moins : un centre plus serré qui peut vibrer au repos.

Pourquoi ici : Sets travel around the centre before the baseline spring resists. Smaller values engage it sooner.

Overall aerodynamic load68%

Une échelle maîtresse sur les deux charges d'axe, appliquée avant leur équilibre individuel. Les profils la laissent en général en place et règlent les deux axes.

Plus : les deux axes chargent plus fort.

Moins : les deux axes s'allègent ensemble.

Pourquoi ici : 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

Active la fenêtre d'engagement basse vitesse du ressort (début/plein en nœuds ci-dessus). Désactivé, le ressort est constant à toute vitesse.

Pourquoi ici : Allows baseline spring strength to rise with indicated airspeed where the control law permits it.

Low-speed spring floor55%

La part du ressort qui survit à l'arrêt, avant que la vitesse ne crée la moindre force aérodynamique. Un plancher haut garde le manche ferme au parking ; un plancher bas donne le jeu de câbles d'un avion léger au parking.

Plus : un manche plus ferme au parking et au roulage.

Moins : un manche mou au parking qui ne s'éveille qu'avec la vitesse.

Pourquoi ici : Sets low-speed spring strength as a fraction of baseline when blending is enabled. One keeps full strength.

Spring engagement start20 kt

La vitesse à laquelle le ressort quitte son plancher basse vitesse vers la pleine raideur : le début du réveil des commandes au roulage de décollage.

Pourquoi ici : Sets the IAS where the low-speed spring blend starts rising. This is a feel threshold, not a flight limit.

Spring engagement full90 kt

La vitesse où le ressort atteint sa pleine raideur. Entre le début et ce point, le centrage se raffermit avec le vent relatif.

Pourquoi ici : Sets the IAS where the low-speed blend reaches baseline strength; high-speed stiffening also uses it.

Vitesse de réglage des forces190

La vitesse indiquée où la charge aérodynamique atteint son niveau de conception. Elle ancre toute la courbe au domaine réel : un 172 charge dès 110 nœuds, un jet bien plus tard.

Plus : les charges arrivent plus tard ; le manche reste léger jusqu'à plus vite.

Moins : les charges arrivent plus tôt et la croisière pèse davantage.

Pourquoi ici : Sets the IAS reference for aerodynamic loading. It is an estimate, not published cruise TAS or a flight limit.

Centre firmness vs speed10%

Combien le centrage lui-même se raidit avec la vitesse, en plus des charges de braquage. Zéro garde un centre constant ; plus fait centrer dur en croisière et souple en tour de piste.

Plus : un centre qui durcit nettement avec la vitesse.

Moins : une sensation de centre constante à toute vitesse.

Pourquoi ici : The high-speed spring-stiffening gain is 0.1. It strengthens the permitted spring response above 90 KIAS, with the squared-speed ratio capped at 5.

Centre stiffening cap5

La limite haute du raidissement lié à la vitesse, pour que le vol très rapide ne remonte pas le ressort sans borne.

Plus : plus de raidissement total permis à haute vitesse.

Moins : le raidissement se bride plus tôt.

Pourquoi ici : Limits the squared airspeed ratio used for high-speed spring stiffening; it is not a device-force cap.

Aileron load72%

La charge de roulis soutenue issue du braquage d'ailerons et de la vitesse, équilibrée indépendamment du tangage. Avec la charge de profondeur, elle fixe l'harmonie des commandes dont parlent les essais.

Plus : des efforts de roulis plus lourds.

Moins : des ailerons plus légers, plus vifs.

Pourquoi ici : 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%

La charge de tangage soutenue issue du braquage de profondeur et de la vitesse, équilibrée indépendamment du roulis. Le levier principal du poids en tangage d'un type. Il ne touche ni ailerons, ni ressort, ni trim, ni buffet.

Plus : des efforts de tangage soutenus plus lourds en vitesse.

Moins : une profondeur plus légère, moins musclée à tenir.

Pourquoi ici : Scales pitch aerodynamic loading; pitch spring travel and trim responses are separate settings.

Max output force55%

Un plafond par force stable de tangage ou roulis avant le périphérique : la garde contre le claquement ou la saturation du matériel en manœuvre forte.

Plus : des pics de force stable plus élevés avant écrêtage.

Moins : un plafond plus doux ; les manœuvres dures s'aplatissent plus tôt.

Pourquoi ici : Caps directed-force output. Native spring effects and device limits remain separate.

Trim

Trim relief (elevator)30%

Combien le trim de profondeur soulage l'effort tenu et déplace le point de repos du manche. À 100 %, un avion bien compensé ne demande aucune pression : le geste réel de compenser la charge.

Plus : le trim retire plus d'effort tenu ; à 100 %, plein trim l'annule.

Moins : vous continuez à tenir de l'effort même compensé.

Pourquoi ici : Pitch relief is independent of cabin pressure and mission fit. Pitch authority 0.3 provides load relief and permitted centre movement; roll authority is 0.14.

YS-11 MSFS manual v1.0.7Local Legend 22: NAMC YS-11
Trim relief (aileron)14%

Le même soulagement pour le trim de roulis. La plupart des avions légers n'ont pas de vrai trim d'ailerons, donc zéro ; les types qui en ont reçoivent une valeur adaptée.

Plus : le trim de roulis retire plus d'effort tenu.

Moins : le trim de roulis fait moins.

Pourquoi ici : Scales supported roll-trim relief and permitted centre movement. Zero removes roll response.

Effect gains · Ground

Runway rumble42%

Vibration de roulement issue de la vitesse des roues et du revêtement : la texture du bitume, de l'herbe ou du gravier sous le train.

Plus : une texture de surface plus forte dans le manche.

Moins : un roulage plus lisse.

Pourquoi ici : Sets rolling texture strength, modified by speed, surface and undercarriage configuration.

Gear bumps32%

Chocs courts et distincts des joints, ornières et surfaces rugueuses : la ponctuation au-dessus du grondement continu.

Plus : des chocs plus nets des joints et ornières.

Moins : des détails de sol plus doux.

Pourquoi ici : Sets gear-bump texture during ground motion, separate from touchdown impact.

Effect gains · Airframe

Stall buffet28%

Buffet de cellule à l'approche du décrochage et pendant l'avertisseur : la voix de cette aile quand elle est mécontente. Les types à décrochage franc reçoivent un buffet modéré, le klaxon porte l'alerte.

Plus : un tremblement pré-décrochage plus fort.

Moins : une aile plus discrète ; le klaxon porte l'alerte.

Pourquoi ici : Sets stall-buffet strength. Zero removes the cue without changing simulator stalls or warnings.

Mach buffet0%

Buffet transsonique près de la limite de Mach. Parlant pour les jets près de MMO, zéro pour pistons et turbopropulseurs qui n'y vont jamais.

Plus : un buffet transsonique plus fort près de la limite de Mach.

Moins : un vol plus lisse à haut Mach.

Pourquoi ici : Sets high-Mach buffet strength; onset and full-strength thresholds are separate.

Flap buffet14%

Vibration basse fréquence de cellule avec les volets dans le vent, dans la fenêtre où ils travaillent vraiment l'air.

Plus : un vol plus rugueux volets au travail.

Moins : des volets d'approche plus doux.

Pourquoi ici : Sets flap buffet at the configured position and speed gates. Flap movement texture is separate.

Gear buffet10%

Le tambourinement du train rentrant sorti dans le flux. Zéro pour les trains fixes, dont la cellule ne change jamais de forme.

Plus : plus de tambourinement train sorti.

Moins : un vol train sorti plus propre.

Pourquoi ici : Sets gear aerodynamic buffet; movement and ground-contact cues are separate.

Stick shaker50%

Le vibreur de manche dédié, déclenché par l'avertisseur de décrochage de l'avion. Seuls les types à vrai vibreur reçoivent une valeur ; les autres comptent sur buffet et klaxon.

Plus : un vibreur plus dur.

Moins : un vibreur plus discret.

Pourquoi ici : Sets triggered shaker strength; inactive while the shaker feature is disabled.

Effect gains · Engine, mechanical & drag

Touchdown thump82%

Le coup unique au toucher, proportionnel au taux de chute : un kiss se murmure, une arrivée ferme cogne.

Plus : un coup plus dur au toucher.

Moins : des arrivées plus douces.

Pourquoi ici : Sets landing-impact strength; landing telemetry and response shape determine the pulse.

Reverse rumble48%

Vibration de roulage sous inversion de poussée ou plage bêta. Zéro pour les types sans reverse.

Plus : un roulage plus rugueux sous reverse.

Moins : une reverse plus discrète.

Pourquoi ici : Sets reverse-thrust vibration with valid reverser and engine conditions. Zero removes the cue.

Engine rumble6%

Vibration continue du moteur suivant le régime du ralenti à la pleine puissance : le rappel permanent que quelque chose brûle du carburant devant.

Plus : plus de moteur dans le manche.

Moins : un moteur plus discret.

Pourquoi ici : Sets estimated engine vibration using configured telemetry and response, not measured cockpit vibration.

Flap motion12%

Vibration continue seulement pendant que le simulateur signale les volets réellement en mouvement. Elle suit la course réelle et les pannes, pas un minuteur estimé.

Plus : plus de vibration volets en mouvement.

Moins : des courses de volets plus discrètes.

Pourquoi ici : Sets texture from observed flap movement; a command without movement does not establish the cue.

Autopilot follow

AP follow authority10%

Jusqu'où les ordres du pilote automatique peuvent bouger le manche physique. Minuscule dans MSFS, où un axe déplacé peut être relu comme entrée pilote ; zéro coupe le suivi.

Plus : le pilote automatique bouge visiblement plus votre manche.

Moins : un suivi à peine perceptible.

Pourquoi ici : 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.

Pourquoi ici : 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.

Pourquoi ici : 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.

Pourquoi ici : 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.

Pourquoi ici : 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.

Pourquoi ici : Enables rate damping with the configured coefficients and control law.

Autopilot

Autopilot · Follow enabledTrue

Whether this feature is active in this profile.

Pourquoi ici : 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.

Pourquoi ici : Permits centering hold during a supported AP state, separate from following a moving target.

Autopilot · Neutral hold strength0.6

Pourquoi ici : Sets admitted AP neutral-hold strength; inactive while neutral hold is disabled.

Aero

Aero · EnabledTrue

Whether this feature is active in this profile.

Pourquoi ici : Enables aerodynamic cues; each still needs nonzero strength and its simulator conditions.

Aero · Max flap index4

Where this effect reaches full strength (or has fully faded, for washouts).

Plus : a more gradual build to a later peak.

Moins : a quicker build.

Pourquoi ici : 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.

Plus : the effect begins later.

Moins : it begins earlier.

Pourquoi ici : 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.

Pourquoi ici : Permits shaker at supported warning conditions; the switch does not establish aircraft equipment.

Ground

Ground · EnabledTrue

Whether this feature is active in this profile.

Pourquoi ici : 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.

Pourquoi ici : Enables engine cues with nonzero settings and valid running-engine telemetry.

Mechanical

Mechanical · EnabledTrue

Whether this feature is active in this profile.

Pourquoi ici : Enables accessory cues with configured strengths and observed accessory movement.

Mechanical · Gain0.12

The strength of this effect.

Plus : a stronger effect.

Moins : a weaker one.

Pourquoi ici : Sets texture from observed gear movement, separate from aerodynamic and touchdown effects.

Tous les réglages du profil
Réglages estimés du profil
ParamètreValeurCe que cela contrôle et pourquoi
Spring strength0.74 The profile supplies selected regional-transport resistance. The baseline spring is 0.74. Its low-speed blend reaches baseline strength at 90 KIAS.
Spring deadband0.05 Sets travel around the centre before the baseline spring resists. Smaller values engage it sooner.
Force gain0.68 The aerodynamic-load gain is 0.68 with an indicated-speed reference of 190 KIAS. This supplies speed-dependent loading alongside the spring.
Master gain0.85 Scales overall profile strength while preserving effect balance, subject to device and output limits.
Dynamic-pressure blendTrue Allows baseline spring strength to rise with indicated airspeed where the control law permits it.
Minimum spring factor0.55 Sets low-speed spring strength as a fraction of baseline when blending is enabled. One keeps full strength.
Spring wake-up speed20 ktSets the IAS where the low-speed spring blend starts rising. This is a feel threshold, not a flight limit.
Spring full-strength speed90 ktSets the IAS where the low-speed blend reaches baseline strength; high-speed stiffening also uses it.
Vitesse de réglage des forces190.0 ktSets the IAS reference for aerodynamic loading. It is an estimate, not published cruise TAS or a flight limit.
Airspeed spring stiffening0.1 The high-speed spring-stiffening gain is 0.1. It strengthens the permitted spring response above 90 KIAS, with the squared-speed ratio capped at 5.
Airspeed stiffening cap5 Limits the squared airspeed ratio used for high-speed spring stiffening; it is not a device-force cap.
Aileron force scale0.72 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 scale1.0 Scales pitch aerodynamic loading; pitch spring travel and trim responses are separate settings.
Maximum output force0.55 Caps directed-force output. Native spring effects and device limits remain separate.
StickFeel · Trim feel enabledTrue Retained for compatibility and group membership. Trim relief, rather than this flag, controls centre movement.
StickFeel · Trim relief enabledTrue Allows trim relief with supported control law and valid telemetry. Axis authorities set its amount.
StickFeel · Elevator authority0.3 Pitch relief is independent of cabin pressure and mission fit. Pitch authority 0.3 provides load relief and permitted centre movement; roll authority is 0.14.
StickFeel · Aileron authority0.14 Scales supported roll-trim relief and permitted centre movement. Zero removes roll response.
StickFeel · Force trim enabledFalse Enables local force trim, separate from aircraft-owned trim and add-on integration qualification.
StickFeel · G load enabledTrue Allows load-factor changes to modify permitted spring laws. Passive fly-by-wire feel can suppress it.
StickFeel · Rate damping enabledTrue Enables rate damping with the configured coefficients and control law.
Autopilot · Follow enabledTrue Following is on at 0.1 authority when a supported, valid autopilot control reference is available.
Autopilot · Follow authority0.1 Sets admitted AP-follow gain, not a percentage of travel. Runtime ownership and input limits still apply.
Autopilot · Neutral hold enabledFalse Permits centering hold during a supported AP state, separate from following a moving target.
Autopilot · Neutral hold strength0.6 Sets admitted AP neutral-hold strength; inactive while neutral hold is disabled.
Aero · EnabledTrue Enables aerodynamic cues; each still needs nonzero strength and its simulator conditions.
Aero · Gain0.28 Sets stall-buffet strength. Zero removes the cue without changing simulator stalls or warnings.
Aero · Gain0 Sets high-Mach buffet strength; onset and full-strength thresholds are separate.
Aero · Gain0.14 Sets flap buffet at the configured position and speed gates. Flap movement texture is separate.
Aero · Max flap index4 Sets the final flap index for detent normalization. UP plus three detents uses maximum index3.
Aero · Min flap index2 Sets the first flap detent that admits buffet; this is a handle index, not degrees.
Aero · Gain0.1 Sets gear aerodynamic buffet; movement and ground-contact cues are separate.
Aero · Shaker enabledFalse Permits shaker at supported warning conditions; the switch does not establish aircraft equipment.
Aero · Amplitude0.5 Sets triggered shaker strength; inactive while the shaker feature is disabled.
Ground · EnabledTrue Enables ground effects; each still needs its own strength and contact or motion telemetry.
Ground · Gain0.42 Sets rolling texture strength, modified by speed, surface and undercarriage configuration.
Ground · Gain0.32 Sets gear-bump texture during ground motion, separate from touchdown impact.
Ground · Gain0.82 Sets landing-impact strength; landing telemetry and response shape determine the pulse.
Ground · Gain0.48 Sets reverse-thrust vibration with valid reverser and engine conditions. Zero removes the cue.
Engine · EnabledTrue Enables engine cues with nonzero settings and valid running-engine telemetry.
Engine · Gain0.06 Sets estimated engine vibration using configured telemetry and response, not measured cockpit vibration.
Mechanical · EnabledTrue Enables accessory cues with configured strengths and observed accessory movement.
Mechanical · Gain0.12 Sets texture from observed flap movement; a command without movement does not establish the cue.
Mechanical · Gain0.12 Sets texture from observed gear movement, separate from aerodynamic and touchdown effects.
Sources publiques 7
  1. Local Legend 22: NAMC YS-11Release announcement · 25 September 2025
  2. YS-11 MSFS manual v1.0.7Manual v1.0.7 · 14 September 2025
  3. Half a century ago: certifying the YS-11藤原 洋, former Civil Aviation Bureau aircraft inspector · Aviation and Culture No.107, summer 2013; online 25 December 2013
  4. PBA YS-11 ferry flight from Malta to MiamiNancy Zeglin recollection, published by David P. Henderson · May 1984 ferry flight
  5. YS-11 data: TomConard’s Piedmont recollectionTomConard · 4 May 2006, post 3 · self-reported former Piedmont first officer
  6. The last Dart-powered YS-11FC flightTadayuki Yoshikawa reporting · captain 渡邉 潤一 interviewed after the 17 March 2021 final flight
  7. ICAO Doc 8643 — aircraft type designatorsPublic search data retrieved 2026-09-14; authority update 2026-09-03

Communauté et corrections

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