Development milestones
First flight: June 12, 1994 ( 1994-06-12 )
機体ライブラリBoeing 777
Aero Icarus from Zürich, Switzerland · CC BY-SA 2.0 · Cathay Pacific Boeing 777-200Boeing 777
A large long-haul twin that introduced Boeing's first commercial fly-by-wire airliner flight controls.
Airlinerプロファイル候補：13
機体を知る
The 777 entered service in 1995 after development with input from major airline customers. Its broad cabin and two very large engines filled a space between the 767 and 747. The programme expanded through different fuselage lengths, range developments and engine choices.
The 777-200ER offers several engine options, while the 777-300ER has its own airframe and equipment. PMDG and FlightFactor provide separate systems documentation for their simulated versions.
Circuits in the first 777 ever built
Among Clark’s favourite flying memories is base training in a 777: taking a large airliner to a quieter airport and practising circuits and touch-and-go landings. The aircraft happened to be the first 777 built, a former Boeing test machine, which added a sense of history to the experience. For a pilot whose enthusiasm had been confirmed by an Air Cadets flight as a teenager, it was a particularly satisfying milestone.
In airline service, Heathrow retained a personal attraction because of childhood family journeys through the airport. He describes enjoying the view over London while reminding himself to concentrate on the touchdown. He also explains why the autopilot does not remove the crew’s work: it gives pilots capacity to consider weather, suitable diversion airports, approaches and the services available on the ground. The interview combines the pleasure of flying with the continuing responsibility of managing the journey.
The stories that returned at a fleet reunion
Nearly two decades after leaving the 777 fleet, Captain Lim attended a reunion with about sixty former colleagues in Kuala Lumpur. Some were pilots he had taught on the F27 in the 1980s who had gone on to command long-haul aircraft. Meeting them brought back the shared decisions and disruptions that had shaped their working lives, as well as the humour of simulator trips and time away from home.
He recalls a weather diversion from Perth to Adelaide, a pressurisation problem after leaving Stockholm and a decision to remain on the ground as a typhoon approached. The reunion also gave him a chance to settle a misunderstanding with a colleague after twenty years. His account is a personal memory of the people around the aircraft; the remembered distances, fuel quantities and operational circumstances have not been adopted as technical specifications.
The responsibility behind a first flight
Looking back three decades after the first 777 flight from Paine Field, Cashman remembered the responsibility of representing everyone who had prepared the aircraft. Engineers, customers, manufacturing staff and maintenance personnel had already completed their part of the work. At the moment of flight, he wanted to be sure that he fulfilled his own part just as well.
The aircraft left a lasting impression on him. Boeing’s written interview highlights describe his enjoyment of flying it and the pride he still felt in the programme thirty years later. His recollection gives the first-flight milestone a human setting: the person at the controls was conscious of a much larger team whose effort made that departure possible.
公開資料 20
- Boeing 777Research background · Wikipedia revision 1373989467 · retrieved 2026-09-12
- Microsoft Flight Simulator aircraft manuals
- PMDG 777 SDK broadcast setup
- PMDG 777-200ER system implementationOfficial developer / designated store catalogue · checked 2026-09-12
- X-Plane aircraft and avionics manuals
- FlightFactor 777 v2 official changelog
- FlightFactor products
- 777-200LR for MSFS 2020 & 2024Official developer / designated store catalogue · checked 2026-09-12
- 777F for MSFS 2020 & 2024Official developer / designated store catalogue · checked 2026-09-12
- 777-300ER for MSFS 2020 & 2024Official developer / designated store catalogue · checked 2026-09-12
- 777-200ER v2 UltimateOfficial developer / designated store catalogue · checked 2026-09-12
- 777-300ER v2 UltimateOfficial developer / designated store catalogue · checked 2026-09-12
- 777 v2 Freighter expansionOfficial developer / designated store catalogue · checked 2026-09-12
- 777 v2 Engine ExpansionOfficial developer / designated store catalogue · checked 2026-09-12
- Bradley Clark: Cathay Pacific B777Interview · 23 February 2017
- Sky Bound Memories: A Boeing 777 Pilot ReunionCaptain Lim · recollection of the 26 April 2024 Malaysia Airlines pilot reunion
- A former test pilot relives the first 777 flightJosh Green and Jen Cram · page dated 27 June 2024; later programme-status text also present
- ICAO Doc 8643 — aircraft type designatorsPublic search data retrieved 2026-09-14; authority update 2026-09-03
- FlightFactor 777-200LR UPGRADE- FlightFactor-777-(200LR)-UpProduct listing captured 2026-09-30; edition scope from the reviewed catalogue
- FlightFactor-777-(200ER)(200LR)-FlightFactor-777-(200ER)(200Product listing captured 2026-09-30; edition scope from the reviewed catalogue
プロファイルによるモデル化
Boeing 777-300ER
Free + ProMSFS 2020MSFS 2024X-Plane 11X-Plane 12
The 777 entered service in 1995 after development with input from major airline customers. Its broad cabin and two very large engines filled a space between the 767 and 747. The programme expanded through different fuselage lengths, range developments and engine choices.
This starting point selects Boeing 777-300ER. Its aircraft-level settings do not select a particular developer’s custom systems.
Spring resistance builds with the selected airspeed response. Directed aerodynamic loading is omitted.
Pitch-trim relief is off. Autopilot following is enabled for supported control references.
この正確なリビジョンは、まだ公開インストールに対応していません。
Controls and trim
The 777 combines fly-by-wire with a conventional yoke, unlike the passive Airbus sidestick. PMDG describes C-star-U laws and artificial feel, with normal/direct behavior and custom trim logic. ER, LR, 300ER and freighter configurations retain different engines and product identities. FlightFactor's v2 X-Plane family is separately scoped from its older 777 package and from PMDG's implementation.
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 strength20%
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: Artificial yoke feel motivates the configured powered-control response; the presence of fly-by-wire does not imply a passive Airbus-style inceptor. The baseline spring is 0.2. Low-speed spring blending is off.
777-200ER777-200LR777-300ER for MSFS 2020 & 2024777F for MSFS 2020 & 2024Spring deadband0%
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.
Forces · Center starting force0.04
この値の理由: Adds smoothly ramped resistance outside the centre deadband. Zero removes this preload.
Forces · Center starting force transition0.05
この値の理由: Sets the travel used to ramp in centre preload. Wider intervals make its onset more gradual.
Overall aerodynamic load0%
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 0 gain omits sustained directed airspeed loading. Spring resistance remains independent.
Airspeed blendingFalse
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 start20 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 full122 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275
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 speed100%
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 1. It strengthens the permitted spring response above 122 KIAS, with the squared-speed ratio capped at 7.8.
Centre stiffening cap7.8
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 load65%
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 0.65 and 0.65, respectively. These stored weights do not create directed aerodynamic loading while that term is inactive. No custom spring-travel curve is enabled.
Elevator load65%
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)0%
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: Aircraft trim-rate and law behavior are documented, but a disabled profile trim response omits their hardware effect rather than reproducing them. Pitch relief is off, with stored authority 0; roll authority is 0.
777-200ER777-200LR777-300ER for MSFS 2020 & 2024777F for MSFS 2020 & 2024Trim relief (aileron)0%
ロールトリムの同じ軽減。多くのGA機には本物のエルロントリムがないためゼロのまま。ロールトリムを持つ機種には相応の値が入ります。
上げると: ロールトリムがより多くの保持力を除去。
下げると: ロールトリムの効きが弱く。
この値の理由: Scales supported roll-trim relief and permitted centre movement. Zero removes roll response.
Effect gains · Ground
Runway rumble40%
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 buffet30%
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 buffet22%
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 buffet14%
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 buffet10%
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 shaker90%
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 thump90%
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 rumble50%
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 authority100%
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 enabledFalse
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 enabledFalse
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 enabledFalse
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 enabledTrue
Whether this feature is active in this profile.
この値の理由: 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.
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 index6
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 enabledTrue
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 | 0.2 | Artificial yoke feel motivates the configured powered-control response; the presence of fly-by-wire does not imply a passive Airbus-style inceptor. The baseline spring is 0.2. Low-speed spring blending is off. |
| Spring deadband | 0.0 | Sets travel around the centre before the baseline spring resists. Smaller values engage it sooner. |
| Forces · Center starting force | 0.04 | Adds smoothly ramped resistance outside the centre deadband. Zero removes this preload. |
| Forces · Center starting force transition | 0.05 | Sets the travel used to ramp in centre preload. Wider intervals make its onset more gradual. |
| Force gain | 0 | The 0 gain omits sustained directed airspeed loading. Spring resistance remains independent. |
| Master gain | 0.85 | Scales overall profile strength while preserving effect balance, subject to device and output limits. |
| Dynamic-pressure blend | False | 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. |
| Spring full-strength speed | 122 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 | 275.0 kt | Sets the IAS reference for aerodynamic loading. It is an estimate, not published cruise TAS or a flight limit. |
| Airspeed spring stiffening | 1.0 | The high-speed spring-stiffening gain is 1. It strengthens the permitted spring response above 122 KIAS, with the squared-speed ratio capped at 7.8. |
| Airspeed stiffening cap | 7.8 | Limits the squared airspeed ratio used for high-speed spring stiffening; it is not a device-force cap. |
| Aileron force scale | 0.65 | Roll and pitch aerodynamic scales are 0.65 and 0.65, respectively. These stored weights do not create directed aerodynamic loading while that term is inactive. No custom spring-travel curve is enabled. |
| Elevator force scale | 0.65 | 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 | False | Allows trim relief with supported control law and valid telemetry. Axis authorities set its amount. |
| StickFeel · Elevator authority | 0 | Aircraft trim-rate and law behavior are documented, but a disabled profile trim response omits their hardware effect rather than reproducing them. Pitch relief is off, with stored authority 0; 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 | False | Allows load-factor changes to modify permitted spring laws. Passive fly-by-wire feel can suppress it. |
| StickFeel · Rate damping enabled | False | 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 | 0.3 | Sets stall-buffet strength. Zero removes the cue without changing simulator stalls or warnings. |
| Aero · Gain | 0.22 | 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 | 6 | 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 | True | Permits shaker at supported warning conditions; the switch does not establish aircraft equipment. |
| Aero · Amplitude | 0.9 | 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 | 0.32 | Sets gear-bump texture during ground motion, separate from touchdown impact. |
| Ground · Gain | 0.9 | Sets landing-impact strength; landing telemetry and response shape determine the pulse. |
| Ground · Gain | 0.5 | 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
- Boeing 777Research background · Wikipedia revision 1373989467 · retrieved 2026-09-12
- 777-200ER777-200ER product control-system descriptionOfficial developer / designated store catalogue · checked 2026-09-12
- 777-200LR777-200LR product control-system descriptionOfficial developer / designated store catalogue · checked 2026-09-12
- 777-300ER for MSFS 2020 & 2024777-300ER productOfficial developer / designated store catalogue · checked 2026-09-12
- 777F for MSFS 2020 & 2024777F productOfficial developer / designated store catalogue · checked 2026-09-12
- Microsoft Flight Simulator aircraft manuals
- PMDG 777 SDK broadcast setup
- X-Plane aircraft and avionics manuals
- FlightFactor 777 v2 official changelog
- FlightFactor products
- 777-200ER v2 UltimateOfficial developer / designated store catalogue · checked 2026-09-12
- 777-300ER v2 UltimateOfficial developer / designated store catalogue · checked 2026-09-12
- 777 v2 Freighter expansionOfficial developer / designated store catalogue · checked 2026-09-12
- 777 v2 Engine ExpansionOfficial developer / designated store catalogue · checked 2026-09-12
- Bradley Clark: Cathay Pacific B777Interview · 23 February 2017
- Sky Bound Memories: A Boeing 777 Pilot ReunionCaptain Lim · recollection of the 26 April 2024 Malaysia Airlines pilot reunion
- A former test pilot relives the first 777 flightJosh Green and Jen Cram · page dated 27 June 2024; later programme-status text also present
- ICAO Doc 8643 — aircraft type designatorsPublic search data retrieved 2026-09-14; authority update 2026-09-03
- FlightFactor 777-200LR UPGRADE- FlightFactor-777-(200LR)-UpProduct listing captured 2026-09-30; edition scope from the reviewed catalogue
- FlightFactor-777-(200ER)(200LR)-FlightFactor-777-(200ER)(200Product listing captured 2026-09-30; edition scope from the reviewed catalogue
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