Development milestones
First flight: 25 October 1991 ( 1991-10-25 )
Developed from: Airbus A300
机型库Airbus A340
MarcelX42 · CC BY-SA 4.0 · Lufthansa A340-313Airbus A340
A four-engine Airbus wide-body developed in parallel with the A330.
Airliner配置文件选项：7 个
了解飞机
The A340 shared substantial programme work with the A330 but used four engines for long-haul operations. The initial -200 and -300 were followed by the much larger -500 and -600 developments, which brought different engines and significant airframe changes.
The A340-600 has its own dimensions, fuel system and equipment. ToLiss's simulator documentation describes the specific flight-control and hydraulic modelling of its implementation.
Finding a runway in a white landscape
Mirpuri's log follows the 2 November 2021 flight of A340-313HGW 9H-SOL from Cape Town to Wolf's Fang. Preparation had taken months, including an advance visit by another captain. Much of the equipment needed to establish the season's operation travelled in the aircraft's own hold. During the flight, updated weather and runway-friction reports helped the crew confirm that conditions remained suitable.
The final approach presented a distinctive visual problem: the ice runway blended into the surrounding white landscape, making height judgement difficult. Mirpuri describes the intense reflection, the importance of the monitoring pilot's calls and the satisfaction of a landing that matched the plan. Applause from the cabin followed as the aircraft slowed. The crew then inspected the setting on foot before an uneventful return. This airline-published account attributes the result to preparation, ground support and crew coordination as well as the aircraft.
Teaching the next crew, and learning from them
In their conversation for Iberia, Ordovás recalls moving through the 727 and A320 before travelling to Miami for A340 training. By the time of the interview, he was an instructor and examiner on the A330 and A340. Menéndez, his friend and former colleague, had taught successive generations of pilots and continued instructing after his airline retirement. Their families' flying careers had crossed repeatedly.
They discuss how instruction had developed beyond technical drills to include judgement, attitudes and cooperation. Ordovás valued the humility needed to identify weaknesses and improve them, while Menéndez felt that teaching gave him energy in return. Both describe professional simulators as convincing enough to produce the physical reactions of a real flight. The joint interview concerns the careers and training work of instructors associated with the A340.
Long-haul flying, changing technology and life between countries
Lindegren describes a career that eventually brought him to the A330 and A340 after the DC-9, MD-11 and A320. In Remo Müller's SWISS profile, he reflects on the continuing need to adapt as paper manuals gave way to tablets and younger colleagues arrived fluent in the new tools. Long-haul flying had captivated him during what was meant to be a temporary assignment to Swissair, and he stayed.
The appeal came with costs. Maintaining a working life in Switzerland while his family lived in Sweden meant missing ordinary time together, as well as visiting distant cities. Near retirement from permanent employment, he was preparing a final rostered trip with friends as his crew and arranging to continue part-time flying. This is a personal account of an A330/A340 captain's working life; the interview does not identify every recalled journey with one specific aircraft variant.
公开来源 13
- Airbus A340Research background · Wikipedia revision 1373352164 · retrieved 2026-09-12
- X-Plane aircraft and avionics manuals
- A340-600 productOfficial developer / designated store catalogue · checked 2026-09-12
- ToLiss A340-600 change log
- ToLiss A340-600 published specification
- A340 Airliner for MSFS-2024Official developer / designated store catalogue · checked 2026-09-12Official developer / designated-store reference · checked 2026-09-14
- Hi Fly lands its first Airbus A340 in Antarctica – captain’s logCarlos Mirpuri · 22 November 2021
- Leading flight instructors past and presentJosé María Ordovás and Ventura Menéndez · November 2017, pages 91–94
- Too tall for fighter jets – perfect for the big wide worldFredrik Lindegren · 15 May 2026
- Simbrief Profiles - A340 Airliner - FAQs - iniBuilds ForumOfficial developer / designated-store reference · checked 2026-09-14
- ICAO Doc 8643 — aircraft type designatorsPublic search data retrieved 2026-09-14; authority update 2026-09-03
- JARDesign 340-500 Airliner-JARDesign-JD340Product listing captured 2026-09-30; edition scope from the reviewed catalogue
- A340-600 Pro MSFS20/24 by Aerosoft / ToLiss | Contrail ShopProduct listing captured 2026-09-30; edition scope from the reviewed catalogue
配置文件如何建模
JARDesign Airbus A340-500
Free + ProX-Plane 12JARDesign
The A340 shared substantial programme work with the A330 but used four engines for long-haul operations. The initial -200 and -300 were followed by the much larger -500 and -600 developments, which brought different engines and significant airframe changes.
This profile selects JARDesign Airbus A340-500 for X-Plane 12.
The spring stays independent of airspeed. Directed aerodynamic loading is omitted.
Pitch-trim relief is off. Autopilot following is off.
此确切修订版尚未开放公开安装。
Controls and trim
Airbus's A340 uses passive sidesticks within its fly-by-wire cockpit philosophy. iniBuilds documents an A340-300 with custom rotation and flare behavior, while ToLiss and Aerosoft's A340-600 products have their own hydraulic, actuator and control-law modeling. A modeled actuator can float or jam without producing a corresponding movement of a passive sidestick. The -300 and -600 retain distinct airframe and engine scope.
The selected implementation
JARDesign's XP12 generation has custom control/hydraulic/electrical/autoflight systems and stated simplifications. Its XP11 downloads remain separate.
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 strength55%
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 selected fixed spring approximates passive sidestick resistance; actuator hinge moments are not passed through as direct hand forces. The baseline spring is 0.55. Low-speed spring blending is off.
Cockpit and flight control familiesA340600Pro, versions, variants and downloadsA340 Airliner for MSFS-2024A340 600Spring deadband1%
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.
Forces · Center starting force0.03
设定理由: The centre preload is 0.03. It ramps outside the 0.01 deadband across 0.05 travel, shaping the passive centre independently of aircraft autotrim.
Forces · Center starting force transition0.05
设定理由: Sets the travel used to ramp in centre preload. Wider intervals make its onset more gradual.
Overall aerodynamic load0%
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 stored 0 aerodynamic-load gain is inactive under the fixed-centre control law.
Airspeed blendingFalse
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 start8 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.
Spring engagement full65 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.
力反馈调校速度250
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.
Centre firmness vs speed0%
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: Adds permitted spring resistance above the full-blend speed. Zero removes this high-speed increase.
Centre stiffening cap2
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 load100%
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 1 and 1, respectively. These stored weights do not create directed aerodynamic loading while that term is inactive. The pitch spring-travel curve reaches output 1 at input 1. The roll spring-travel curve reaches output 0.3 at input 1. Spring-travel response contributes separately to axis balance.
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 force55%
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.
Trim
Trim relief (elevator)0%
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: Normal-law automatic trim changes the aircraft's stabilizer state independently of the fixed hardware centre. Pitch relief is off, with stored authority 0; roll authority is 0.
Cockpit and flight control familiesA340600Pro, versions, variants and downloadsA340 Airliner for MSFS-2024A340 600Trim relief (aileron)0%
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 rumble0%
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 bumps0%
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
Stall buffet6%
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 buffet6%
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 buffet0%
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 buffet0%
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.
Stick shaker50%
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.
Effect gains · Engine, mechanical & drag
Touchdown thump0%
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 rumble0%
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 rumble0%
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 motion0%
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.
Spring response
SpringResponse · Travel enabledTrue
Whether this feature is active in this profile.
设定理由: Applies the configured pitch and roll spring travel curves.
SpringResponse · Output1
设定理由: Sets response at the second pitch-curve point; it is an endpoint only if its input position is full travel.
SpringResponse · Output0.3
设定理由: Sets response at the second roll-curve point; its input position and other points determine the travel law.
Stick feel
StickFeel · Trim feel enabledFalse
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 enabledFalse
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 enabledFalse
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 enabledFalse
Whether this feature is active in this profile.
设定理由: Enables rate damping with the configured coefficients and control law.
Autopilot
Autopilot · Follow enabledFalse
Whether this feature is active in this profile.
设定理由: Autopilot following is off; the configured spring and load retain the hardware feel. Separate neutral hold is on at strength 0.28, when a supported autopilot state admits it.
Autopilot · Neutral hold enabledTrue
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 strength0.28
设定理由: Sets admitted AP neutral-hold strength; inactive while neutral hold is disabled.
Aero
Aero · EnabledTrue
Whether this feature is active in this profile.
设定理由: 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).
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 index2
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 · Shaker enabledFalse
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 · EnabledFalse
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 · EnabledFalse
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
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 | 0.55 | The selected fixed spring approximates passive sidestick resistance; actuator hinge moments are not passed through as direct hand forces. The baseline spring is 0.55. Low-speed spring blending is off. |
| Spring deadband | 0.01 | Sets travel around the centre before the baseline spring resists. Smaller values engage it sooner. |
| Forces · Center starting force | 0.03 | The centre preload is 0.03. It ramps outside the 0.01 deadband across 0.05 travel, shaping the passive centre independently of aircraft autotrim. |
| 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 stored 0 aerodynamic-load gain is inactive under the fixed-centre control law. |
| 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 | 8 kt | Sets the IAS where the low-speed spring blend starts rising. This is a feel threshold, not a flight limit. |
| Spring full-strength speed | 65 kt | Sets the IAS where the low-speed blend reaches baseline strength; high-speed stiffening also uses it. |
| 力反馈调校速度 | 250 kt | Sets the IAS reference for aerodynamic loading. It is an estimate, not published cruise TAS or a flight limit. |
| Airspeed spring stiffening | 0 | Adds permitted spring resistance above the full-blend speed. Zero removes this high-speed increase. |
| Airspeed stiffening cap | 2 | Limits the squared airspeed ratio used for high-speed spring stiffening; it is not a device-force cap. |
| Aileron force scale | 1 | Roll and pitch aerodynamic scales are 1 and 1, respectively. These stored weights do not create directed aerodynamic loading while that term is inactive. The pitch spring-travel curve reaches output 1 at input 1. The roll spring-travel curve reaches output 0.3 at input 1. Spring-travel response contributes separately to axis balance. |
| Elevator force scale | 1 | Scales pitch aerodynamic loading; pitch spring travel and trim responses are separate settings. |
| Maximum output force | 0.55 | Caps directed-force output. Native spring effects and device limits remain separate. |
| SpringResponse · Travel enabled | True | Applies the configured pitch and roll spring travel curves. |
| SpringResponse · Output | 1 | Sets response at the second pitch-curve point; it is an endpoint only if its input position is full travel. |
| SpringResponse · Output | 0.3 | Sets response at the second roll-curve point; its input position and other points determine the travel law. |
| 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 | Normal-law automatic trim changes the aircraft's stabilizer state independently of the fixed hardware centre. 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 | False | Autopilot following is off; the configured spring and load retain the hardware feel. Separate neutral hold is on at strength 0.28, when a supported autopilot state admits it. |
| 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 | True | Permits centering hold during a supported AP state, separate from following a moving target. |
| Autopilot · Neutral hold strength | 0.28 | 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 | 0.06 | Sets stall-buffet strength. Zero removes the cue without changing simulator stalls or warnings. |
| Aero · Gain | 0.06 | Sets high-Mach buffet strength; onset and full-strength thresholds are separate. |
| Aero · Gain | 0 | Sets flap buffet at the configured position and speed gates. Flap movement texture is separate. |
| Aero · Max flap index | 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 | 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 | False | Enables ground effects; each still needs its own strength and contact or motion telemetry. |
| Ground · Gain | 0 | Sets rolling texture strength, modified by speed, surface and undercarriage configuration. |
| Ground · Gain | 0 | Sets gear-bump texture during ground motion, separate from touchdown impact. |
| Ground · Gain | 0 | 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 | False | Enables engine cues with nonzero settings and valid running-engine telemetry. |
| Engine · Gain | 0 | 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 | Sets texture from observed flap movement; a command without movement does not establish the cue. |
| Mechanical · Gain | 0 | Sets texture from observed gear movement, separate from aerodynamic and touchdown effects. |
公开来源 16
- Airbus A340Research background · Wikipedia revision 1373352164 · retrieved 2026-09-12
- Cockpit and flight control familiesAirbus cockpit family descriptions; Airbus cockpit commonality, sidestick philosophy; Airbus cockpit commonality
- A340600Pro, versions, variants and downloadsFlight dynamics, systems and aircraft-state features; Requirements and version1.0.3-1.0.5 history
- A340 Airliner for MSFS-2024A340 Airliner product and featuresOfficial developer / designated store catalogue · checked 2026-09-12Official developer / designated-store reference · checked 2026-09-14
- A340 600A340-600 specific featuresOfficial developer / designated store catalogue · checked 2026-09-12
- Exact developer aircraft pageCurrent XP12 requirements, systems and exact variant; Current version, XP12 requirements and systems list
- X-Plane aircraft and avionics manuals
- ToLiss A340-600 change log
- ToLiss A340-600 published specification
- Hi Fly lands its first Airbus A340 in Antarctica – captain’s logCarlos Mirpuri · 22 November 2021
- Leading flight instructors past and presentJosé María Ordovás and Ventura Menéndez · November 2017, pages 91–94
- Too tall for fighter jets – perfect for the big wide worldFredrik Lindegren · 15 May 2026
- Simbrief Profiles - A340 Airliner - FAQs - iniBuilds ForumOfficial developer / designated-store reference · checked 2026-09-14
- ICAO Doc 8643 — aircraft type designatorsPublic search data retrieved 2026-09-14; authority update 2026-09-03
- JARDesign 340-500 Airliner-JARDesign-JD340Product listing captured 2026-09-30; edition scope from the reviewed catalogue
- A340-600 Pro MSFS20/24 by Aerosoft / ToLiss | Contrail ShopProduct listing captured 2026-09-30; edition scope from the reviewed catalogue
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