PIPER / GENERAL AVIATION

Piper PA-18 Super Cub

A tandem-seat utility aircraft whose light structure and high wing suit bush, towing and recreational work.

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Type designatorsPA18Models & sources ↓

Choose the version you fly to narrow the edition-specific reading.

PropulsionSingle piston
ConfigurationTandem seats · Tailwheel
Simulator ecosystemsX-Plane
YOUR AIRCRAFT COMPANION

Start here

A few places to begin, from the aircraft’s story to the people who fly it.

Introduction

Meet the aircraft

The Super Cub joined Piper's range in 1949, developing earlier Cub designs with more power and equipment. It retained the braced high wing, tandem cabin and tailwheel layout. Its working roles include glider towing, banner towing and remote-area transport.

Aircraft background

Wikipedia contributors · Read more ↗
Pilot account

A factory-fresh working Cub in 1975

Garvey borrowed a new 150-horsepower Super Cub at the factory before its owner, Piper dealer Jim Porter, took it home. His report places it in an interesting period: Piper was promoting its newer designs while customers who needed a Cub already knew where to find one.

AOPA Pilot, July 1975; republished in AOPA’s Super Cub fact sheet. New PA-18-150 loaned by Jim Porter.

AOPA Pilot · Read more ↗
Simulator systems

Finding the controls in Laminar’s PA-18-150

Laminar identifies its model as a PA-18-150. The cockpit guide places the throttle, carburettor-heat control and rotary trim handle on the left side, with a separate three-position flap lever. It describes brake pedals distinct from the rudder pedals, overhead fuel sight gauges and an electrical switch panel. The sight gauges provide approximate indications, with reduced accuracy at low fuel levels.

Piper PA-18 Super Cub · Laminar Research · X-Plane 12

Laminar Research · Read more ↗
WATCH & EXPLORE

Into the cockpit

YouTube
Flight video

Fishing Flying & Outdoor Adventures! · 1 min ·

✈️ Desert Takeoffs & Landings | PA-18 Super Cub Bush Flying 🏜️

A Super Cub pilot practices desert takeoffs and landings.

Real aircraft · Piper PA-18 Super Cub

Watch on YouTube ↗

Preview images are served by AirframeDB. Videos open on YouTube only when you choose to watch.

THE AIRCRAFT

Meet Piper PA-18 Super Cub

The Super Cub joined Piper's range in 1949, developing earlier Cub designs with more power and equipment. It retained the braced high wing, tandem cabin and tailwheel layout. Its working roles include glider towing, banner towing and remote-area transport.

Many individual aircraft are modified with different engines, wheels and equipment. Each simulator package identifies its represented variant and cockpit.

Research-based aircraft backgroundWikipedia contributors · Piper PA-18 Super Cub ↗
FAMILY, MODELS & VARIANTS

Piper PA-18 Super Cub

Piper → · Explore the family →

AIRCRAFT IDENTITY

Aircraft type designators

Use the code for the model you are flying. The linked authority lists the applicable aircraft.

HOW IT CAME TO BE

History & design

UNDER THE SKIN

Systems & details

A Cub adapted to working from rough ground

Laminar’s background chapter describes a fabric-covered steel-tube fuselage, a braced high wing and the extra power, flaps and wing tanks that distinguish the Super Cub from the earliest Cub designs. It also describes the broad modification culture around the type, including large low-pressure tyres, cargo racks and additional storage. Those visible changes help explain why two PA-18 photographs can show quite different working equipment.

Laminar Research PA-18 manual · PDF p.4 · aircraft background
Laminar Research · Piper PA-18 Super Cub POH ↗
FROM THE COCKPIT

Pilot accounts

A factory-fresh working Cub in 1975

William Garvey

Garvey borrowed a new 150-horsepower Super Cub at the factory before its owner, Piper dealer Jim Porter, took it home. His report places it in an interesting period: Piper was promoting its newer designs while customers who needed a Cub already knew where to find one. The aeroplane's fabric covering, tandem seats and simple starting controls made its older lineage immediately apparent, even with the extra power and flaps of the Super Cub.

For the flight, two people and full tanks left the aircraft below its permitted maximum weight. Garvey reported a strong climb that continued at 4,000 feet. He tried stalls with and without power and flap, describing mild breaks and prompt recovery in each case. A half-flap arrival then showed the compact landing performance that helped explain the aircraft's working reputation. His brief evaluation conveys a practical, capable machine encountered during production, with the results tied to that flight's loading rather than an assumed performance standard for today's many modified Cubs.

AOPA Pilot, July 1975; republished in AOPA’s Super Cub fact sheet. New PA-18-150 loaned by Jim Porter.

Read the full account · AOPA Pilot ↗

Rediscovering the Super Cub, one landing at a time

Budd Davisson

Davisson returned to the PA-18 after roughly fifteen years away, flying Tom Hampton's restored 150-horsepower Super Cub on the same afternoon as an older J-2. Its larger tyres, comfortable seats and stronger climb made the family resemblance feel distinctly more capable. He liked the control response and could see ahead well enough on the ground without the weaving taxi he might have expected from a tailwheel aircraft. His comparison concerns these particular Cubs, not every version carrying the name.

The landings provided a candid account of relearning the aeroplane. His first clean approach floated and ended with a bounce on the large tyres. Half flap made the next descent easier to manage and reduced the float. For the final attempt, he used full flap but let the speed decay too early, leaving little elevator authority for the flare and another untidy arrival. He did not perform stalls on this flight.

Budd Davisson flight report, reproduced by Pilotfriend with Airbum credit; undated. Restored PA-18 flown alongside a J-2 comparison.

Read the full account · Pilotfriend / Budd Davisson ↗

From a Cessna 210 to an Alaskan float Cub

Crista Worthy

Worthy first flew a Super Cub in 2013 at Alaska Float Ratings in Moose Pass. Most of her previous experience had been in a Cessna 210, so she expected the stick and left-hand throttle to require adjustment. Instead, both felt natural almost immediately. She flew two 160-horsepower examples with different floats and panels, learning the unfamiliar work of manoeuvring on water and choosing a takeoff direction without a marked runway.

From the front seat, the view to either side became a large part of the attraction: the flights passed turquoise lakes and glacier-covered mountains. She found the float Cub much more responsive than the heavier Cessna she knew, while still feeling steady in the canyon winds she encountered. Simulated power-loss exercises also made the extra drag of the floats memorable. Her account is a recollection of supervised seaplane training, and her strongest impression was the simple pleasure of it; she remembers finishing flights with her face aching from smiling.

22 January 2016 article by R. K. Dick Williams with Crista Worthy, republished by High Sierra Pilots. Worthy’s separate first-person section recalls 2013 float training.

Read the full account · High Sierra Pilots / Disciples of Flight ↗
VIRTUAL VERSIONS

In your simulator

Systems, equipment and documentation for each developer’s aircraft.

Compare simulator versions →
X-Plane 12

Piper PA-18 Super Cub

Laminar Research · Released

X-Plane 12Included / first-party

Aircraft

Edition / package Desktop

Finding the controls in Laminar’s PA-18-150

Laminar identifies its model as a PA-18-150. The cockpit guide places the throttle, carburettor-heat control and rotary trim handle on the left side, with a separate three-position flap lever. It describes brake pedals distinct from the rudder pedals, overhead fuel sight gauges and an electrical switch panel. The sight gauges provide approximate indications, with reduced accuracy at low fuel levels. The guide maps this particular simulated cockpit, including its installed equipment.

Laminar Research · Piper PA-18 Super Cub POH ↗

Laminar Research PA-18 manual · PDF pp.6,15–18 · simulator cockpit guide

The represented Super Cub cockpit

Laminar's Super Cub guide identifies pitch trim, stick controls and the installed instruments. It documents this particular aircraft's panel rather than proving that every Super Cub has the same navigation or automatic-flight equipment.

Laminar Research · Piper PA-18 Super Cub POH ↗

Archived simulator manual; installed package revision not observed · PDF pp.7-8,20

X-Plane 12 Enhancement

Piper PA-18 Super Cub

SimCoders · Released

X-Plane 12Third-party add-on

Enhancement

Products and variants
ProductSimulatorProduct type
Reality Expansion Pack · Default XP12 Piper Super Cub ↗ReleasedX-Plane 12 Enhancement
THE NUMBERS

Aircraft specifications

Published figures for the named real-aircraft variant. Simulator equipment and performance can differ.

Specifications (PA-18-150 landplane)Piper PA-18 Super Cub · Specifications (PA-18-150 landplane) · real aircraft; source units retained
SpecificationPublished value
Length22 ft 7 in (6.88 m)
Wingspan35 ft 2 + 1 ⁄ 2 in (10.732 m)
Height6 ft 8 + 1 ⁄ 2 in (2.045 m)
Wing area178.5 sq ft (16.58 m² )
Empty weight930 lb (422 kg)
Max takeoff weight1,750 lb (794 kg)
Powerplant1 × Lycoming O-320 air-cooled flat four engine, 150 hp (110 kW)
Maximum speed130 mph (209 km/h, 113 kn)
Cruise speed115 mph (185 km/h, 100 kn) (75% power)
Stall speed43 mph (69 km/h, 37 kn) (flaps down)
Range460 mi (740 km, 400 nmi)
Service ceiling19,000 ft (5,800 m)
Rate of climb960 ft/min (4.9 m/s)
Wikipedia contributors · Piper PA-18 Super Cub ↗
GO TO THE SOURCE

Manuals & resources

Find your next read

Choose a topic for a short introduction and a link to the original source. Simulator references identify the developer and edition they cover.

Simulator documentation

Finding the controls in Laminar’s PA-18-150Piper PA-18 Super Cub · Laminar Research · X-Plane 12

Laminar identifies its model as a PA-18-150. The cockpit guide places the throttle, carburettor-heat control and rotary trim handle on the left side, with a separate three-position flap lever. It describes brake pedals distinct from the rudder pedals, overhead fuel sight gauges and an electrical switch panel. The sight gauges provide approximate indications, with reduced accuracy at low fuel levels. The guide maps this particular simulated cockpit, including its installed equipment.

Laminar Research PA-18 manual · PDF pp.6,15–18 · simulator cockpit guide

Laminar Research · Read the source ↗
The represented Super Cub cockpitPiper PA-18 Super Cub · Laminar Research · X-Plane 12

Laminar's Super Cub guide identifies pitch trim, stick controls and the installed instruments. It documents this particular aircraft's panel rather than proving that every Super Cub has the same navigation or automatic-flight equipment.

Archived simulator manual; installed package revision not observed · PDF pp.7-8,20

Laminar Research · Read the source ↗

Pilot account

A factory-fresh working Cub in 1975AOPA Pilot, July 1975; republished in AOPA’s Super Cub fact sheet. New PA-18-150 loaned by Jim Porter.

Garvey borrowed a new 150-horsepower Super Cub at the factory before its owner, Piper dealer Jim Porter, took it home. His report places it in an interesting period: Piper was promoting its newer designs while customers who needed a Cub already knew where to find one. The aeroplane's fabric covering, tandem seats and simple starting controls made its older lineage immediately apparent, even with the extra power and flaps of the Super Cub.

William Garvey

AOPA Pilot · Read the source ↗
Rediscovering the Super Cub, one landing at a timeBudd Davisson flight report, reproduced by Pilotfriend with Airbum credit; undated. Restored PA-18 flown alongside a J-2 comparison.

Davisson returned to the PA-18 after roughly fifteen years away, flying Tom Hampton's restored 150-horsepower Super Cub on the same afternoon as an older J-2. Its larger tyres, comfortable seats and stronger climb made the family resemblance feel distinctly more capable. He liked the control response and could see ahead well enough on the ground without the weaving taxi he might have expected from a tailwheel aircraft.

Budd Davisson

Pilotfriend / Budd Davisson · Read the source ↗

Read the original documentation from the people who created it. Manuals open on their publisher’s website.

Manual

↗Piper PA-18 Super Cub POHLaminar Research ↗X-Plane 12 Desktop ManualLaminar Research ↗X-Plane aircraft and avionics manualsLaminar Research

Aircraft background

↗Piper PA-18 Super CubWikipedia contributors · Research background · Wikipedia revision 1331579518 · retrieved 2026-09-12

Product

↗Reality Expansion Pack · Default XP12 Piper Super CubSimCoders · Official developer / designated store catalogue · checked 2026-09-12

Type designator

↗ICAO Doc 8643 — aircraft type designatorsInternational Civil Aviation Organization · Public search data retrieved 2026-09-14; authority update 2026-09-03
AIRCRAFT AND FEEL

Built-in force-feedback profiles

Read the documentary basis, editable starting settings and remaining questions for the aircraft you fly. Each explanation refers to the exact profile revision shown.

Catalogue programme-20261022-v1 · 4 profile choices

FFB-BRIDGE BUILT-IN PROFILE

Piper PA-18 Super Cub Straight Floats

Free and ProRevision 1Partial review

A tandem-seat utility aircraft whose light structure and high wing suit bush, towing and recreational work.

Aircraft and simulator scope

  • Piper PA-18 Super Cub Straight Floats · MSFS 2020 · Variant starting point
  • Piper PA-18 Super Cub Straight Floats · MSFS 2024 · Variant starting point
  • Piper PA-18 Super Cub Straight Floats · X-Plane 12 · Variant starting point

Piper PA-18 Super Cub Straight Floats universal civil family/configuration. Documentary mechanism clauses keep the source's stated aircraft or family scope; simulator targets are Bridge selection scopes.

The simulator model and controls

A tandem-seat utility aircraft whose light structure and high wing suit bush, towing and recreational work.

How this profile feels

Spring resistance builds with the selected airspeed response. A separate aerodynamic term adds speed-dependent control load.

Pitch-trim relief is off. Autopilot following is off.

Aircraft and configuration

The PA18 cockpit manual identifies a control stick for pitch and roll and a rotary pitch-trim handle.

About the values

Strengths are normalized hardware-feel settings. They set the effect balance; hand force depends on the device and its limits. The IAS reference is a tuning value.

What the documentation establishes

The PA18 cockpit manual identifies a control stick for pitch and roll and a rotary pitch-trim handle.

Documentary review and sources

These decisions describe the documentary basis and remaining gaps for this revision. Aircraft documentation and a starting setting describe different kinds of evidence.

Speeds and limits
Inherited

The indicated-speed references set the profile response scale; they are separate from aircraft operating limits.

Simulator integration
Not yet reviewed

The profile targets msfs2020, msfs2024, xplane12. Add-on-specific controls use only the supported references configured by this profile.

Force-feedback settings
Inherited

The settings define the profile’s effect balance. Device output limits affect physical hand force.

Starting settings and their rationale

These configured values are starting estimates. The explanations describe what each setting controls; physical validation appears separately below.

Estimated starting settings · revision 1
SettingStarting valueWhat it controls and why
Spring strengthStarting value0.74 What it controls and whyThis profile uses reversible-control loading for Piper PA-18 Super Cub. The baseline spring is 0.74. Its low-speed blend reaches baseline strength at 42.5 KIAS.
Master force gainStarting value0.85 What it controls and whyScales overall profile strength while preserving effect balance, subject to device and output limits.
Profile force gainStarting value0.8 What it controls and whyThe aerodynamic-load gain is 0.8 with an indicated-speed reference of 85 KIAS. This supplies speed-dependent loading alongside the spring.
Force tuning speed/referenceStarting value85 ktWhat it controls and whySets the IAS reference for aerodynamic loading. It is an estimate, not published cruise TAS or a flight limit.
Spring response reference speedStarting value42.5 ktWhat it controls and whySets the IAS where the low-speed blend reaches baseline strength; high-speed stiffening also uses it.
Aileron force scaleStarting value0.68 What it controls and whyRoll and pitch aerodynamic scales are 0.68 and 1, respectively. They set the aerodynamic axis balance. No custom spring-travel curve is enabled.
Elevator force scaleStarting value1 What it controls and whyScales pitch aerodynamic loading; pitch spring travel and trim responses are separate settings.
Trim feelStarting valueDisabled What it controls and whyRetained for compatibility and group membership. Trim relief, rather than this flag, controls centre movement.
Trim reliefStarting valueDisabled What it controls and whyAllows trim relief with supported control law and valid telemetry. Axis authorities set its amount.
Autopilot followStarting valueDisabled What it controls and whyAutopilot following is off; the configured spring and load retain the hardware feel.
Autopilot neutral holdStarting valueDisabled What it controls and whyPermits centering hold during a supported AP state, separate from following a moving target.
Output force limitStarting value0.55 What it controls and whyCaps directed-force output. Native spring effects and device limits remain separate.
All 44 starting settings and their rationale

The settings define the profile’s effect balance. Device output limits affect physical hand force.

Estimated starting settings · revision 1
SettingStarting valueWhat it controls and why
Spring strengthStarting value0.74 What it controls and whyThis profile uses reversible-control loading for Piper PA-18 Super Cub. The baseline spring is 0.74. Its low-speed blend reaches baseline strength at 42.5 KIAS.
Profile force gainStarting value0.8 What it controls and whyThe aerodynamic-load gain is 0.8 with an indicated-speed reference of 85 KIAS. This supplies speed-dependent loading alongside the spring.
Master force gainStarting value0.85 What it controls and whyScales overall profile strength while preserving effect balance, subject to device and output limits.
Output force limitStarting value0.55 What it controls and whyCaps directed-force output. Native spring effects and device limits remain separate.
Elevator force scaleStarting value1 What it controls and whyScales pitch aerodynamic loading; pitch spring travel and trim responses are separate settings.
Aileron force scaleStarting value0.68 What it controls and whyRoll and pitch aerodynamic scales are 0.68 and 1, respectively. They set the aerodynamic axis balance. No custom spring-travel curve is enabled.

Piper PA-18 Super Cub Straight Floats: 85 indicated knots is the inherited feel reference, not cruise TAS, a published flight limit or a measured force threshold.

Estimated starting settings · revision 1
SettingStarting valueWhat it controls and why
Force tuning speed/referenceStarting value85 ktWhat it controls and whySets the IAS reference for aerodynamic loading. It is an estimate, not published cruise TAS or a flight limit.
QSpring Start KnotsStarting value8 ktWhat it controls and whySets the IAS where the low-speed spring blend starts rising. This is a feel threshold, not a flight limit.
Spring response reference speedStarting value42.5 ktWhat it controls and whySets the IAS where the low-speed blend reaches baseline strength; high-speed stiffening also uses it.

Piper PA-18 Super Cub Straight Floats: generic device trim feel, trim relief, force trim, hydraulic trim centering, autopilot following and neutral hold are disabled because portable state and neutral-motion contracts remain unqualified.

Estimated starting settings · revision 1
SettingStarting valueWhat it controls and why
Trim feelStarting valueDisabled What it controls and whyRetained for compatibility and group membership. Trim relief, rather than this flag, controls centre movement.
Trim reliefStarting valueDisabled What it controls and whyAllows trim relief with supported control law and valid telemetry. Axis authorities set its amount.
Force Trim EnabledStarting valueDisabled What it controls and whyEnables local force trim, separate from aircraft-owned trim and add-on integration qualification.
Autopilot followStarting valueDisabled What it controls and whyAutopilot following is off; the configured spring and load retain the hardware feel.
Autopilot neutral holdStarting valueDisabled What it controls and whyPermits centering hold during a supported AP state, separate from following a moving target.

Exact configured values with software explanations. Force magnitudes remain editable estimates; disabled features retain inactive values.

Estimated starting settings · revision 1
SettingStarting valueWhat it controls and why
Spring deadbandStarting value0.045 What it controls and whySets travel around the centre before the baseline spring resists. Smaller values engage it sooner.
QBlend EnabledStarting valueEnabled What it controls and whyAllows baseline spring strength to rise with indicated airspeed where the control law permits it.
QSpring Minimum FactorStarting value0.5 What it controls and whySets low-speed spring strength as a fraction of baseline when blending is enabled. One keeps full strength.
Airspeed spring stiffening gainStarting value0.15 What it controls and whyThe high-speed spring-stiffening gain is 0.15. It strengthens the permitted spring response above 42.5 KIAS, with the squared-speed ratio capped at 5.
Airspeed spring stiffening limitStarting value5 What it controls and whyLimits the squared airspeed ratio used for high-speed spring stiffening; it is not a device-force cap.
Elevator AuthorityStarting value0 What it controls and whyThe profile uses the trim behaviour configured below. Pitch relief is off, with stored authority 0; roll authority is 0.
Aileron AuthorityStarting value0 What it controls and whyScales supported roll-trim relief and permitted centre movement. Zero removes roll response.
GLoad EnabledStarting valueEnabled What it controls and whyAllows load-factor changes to modify permitted spring laws. Passive fly-by-wire feel can suppress it.
Rate Damping EnabledStarting valueEnabled What it controls and whyEnables rate damping with the configured coefficients and control law.
Autopilot follow authorityStarting value0.1 What it controls and whySets admitted AP-follow gain, not a percentage of travel. Runtime ownership and input limits still apply.
Autopilot neutral hold strengthStarting value0.6 What it controls and whySets admitted AP neutral-hold strength; inactive while neutral hold is disabled.
EnabledStarting valueEnabled What it controls and whyEnables aerodynamic cues; each still needs nonzero strength and its simulator conditions.
GainStarting value0.35 What it controls and whySets stall-buffet strength. Zero removes the cue without changing simulator stalls or warnings.
GainStarting value0 What it controls and whySets high-Mach buffet strength; onset and full-strength thresholds are separate.
GainStarting value0 What it controls and whySets flap buffet at the configured position and speed gates. Flap movement texture is separate.
Maximum flap indexStarting value3 What it controls and whySets the final flap index for detent normalization. UP plus three detents uses maximum index3.
Minimum flap indexStarting value2 What it controls and whySets the first flap detent that admits buffet; this is a handle index, not degrees.
GainStarting value0 What it controls and whySets gear aerodynamic buffet; movement and ground-contact cues are separate.
Shaker EnabledStarting valueDisabled What it controls and whyPermits shaker at supported warning conditions; the switch does not establish aircraft equipment.
Stick shaker amplitudeStarting value0.5 What it controls and whySets triggered shaker strength; inactive while the shaker feature is disabled.
EnabledStarting valueEnabled What it controls and whyEnables ground effects; each still needs its own strength and contact or motion telemetry.
GainStarting value0.4 What it controls and whySets rolling texture strength, modified by speed, surface and undercarriage configuration.
GainStarting value0.25 What it controls and whySets gear-bump texture during ground motion, separate from touchdown impact.
GainStarting value0.65 What it controls and whySets landing-impact strength; landing telemetry and response shape determine the pulse.
GainStarting value0 What it controls and whySets reverse-thrust vibration with valid reverser and engine conditions. Zero removes the cue.
EnabledStarting valueEnabled What it controls and whyEnables engine cues with nonzero settings and valid running-engine telemetry.
GainStarting value0.12 What it controls and whySets estimated engine vibration using configured telemetry and response, not measured cockpit vibration.
EnabledStarting valueEnabled What it controls and whyEnables accessory cues with configured strengths and observed accessory movement.
GainStarting value0.12 What it controls and whySets texture from observed flap movement; a command without movement does not establish the cue.
GainStarting value0 What it controls and whySets texture from observed gear movement, separate from aerodynamic and touchdown effects.
Limits and open questions
  • The source establishes supported float configuration, not a manufacturer float supplement. No automatic contact-preset switch or custom REP engine/HeadShake interface is inherited. The trim-mechanism conflict remains unresolved.
  • Generic selection scope; installed add-on matching, custom states and device operation remain unqualified.
  • Force magnitudes and cue amplitudes are inherited estimates; no physical calibration or certification is claimed.

Physical validation

No physical force validation is recorded in this public catalogue for this revision. Documentary review and software checks do not establish how a particular device feels.

FFB-Bridge maintains this profile’s revisions and tuning discussion.

Revision 1 and download availability in FFB-Bridge ↗
Exact profile identity
Profile
airframe-piper-pa18-super-cub-straight-floats
Artifact SHA-256
43e49d14d91807d2e1fd89a27a8520331be71f7d4f0114f58ecb643155c24982
Bytes
13785
Spring strength
Forces.SpringStrength
Profile force gain
Forces.ForceGain
Master force gain
Forces.MasterGain
Output force limit
Forces.MaxOutputForce
Elevator force scale
Forces.ElevatorForceScale
Aileron force scale
Forces.AileronForceScale
Force tuning speed/reference
Forces.CruiseSpeedRefKnots
QSpring Start Knots
Forces.QSpringStartKnots
Spring response reference speed
Forces.QSpringFullKnots
Trim feel
StickFeel.TrimFeelEnabled
Trim relief
StickFeel.TrimReliefEnabled
Force Trim Enabled
StickFeel.ForceTrimEnabled
Autopilot follow
Autopilot.FollowEnabled
Autopilot neutral hold
Autopilot.NeutralHoldEnabled
Spring deadband
Forces.SpringDeadband
QBlend Enabled
Forces.QBlendEnabled
QSpring Minimum Factor
Forces.QSpringMinimumFactor
Airspeed spring stiffening gain
Forces.SpringAirspeedStiffenGain
Airspeed spring stiffening limit
Forces.SpringAirspeedStiffenCap
Elevator Authority
StickFeel.TrimRelief.ElevatorAuthority
Aileron Authority
StickFeel.TrimRelief.AileronAuthority
GLoad Enabled
StickFeel.GLoadEnabled
Rate Damping Enabled
StickFeel.RateDampingEnabled
Autopilot follow authority
Autopilot.FollowAuthority
Autopilot neutral hold strength
Autopilot.NeutralHoldStrength
Enabled
Aero.Enabled
Gain
Aero.Stall.Gain
Gain
Aero.Mach.Gain
Gain
Aero.Flap.Gain
Maximum flap index
Aero.Flap.MaxFlapIndex
Minimum flap index
Aero.Flap.MinFlapIndex
Gain
Aero.Gear.Gain
Shaker Enabled
Aero.ShakerEnabled
Stick shaker amplitude
Aero.Shaker.Amplitude
Enabled
Ground.Enabled
Gain
Ground.Rumble.Gain
Gain
Ground.Bumps.Gain
Gain
Ground.Thump.Gain
Gain
Ground.Reverse.Gain
Enabled
Engine.Enabled
Gain
Engine.Rumble.Gain
Enabled
Mechanical.Enabled
Gain
Mechanical.FlapMotion.Gain
Gain
Mechanical.GearMotion.Gain
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