Qualification and Approval Guide (QAG) for the FlyThisSim ......2016/03/30 · Enhanced electrical modeling of aircraft busses ensuring electrical and avionics systems integrate as

Qualification and Approval Guide (QAG) for the FlyThisSim Touch Trainer V2.82

FlyThisSim Compliance Table for the FTS TouchTrainer Page 1

TOUCHTrainer BATD

FlyThisSim, FlyThisSim L.L.C. 102 Cross St. Suite 110

San Luis Obispo, CA 9340 1 (844) 746-2846

http://www.flythissim.com

FTS TouchTrainer 210

Qualification and Approval Guide (QAG) for the FlyThisSim Touch

Trainer FAA APPROVED QAG March 30, 2016

Neil D. Rose Acting Manager, Airmen Training and Certification Branch, AFS-810

http://www.flythissim.com/



Table of Contents

QUALIFICATION AND APPROVAL GUIDE (QAG) FOR THE FLYTHISSIM TOUCH TRAINER ......................................... 1

OVERVIEW STATEMENT ......................................................................................................................................... 4

AVIATION TRAINING DEVICE (ATD) DESCRIPTION .................................................................................................. 5

DEVICE/MODEL DESCRIPTION/PARTS LIST ............................................................................................................. 9

DETAILED PARTS LIST....................................................................................................................................................10

Hardware ...........................................................................................................................................................11

Common Components ........................................................................................................................................13

PHYSICAL CONTROL CONFIGURATIONS .............................................................................................................................13

PHYSICAL CONTROLS ....................................................................................................................................................14

SIMULATOR INSTRUCTOR OPERATING SYSTEM ...................................................................................................................17

DESIGN CRITERIA (LIST OF BATD AND/OR AATD QUALIFYING ITEMS FROM AC) .................................................. 19

AIRCRAFT CONFIGURATIONS AND SOFTWARE COMPATIBILITY STATEMENT ....................................................... 29

TOUCHTRAINER INSTRUMENT PANEL CONFIGURATIONS ......................................................................................................31

CIRRUS AIRCRAFT.........................................................................................................................................................31

Cirrus Performance and CG ................................................................................................................................31

Cirrus SR20/22/22TN and 22T(Perspective) .......................................................................................................33

Cirrus SR 20/22/22TN Avidyne and 2 * GNS 430W ............................................................................................34

Cirrus SR 20/22 G1 Analog with 2* GNS 430W ..................................................................................................35

CESSNA......................................................................................................................................................................36

Cessna Performance and GC ..............................................................................................................................36

Cessna 172 SP.....................................................................................................................................................38

Cessna 172 S RG .................................................................................................................................................39

Cessna 182, 182T, 182T RG (Cessna 182 T RG shown) .......................................................................................40

Cessna 172 NAV III .............................................................................................................................................41

Cessna 172 RG NAV III ........................................................................................................................................42

Cessna 206 RG NAV III ........................................................................................................................................43

Cessna 182 RG NAV III ........................................................................................................................................44

DIAMOND ..................................................................................................................................................................45

Diamond Performance and CG ...........................................................................................................................45

Diamond DA 20 ..................................................................................................................................................46

Diamond DA40 G1000........................................................................................................................................47

Diamond DA42 G1000........................................................................................................................................47

Cessna 350/400 (Corvalis) ..................................................................................................................................49

Cessna 350/400 Performance and CG ................................................................................................................49

Cessna 350 and 400 Avidyne ..............................................................................................................................50

Cessna 350/400 G1000 ......................................................................................................................................51

BEECH AIRCRAFT .........................................................................................................................................................52

PERFORMANCE AND CG ................................................................................................................................................52

Beech Bonanza: Analog Instrumentation KFC 200 Autopilot ............................................................................54

Beech Bonanza: G500/KFC 200 Autopilot .........................................................................................................55



Beech Baron: Analog Instrumentation KFC 200 Autopilot .................................................................................56

Beech Baron: Analog Instrumentation KFC 200 Autopilot .................................................................................57

Beech Baron: G500 Instrumentation KFC 200 Autopilot ....................................................................................58

Beech Baron: G1000, GFC 700 Autopilot ............................................................................................................59

PIPER AIRCRAFT...........................................................................................................................................................60

Piper Performance and CG .................................................................................................................................60

Piper Arrow Analog GNS530W Piper III Autopilot ..............................................................................................65

Piper Cherokee G500, GNS530W and Piper IIB Autopilot ..................................................................................66

Piper Meridian G1000 ........................................................................................................................................66

Piper Seneca Analog 530 Piper IIIB Autopilot .....................................................................................................66

Piper Warrior Analog GNS530W Piper III Autopilot ...........................................................................................67

Piper Malibu .......................................................................................................................................................68

Piper Saratoga Avidyne ......................................................................................................................................69

Rockwell Commander 112 and 114 ....................................................................................................................70

Rockwell Commander Performance and CG.......................................................................................................70

Rockwell Commander.........................................................................................................................................71

VISUAL SYSTEM ................................................................................................................................................... 72

1. Standard. ....................................................................................................................................................72

2. VisX. ............................................................................................................................................................73

3. Visual Motion 100 and 210. .......................................................................................................................74

3. FUNCTIONS AND MANEUVERS CHECKLIST ....................................................................................................... 75



Overview Statement

Compliance Statement

This Qualification and Approval Guide (QAG) includes a detailed description of all components,

functions, and capabilities for the FlyThisSim TouchTrainer mode. This includes any optional

aircraft configurations with quality color pictures and diagrams. The required information as

described in the current advisory circular, AC 61-136A / FAA Approval of Aviation Training

Devices (ATD) and Their Use for Training and Experience, required for FAA approval, is

contained within this document. This includes listing all the required qualifying items, functions,

and capabilities. This QAG is used to clearly describe and verify the functionality of this aviation

training device platform confirming its suitability for airman training and experience. A valid

FAA Letter of Authorization (LOA) specifying the ATD allowances must also accompany the

training device when utilized for airman training or experience requirements as specified in 14

CFR §61 or 141.

This ATD must maintain its original performance and function without degradation. The

operator of this device is required to maintain its condition and functionally when used to satisfy

airmen training or experience requirements.

Only the configurations approved for this model, as described within this QAG, can be utilized

when satisfying FAA experience or training requirements. Any additions, changes, or revisions

to the model or to the available configurations described within this document must be approved

in writing by The General Aviation and Commercial Division, AFS-800. Operators who use

these trainers to satisfy FAA pilot training or experience requirements are obligated to allow

FAA inspection to ensure acceptable function, qualification, and compliance.

Any questions concerning FAA approval or use of ATDs should be directed to the General

Aviation and Commercial Division, AFS-800.



Aviation Training Device (ATD) Description The TouchTrainer enables pilots to practice normal and emergency aircraft procedures, Instrument

Flight Rules (IFR) procedures and the operation of Technically Advanced Aircraft (TAA).

Typical Standard TouchTrainer featuring two touch monitors, a joystick, rudder pedals, and a throttle

Typical Enhanced TouchTrainer VX featuring two touch monitors, a joystick, rudder pedals, throttle;



Typical Enhanced TouchTrainer featuring two touch monitors, a joystick, rudder pedals, throttle; With add on visual system (Visual Motion VM).

Typical Enhanced TouchTrainer featuring two touch monitors, a joystick, rudder pedals, throttle; With add on visual system (Floor Mount (FM) 100).



Typical Enhanced TouchTrainer featuring two touch monitors, a joystick, rudder pedals, throttle; With add on visual system (Floor Mount (FM) 210).

The TouchTrainer interfaces to the pilot through physical joystick/yoke, throttle quadrant, rudder pedals

and multiple high resolution touch screens. The touch screens and TouchTrainer software provide

natural control of aircraft systems and rapid reconfiguration so each aircraft simulated can be accurately

represented.

The TouchTrainer includes:

The most advanced avionics simulations for TAA aircraft with accurate unique representations

of G1000, G500, Perspective, Garmin GNS 530 WAAS, Garmin GNS 430 WAAS, Aspen Evolution

and Avidyne Entegra V7 using SimAVIO2 from FlyThisSim.

Smooth responsive flight simulation using the industry standard and constantly improving X-

Plane flight simulator.

GPS WAAS simulation integrated with avionics and custom autopilots that include fully coupled

leg, altitude and glideslope capture and tracking.

Enhanced electrical modeling of aircraft busses ensuring electrical and avionics systems

integrate as aircraft.

Validated, current data for airports and GPS approaches from the National Flight Database.



X-Plane flight models tuned for IFR ‘Pitch and Power’ and systems.

Accurate facsimiles of aircraft instrumentation, switches and controls depicted on multiple

touch screens configured in layouts appropriate for IFR simulator operations.

Touch screens provide a natural method of control that enables each aircraft simulated to have

a unique and realistic presentation; pilots can fly the simulator without learning a new

configuration.

Failures of aircraft systems designed to test pilot knowledge uniquely activated by either touch

or keyboard.

Low cost, attractive, commercially available computer and aircraft facsimile hardware.

The TouchTrainer includes a simple to use instrument panel editing tool. The editing tool

constrains the user, only allowing instrumentation applicable to a selected specific aircraft type

and model to be edited. Instrument placard, limits, captions and scales automatically adjust to

the aircraft type and model. The editing tool enables users to:

o Change the instrument panel background appearance

o Add, remove, scale and reposition instrumentation, avionics, autopilots, text and other

elements displayed on the instrument panel.

o Load, edit and save instrument panel configurations.

Optionally customers can purchase

o VX: A 100 degree * 35 degree high performance visual system.

o VM 100: A 100 degree * 70 degree high performance large display visual system

o VM 210: A 210 degree * 70 degree high performance large display visual system

o A purpose built table that allows rapid reconfiguration between yoke and joystick

controlled aircraft simulations.

o A purpose built cockpit with one or two seats and ergonomically correct locations for

throttles (vernier and lever), side-stick, yoke and rudder pedals



Device/Model Description/Parts List The TouchTrainer consists of the following:

SimAVIO2 TAA simulation from FTS

X-Plane flight simulator program from Laminar Research

FTS validated and enhanced flight model and systems data

A computer system loaded with the Windows operating system

Joystick or Yoke

Throttle quadrant, Vernier or Lever based

Main touch screen monitor

Auxiliary touch screen monitor

Rudder Pedals

Table or cockpit environment.

The TouchTrainer may also be provided with a choice of high performance visual systems and cockpit

environments consisting of:

VX 100 Degree Field of View Visual System

An upgraded computer system with a faster processor, motherboard and two high performance

graphics processors

Three 24 inch monitors, power supplies and mounting hardware

Reformatted instrumentation layouts taking advantage of the extra instrumentation screen

space freed up by this visual system.

VM 100 Degree Field of View Visual System

An upgraded computer system with a faster processor, motherboard and two high performance

graphics processors

Three 60 inch monitors, power supplies and mounting hardware



VM 210 Degree Field of View Visual System

Driven by a dedicated computer system with three high performance graphics cards this system

connects with the standard TouchTrainer computer for Instrumentation and system

management tasks.

Six 60 inch monitors, power supplies and mounting hardware





Detailed Parts List

Item Name Manufacturer Model Version Product Details

1 Cockpit FlyThisSim FM v1.0 FM 210 FM 100

This encompasses all of the formed ABS cockpit parts including: Symmetric Base, Cockpit Cowl, FM Table, FM Center Console, Central Console Lower, Cup holder, Bolster, Main legs

2 Visual Computer

FlyThisSim Gold N/A FM 210 Custom built PC: MSI X-99 Motherboard with 24GB RAM 3x GTX 970 Graphics Cards 750W Power Supply Intel Core i7 Quad-Core Processor 240GB Solid State Drive

3 Avionics Computer

FlyThisSim Green N/A FM 210 Std

Custom built PC: MSI 760GM- E51 Motherboard with 8GB Ram GTX 750 Ti Graphics Card 500W Power Supply AMD Quad-Core Processor 120GB Solid State Drive

4 Rudder Pedals Saitek Pro Flight Combat

N/A All Aluminum Pedals with independent toe brakes, self- centering and adjustable damping

5 Throttle Quadrant(s)

Saitek Pro Flight PZ45, TPM

N/A All USB Powered throttle. Fully customizable throttle assemblies to suit single and twin configurations.

6 Control Stick Logitech Extreme 3D N/A All USB Powered Control stick with 8-way programmable hat switch, PTT switch

7 Control Yoke Saitek Pro Flight Cessna

N/A All USB control yoke with steel shaft, 8-way programmable hat switch, 2 single programmable buttons

8 Trim Wheel Saitek Pro Flight Cessna Trim

N/A FM 210 USB Powered 9 full rotation trim wheel

9 Visual Display Monitor

Vizio E60-c3 N/A FM 210 FM 100

VM 100

60 Inch 1920 x 1080p LED TV at 60 HZ

10 Avionics Monitor

Planar Helium PCT2485

N/A All 24 Inch 1920x1080p glass front multi-touch monitor

11 Avionics Monitor

Neway CL9701NT N/A All 9.7 Inch 1280x1024 resistive touch LCD Monitor

12 Wireless Adapter

edimax EW-7811Un N/A All USB A Wi-Fi 802.11n 150Mbps

13 Intercom FlightCom IISX N/A FM 210 FM100

Voice activated portable 2-place intercom, with squelch, volume,



and pilot isolation controls

14 External Speakers

Bose Companion II N/A FM 210 FM 100

Powered external 2.0 speakers

15 Keyboard/ touchpad

Logitech K400 N/A All Wireless Keyboard with Built-In Touchpad with 10 meter range

16 Simulation Engine Visual

X-Plane Global v10.45 All Software used to calculate aircraft performance data, I/O controls, weather, visuals, and sounds

17 Simulation Engine

Avionics

FlyThisSim SimAVIO v2.96.335 All Software used for avionics, engine and electrics modeling, GPS, Instructor Station controls

18 Operating system Visual

Linux Xubuntu v14.04 FM 210 Computer Operating system for Visual Computer

19 Operating System Avionics

Windows Windows v8.1 All Computer Operating system for Avionics Computer

20 Instrument Procedures and Navigational database

All Worldwide aviation database from FAA National Flight Database and Navtech Inc.

Hardware

All hardware and computer components are readily available and commercial quality. The Touch

Trainer hardware and software combination have been tested to ensure:

Smooth performance of the flight simulator and other software components

At least 20Hz for the flight simulator

At least 15Hz for instrumentation except where aircraft equipment has a slower update rate.

Adequate size and resolution of touch monitors. Instrument indications can be read and touch

sensitive areas easily actuated.

Some text used for decoration may not be to this standard

Expansion. Future releases of software can be expected to perform adequately and additional

hardware components added without major upgrading of equipment. Expansion capabilities

will be somewhat limited because of cost.

Software The software integrated into the TouchTrainer is classified into functional areas and described

below.

Flight Simulation including aircraft performance, out of the window view (OOW) and instructor

operation station (IOS). The Touch Trainer uses Laminar Researches X-Plane as its flight

simulation component.



Aircraft Models. The aircraft models (.acf files) have been modified and approved for use by

FTS. These models are enhanced or replaced by SimAVIO to provide additional aircraft specific

electrical and navigational systems data to improve simulation fidelity. Other aircraft models

should not be used. Use of a non-approved aircraft model will be detected and the user

informed of the status. If this status window is displayed the training should be halted until the

correct model is loaded.

Out of the Window View (OOW). The OOW field of view is approximately 45 degrees horizontal

by 15 degrees vertical. With practice this is adequate for takeoff and landing but is not

optimized for VFR training. Where the VX visual system option is provided the OOW view is

approximately 100 * 35 degrees displayed on three monitors above the main touch screen. This

allows more screen space for instrumentation on the main touch screen allowing more accurate

instrument panel representations. It also extends functionality into VFR training such as; airfield

ground handling and signage interpretation, cross country mission rehearsal and map

interpretation. It also provides a more immersive environment and attractive training device.

Out of the window views can also be displayed on 100 degrees horizontal and 70 degree vertical

FOV or 200 degrees horizontal and 70 degree vertical FOV

Aircraft systems including electrical buses and distribution

The TouchTrainer enhances X-Plane to provide additional aircraft specific systems modeling of

electrical busses so that the aircraft checklists can be used. However, not every component in

the aircraft is modeled. This means that while electrical bus state, voltages and equipment

connectivity to the busses are modeled correctly bus loads are typical and may be incorrect for

ancillary equipment.

Simulation of TAA avionics systems including autopilot.

The TouchTrainer enhances or replaces the autopilot system to be an aircraft specific simulation.

It provides its own modeling of reduction of vertical velocity commanded before altitude

capture, leg interception and GPS glideslope capture. In particular the TouchTrainer has

enhanced autopilot operation for missed approach sequences ensuring correct operation.

The TouchTrainer enhances X-Plane with a complete WAAS GPS Flight Deck simulation, FTS’s

SimAVIO2 is used to provide these facilities.

Integration of hardware devices such as touch screens and aircraft facsimile hardware

X-Plane integrates to flying, trim, throttle and mixture controls

SimAVIO2 integrates to avionics control hardware.

Audio

o X-Plane is used to generate aircraft environment and equipment sounds such as engine

noise, wheel rumble, marker and Morse code and aerodynamic noise.

o SimAVIO is used to generate all other avionics specific warning tones

Navigation Data. The following features are available:

Airspace. Class A, B, C, D and special use airspace, airports, obstacles, navigational beacons are

provided in PFD and MFD map presentations.

o Terrain. Terrain is represented as a Shaded Relief Map, in order to keep load times to a

minimum and reduce memory requirements this data is typically half to one quarter of



the resolution in the aircraft. The effects of this can only be seen at lower map ranges

when few coastal airfields may appear to be in the water.

o Cultural Data. Roads, geographical boundaries coastline etc. are typical of the

geographical data seen on Flight Deck equipment. Not all the geographical layers seen

on specific equipment are available.

o Aeronautical Data. The National Flight Database (NFD) from the FAA is used to provide

airport and approach waypoint, NDB, VOR and other data.

o GPS, RNAV, ILS, LOC, VOR, and NDB based approaches with GPS overlays for initial and

missed approach segments.

Common Components

The computer system hardware and software, simulator software and Instructor and simulator controls

are common to all versions of the TouchTrainer. Reconfiguration of a TouchTrainer to simulate different

aircraft requires the user to load a different aircraft model file. This will change aircraft performance,

instrument panel and avionics configurations. Different aircraft models may require the TouchTrainer

physical controls configuration to be adjusted.

Physical Control Configurations Typical arrangements of control columns, side-sticks, yokes, throttles and rudder pedals are shown

below.

The Touch Trainer can be easily and quickly reconfigured to simulate aircraft of different configurations. When the desktop configuration is changed the user must shut down the simulator, replace the controls and restart. Software test routines ensure that physical controls are connected correctly after reconfiguration disabling the simulator in case of a fault conditions. Where TouchTrainers have table and cockpit environments control configurations are similarly reconfigurable

Yoke Vernier Throttle/Prop/Mixture, Rudder Pedals



Yoke, TPM Linear Throttles, Rudder Pedals Sidestick, Cirrus SIMPLE, Rudder Pedals

Yoke, Twin FADEC Throttles, Rudder Pedals Yoke, Twin TPM/PTM, Rudder Pedals

Physical Controls Within the above configurations aircraft with side-sticks, control columns, yokes, lever and Vernier

throttles are supported. Physical controls used are commercial off the shelf products that connect to

the TouchTrainer via USB. The TouchTrainer only uses the levers and buttons identified below.



The ‘Top Hat’ control on the joystick controls aileron and elevator trim. No other buttons or levers are operational

The Joystick controls aileron and position with left/right movement, elevator position with fore/aft movement. Rudder position is controlled by twisting the Joystick.

Throttle and Mixture controls are fitted to the Throttle Quadrant

Joystick and throttle controls

Throttle, propeller and mixture controls.

Throttle control for Complex Aircraft



Elevator and Aileron trim top hat switch

Throttle, propeller and mixture controls. The switches are not

used.

Yoke and Vernier style throttle controls

Rudder Pedals with Toe Brakes



Simulator Instructor Operating System

FlyThisSim Touch Screen Instructors Operating System.

The FlyThisSim Touch Instructor Operating Station is fully compliant with the requirements of section 8f

of AC 61 136. The IOS runs on a touch screen PC or laptop and is connected to the main simulator by

wireless network. The TTIOS allows the following functionality to be remotely controlled without

interrupting the flow of the simulated flight.

Reposition: The simulator can be repositioned to any airport or any position in the air. Re-

positioning in the air is compliant with AC-61-136 requirements

Malfunctions: The instructor can disable any of the instruments prior to or during a training

session, and is able to simulate failure of any of the instruments without stopping or freezing

the simulation to affect the failure.

Weather: The instructor has real time control over wind speed and direction, turbulence,

surface temperature, sea level barometric setting, cloud type, base and top altitudes and

atmospheric visibility.

Fuel: Fuel levels may be set manually or to tabs or full levels appropriate for the aircraft

Scenarios: Real time scenarios can be loaded and run. Scenarios allow the TouchTrainer to

deliver pre constructed exercises and score the student’s performance.



Student Monitoring: The TIOS allows remote monitoring of simulated aircraft position,

orientation, engine and main aircraft systems state. The simulator may be paused at any time

for instructional purposes.

Simulator Control: Loading of different aircraft and avionics configurations.

TTIOS Simulator Monitoring, Map and Reposition Controls



Design Criteria (List of BATD and/or AATD qualifying items from AC) This document comprises of a full system description of the FlyThisSim TouchTrainer described in the

accompanying document “TouchTrainer: System Description and a compliance table as required by AC

61-136 paragraph 8.

FTS has analyzed the requirements of AC 61-136 and mapped the FlyThisSim TouchTrainer v1.01

capabilities to them.

The following sections of AC 61-136 are provided:

• 3c (1), (2), (3) and (5)

• 4b • 8a to 8f inclusive

Ref Requirement Compliant Notes

3.c CRITERIA FOR APPROVAL AND

ACCEPTANCE OF A BATD.

The QAG should:

(1) Contain a detailed description of the hardware and software components that comprise the device configuration presented for approval. A detailed

description should be submitted for each device

configuration if approval for more than one device

configuration is desired. The description of the

hardware and software components must include the

manufacturer and model or version number of each

component, or other such information necessary to

correctly identify each component in the particular

configuration;

Yes A detailed description can be found in the attached document: “TouchTrainer: System Description”

(2) Contain a word-for-word listing of each title,

number, and letter item listed in paragraph 8 of this

appendix and state the following information for

each item:

• The operation or role of the item as appropriate

to the aircraft or family of aircraft being

represented,

• The value for each quantitative requirement

that either meets or exceeds the minimum

values required by that paragraph, and

• If the aircraft or family of aircraft represented

by the device does not have the referenced

item, report it as in the following examples: “Carburetor Heat-N/A,” “Cowl Flaps-N/A,”

Yes See Ref 8 in this document



or “Retractable Landing Gear-N/A.”

(3) Contain color photographs of the assembled unit

in the intended device configuration. The

photographs should be of a quality that clearly

shows the overall component arrangement, features,

ergonomics, and operation of each hardware control

listed in paragraph 8, as appropriate to the aircraft or family of aircraft being represented;

Yes Color photographs can be found in the attached document: “TouchTrainer: System Description”

(5) Provide operating instructions or manual

including at least a detailed explanation of the device

operating system, installation of components and/or

modules, all commands and menus, system setup,

operation, troubleshooting suggestions, and

appropriate aircraft operating information. The

device operating manual and installation materials may be sent separately.

Yes These items are provided in the attached “The TouchTrainer Simulator Pilots Operational Handbook”



Section 8. FlyThisSim TouchTrainer BATD Design Criteria

Ref Requirement Compliant Notes 8.a Controls

(1) Physical flight and aircraft system controls should be recognizable as to their function and how they are to be

manipulated solely from their appearance. Physical flight

and aircraft system controls eliminate the use of interfaces such as a keyboard, mouse, or gaming joystick to control

the represented aircraft model in simulated flight.

Yes FTS TouchTrainer can be operated entirely through the use of touch screens and other physical flight and aircraft system controls. The touch screens allow immediate recognition of controls through the display of photo realistic images. Manipulation is natural and obvious.

(2) For the purposes of this AC, virtual control is any input device to control aspects of the simulation (such as

setting aircraft configuration, location, and weather) and

to program, pause, or freeze the device. Virtual controls

should be primarily for the instructor’s use.

Yes Instructor’s controls are described in the accompanying document:

“TouchTrainer: System Description”

(3) Except for setup and/or fault mode entry, neither the

keyboard nor the mouse may be used to set or position any

feature of the BATD in the represented aircraft for the

maneuvers or flight training to be accomplished. See the

control requirements listed below for necessary equipment

as applicable to the aircraft model represented. The pilot

must operate the additional equipment needed in order to

accomplish a training procedure as listed in this appendix

in the same manner in which it would be operated in the

represented aircraft. For example, landing gear, wing

flaps, cowl flaps, carburetor heat control, and mixture,

propeller, and throttle controls.

Yes All pilot operated controls are actuated by touch screen except for elevator, aileron, rudder, elevator, aileron and rudder trim, throttle, and mixture controls. In all cases manipulation is natural and obvious.

(4) The physical arrangement, appearance, and operation

of controls, instruments, and switches required by this

appendix should model at least one aircraft in the family

of aircraft represented as closely as practicable.

Manufacturers are expected to use their best efforts to

recreate the appearance, arrangement, operation, and

function of realistically placed physical switches and other

required controls representative of a generic aircraft

instrument panel that includes at least the following:

• Master/battery;

• Magnetos for each engine (as applicable);

• Alternators for each engine; • Fuel boost pumps for each engine;

• Avionics master;

• Pitot heat; and • Rotating beacon/strobe, navigation, taxi, and

landing lights.

Yes The appearance and arrangement of all controls for the aircraft simulated can be found in the accompanying

document: “TouchTrainer: System Description”

These items are operated by touch screen where they are represented ‘as aircraft’.



(5) When an FAA-approved BATD is in use, only the software package evaluated and approved by the FAA may be loaded for use to avoid negative impact on

available system resources. This may require a separate

user profile for ATD operation.

Yes The TouchTrainer uses a separate profile for operation

8.b Control Requirements

(1) Airplane.

(a) A self-centering displacement yoke or control stick

that allows continuous adjustment of pitch and bank; (b) Self-centering rudder pedals that allow continuous

adjustment of yaw; (c) Throttle or power control(s) that allows continuous

movement from idle to full power settings; (d) Mixture/condition, propeller, and throttle/power

control(s) as applicable to the aircraft or family of aircraft

represented; and (e) Controls for the following items, as applicable to the

airplane or family of airplanes represented:

• Wing flaps,

• Pitch trim,

• Communication and navigation radios,

• Clock or timer,

• Gear handle (if applicable), • Transponder,

• Altimeter,

• Microphone with push-to-talk switch), • Carburetor heat

• Cowl flaps (if applicable).

Yes

The following items are actuated by touchscreen

Wing Flaps

Communication and Nav Radios

Clock or Timer

Transponder

Altimeter

Gear Handle

Carburetor heat

Cowl Flaps

8.c Control Inputs

(1) Time from control input to recognizable system

response (transport delay) must be 300 milliseconds or

less. The manufacturer listed in the approval guide

submitted for FAA approval must certify to this standard.

Yes Maximum transport delay is calculated as 2*X-Plane iteration period (33msec) + 1*SimAVIO iteration period (66msec) + 2*screen refresh period (18msec).

Maximum Transport Delay is: 2*33 +66 +2* 18= 168 milliseconds

(2) The control inputs must be tested by the computer and

software at each start-up and displayed as a confirmation

message or a warning message that the transport delay

time or any design parameter is out of original tolerances.

This test should consider the items listed under “Display

Yes The TouchTrainer Supervisor program tests control inputs and displays a confirmation message as required.



Requirements” in paragraph d below.

8.d Display Requirements

(1) Instruments and Indicators as appropriate and applicable to the aircraft or family of aircraft represented:

• Flight instruments in a standard

configuration, represented either as

separate traditional “round” flight

instruments, or as an electronic primary

flight instrument display with

reversionary and back-up flight

instruments.

• A sensitive altimeter with incremental

markings each 20 feet or less, operable

throughout the normal operating range of

the aircraft or family of aircraft

represented.

• A magnetic compass which displays

incremental markings typical of that

shown in the aircraft or family of aircraft

represented.

• A heading indicator with incremental

markings each 5 degrees or less,

displayed on a 360 degree circle. Arc

segments of less than 360 degrees may be

selectively displayed if desired or required, as applicable to the aircraft or

family of aircraft represented.

• An airspeed indicator with incremental

markings as shown on the aircraft or

family of aircraft represented; airspeed

markings of less than 40 knots need not

be displayed.

• A vertical speed indicator with incremental

markings each 100 feet per minute (fpm)

for both climb and descent, for the first

1,000 fpm of climb and descent, and at

each 500 fpm climb and descent for the

remainder of a minimum ± 2,000 fpm

total display, or as applicable to the

aircraft or family of aircraft being

represented.

• A gyroscopic rate-of-turn indicator or

equivalent with appropriate markings for

Yes Images of simulated instruments and indicators are displayed in the TouchTrainer System Description provided with this document.



a rate of 3 degrees per second turn for left

and right turns. If a turn and bank

indicator is used, the 3 degrees per second

rate index must be inside of the maximum

deflection of the indicator.

• A slip and skid indicator with coordination

information displayed in the conventional

skid ball format where a coordinated

flight condition is indicated with the ball

in the center position. A split image

triangle indication may be used if

applicable to the aircraft or family of

aircraft being represented.

• An attitude indicator with incremental

markings each 5 degrees of pitch or less,

from 20 degree pitch up to 40 degree

pitch down or as applicable to the aircraft

or family of aircraft represented. Bank

angles must be identified at “wings level” and at 10, 20, 30, and 60 degrees of bank

(with an optional additional identification

at 45 degrees) in left and right banks.

• Engine instruments as applicable to the

aircraft or family of aircraft being

represented, providing markings for

normal ranges and minimum and

maximum limits.

• A suction gauge or instrument pressure

gauge, as applicable, with a display

applicable to the aircraft or family of

aircraft represented.

• A flap setting indicator that displays the

current flap setting. Setting indications

should be typical of that found in an

actual aircraft.

• A pitch trim indicator with a display that

shows zero trim and appropriate indices

of airplane nose down and airplane nose

up trim, as would be found in an aircraft.

• Communication radio(s) with display(s) of

the radio frequency in use.

• Navigation radio(s) capable of replicating

both precision and non-precision



instrument, including approach procedures (each with an aural identification feature), and a marker

beacon receiver. For example, an ILS,

non-directional radio beacon (NDB),

Global Positioning System (GPS),

Localizer (LOC) or Very high frequency

Omnidirectional Range (VOR).

Graduated markings as indicated below

must be present on each indication as

applicable. The marking should include:

o One-half dot or less for course/glide

slope deviation (i.e., VOR, LOC, or ILS),

o 5 degrees or less for bearing deviation

for automatic direction finder (ADF) and radio magnetic indicator (RMI), as applicable,

o A clock with incremental markings for

each minute and second, or a timer with a display of minutes and

seconds,

o A magnetic compass with incremental

markings each 10 degrees or less; The compass must display the proper lead or lag during turns,

o A transponder panel that displays the

current transponder setting, and

o A fuel quantity indicator(s) that

displays the fuel remaining, either in analog or digital format, as appropriate for the aircraft or family of aircraft represented.

(2) All instrument displays listed above must be visible

during all flight operations. The update rate of all displays

must provide an image of the instrument that:

• Does not appear to be out of focus or

illegible,

• Does not appear to “jump” or “step” to a

distracting degree during operation, and

• Does not appear with distracting jagged lines

Yes



or edges.

(3) Display update must be at a frequency of 10 hertz (Hz)

or higher. Each display must sense a change and react at a

value less than the stated. Display updates must display all

changes (within the total range of the replicated

instrument) that are equal to or greater than the values

stated below:

• Airspeed indicator: change of 5 knots,

• Attitude indicator: change of 2 degrees in

pitch and bank, • Altimeter: change of 10 feet,

• Turn and bank: change of ¼ standard rate

turn,

• Heading indicator: change of 2 degrees,

• Vertical speed indicator (VSI): change of 100

fpm,

• Tachometer: change of 25 rpm or 2 percent of

turbine speed

• VOR/ILS: change of 1 degree for VOR or ¼

of 1 degree for ILS,

• ADF: change of 2 degrees, • GPS: change as appropriate for the model of

GPS navigator represented Clock or timer: change of 1 second

Yes Display update frequency is at least 15Hz

(4) Displays must reflect dynamic behavior of an actual aircraft display (e.g., a VSI reading of 500 fpm must

reflect a corresponding movement in altimeter, and an

increase in power must reflect an increase in rpm

indication or power indicator).

Yes

8.e Flight Dynamics

(1) Flight dynamics of the ATD should be comparable to the way the represented training aircraft performs and

handles. However, there is no requirement for an ATD to

have control loading to exactly replicate any particular

aircraft. An air data-handling package is not required for

determination of forces to simulate during the

manufacturing process.

Yes “TouchTrainer” provides an accurate representation of the aircraft flight characteristics for basic and instrument training.

(2) Aircraft performance parameters (such as maximum speed, cruise speed, stall speed, maximum climb rate, hovering/sideward/forward/rearward flight) should be

comparable to the aircraft or family of aircraft being

represented.

Yes

(3) Aircraft vertical lift component must change as a

function of bank, comparable to the way the aircraft or

Yes



family of aircraft being represented performs and handles.

(4) Changes in flap setting, slat setting, gear position,

collective control or cyclic control must be accompanied

by changes in flight dynamics, comparable to the way the

aircraft or family of aircraft represented performs and handles.

Yes

(5) The presence and intensity of wind and turbulence

must be reflected in the handling and performance

qualities of the simulated aircraft and should be comparable to the way the aircraft or family of aircraft represented performs and handles.

Yes

8.f Instructional Management Requirements

(1) The instructor must be able to pause/freeze the system

at any point for the purpose of administering instruction

regarding the task.

Yes Details of instructor’s controls can be found above

(2) If a training session begins with the “aircraft in the air”

and ready for the performance of a particular procedural

task, the instructor must be able to manipulate the following system parameters independently of the

simulation:

• Aircraft geographic location,

• Aircraft heading,

• Aircraft airspeed,

• Aircraft altitude, and • Wind direction, speed, and turbulence.

Yes

(3) The system must be capable of recording both a

horizontal and vertical track of aircraft movement for later

playback and review.

Yes

(4) The instructor must be able to disable any of the

instruments prior to or during a training session, and be

able to simulate failure of any of the instruments without

stopping or freezing the simulation to affect the failure.

Yes

(5) The ATD must have at least a navigational area

database that is local to the training facility to allow

reinforcement of procedures learned during actual flight in

that area. All navigational data must be based on

procedures as published per 14 CFR part 97.

Yes



4 COMPATIBILITY STATEMENT FOR SOFTWARE AND HARDWARE COMPONENTS.

TouchTrainer Software: “This is to certify that FTS has

demonstrated that the operating system and/or functional

kernel(s) X-Plane V10.5, SimAVIO v2.9 and Windows

Operating System, is fully compatible with the FTS TouchTrainer and can assure that the

communications/transport data latency is not greater than 300

milliseconds all analog and digital input signals meet the

performance criteria established for software performance by

FTS.”

Yes Refer to Software Compatibility Statement enclosed



Aircraft Configurations and Software Compatibility Statement The TouchTrainer simulates the aircraft and equipment detailed below.

Manufacturer Type Avionics Fit

Cirrus SR 20 G1 SR 22 G1

Analog instrumentation with Avidyne Version 7 MFD, 2 * GNS 430W GPS units, STEC 55X, Garmin GMA 327 Transponder and Garmin GMA 347 Communications Control unit

SR 20 G2 SR 22 G2 SR 22 G2(TN)

Avidyne Electronic Flight Deck Version 7 PFD and MFD, 2 * GNS 430W GPS units, STEC 55X, Garmin GMA 327 Transponder and Garmin GMA 347 Communications Control unit. Optional DFC 90 autopilot

SR 20 G3 SR 22 G3 SR 22 G3(TN) SR 22 G3(T) SR 22T G5

Garmin Perspective PFD and MFD, Electronic Flight Deck with GCU 478 (MFD FMS) Controls and GFC 700 autopilot. Optional STEC 55x autopilot.

Cessna C172SP C172 RG

Analog instrumentation, GNS 430W GPS unit, KX 155 NavCom, STEC 55X, Garmin GMA 327 Transponder and Garmin GMA 347 Communications Control unit, 2 * OBI

C182 C182-RG C182T-RG

Analog instrumentation, GNS 430W GPS unit, KX 155 NavCom, STEC 55X, Garmin GMA 327 Transponder and Garmin GMA 347 Communications Control unit, 1 * OBI and HIS

C172 Nav III C172 Nav III RG C182 Nav III C182 Nav III RG

Garmin Nav III G1000 and GFC 700 autopilot for Cessna

C206 Nav III RG Garmin Nav III G1000 and GFC 700 autopilot for Cessna

C350 Garmin Nav III G1000 and GFC 700 autopilot for Cessna Corvallis

C400 Garmin Nav III G1000 and GFC 700 autopilot for Cessna Corvallis

C350 Avidyne Electronic Flight Deck Version 7 PFD and MFD, 2 * GNS 430W GPS units, STEC 55X, Garmin GMA 327 Transponder and Garmin GMA 347 Communications Control unit.

C400 Avidyne Electronic Flight Deck Version 7 PFD and MFD, 2 * GNS 430W GPS units, STEC 55X, Garmin GMA 327 Transponder and Garmin GMA 347 Communications Control unit.

Diamond DA 20 Analog instrumentation, GNS 430W GPS unit, KX 155 NavCom, STEC 55X, Garmin GMA 327 Transponder and Garmin GMA 347 Communications Control unit, 1 * OBI

DA 40 DA 42

Garmin G1000 and GFC 700 autopilot for Diamond

Beech Bonanza Analog Instrumentation KFC 200 Autopilot, GNS 430W, GNS 530W, GMA 327 Transponder

Bonanza Garmin G500 Flight Deck and Analog Instrumentation KFC 200 Autopilot, GNS 430W, GNS 530W, GMA 327 Transponder

Bonanza Garmin G1000 Flight Deck, GFC 700 Autopilot for Beech Bonanza

Baron Analog Instrumentation KFC 200 Autopilot, GNS 430W, GNS 530W, GMA 327 Transponder



Baron Analog Instrumentation KFC 200 Autopilot, GNS 530W, KX 155, GMA 327 Transponder

Baron G500 Instrumentation KFC 200 Autopilot GNS 430W, GNS 530W, GMA 327 Transponder

Baron Garmin G1000 Flight Deck, GFC 700 Autopilot for Beech Baron Manufacturer Type Avionics Fit

Piper Warrior Analog instrumentation, GNS 530W, GNS 430W GPS unit, Piper III, Garmin GMA 327 Transponder and Garmin GMA 347 Communications Control unit, 2 * OBI

Arrow Analog instrumentation, GNS 530W, GNS 430W GPS unit, KX 155, Piper III, Garmin GMA 327 Transponder and Garmin GMA 347 Communications Control unit, 2 * OBI

Malibu Analog instrumentation, GNS 530W, GNS 430W GPS unit, STEC 55X, KX 155, Garmin GMA 327 Transponder and Garmin GMA 347 Communications Control unit, 2 * OBI

Cherokee Garmin G500, GNS530W, KX155, Piper IIIB and STEC 55X autopilot, Garmin GMA 327 Transponder and Garmin GMA 347 Communications Control unit, 1 * OBI

Meridian Garmin G1000 and GFC 700 autopilot for Piper Meridian

Seneca Analog Instrumentation, Aspen PFD, GNS530W, KX155, Piper IIIB and STEC 55X autopilot, Garmin GMA 327 Transponder and Garmin GMA 347 Communications Control unit, 1 * OBI

Saratoga Garmin G1000 and GFC 700 autopilot for Piper Saratoga, Avidyne, 2* Garmin GNS 430, STEC 55x, Garmin GMA 327 Transponder and Garmin GMA 347 Communications Control unit, 1 * OBI

Rockwell Commander

114/112 Garmin G500, STEC 55x GNS 530, KX 155, Garmin GMA 327 Transponder and Garmin GMA 347 Communications Control unit, 1 * OBI



TouchTrainer Instrument Panel Configurations Each main instrument and secondary instrument panel available shown below.

Cirrus Aircraft

Cirrus Performance and CG

Aircraft Altitude (STP) ft

Max TO Weight lbs

Vne KIAS

100% Power KTAS

Stall (Vs KIAS) Vy ft/min

Cirrus SR 20 G1/2/3 SL 3000 201 162 61 750

5000 155 500

Cirrus SR 22 G1/2/3/5

SL 3400 201 186 65 1300

5000 180 900

Cirrus SR 22 TN/T G3/5

SL 3400 201 186 65 1300

5000 190 1300

Cirrus SR 20



Cirrus SR 22

Cirrus SR 22(T)





Cirrus SR 20/22/22TN Avidyne and 2 * GNS 430W



Cirrus SR 20/22 G1 Analog with 2* GNS 430W



Cessna

Cessna Performance and GC

Aircraft Altitude (STP) ft Max TO Weight lbs Vne KIAS

100% Power KTAS

Stall (Vs KIAS)

Vy ft/min

Cessna 172 SP SL 2550 161 128 51 750

5000 126 700

Cessna 182 SL 3100 188 150 49 1050

5000 148 800

Cessna T182 SL 3100 188 148 49 1000

5000 150 1000

Cessna T206H SL 3600 180 145 56 1100

5000 147 1100

Cessna 172SP



Cessna 182

Cessna 206



Cessna 172 SP



Cessna 172 S RG



Cessna 182, 182T, 182T RG (Cessna 182 T RG shown)



Cessna 172 NAV III



Cessna 172 RG NAV III









Diamond

Diamond Performance and CG


100% Power KTAS

Stall (Vs KIAS)

Vy ft/min

DA 20 SL 1770 164 130 44 800

5000 127 650

DA 40 SL 2535 178 143 52 900

5000 135 600

DA 42 SL 3935 194 164 57 2000

5000 167 1550

DA 20

Diamond DA 40

Diamond



Diamond DA 42

Diamond DA 20

Diamond DA 20



Diamond DA40 G1000

Diamond DA42 G1000





Cessna 350/400 (Corvalis)

Cessna 350/400 Performance and CG


100% Power KTAS

Stall (Vs KIAS)

Vy ft/min

C350 SL 3600 230 182 60 1285

5000 175 1000

C400 SL 3600 230 182 60 1285

5000 193 1285

Cessna 350



Cessna 400

Cessna 350 and 400 Avidyne



Cessna 350/400 G1000

Cessna 350/400 G1000



Beech Aircraft

Performance and CG


Max TO Weight lbs

Vne KIAS

100% Power KTAS

Stall (Vs KIAS)

Vy ft/min

Bonanza A36

SL 3600 204 168 62 1050

5000 165 750

Baron G36

SL 5500 223 188 (24.5”/2500) 83 1600

5000 203(24.5”/2500) 1300

A36 Beech Bonanza



G58 Beech Baron



Beech Bonanza: Analog Instrumentation KFC 200 Autopilot

A36 Bonanza



Beech Bonanza: G500/KFC 200 Autopilot



Beech Baron: Analog Instrumentation KFC 200 Autopilot



Beech Baron: Analog Instrumentation KFC 200 Autopilot



Beech Baron: G500 Instrumentation KFC 200 Autopilot



Beech Baron: G1000, GFC 700 Autopilot



Piper Aircraft

Piper Performance and CG


100% Power KTAS

Stall (Vs KIAS)

Vy ft/min

Archer PA-28-181 0 2550 154 134 45 680

5000 131 460

Arrow PA-28R-200 0 2650 186 175 56 900

5000 172 630

Warrior PA28-161 0 2440 160 126 44 650

5000 400

Seneca PA 0 4200 204 182 66 1350

5000 178 1100


Max TO Weight lbs

Vne KIAS

100% Power KTAS

Stall (Vs KIAS)

Vy ft/min

PA 46-500 TP Meridian

0 5092 187 183 79 1500

18000 241 1000

PA 32 R 301 Saratoga 0 3600 191 158 67 1057

5000 152 850

PA 46 350 P Malibu 4340 203 165 72 1900

178 1700



Piper Archer

Piper Arrow



Piper Warrior

Piper Seneca



Piper Meridian

Piper Saratoga



Piper Malibu



Piper Arrow Analog GNS530W Piper III Autopilot



Piper Cherokee G500, GNS530W and Piper IIB Autopilot

Piper Meridian G1000

Piper Seneca Analog 530 Piper IIIB Autopilot



Piper Warrior Analog GNS530W Piper III Autopilot



Piper Malibu



Piper Saratoga Avidyne



Rockwell Commander 112 and 114

Rockwell Commander Performance and CG


100% Power KTAS

Stall (Vs KIAS)

Vy ft/min

Commander 112 SL 2650 180 135 61 1020

5000 129 500

Commander 114 SL 3140 187 156 61 1200

5000 149 700

Commander 112

Commander 114 TC



Rockwell Commander

Rockwell Commander 112

Rockwell Commander 114 G500



Visual System The TouchTrainer can be provided with one of three visual systems. All visual systems are

day/dusk/night compatible and capable of simulating multiple weather conditions both VFR and VFR.

Update rates are fast and consistent providing the effect of smooth movement of the simulated aircraft.

1. Standard. The Standard TouchTrainer visual system shares its display with the TouchTrainer

instrument display system taking approximately 30% of the area of the display. The standard

visual system requires no special hardware.

The Standard Visual System



2. VisX. The Vis X system is displayed on 3 special purpose monitors mounted above the main

instrumentation touchscreen. This enables both touchscreens to be dedicated to

instrumentation and a wide visual system to be displayed on three dedicated monitors.

The TouchTrainer fitted with the VisX Visual System



3. Visual Motion 100 and 210. The Visual Motion system is displayed on 3 large special

purpose monitors mounted behind the TouchTrainer. This enables both touchscreens to be

dedicated to instrumentation and a very large visual system to be displayed on three dedicated

monitors.

The TouchTrainer fitted with the ‘Visual Motion 100’ visual system

The TouchTrainer fitted with the ‘Visual Motion 210’ visual system



3. Functions and Maneuvers Checklist



Functions and Maneuvers Yes, No, or N/A

a. Preparation for Flight (1) Preflight Yes

b. Pre-Takeoff (1) Engine start Yes

(2) Brake operation Yes

c. Takeoff (1) AIRPLANE Takeoff Yes

(i) Power plant checks Yes

(ii) Acceleration characteristics Yes

(iii) Nose wheel and rudder steering Yes

(iv) Effect of crosswind Yes

(v) Instrument Yes

(vi) Landing gear, wing flap operation Yes

(2) HELICOPTER Takeoff

(i) Power plant checks N/A

(ii) From Hover N/A

(iii) From Ground N/A

(iv) Vertical N/A

(v) Running N/A

d. In-Flight Operation (1) AIRPLANE In-flight Operation

(i) Climb Yes

(a) Normal Yes

(b) One engine inoperative procedures Yes

(ii) Cruise (a) Performance Characteristics (speed vs. power) Yes

(b) Normal & Steep Turns Yes

(c) Performance Turns Yes

(d) Approach to Stalls, i.e. stall warning Cruise, Takeoff & Approach and Landing Configurations

Yes

(e) High Angle of Attack Maneuvers Cruise, Takeoff & Approach and Landing Configurations

Yes

(f) In Flight engine Shutdown Yes

(g) In Flight engine Start Yes

Functions and Maneuvers Check or N/A

(2) HELICOPTER In Flight Operation (i) Hovering N/A

(a) Forward N/A

(b) Rearward N/A

(c) Sideward N/A

(d) Turns N/A

(ii) Climb N/A

(iii) Cruise N/A

(a) Performance Characteristics N/A

(b) Turns N/A

(i) Recovery N/A

(ii) Skidding N/A



(iii) Slipping N/A

(c) In Flight Engine Shutdown N/A

(d) In Flight Engine Start N/A

(iv) Decent N/A

e. Approaches

(1) Non-Precision Yes

(i) GPS and LPV Yes

(i) GPS- WAAS (optional) Yes

(ii) GPS- LAAS (optional) Yes

(iii) All Engines Operating Yes

(iv) One or More Engines Inoperative Yes

(v) Approach Procedures ( NDB, VOR, DME Arc, LOC/BC, LOC, LDA, SDF, ASR, LNAV/VNAV)

Yes

(2) Precision Yes

(i) ILS Yes

(ii) GLS Yes

(iii) Effects of Crosswind Yes

(iv) With engine(s) inoperative Yes

(v) Missed Approach Yes

(A) Normal Yes

(B) With Engine(s) inoperative Yes

(C) From Steep Glide Slope Yes

f. Surface Operations (AIRPLANE-Post Landing)

(1) Landing roll Yes

(2) Braking Operation Yes

(3) Reverse thrust Operation, if applicable Yes

g. Any Flight Phase

(1) Aircraft and Power Plant Systems Yes

(i) Electrical Yes

(ii) Flaps (Airplane) Yes

(iii) Fuel & Oil Yes

(iv) Landing Gear(Airplane) Yes

(2) Flight Management and Guidance Systems (i) Auto Pilot (AATD only) Yes

(ii) Flight Director (AATD only) / System Displays Yes

(iii) Navigation Systems Yes

Functions and Maneuvers Check or N/A

(iv) Stall Warning Avoidance (Airplane) Yes

(v) Multi-Function Displays Yes

(3) Airborne Procedures (i) Holding Yes

(4) Engine Shutdown and Parking (i) Systems operation Yes

(ii) Parking Brake Operation (Airplane) Yes

h. Replicate any emergency procedure checklist action items published in the Aircraft Flight Manual

Yes



Any changes or modifications to this device which have not been reviewed, evaluated, and approved in

writing by General Aviation and Commercial Division, AFS-800 may terminate FAA approval of this

aviation training device.

Documents

Qualification and Approval Guide (QAG) for the FlyThisSim ......2016/03/30 · Enhanced electrical modeling of aircraft busses ensuring electrical and avionics systems integrate as