Basic Aviation Training Device

Transcription

1 FLYIT SIMULATORS, Inc. Basic Aviation Training Device Model PHS - 1 FLYIT Simulators Inc. 5931Sea Lion Pl #110 Carlsbad, CA USA Revised on 10/30/2014 Page 1 of 53

2 Device Description and Overview Table of Contents Model: PHS OPTION OPTION COMPUTER:... 6 AVIONICS:... 7 VISUAL SYSTEM:... 7 INSTRUCTOR OPERATING STATION (IOS):... 7 SOUND:... 7 SOFTWARE:... 8 FLIGHT CONFIGURATIONS INCLUDED IN THIS ATD... 8 POWER REQUIREMENT... 8 INSTRUCTOR OPERATING STATION MENU OVERVIEW FLIGHTS MENU LOAD FLIGHTS MENU FUEL AND PAYLOAD SYSTEM FAILURES TIME AND SEASON AIRPORTS MAP WEATHER ADVANCED WEATHER (CLOUDS) ADVANCED WEATHER (WIND) ADVANCED WEATHER (TEMP/PRESSURE) ADVANCED WEATHER (VISIBILITY) OPTIONS FLIGHT ANALYSIS INSTRUCTOR MAP SCREEN CONFIGURATION COCKPIT PHOTOS AIRCRAFT CONFIGURATION 1: BELL AIRCRAFT CONFIGURATION 2: SCHWEIZER Revised on 10/30/2014 Page 2 of 53

3 Device Description and Overview AIRCRAFT CONFIGURATION 3: HUGHS MD AIRCRAFT CONFIGURATION 4: R AIRCRAFT CONFIGURATION 5: R BATD DESIGN CRITERIA CONTROLS CONTROL REQUIREMENTS CONTROL INPUTS DISPLAY REQUIREMENTS FLIGHT DYNAMICS REQUIREMENTS INSTRUCTIONAL MANAGEMENT REQUIREMENTS TASK REQUIREMENTS LIST BASIC AVIATION TRAINING DEVICE CHECKLIST Revised on 10/30/2014 Page 3 of 53

4 Device Description and Overview NOTE: THIS QUALIFICATION and APPROVAL GUIDE CONTAINS: THE BATD APPROVAL CRITERIA AS DEFINED IN AC APPENDIX 2 Revised on 10/30/2014 Page 4 of 53

5 DEVICE DESCRIPTION AND OVERVIEW DETAILED DEVICE DESCRIPTION AND OVERVUE Revised on 10/30/2014 Page 5 of 53

6 DEVICE DESCRIPTION AND OVERVIEW Model: PHS-1 SN: N9301H N9333H Microsoft Flight Simulator 2002 Rear projected front view screen Monitor in cockpit for gauges Bendix/King Silver Crown radios Instructor desk with cockpit and front screen view monitors (2) and printer FLYIT HELICOPTER ATD SPECIFICATIONS: OPTION 1 Installed in the FLYIT 18 trailer/classroom (Ships completely assembled, plug and fly) When transported, no configuration changes are possible and unit is self-checked at startup OPTION 2 Installed in a room 19 x 11 (Cockpit ships completely assembled) INCLUDES: -Complete full size cockpit with dual controls -Interchangeable Robinson cyclic and standard cyclic -Pitch and roll trim on cyclic -Standard collective with twist throttle -Anti torque pedals (adjustable) -Center console with COM/Nav radios, system switches, aircraft lighting, pause and reset (lighted) -CRT or LCD monitor displays flight and engine gages -Airframe vibration COMPUTER: -AMD Athlon processor, 20 GB state hard drive. 512MB Ram -Spare hard drive -Computer is aluminum case rack mounted in cockpit Revised on 10/30/2014 Page 6 of 53

7 DEVICE DESCRIPTION AND OVERVIEW AVIONICS: Nav/Com 1 Bendix /King Silver Crown Nav/Com 2 Bendix /King Silver Crown (VOR, LOC, G/S) dual ADF DME Transponder mode C -HSI ON APPROPRIATE MODELS (all avionics are simulated but are sized and perform like the actual units) VISUAL SYSTEM: -1-XGA high resolution 1024x768 LCD projector, 78 X93 with rear projection screen and spare bulb Pilot sees ground across pilot s feet (Ground Reference Out the Window View) INSTRUCTOR OPERATING STATION (IOS): SOUND: Two monitors, inkjet printer (prints flight path) -Wireless keyboard & mouse -Displays all information -Select any meteorological conditions -Reposition aircraft, select aircraft, location/set up, save flights, failures, training scenarios, and student review -5 speaker subwoofer sound system built into cockpit System and environmental sound Revised on 10/30/2014 Page 7 of 53

8 DEVICE DESCRIPTION AND OVERVIEW SOFTWARE: Microsoft Flight Simulator 2002, with 22,000 airport Whole world is simulated Primary and back up hard drives contain operating system and simulation FLIGHT CONFIGURATIONS INCLUDED IN THIS ATD -This ATD includes Five FLYIT programmed helicopter flight configurations: -Piston Robinson R22, R44, Schweizer 300, -Turbine MD 500, Bell 206 POWER REQUIREMENT 110V is standard 220 on Request Revised on 10/30/2014 Page 8 of 53

9 DEVICE DESCRIPTION AND OVERVIEW CENTER CONSOLE ( TOP KNOBS CONTROL FLIGHT INSTRUMENTS) Revised on 10/30/2014 Page 9 of 53

10 DEVICE DESCRIPTION AND OVERVIEW COLLECTIVE SWITCH BOX Revised on 10/30/2014 Page 10 of 53

11 DEVICE DESCRIPTION AND OVERVIEW INSTRUCTOR OPERATING STATION MENU OVERVIEW Pressing the ALT key on the keyboard will bring up the Main Menu bar at the top of the screen on the out the window view. (Figure 2.10) Within this menu are many options that will allow you to manipulate the settings of the simulator. Carefully read the following descriptions of each menu section to familiarize you with the various settings. Incorrectly setting an option may render the simulator inoperative. Revised on 10/30/2014 Page 11 of 53

12 DEVICE DESCRIPTION AND OVERVIEW FLIGHTS MENU Revised on 10/30/2014 Page 12 of 53

13 DEVICE DESCRIPTION AND OVERVIEW LOAD FLIGHTS MENU FIGURE 2.21 Revised on 10/30/2014 Page 13 of 53

14 DEVICE DESCRIPTION AND OVERVIEW FUEL AND PAYLOAD Revised on 10/30/2014 Page 14 of 53

15 DEVICE DESCRIPTION AND OVERVIEW SYSTEM FAILURES Revised on 10/30/2014 Page 15 of 53

16 DEVICE DESCRIPTION AND OVERVIEW TIME AND SEASON Revised on 10/30/2014 Page 16 of 53

17 DEVICE DESCRIPTION AND OVERVIEW AIRPORTS Revised on 10/30/2014 Page 17 of 53

18 DEVICE DESCRIPTION AND OVERVIEW MAP Revised on 10/30/2014 Page 18 of 53

19 DEVICE DESCRIPTION AND OVERVIEW WEATHER Revised on 10/30/2014 Page 19 of 53

20 DEVICE DESCRIPTION AND OVERVIEW ADVANCED WEATHER (CLOUDS) window. Revised on 10/30/2014 Page 20 of 53

21 DEVICE DESCRIPTION AND OVERVIEW ADVANCED WEATHER (WIND) ADVANCED WEATHER (TEMP/PRESSURE) Revised on 10/30/2014 Page 21 of 53

22 DEVICE DESCRIPTION AND OVERVIEW ADVANCED WEATHER (VISIBILITY) OPTIONS Revised on 10/30/2014 Page 22 of 53

23 DEVICE DESCRIPTION AND OVERVIEW FLIGHT ANALYSIS Revised on 10/30/2014 Page 23 of 53

24 DEVICE DESCRIPTION AND OVERVIEW INSTRUCTOR MAP SCREEN Revised on 10/30/2014 Page 24 of 53

25 DEVICE DESCRIPTION AND OVERVIEW CONFIGURATION COCKPIT PHOTOS The following configurations are selectable from the IOS (Instructor Operating Station) also called The ICC (Instructor Command Center). The configurations can be flown VFR or IFR even though the configurations are labeled IFR, although lacking GPS capability Revised on 10/30/2014 Page 25 of 53

26 DEVICE DESCRIPTION AND OVERVIEW AIRCRAFT CONFIGURATION 1: BELL 206 INSTRUMENT PANEL CYCLIC CONTROL CENTER CONSOLE Revised on 10/30/2014 Page 26 of 53

27 DEVICE DESCRIPTION AND OVERVIEW AIRCRAFT CONFIGURATION 2: SCHWEIZER 300 INSTRUMENT PANEL CYCLIC CONTROL CENTER CONSOLE Revised on 10/30/2014 Page 27 of 53

28 C Y C L I C DEVICE DESCRIPTION AND OVERVIEW AIRCRAFT CONFIGURATION 3: HUGHS MD 500 C O N T R O L C E N T E R C O N S O L E INSTRUMENT PANEL CYCLIC CONTROL CENTER CONSOLE Revised on 10/30/2014 Page 28 of 53

29 AIRCRAFT CONFIGURATION 4: R22 DEVICE DESCRIPTION AND OVERVIEW INSTRUMENT PANEL CYCLIC CONTROL CENTER CONSOLE Revised on 10/30/2014 Page 29 of 53

30 AIRCRAFT CONFIGURATION 5: R44 DEVICE DESCRIPTION AND OVERVIEW INSTRUMENT PANEL CYCLIC CONTROL CENTER CONSOLE Revised on 10/30/2014 Page 30 of 53

31 BATD DESIGN CRITERIA BATD DESIGN CRITERIA CONTROLS The FAA requirements are listed in black followed by the compliance information for this FLYIT ATD listed in blue print. The QAG is the primary means for finding a BATD acceptable for use in part 61 pilot training or approved part 141 pilot school training curricula. The QAG will be used to determine that an ATD meets or exceeds minimum FAA design criteria outlined in this appendix. A BATD found acceptable for use IAW this appendix will typically be limited to training procedural tasks only. However, they may also be used to meet instrument experience requirements when specifically authorized. Each QAG submitted to the FAA for evaluation must state the make and model of aircraft or family of aircraft being represented and used as the basis for the following criteria: CONTROLS. a. A BATD must provide certain physical controls and may provide some virtual 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. (1). This BATD has a complete full size cockpit with switches like actual aircraft in their normal locations and dual controls with -interchangeable Robinson cyclic and standard cyclic Revised on 10/30/2014 Page 31 of 53

32 BATD DESIGN CRITERIA CONTROLS (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. (2) Instructor Operating Station (IOS) allows for virtual control, allowing the instructor to control aspects of the simulation (such as setting aircraft configuration, location, and weather) and to program, pause, or freeze the device. (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. (3) Except for setup and/or fault mode entry, neither the keyboard nor the mouse are used to set or position any feature of the BATD in the represented aircraft for the maneuvers or flight training to be accomplished.. The pilot must operate the additional equipment needed in order to accomplish a training procedure as listed as listed here in the same manner in which it would be operated in the represented aircraft. For example carburetor heat control, and mixture, and throttle controls. (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: a. Master/battery; b. Magnetos for each engine (as applicable); Revised on 10/30/2014 Page 32 of 53

33 c. Alternators for each engine; BATD DESIGN CRITERIA CONTROLS d. Fuel boost pumps for each engine; e. Avionics master; f. Pitot heat; and g. Rotating beacon/strobe, navigation, taxi, and landing lights. (4) The physical arrangement, appearance, and operation of controls, instruments, and switches required by this appendix model the aircraft represented as closely as practicable. Configurations included are: Piston Robinson R22, R44, Schweizer 300. Turbine MD 500, Bell 206. All configurations include: a. Master/battery; b. Magnetos for each engine (as applicable); c. Alternators for each engine; d. Fuel boost pumps for each engine; e. Avionics master; f. Pitot heat; and g. Rotating beacon/strobe, navigation, taxi, and landing lights. (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. (5)The only software that can be used in this FLYIT simulator is that which is loaded automatically at turn-on at the IOS and is self-checked at startup. Revised on 10/30/2014 Page 33 of 53

34 CONTROL REQUIREMENTS. Helicopter. BATD DESIGN CRITERIA Control Requirements (a) A cyclic control stick that tilts the main rotor disk by changing the pitch angle of the rotor blades in their cycle of rotation; (b) A collective pitch control that changes the pitch angle of all main rotor blades simultaneously; (c) Throttle/power control that allows continuous movement from idle to full power setting (d) Anti-torque pedals that allow continuous adjustment of the tail rotor heading (e) Mixture/ condition control applicable to all configurations included (f) Controls included for each of the helicopter configurations included Communication and Nav radios Clock and timer Transponder Sensitive adjustable altimeter Microphone with push to talk Carburetor heat for appropriate configurations Revised on 10/30/2014 Page 34 of 53

35 BATD DESIGN CRITERIA Control Requirements Physical flight and aircraft system controls are provided as follows: This ATD has a complete full size cockpit with dual controls with interchangeable Robinson cyclic and standard cyclic. a. A cyclic control stick that tilts the main rotor disk by changing the pitch angle of the rotor blades in their cycle of rotation; b. A collective pitch control that changes the pitch angle of all main rotor blades simultaneously; c. Throttle/power control that allows continuous movement from idle to full power setting d. Anti-torque pedals that allow continuous adjustment of the tail rotor heading e. Mixture/ condition control applicable to all configurations included f. Controls included for each of the helicopter configurations included Communication and Nav radios Clock and timer Transponder Sensitive adjustable altimeter Microphone with push to talk Carburetor heat for appropriate configurations Cowl flaps on appropriate helicopters Revised on 10/30/2014 Page 35 of 53

36 BATD DESIGN CRITERIA Control Inputs 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. (1) This is to certify that Microsoft Corp., the owner and developer of the FS 2002 Simulator Engine, has evaluated that their software application works with industry standard PC's and USB flight control devices. FLYIT Simulators Inc. utilizes Industry standard USB flight control devices for all pilot input. All input control devices meet the USB 1.0 industry standard specified interfaces. FLYIT SIMULATORS, INC.., the component integrator, has determined that the transport delay time is less than 300 milliseconds, and that all analog and digital input signals meet the performance criteria established for the software." Revised on 10/30/2014 Page 36 of 53

37 BATD DESIGN CRITERIA Control Inputs (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 Requirements in paragraph d below. ((2) The control inputs are automatically 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 computer system has push to talk screen to initiate self-tests s e e Fig. 1. Press either Push To Talk Button to Perform Self-Test If this screen does not go away, perform simulator shutdown procedure and restart Fig 1. Self-Test Screen. After self-test is complete a screen shot appears. See Fig 2. Self-Test Complete If this current session will be used for instrument/currency requirements required by 14CFR part 61.57(c), the visual component during instrument approaches must be configured to Instrument Meteorological Conditions [IMC] until reaching Decision Height [DH], Decision Altitude [DA], or Minimum Descent Altitude [MDA as appropriate. Additionally, all instruments and equipment required for visual and instrument flight rules listed in part must be functional Press either Push To Talk to continue Fig 2. Push to talk to continue after acknowledgement of self-test Revised on 10/30/2014 Page 37 of 53

38 DISPLAY REQUIREMENTS. BATD DESIGN CRITERIA 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 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. Revised on 10/30/2014 Page 38 of 53

39 BATD DESIGN CRITERIA Display Requirements 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 nonprecision instrument, including approach procedures (each with an aural identification feature), and a marker beacon receiver. For example, an ILS, non-directional radio beacon (NDB), 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: One-half dot or less for course/glide slope deviation (i.e., VOR, LOC, or ILS), 5 degrees or less for bearing deviation for automatic direction finder (ADF) and radio magnetic indicator (RMI), as applicable, Revised on 10/30/2014 Page 39 of 53

40 BATD DESIGN CRITERIA Display Requirements A clock with incremental markings for each minute and second, or a timer with a display of minutes and seconds, A magnetic compass with incremental markings each 10 degrees or less; The compass must display the proper lead or lag during turns, A transponder panel that displays the current transponder setting, and 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. (1) This FLYIT ATD includes the following 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. Revised on 10/30/2014 Page 40 of 53

41 BATD DESIGN CRITERIA Display Requirements A gyroscopic rate-of-turn indicator with appropriate markings for a rate of 3 degrees per second turn for left and right turns. When a turn and bank indicator is used, the 3 degrees per second rate index is 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. 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 are 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. Revised on 10/30/2014 Page 41 of 53

42 BATD DESIGN CRITERIA Display Requirements Navigation radio(s) capable of replicating both precision and nonprecision instrument, including approach procedures (each with an aural identification feature), and a marker beacon receiver. For example, an ILS, non-directional radio beacon (NDB Localizer (LOC) or Very high frequency Omnidirectional Range (VOR). Graduated markings as indicated below are present on each indication as applicable. The marking include: One-half dot or less for course/glide slope deviation (i.e., VOR, LOC, or ILS), 5 degrees or less for bearing deviation for automatic direction finder (ADF) and radio magnetic indicator (RMI), as applicable, A clock with incremental markings for each minute and second, or a timer with a display of minutes and seconds, A magnetic compass with incremental markings each 10 degrees or less; The compass must display the proper lead or lag during turns, A transponder panel that displays the current transponder setting, and 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. Revised on 10/30/2014 Page 42 of 53

43 BATD DESIGN CRITERIA Display Requirements (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 or edges (2) All instrument displays listed above are visible during all flight operations The clarity of instruments displayed is of very high quality using flat panel LCD displays. All instruments are focused and do not jump or step and are not distracting The update rate of all displays provides an image of the instruments 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 or edges. Revised on 10/30/2014 Page 43 of 53

44 BATD DESIGN CRITERIA Display Requirements (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, Clock or timer: change of 1 second. Revised on 10/30/2014 Page 44 of 53

45 BATD DESIGN CRITERIA Display Requirements (3) All of the displays in the FLYIT simulator update at a frequency of 60 HZ or higher vs the 10HZ minimum. Display updates 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, Clock or timer: change of 1 second. (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 the rpm indication or power indicator). (4) Displays 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 the rpm indication or power indicator). Revised on 10/30/2014 Page 45 of 53

46 BATD DESIGN CRITERIA Flight Dynamics Requirements FLIGHT DYNAMICS REQUIREMENTS (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. (1) Flight dynamics of the ATD are comparable to the way the represented training aircraft perform and handle. This has been determined by expert pilots evaluating the handling qualities the flight models in this FLYIT ATD which has helicopter models very close to the actual helicopters through use of the Lockheed Prepar3D software (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 (2) Aircraft performance parameters (such as maximum speed, cruise speed, stall speed, maximum climb rate, hovering/sideward/forward/rearward flight) are comparable to the aircraft or family of aircraft being represented (3) Aircraft vertical lift component must change as a function of bank, comparable to the way the aircraft or family of aircraft being represented performs and handles. (3) Aircraft vertical lift component changes as a function of bank, comparable to the way the aircraft or family of aircraft being represented performs and handles. Revised on 10/30/2014 Page 46 of 53

47 BATD DESIGN CRITERIA Flight Dynamics Requirements (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. (4) Changes in, collective control or cyclic control are accompanied by changes in flight dynamics, comparable to the way the aircraft or family of aircraft represented performs and handles. (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. (5) The presence and intensity of wind and turbulence is reflected in the handling and performance qualities of the simulated aircraft and are comparable to the way the aircraft or family of aircraft represented performs and handles. Revised on 10/30/2014 Page 47 of 53

48 FUNCTION AND SUBJECTIVE TEST CRITERIA Instructional Management Requirements 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. (1) The instructor can pause/freeze the system at any point for the purpose of administering instruction regarding the task via the IOS or a button on the instrument panel if the instructor is in a pilot seat. (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. (2) If a training session begins with the aircraft in the air and ready for the performance of a particular procedural task, the instructor can manipulate the following system parameters independently of the simulation: Aircraft geographic location, Aircraft heading, Aircraft airspeed, Aircraft altitude, and Wind direction, speed, and turbulence (3) The system must be capable of recording both a horizontal and vertical track of the aircraft movement for later playback and review. (3) The system records both a horizontal and vertical track of aircraft movement for later playback. The system records both a horizontal and vertical track of aircraft movement for later playback and review and printout through the printer at the IOS (Instructor Operating Station.) Revised on 10/30/2014 Page 48 of 53

49 FUNCTION AND SUBJECTIVE TEST CRITERIA Instructional Management Requirements (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. (4) The instructor can disable any of the instruments s prior to or during a training session, and can simulate failure of any of the instruments without stopping or freezing the simulation to affect the failures. (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. (5) All navigational data are based on procedures as published per 14 CFR part 97. The FLYIT ATD contains the Jeppesen world wide database of more than 25,000 airports with ILS,ADF, and VOR approaches. Revised on 10/30/2014 Page 49 of 53

50 FUNCTION AND SUBJECTIVE TEST CRITERIA Task Requirements List TASK REQUIREMENTS LIST. An ATD having the features specified above may be approved for use in procedural training in the instrument flight tasks listed in this appendix. Revised on 10/30/2014 Page 50 of 53

51 FUNCTION AND SUBJECTIVE TEST CRITERIA BATD Checklist BASIC AVIATION TRAINING DEVICE CHECKLIST Functions and Maneuvers a. Preparation for Flight (1) Preflight b. Pre-Takeoff (1) Engine start NO (2) Brake operation Yes, No, or c. Takeoff (1) AIRPLANE Takeoff (i) Power plant checks (ii) Acceleration characteristics (iii) Nose wheel and rudder steering (iv) Effect of crosswind (v) Instrument (vi) Landing gear, wing flap operation (2) HELICOPTER Takeoff (i) Power plant checks (ii) From Hover (iii) From Ground (iv) Vertical (v) Running d. In-Flight Operation (1) AIRPLANE In-flight Operation (i) Climb (a) Normal (b) One engine inoperative procedures (ii) Cruise (a) Performance Characteristics (speed vs. power) (b) Normal & Steep Turns (c) Performance Turns (d) Approach to Stalls, i.e. stall warning Cruise, Takeoff & Approach and Landing Configurations (e) High Angle of Attack Maneuvers Cruise, Takeoff & Approach and Landing Configurations (f) In Flight engine Shutdown (g) In Flight engine Start Functions and Maneuvers (2) HELICOPTER In Flight Operation Check or Revised on 10/30/2014 Page 51 of 53

52 FUNCTION AND SUBJECTIVE TEST CRITERIA BATD Checklist (i) Hovering (a) Forward (b) Rearward (c) Sideward (d) Turns (ii) Climb (iii) Cruise (a) Performance Characteristics (b) Turns (i) Recovery (ii) Skidding (iii) Slipping (c) In Flight Engine Shutdown (d) In Flight Engine Start (iv) Decent NO e. Approaches (1) Non-Precision (i) GPS and LPV (ii) GPS- LAAS (optional) (iii) All Engines Operating (iv) One or More Engines Inoperative (v) Approach Procedures ( NDB, VOR, DME Arc, LOC/BC, LOC, LDA, SDF, ASR) (2) Precision (i) ILS (ii) GLS (iii) Effects of Crosswind (iv) With engine(s) inoperative (v) Missed Approach (A) Normal (B) With Engine(s) inoperative (C) From Steep Glide Slope f. Surface Operations (AIRPLANE-Post Landing) (1) Landing roll (2) Braking Operation (3) Reverse thrust Operation, if applicable g. Any Flight Phase (1) Aircraft and Power Plant Systems (i) Electrical (ii) Flaps (Airplane) (iii) Fuel & Oil Revised on 10/30/2014 Page 52 of 53

53 FUNCTION AND SUBJECTIVE TEST CRITERIA BATD Checklist (iv) Landing Gear(Airplane) (2) Flight Management and Guidance Systems (i) Auto Pilot (AATD only) (ii) Flight Director (AATD only) / System Displays (iii) Navigation Systems Functions and Maneuvers (iv) Stall Warning Avoidance (Airplane) (v) Multi-Function Displays (3) Airborne Procedures (i) Holding (4) Engine Shutdown and Parking (i) Systems operation (ii) Parking Brake Operation (Airplane) h. Replicate any emergency procedure checklist action items published in the Aircraft Flight Manual Check or Revised on 10/30/2014 Page 53 of 53