gaca_gov_sa · form · processed · 115 chunks
GACA العامه للطيران المدني General Authority of Civil Aviation [Non-Text] FLIGHT TRAINING DEVICE (FTD) QUALIFICATION TEST CHECKLIST GACAR PART - 60 <table><tr><td>• FTD Organization Name</td><td colspan="5"></td></tr><tr><td>• FTD Qualification Level</td><td>□ 4</td><td>□ 5</td><td>□ 6</td><td colspan="2">□ 7</td></tr><tr><td>• FTD Qualification Type</td><td>□ Initial Qualification</td><td>□ Qualification renewal</td><td>□ Modifications</td><td colspan="2">□ Re-location</td></tr><tr><td>• FTD Manufacturer Name</td><td></td><td></td><td></td><td colspan="2"></td></tr><tr><td>• FTD Serial No</td><td colspan="5"></td></tr><tr><td>• FTD Qualification Number</td><td colspan="5"></td></tr><tr><td>• FTD Qualification Expiry Date (dd/mm/yy)</td><td colspan="5"></td></tr></table> <table><tr><td colspan="4"></td><td colspan="2">Compliance</td></tr><tr><td>Entry Number</td><td>General FTD Requirements</td><td>FTD Level</td><td>Notes/Information</td><td>Yes</td><td>No</td></tr><tr><td>1.</td><td>General Flight deck Configuration.</td><td>See next</td><td>NA</td><td>□</td><td>□</td></tr><tr><td>1.a.</td><td>The FTD must have a flight deck that is a replica of the airplane simulated with controls, equipment, observable flight deck indicators, circuit breakers, and bulkheads properly located, functionally accurate and replicating the airplane. The direction of movement of controls and switches must be identical to that in the airplane. Pilot seat(s) must afford the capability for the occupant to be able to achieve the design “eye position.” Equipment for the operation of the flight deck windows must be included, but the actual windows need not be operable. Fire axes, extinguishers, and spare light bulbs must be available in the flight FTD but may be relocated to a suitable location as near as practical to the original position. Fire axes, landing gear pins, and any similar purpose instruments need only be represented in silhouette. The use of electronically displayed images with physical overlay or masking for FTD instruments and/or instrument panels is acceptable provided:(1) All instruments and instrument panel layouts are dimensionally correct with differences, if any, being imperceptible to the pilot;(2) Instruments replicate those of the airplane including full instrument functionality and embedded logic;(3) Instruments displayed are free of quantization (stepping);(4) Instrument display characteristics replicate those of the airplane including resolution, colors, luminance, brightness, fonts, fill patterns, line styles and symbology;(5) Overlay or masking, including bezels and bugs, as applicable, replicates the airplane panel(s);(6) Instrument controls and switches replicate and operate with the same technique, effort, travel and in the same direction as those in the airplane;(7) Instrument lighting replicates that of the airplane and is operated from the FSTD control for that lighting and, if applicable, is at a level commensurate with other lighting operated</td><td>6,7</td><td>For FTD purposes, the flight deck consists of all that space forward of a cross section of the fuselage at the most extreme aft setting of the pilots' seats including additional, required flight crewmember duty stations and those required bulkheads aft of the pilot seats. For clarification, bulkheads containing only items such as landing gear pin storage compartments, fire axes and extinguishers, spare light bulbs, aircraft documents pouches are not considered essential and may be omitted.For Level 6 FTDs, flight deck windowpanes may be omitted where non-distracting and subjectively acceptable to conduct qualified training tasks.</td><td>□</td><td>□</td><td>□</td></tr></table> GACA-AVSES-OPS-F050 Rev: 4, Date: 28 Jul 25 Page 1 of 91 GACA العامه للطيران المدني General Authority of Civil Aviation [Non-Text] FLIGHT TRAINING DEVICE (FTD) QUALIFICATION TEST CHECKLIST GACAR PART - 60 <table><tr><td rowspan="3"></td><td>by that same control; and</td><td rowspan="3"></td><td rowspan="3"></td><td></td><td></td><td></td></tr><tr><td>(8) As applicable, instruments must have faceplates that replicate those in the airplane; and</td><td>□</td><td>□</td><td>□</td></tr><tr><td>Level 7 FTD only.The display image of any three-dimensional instrument, such as an electro-mechanical instrument, should appear to have the same three-dimensional depth as the replicated instrument. The appearance of the simulated instrument, when viewed from the principal operator's angle, should replicate that of the actual airplane instrument. Any instrument reading inaccuracy due to viewing angle and parallax present in the actual airplane instrument should be duplicated in the simulated instrument display image. Viewing angle error and parallax must be minimized by shared instruments such as engine displays and standby indicators.</td><td></td><td>□</td><td>□</td><td>□</td></tr><tr><td>1.b.</td><td>The FTD must have equipment (e.g., instruments, panels, systems, circuit breakers, and controls) simulated sufficiently for the authorized training/checking events to be accomplished. The installed equipment must be located in a spatially correct location and may be on a flight deck or an open flight deck area. Additional equipment required for the authorized training/checking events must be available in the FTD but may be located in a suitable location as near as practical to the spatially correct position. Actuation of equipment must replicate the appropriate function in the airplane. Fire axes, landing gear pins, and any similar purpose instruments need only be represented in silhouette.</td><td>4,5</td><td>None</td><td>□</td><td>□</td><td>□</td></tr><tr><td>1.c.</td><td>Those circuit breakers that affect procedures or result in observable flight deck indications must be properly located and functionally accurate.</td><td>7</td><td>None</td><td>□</td><td>□</td><td>□</td></tr><tr><td>2.</td><td>Programming</td><td>See next</td><td>None</td><td>□</td><td>□</td><td>□</td></tr><tr><td>2.a.1.</td><td>The FTD must provide the proper effect of aerodynamic changes for the combinations of drag and thrust normally encountered in flight. This must include the effect of change in airplane attitude, thrust, drag, altitude, temperature, and configuration.Level 6 additionally requires the effects of changes in gross weight and center of gravity.Level 5 requires only generic aerodynamic programming.An SOC is required.</td><td>5,6</td><td>None</td><td>□</td><td>□</td><td>□</td></tr><tr><td>2.a.2.</td><td>A flight dynamics model that accounts for various combinations of drag and thrust normally encountered in flight must correspond to actual flight conditions, including the effect of change in airplane attitude, thrust, drag, altitude, temperature, gross weight, moments of inertia, center of gravity location, and configuration.The effects of pitching attitude and of fuel slosh on the aircraft center of gravity must be simulated.An SOC is required.</td><td>7</td><td>None</td><td>□</td><td>□</td><td>□</td></tr><tr><td>2.b.</td><td>The FTD must have the computer capacity, accuracy, resolution, and dynamic response needed to meet the qualification level sought.An SOC is required.</td><td>4,5,6,7</td><td>None</td><td>□</td><td>□</td><td>□</td></tr><tr><td>2.c.1.</td><td>Relative responses of the flight deck instruments must be measured by latency tests, or transport delay tests, and may not exceed 300 milliseconds. The instruments must</td><td>5,6</td><td>The intent is to verify that the FTD provides instrument</td><td>□</td><td>□</td><td>□</td></tr></table> GACA-AVSES-OPS-F050 Rev: 4, Date: 28 Jul 25 Page 2 of 91 GACA العامه للطيران المدني General Authority of Civil Aviation [Non-Text] FLIGHT TRAINING DEVICE (FTD) QUALIFICATION TEST CHECKLIST GACAR PART - 60 <table><tr><td rowspan="2"></td><td>respond to abrupt input at the pilot's position within the allotted time, but not before the time when the airplane responds under the same conditions.(1) Latency: The FTD instrument and, if applicable, the motion system and the visual system response must not be prior to that time when the airplane responds and may respond up to 300 milliseconds after that time under the same conditions.</td><td rowspan="2"></td><td rowspan="2">cues that are, within the stated time delays, like the airplane responses. For airplane response, acceleration in the appropriate, corresponding rotational axis is preferred.Additional information regarding Latency and Transport Delay testing may be found in Appendix A, Attachment 2, paragraph 15.</td><td></td><td></td><td></td></tr><tr><td>(2) Transport Delay: As an alternative to the Latency requirement, a transport delay objective test may be used to demonstrate that the FTD system does not exceed the specified limit. The sponsor must measure all the delay encountered by a step signal migrating from the pilot's control through all the simulation software modules in the correct order, using a handshaking protocol, finally through normal output interfaces to the instrument display and, if applicable, the motion system, and the visual system.</td><td></td><td></td><td></td></tr><tr><td>2.c.2.</td><td>Relative responses of the motion system, visual system, and flight deck instruments, measured by latency tests or transport delay tests. Motion onset should occur before the start of the visual scene change (the start of the scan of the first video field containing different information) but must occur before the end of the scan of that video field. Instrument response may not occur prior to motion onset. The test results must be within the following limits:100 ms for the motion (if installed) and instrument systems; and 120 ms for the visual system.</td><td>7</td><td>The intent is to verify that the FTD provides instruments, motion, and visual cues that are, within the stated time delays, like the airplane responses. For airplane response, acceleration in the appropriate, corresponding rotational axis is preferred.</td><td></td><td></td><td></td></tr><tr><td>2.d.</td><td>Ground handling and aerodynamic programming must include the following:</td><td>See next</td><td>None</td><td></td><td></td><td></td></tr><tr><td>2.d.1.</td><td>Ground effect.</td><td>7</td><td>Ground effect includes modeling that accounts for round out, flare, touchdown, lift, drag, pitching moment, trim, and power while in ground effect.</td><td></td><td></td><td></td></tr><tr><td>2.d.2.</td><td>Ground reaction</td><td>7</td><td>Ground reaction includes modeling that accounts for strut deflections, tire friction, and side forces. This is the reaction of the airplane upon contact with the runway during landing and may differ with changes in factors such as gross weight, air speed, or rate of descent on touchdown.</td><td></td><td></td><td></td></tr><tr><td>2.d.3</td><td>Ground handling characteristics, including aerodynamic and ground reaction modeling including steering inputs, operations with crosswind, gusting crosswind, braking, thrust</td><td>7</td><td>None</td><td></td><td></td><td></td></tr></table> GACA-AVSES-OPS-F050 Rev: 4, Date: 28 Jul 25 Page 3 of 91 GACA العامه للطيران المدني General Authority of Civil Aviation [Non-Text] FLIGHT TRAINING DEVICE (FTD) QUALIFICATION TEST CHECKLIST GACAR PART - 60 <table><tr><td></td><td>reversing, deceleration, and turning radius.</td><td></td><td></td><td></td><td></td><td></td></tr><tr><td>2.e.</td><td>If the aircraft being simulated is one of the aircraft listed in § 121.358, Low-altitude windshear system equipment requirements, the FTD must employ windshear models that provide training for recognition of windshear phenomena and the execution of recovery procedures. Models must be available to the instructor/evaluator for the following critical phases of flight:(1) Prior to takeoff rotation.(2) At liftoff.(3) During the initial climb; and(4) On final approach, below 500 ft AGL.The QTG must reference the GACA Windshear Training Aid or present alternate airplane related data, including the implementation method(s) used. If the alternate method is selected, wind models from the Royal Aerospace Establishment (RAE), the Joint Airport Weather Studies (JAWS) Project and other recognized sources may be implemented but must be supported and properly referenced in the QTG.The addition of realistic levels of turbulence associated with each required windshear profile must be available and selectable to the instructor. In addition to the four basic windshear models required for qualification, at least two additional “complex” windshear models must be available to the instructor which represent the complexity of actual windshear encounters. These models must be available in the takeoff and landing configurations and must consist of independent variable winds in multiple simultaneous components. The Windshear Training Aid provides two such example “complex” windshear models that may be used to satisfy this requirement.</td><td>7</td><td>Windshear models may consist of independent variable winds in multiple simultaneous components.The GACA Windshear Training Aid presents one acceptable means of compliance with FTD wind model requirements.The FTD should employ a method to ensure the required survivable and non-survivable windshear scenarios are repeatable in the training environment.For Level 7 FTDs, windshear training tasks may only be qualified for aircraft equipped with a synthetic stall warning system. The qualified windshear profile(s) are evaluated to ensure the synthetic stall warning (and not the stall buffet) is first indication of the stall.</td><td>□</td><td>□</td><td>□</td></tr><tr><td rowspan="8">2.f.</td><td>The FTD must provide manual and automatic testing of FTD hardware and software programming to determine compliance with FTD objective tests as prescribed in Attachment 2 of this appendix.An SOC is required.</td><td rowspan="8">7</td><td rowspan="8">Automatic “flagging” of out-of-tolerance situations is encouraged.</td><td>□</td><td>□</td><td>□</td></tr><tr><td>The FTD must accurately reproduce the following runway conditions:(1) Dry;</td><td>□</td><td>□</td><td>□</td></tr><tr><td>(2) Wet;</td><td>□</td><td>□</td><td>□</td></tr><tr><td>(3) Icy;</td><td>□</td><td>□</td><td>□</td></tr><tr><td>(4) Patchy Wet;</td><td>□</td><td>□</td><td>□</td></tr><tr><td>(5) Patchy Icy; and</td><td>□</td><td>□</td><td>□</td></tr><tr><td>(6) Wet on Rubber Residue in Touchdown Zone.An SOC is required.</td><td>□</td><td>□</td><td>□</td></tr><tr><td>2.h.</td><td>The FTD must simulate:</td><td>FTD pitch, side loading, and</td><td>□</td><td>□</td><td>□</td></tr></table> GACA-AVSES-OPS-F050 Rev: 4, Date: 28 Jul 25 Page 4 of 91 GACA العامه للطيران المدني General Authority of Civil Aviation [Non-Text] FLIGHT TRAINING DEVICE (FTD) QUALIFICATION TEST CHECKLIST GACAR PART - 60 <table><tr><td rowspan="2"></td><td>(1) brake and tire failure dynamics, including antiskid failure; and</td><td rowspan="2">7</td><td rowspan="2">directional control characteristics should be representative of the airplane.</td><td></td><td></td><td></td></tr><tr><td>(2) decreased brake efficiency due to high brake temperatures, if applicable. An SOC is required</td><td>□</td><td>□</td><td>□</td></tr><tr><td rowspan="3">2.i.</td><td>Engine and Airframe Icing Modeling that includes the effects of icing, where appropriate, on the airframe, aerodynamics, and the engine(s). Icing models must simulate the aerodynamic degradation effects of ice accretion on the airplane lifting surfaces including loss of lift, decrease in stall angle of attack, change in pitching moment, decrease in control effectiveness, and changes in control forces in addition to any overall increase in drag.</td><td rowspan="3">7</td><td rowspan="3">SOC should be provided describing the effects which provide training in the specific skills required for recognition of icing phenomena and execution of recovery. The SOC should describe the source data, and any analytical methods used to develop ice accretion models including verification that these effects have been tested. Icing effects simulation models are only required for those airplanes authorized for operations in icing conditions. Icing simulation models should be developed to provide training in the specific skills required for recognition of ice accumulation and execution of the required response. See Attachment 7 of this Appendix for further guidance material.</td><td rowspan="3">□</td><td rowspan="3">□</td><td rowspan="3">□</td></tr><tr><td>Aircraft systems (such as the stall protection system and auto flight system) must respond properly to ice accretion consistent with simulated aircraft.</td></tr><tr><td>Aircraft OEM data or other acceptable analytical methods must be utilized to develop ice accretion models that are representative of the simulated aircraft's performance degradation in a typical in-flight icing encounter. Acceptable analytical methods may include wind tunnel analysis and/or engineering analysis of the aerodynamic effects of icing on the lifting surfaces coupled with tuning and supplemental subjective assessment by a subject matter expert pilot.SOC required.</td></tr><tr><td rowspan="8">2.j.</td><td>The aerodynamic modeling in the FTD must include:(1) Low-altitude level-flight ground effect.</td><td rowspan="6">7</td><td rowspan="6">See Attachment 2 of this appendix, paragraph 5, for further information on ground effect.</td><td>□</td><td>□</td><td>□</td></tr><tr><td>(2) Mach effect at high altitude;</td><td>□</td><td>□</td><td>□</td></tr><tr><td>(3) Normal and reverse dynamic thrust effect on control surfaces;</td><td>□</td><td>□</td><td>□</td></tr><tr><td>(4) Aeroelastic representations; and</td><td>□</td><td>□</td><td>□</td></tr><tr><td>(5) Nonlinearities due to sideslip.</td><td>□</td><td>□</td><td>□</td></tr><tr><td>An SOC is required and must include references to computations of aeroelastic representations and of nonlinearities due to sideslip.</td><td>□</td><td>□</td><td>□</td></tr><tr><td>2.k.</td><td>The FTD must have aerodynamic and ground reaction modeling for the effects of reverse</td><td>7</td><td>None</td><td>□</td><td>□</td><td>□</td></tr></table> GACA-AVSES-OPS-F050 Rev: 4, Date: 28 Jul 25 Page 5 of 91 GACA العامه للطيران المدني General Authority of Civil Aviation [Non-Text] FLIGHT TRAINING DEVICE (FTD) QUALIFICATION TEST CHECKLIST GACAR PART - 60 <table><tr><td></td><td>thrust on directional control, if applicable.An SOC is required.</td><td></td><td></td><td></td><td></td><td></td></tr><tr><td>3.</td><td>Equipment Operation.</td><td>See next</td><td>None</td><td>□</td><td>□</td><td>□</td></tr><tr><td>3.a.</td><td>All relevant instrument indications involved in the simulation of the airplane must automatically respond to control movement or external disturbances to the simulated airplane, e.g., turbulence or windshear. Numerical values must be presented in the appropriate units.For Level 7 FTDs, instrument indications must also respond to effects resulting from icing.</td><td>5,6,7</td><td>None</td><td>□</td><td>□</td><td>□</td></tr><tr><td>3.b.1</td><td>Navigation equipment must be installed and operated within the tolerances applicable for the airplane.Levels 6 must also include communication equipment (inter-phone and air/ground) like that in the airplane and, if appropriate to the operation being conducted, an oxygen mask microphone system.Level 5 need to have only that navigation equipment necessary to fly an instrument approach.</td><td>5,6</td><td>None</td><td>□</td><td>□</td><td>□</td></tr><tr><td>3.b.2.</td><td>Communications, navigation, caution, and warning equipment must be installed and operated within the tolerances applicable for the airplane.Instructor control of internal and external navigational aids. Navigation aids must be usable within range or line-of-sight without restriction, as applicable to the geographic area.</td><td>7</td><td>See Attachment 3 of this appendix for further information regarding long-range navigation equipment.</td><td>□</td><td>□</td><td>□</td></tr><tr><td>3.b.3.</td><td>Complete navigation database for at least 3 airports with corresponding precision and non-precision approach procedures, including navigational database updates.</td><td>7</td><td>None</td><td>□</td><td>□</td><td>□</td></tr><tr><td></td><td>Installed systems must simulate the applicable airplane system operation, both on the ground and in flight. Installed systems must be operative to the extent that applicable normal, abnormal, and emergency operating procedures included in the sponsor's training programs can be accomplished.</td><td rowspan="3">4,5,6</td><td rowspan="3">None</td><td rowspan="3">□</td><td rowspan="3">□</td><td rowspan="3">□</td></tr><tr><td>3.c.1.</td><td>Level 6 must simulate all applicable airplane flight, navigation, and systems operation.Level 5 must have at least functional flight and navigational controls, displays, and instrumentation.Level 4 must have at least one airplane system installed and functional.</td></tr><tr><td>3.c.2.</td><td>Simulated airplane systems must operate as the airplane systems operate under normal, abnormal, and emergency operating conditions on the ground and in flight.Once activated, proper systems operation must result from system management by the crew member and not require any further input from the instructor's controls.</td></tr></table> GACA-AVSES-OPS-F050 Rev: 4, Date: 28 Jul 25 Page 6 of 91 GACA العامه للطيران المدني General Authority of Civil Aviation [Non-Text] FLIGHT TRAINING DEVICE (FTD) QUALIFICATION TEST CHECKLIST GACAR PART – 60 <table><tr><td></td><td></td><td>equipment manufacturer or alternative approved data for the airplane system or component.At a minimum, alternate approved data should validate the operation of all normal, abnormal, and emergency operating procedures and training tasks the FSTD is qualified to conduct.</td><td></td><td></td><td></td></tr><tr><td>3.d.</td><td>The lighting environment for panels and instruments must be sufficient for the operation being conducted.</td><td>4,5,6,7</td><td>Back-lighted panels and instruments may be installed but are not required.</td><td>□</td><td>□</td><td>□</td></tr><tr><td>3.e.</td><td>The FTD must provide control forces and control travel that corresponds to the airplane being simulated. Control forces must react in the same manner as in the airplane under the same flight conditions. For Level 7 FTDs, control systems must replicate airplane operation for the normal and any non-normal modes including back-up systems and should reflect failures of associated systems. Appropriate cockpit indications and messages must be replicated.</td><td>6,7</td><td>None</td><td>□</td><td>□</td><td>□</td></tr><tr><td>3.f.</td><td>The FTD must provide control forces and control travel of sufficient precision to manually fly an instrument approach.</td><td>5</td><td>None</td><td>□</td><td>□</td><td>□</td></tr><tr><td>3.e.</td><td>FTD control feel dynamics must replicate the airplane. This must be determined by comparing a recording of the control feel dynamics of the FTD to airplane measurements. For initial and upgrade qualification evaluations, the control dynamic characteristics must be measured and recorded directly from the flight deck controls, and must be accomplished in takeoff, cruise, and landing flight conditions and configurations.</td><td>7</td><td>None</td><td>□</td><td>□</td><td>□</td></tr><tr><td>4.</td><td>Instructor or Evaluator Facilities.</td><td>See next</td><td>None</td><td>□</td><td>□</td><td>□</td></tr><tr><td>4.a.1</td><td>In addition to the flight crewmember stations, suitable seating arrangements for an instructor/check airman and GACA Inspector must be available. These seats must provide adequate view of crewmember's panel(s).</td><td>4,5,6</td><td>These seats need not be a replica of an aircraft seat and maybe as simple as an office chair placed in an appropriate position.</td><td>□</td><td>□</td><td>□</td></tr><tr><td>4.a.2</td><td>In addition to the flight crewmember stations, the FTD must have at least two suitable seats for the instructor/check airman and GACA inspector. These seats must provide adequate vision to the pilot's panel and forward windows. All seats other than flight crew seats need not represent those found in the airplane but must be adequately secured to the floor and equipped with similar positive restraint devices.</td><td>7</td><td>The NSPM will consider alternatives to this standard for additional seats based on unique flight deck configurations.</td><td>□</td><td>□</td><td>□</td></tr><tr><td>4.b.1</td><td>The FTD must have instructor controls that permit activation of normal, abnormal, and</td><td>4,5,6</td><td>None</td><td>□</td><td>□</td><td>□</td></tr></table> GACA-AVSES-OPS-F050 Rev: 4, Date: 28 Jul 25 Page 7 of 91 GACA العامه للطيران المدني General Authority of Civil Aviation [Non-Text] FLIGHT TRAINING DEVICE (FTD) QUALIFICATION TEST CHECKLIST GACAR PART - 60 <table><tr><td></td><td>emergency conditions as appropriate. Once activated, proper system operation must result from system management by the crew and not require input from the instructor controls.</td><td></td><td></td><td></td><td></td><td></td></tr><tr><td>4.b.2.</td><td>The FTD must have controls that enable the instructor/evaluator to control all required system variables and insert all abnormal or emergency conditions into the simulated airplane systems as described in the sponsor's GACA-approved training program; or as described in the relevant operating manual as appropriate.</td><td>7</td><td>None</td><td>□</td><td>□</td><td>□</td></tr><tr><td>4.c.</td><td>The FTD must have instructor controls for all environmental effects expected to be available at the IOS, e.g., clouds, visibility, icing, precipitation, temperature, storm cells and microbursts, turbulence, and intermediate and high-altitude wind speed and direction.</td><td>7</td><td>None</td><td>□</td><td>□</td><td>□</td></tr><tr><td>4.d.</td><td>The FTD must provide the instructor or evaluator with the ability to present ground and air hazards.</td><td>7</td><td>For example, another airplane crossing the active runway or converging airborne traffic.</td><td>□</td><td>□</td><td>□</td></tr><tr><td>5.</td><td>Motion System.</td><td>See next</td><td></td><td>□</td><td>□</td><td>□</td></tr><tr><td>5.a</td><td>The FTD may have a motion system, if desired, although it is not required. If a motion system is installed and additional training, testing, or checking credits are being sought on the basis of having a motion system, the motion system operation may not be distracting and must be coupled closely to provide integrated sensory cues. The motion system must also respond to abrupt input at the pilot's position within the allotted time, but not before the time when the airplane responds under the same conditions.</td><td>5,6,7</td><td>he motion system standards set out in part 60, Appendix A for at least Level A simulators is acceptable.</td><td>□</td><td>□</td><td>□</td></tr><tr><td>5.b</td><td>If a motion system is installed, it must be measured by latent tests or transport delay tests and may not exceed 300 milliseconds. Instrument response may not occur prior to motion onset.</td><td>6,7</td><td>The motion system standards set out in part 60, Appendix A for at least Level A simulators is acceptable.</td><td>□</td><td>□</td><td>□</td></tr><tr><td colspan="2">6. Visual System.</td><td>See next</td><td>None</td><td>□</td><td>□</td><td>□</td></tr><tr><td>6.a</td><td>The FTD may have a visual system, if desired, although it is not required. If a visual system is installed, it must meet the following criteria:</td><td>4,5,6</td><td>None</td><td>□</td><td>□</td><td>□</td></tr><tr><td>6.a.1</td><td>The visual system must respond to abrupt input at the pilot's position. An SOC is required.</td><td>5,6</td><td>None</td><td>□</td><td>□</td><td>□</td></tr><tr><td>6.a.2</td><td>The visual system must have at least a single channel, non-collimated display. An SOC is required.</td><td>4,5,6</td><td>None</td><td>□</td><td>□</td><td>□</td></tr><tr><td>6.a.3</td><td>The visual system must provide at least a field-of-view of 18° vertical / 24° horizontal for the pilot flying.An SOC is required.</td><td>4,5,6</td><td>None</td><td>□</td><td>□</td><td>□</td></tr><tr><td>6.a.4</td><td>The visual system must provide for a maximum parallax of 10° per pilot. An SOC is required.</td><td>4,5,6</td><td>None</td><td>□</td><td>□</td><td>□</td></tr><tr><td>6.a.5.</td><td>The visual scene content may not be distracting.An SOC is required.</td><td>4,5,6</td><td>None</td><td>□</td><td>□</td><td>□</td></tr><tr><td>6.a.6.</td><td>The minimum distance from the pilot's eye position to the surface of a direct view display may not be less than the distance to any front panel instrument. An SOC is required.</td><td></td><td>None</td><td>□</td><td>□</td><td>□</td></tr></table> GACA-AVSES-OPS-F050 Rev: 4, Date: 28 Jul 25 Page 8 of 91 GACA العامه للطيران المدني General Authority of Civil Aviation [Non-Text] FLIGHT TRAINING DEVICE (FTD) QUALIFICATION TEST CHECKLIST GACAR PART - 60 <table><tr><td>6.a.7.</td><td>The visual system must provide for a minimum resolution of 5 arc- minutes for both computed and displayed pixel size.An SOC is required.</td><td>4,5,6</td><td>None</td><td>□</td><td>□</td><td>□</td></tr><tr><td>6.b</td><td>If a visual system is installed and additional training, testing, or checking credits are being sought on the basis of having a visual system, a visual system meeting the standards set out for at least a Level An FFS (see Appendix A of this part) will be required. A “direct-view,” non-collimated visual system (with the other requirements for a Level A visual system met) may be considered satisfactory for those installations where the visual system design “eye point” is appropriately adjusted for each pilot’s position such that the parallax error is at or less than 10° simultaneously for each pilot.An SOC is required.</td><td>6</td><td>Directly projected, non-collimated visual displays may prove to be unacceptable for dual pilot applications.</td><td>□</td><td>□</td><td>□</td></tr><tr><td>6.c</td><td>The FTD must have a visual system providing an out-of-the-flight deck view.</td><td>7</td><td>None</td><td>□</td><td>□</td><td>□</td></tr><tr><td>6.d</td><td>The FTD must provide a continuous visual field-of-view of at least 176° horizontally and 36° vertically or the number of degrees necessary to meet the visual ground segment requirement, whichever is greater. The minimum horizontal field-of-view coverage must be plus and minus one-half (1/2) of the minimum continuous field-of-view requirement, centered on the zero-degree azimuth line relative to the aircraft fuselage.An SOC is required and must explain the system geometry measurements including system linearity and field-of-view.Collimation is not required but parallax effects must be minimized (not greater than 10° for each pilot when aligned for the point midway between the left and right seat eyepoints).</td><td>7</td><td>The horizontal field-of-view is traditionally described as a 180° field-of-view. However, the field-of-view is technically no less than 176°.Additional field-of-view capability may be added at the sponsor's discretion provided the minimum fields of view are retained.</td><td>□</td><td>□</td><td>□</td></tr><tr><td>6.e</td><td>The visual system must be free from optical discontinuities and artifacts that create non-realistic cues.</td><td>7</td><td>Non-realistic cues might include image “swimming” and image “roll-off,” that may lead a pilot to make incorrect assessments of speed, acceleration, or situational awareness.</td><td>□</td><td>□</td><td>□</td></tr><tr><td>6.f</td><td>The FTD must have operational landing lights for night scenes. Where used, dusk (or twilight) scenes require operational landing lights.</td><td>7</td><td>None</td><td>□</td><td>□</td><td>□</td></tr><tr><td rowspan="3">6.g.</td><td>The FTD must have instructor controls for the following:(1) Visibility in statute miles (km) and runway visual range (RVR) in ft.(m);</td><td rowspan="3">7</td><td rowspan="3">None</td><td>□</td><td>□</td><td>□</td></tr><tr><td>(2) Airport selection; and</td><td>□</td><td>□</td><td>□</td></tr><tr><td>(3) Airport lighting.</td><td>□</td><td>□</td><td>□</td></tr><tr><td>6.h.</td><td>The FTD must provide visual system compatibility with dynamic response programming.</td><td>7</td><td>None</td><td>□</td><td>□</td><td>□</td></tr><tr><td>6.i.</td><td>The FTD must show that the segment of the ground visible from the FTD flight deck is the same as from the airplane flight deck (within established tolerances) when at the correct air speed, in the landing configuration, at the appropriate height above the touchdown zone, and with appropriate visibility.</td><td>7</td><td>This will show the modeling accuracy of RVR, glideslope, and localizer for a given weight, configuration, and</td><td>□</td><td>□</td><td>□</td></tr></table> GACA-AVSES-OPS-F050 Rev: 4, Date: 28 Jul 25 Page 9 of 91 GACA العامه للطيران المدني General Authority of Civil Aviation FLIGHT TRAINING DEVICE (FTD) QUALIFICATION TEST CHECKLIST GACAR PART - 60 <table><tr><td></td><td></td><td></td><td>speed within the airplane's operational envelope for a normal approach and landing.</td><td></td><td></td><td></td></tr><tr><td rowspan="2">6.j.</td><td>The FTD must provide visual cues necessary to assess sink rates (provide depth perception) during takeoffs and landings, to include:(1) Surface on runways, taxiways, and ramps; and</td><td rowspan="2">7</td><td rowspan="2">None</td><td>□</td><td>□</td><td>□</td></tr><tr><td>(2) Terrain features.</td><td>□</td><td>□</td><td>□</td></tr><tr><td>6.k.</td><td>The FTD must provide for accurate portrayal of the visual environment relating to the FTD attitude.</td><td>7</td><td>Visual attitude vs. FTD attitude is a comparison of pitch and roll of the horizon as displayed in the visual scene compared to the display on the attitude indicator</td><td>□</td><td>□</td><td>□</td></tr><tr><td>6.l.</td><td>The FTD must provide quick confirmation of visual system color, RVR, focus, and intensity. An SOC is required.</td><td>7</td><td>None</td><td>□</td><td>□</td><td>□</td></tr><tr><td>6.m.</td><td>The FTD must be capable of producing at least 10 levels of occulting.</td><td>7</td><td>None</td><td>□</td><td>□</td><td>□</td></tr><tr><td>6.n.</td><td>Night Visual Scenes. When used in training, testing, or checking activities, the FTD must provide night visual scenes with sufficient scene content to recognize the airport, the terrain, and major landmarks around the airport. The scene content must allow a pilot to successfully accomplish a visual landing. Scenes must include a definable horizon and typical terrain characteristics such as fields, roads and bodies of water and surfaces illuminated by airplane landing lights.</td><td>7</td><td>None</td><td>□</td><td>□</td><td>□</td></tr><tr><td>6.o.</td><td>Dusk (or Twilight) Visual Scenes. When used in training, testing, or checking activities, the FTD must provide dusk (or twilight) visual scenes with sufficient scene content to recognize</td><td>7</td><td>None</td><td>□</td><td>□</td><td>□</td></tr><tr><td></td><td>the airport, the terrain, and major landmarks around the airport. The scene content must allow a pilot to successfully accomplish a visual landing. Dusk (or twilight) scenes, as a minimum, must provide full color presentations of reduced ambient intensity, sufficient surfaces with appropriate textural cues that include self-illuminated objects such as road networks, ramp lighting and airport signage, to conduct a visual approach, landing and airport movement (taxi). Scenes must include a definable horizon and typical terrain characteristics such as fields, roads and bodies of water and surfaces illuminated by airplane landing lights. If provided, directional horizon lighting must have correct orientation and be consistent with surface shading effects. Total night or dusk (twilight) scene content must be comparable in detail to that produced by 10,000 visible textured surfaces and 15,000 visible lights with sufficient system capacity to display 16 simultaneously moving objects.An SOC is required.</td><td>7</td><td>None</td><td>□</td><td>□</td><td>□</td></tr></table> GACA-AVSES-OPS-F050 Rev: 4, Date: 28 Jul 25 Page 10 of 91 GACA العامه للطيران المدني General Authority of Civil Aviation [Non-Text] FLIGHT TRAINING DEVICE (FTD) QUALIFICATION TEST CHECKLIST GACAR PART - 60 <table><tr><td>6.p.</td><td>Daylight Visual Scenes. The FTD must provide daylight visual scenes with sufficient scene content to recognize the airport, the terrain, and major landmarks around the airport. The scene content must allow a pilot to successfully accomplish a visual landing. Any ambient lighting must not “washout” the displayed visual scene. Total daylight scene content must be comparable in detail to that produced by 10,000 visible textured surfaces and 6,000 visible lights with sufficient system capacity to display 16 simultaneously moving objects. The visual display must be free of apparent and distracting quantization and other distracting visual effects while the FTD is in motion.An SOC is required.</td><td>7</td><td>None</td><td></td><td></td><td></td></tr><tr><td>6.q.</td><td>The FTD must provide operational visual scenes that portray physical relationships known to cause landing illusions to pilots.</td><td>7</td><td>For example: short runways, landing approaches over water, uphill or downhill runways, rising terrain on the approach path, unique topographic features.</td><td></td><td></td><td></td></tr><tr><td>6.r.</td><td>The FTD must provide special weather representations of light, medium, and heavy precipitation near a thunderstorm on takeoff and during approach and landing.Representations need only be presented at and below an altitude of 2,000 ft. (610 m) above the airport surface and within 10 miles (16 km) of the airport.</td><td>7</td><td>None</td><td></td><td></td><td></td></tr><tr><td>6.s.</td><td>The FTD must present visual scenes of wet and snow-covered runways, including runway lighting reflections for wet conditions, partially obscured lights for snow conditions, or suitable alternative effects.</td><td>7</td><td>None</td><td></td><td></td><td></td></tr><tr><td>6.t.</td><td>The FTD must present realistic color and directionality of all airport lighting.</td><td>7</td><td>None</td><td></td><td></td><td></td></tr><tr><td rowspan="10">6.u.</td><td>The following weather effects as observed on the visual system must be simulated and respective instructor controls provided.(1) Multiple cloud layers with adjustable bases, tops, sky coverage and scud effect;</td><td rowspan="10">7</td><td rowspan="10">Scud effects are low, detached, and irregular clouds below a defined cloud layer.</td><td></td><td></td><td></td></tr><tr><td>(2) Storm cells activation and/or deactivation</td><td></td><td></td><td></td></tr><tr><td>(3) Visibility and runway visual range (RVR), including fog and patchy fog effect;</td><td></td><td></td><td></td></tr><tr><td>(4) Effects on own ship external lighting;</td><td></td><td></td><td></td></tr><tr><td>(5) Effects on airport lighting (including variable intensity and fog effects);</td><td></td><td></td><td></td></tr><tr><td>(6) Surface contaminants (including wind blowing effect);</td><td></td><td></td><td></td></tr><tr><td>(7) Variable precipitation effects (rain, hail, snow);</td><td></td><td></td><td></td></tr><tr><td>(8) In-cloud airspeed effect; and</td><td></td><td></td><td></td></tr><tr><td>(9) Gradual visibility changes entering and breaking out of cloud.</td><td></td><td></td><td></td></tr><tr><td rowspan="2">6.v.</td><td>The simulator must provide visual effects for:</td><td rowspan="2">7</td><td rowspan="2">Visual effects for light poles and raised edge lights are for the purpose of providing</td><td></td><td></td></tr><tr><td>(1) Light poles.</td><td></td><td></td></tr><tr><td></td><td>(2) Raised edge lights as appropriate; and</td><td></td><td></td><td></td><td></td><td></td></tr></table> GACA-AVSES-OPS-F050 Rev: 4, Date: 28 Jul 25 Page 11 of 91 GACA العامه للطيران المدني General Authority of Civil Aviation [Non-Text] FLIGHT TRAINING DEVICE (FTD) QUALIFICATION TEST CHECKLIST GACAR PART - 60 <table><tr><td></td><td>(3) Glow associated with approach lights in low visibility before physical lights are seen,</td><td></td><td>additional depth perception during takeoff, landing, and taxi training tasks. Three-dimensional modeling of the actual poles and stanchions is not required.</td><td>□</td><td>□</td><td>□</td></tr><tr><td>7.</td><td>Sound System.</td><td>See next</td><td>None</td><td>□</td><td>□</td><td>□</td></tr><tr><td>7.a.</td><td>The FTD must provide flight deck sounds that result from pilot actions that correspond to those that occur in the airplane.</td><td>6,7</td><td>None</td><td>□</td><td>□</td><td>□</td></tr><tr><td>7.b.</td><td>The volume control must have an indication of sound level setting which meets all qualification requirements.</td><td>7</td><td>This indication is of the sound level setting as evaluated during the FTD's initial evaluation.</td><td>□</td><td>□</td><td>□</td></tr><tr><td>7.c.</td><td>The FTD must accurately simulate the sound of precipitation, windshield wipers, and other significant airplane noises perceptible to the pilot during normal and abnormal operations and include the sound of a crash (when the FTD is landed in an unusual attitude or in excess of the structural gear limitations); normal engine and thrust reversal sounds; and the sounds of flap, gear, and spoiler extension and retraction. Sounds must be directionally representative.An SOC is required.</td><td>7</td><td>None</td><td>□</td><td>□</td><td>□</td></tr><tr><td>7.d</td><td>The FTD must provide realistic amplitude and frequency of flight deck noises and sounds. FTD performance must be recorded, subjectively assessed for the initial evaluation, and be made a part of the QTG.</td><td>7</td><td></td><td>□</td><td>□</td><td>□</td></tr></table> GACA-AVSES-OPS-F050 Rev: 4, Date: 28 Jul 25 Page 12 of 91 GACA العامه للطيران المدني General Authority of Civil Aviation [Non-Text] FLIGHT TRAINING DEVICE (FTD) QUALIFICATION TEST CHECKLIST GACAR PART - 60 QPS REQUIREMENTS <table><tr><td colspan="7">In order to be qualified at the FTD qualification level indicated, the FTD must be able to perform at least the tasks associated with that level of qualification. See Notes 1, 2 and 3 at the end of the Table.</td><td colspan="3">Compliance</td></tr><tr><td colspan="7"></td><td colspan="3">Compliance</td></tr><tr><td>Entry Number</td><td colspan="3">Subjective Requirements</td><td>FTD Level</td><td colspan="2">Notes/Information</td><td>Yes</td><td>No</td><td>NA</td></tr><tr><td>1.</td><td colspan="3">Preflight Procedures</td><td>See next</td><td colspan="2">None</td><td>□</td><td>□</td><td>□</td></tr><tr><td>1.a.</td><td colspan="3">Preflight Inspection (flight deck only)</td><td>4(a),5(a),6,7</td><td colspan="2">None</td><td>□</td><td>□</td><td>□</td></tr><tr><td>1.b.</td><td colspan="3">Engine Start</td><td>4(a),5(a),6,7</td><td colspan="2">None</td><td>□</td><td>□</td><td>□</td></tr><tr><td>1.c.</td><td colspan="3">Taxiing</td><td>7(t)</td><td colspan="2">None</td><td>□</td><td>□</td><td>□</td></tr><tr><td>1.d.</td><td colspan="3">Pre-takeoff Checks</td><td>4(a),5(a),6,7</td><td colspan="2">None</td><td>□</td><td>□</td><td>□</td></tr><tr><td>2.</td><td colspan="3">Takeoff and Departure Phase.</td><td>See next</td><td colspan="2">None</td><td>□</td><td>□</td><td>□</td></tr><tr><td>2.a.</td><td colspan="3">Normal and Crosswind Takeoff</td><td>7(t)</td><td colspan="2">None</td><td>□</td><td>□</td><td>□</td></tr><tr><td>2.b.</td><td colspan="3">Instrument Takeoff</td><td>7(t)</td><td colspan="2">None</td><td>□</td><td>□</td><td>□</td></tr><tr><td>2.c.</td><td colspan="3">Engine Failure During Takeoff</td><td>7(t)</td><td colspan="2">None</td><td>□</td><td>□</td><td>□</td></tr><tr><td>2.d.</td><td colspan="3">Rejected Takeoff (requires visual system)</td><td>6(a),7</td><td colspan="2">None</td><td>□</td><td>□</td><td>□</td></tr><tr><td>2.e.</td><td colspan="3">Departure Procedure</td><td>5,6,7</td><td colspan="2">None</td><td>□</td><td>□</td><td>□</td></tr><tr><td>3.</td><td colspan="3">Inflight Maneuvers.</td><td>See next</td><td colspan="2"></td><td>□</td><td>□</td><td>□</td></tr><tr><td>3.a.</td><td colspan="3">Steep Turns</td><td>5,6,7</td><td colspan="2"></td><td>□</td><td>□</td><td>□</td></tr><tr><td>3.b.</td><td colspan="3">Approaches to Stalls</td><td>5(a),6,7</td><td colspan="2">Approach to stall maneuvers qualified only where the aircraft does not exhibit stall buffet as the first indication of the stall.</td><td>□</td><td>□</td><td>□</td></tr><tr><td>3.c.</td><td colspan="3">Engine Failure-Multienge Airplane</td><td>5(a),6,7</td><td colspan="2">None</td><td>□</td><td>□</td><td>□</td></tr><tr><td>3.d.</td><td colspan="3">Engine Failure-Single-Engine Airplane</td><td>5(a),6,7</td><td colspan="2">None</td><td>□</td><td>□</td><td>□</td></tr><tr><td>3.e.</td><td colspan="3">Specific Flight Characteristics incorporated into the user's GACA approved flight training program.</td><td>4(a),5(a),6(a),7(a)</td><td colspan="2">Level 4 FTDs have no minimum requirement for aerodynamic programming and are generally not qualified to conduct in-flight maneuvers.</td><td>□</td><td>□</td><td>□</td></tr><tr><td>3.f</td><td colspan="3">Windshear Recovery</td><td>7(t)</td><td colspan="2">For Level 7 FTD, windshear recovery may be qualified at</td><td>□</td><td>□</td><td>□</td></tr></table> GACA-AVSES-OPS-F050 Rev: 4, Date: 28 Jul 25 Page 13 of 91 GACA العامه للطيران المدني General Authority of Civil Aviation [Non-Text] FLIGHT TRAINING DEVICE (FTD) QUALIFICATION TEST CHECKLIST GACAR PART - 60 <table><tr><td></td><td></td><td></td><td>the Sponsor's option. See Table B1A for specific requirements and limitations.</td><td></td><td></td><td></td></tr><tr><td>4.</td><td>Instrument Procedures</td><td>See next</td><td>None</td><td>□</td><td>□</td><td>□</td></tr><tr><td>4.a</td><td>Standard Terminal Arrival / Flight Management System Arrivals Procedures</td><td>5(a),6,7</td><td>None</td><td>□</td><td>□</td><td>□</td></tr><tr><td>4.b.</td><td>Holding</td><td>5(a),6,7</td><td></td><td>□</td><td>□</td><td>□</td></tr><tr><td>4.c.</td><td>Precision Instrument</td><td></td><td></td><td>□</td><td>□</td><td>□</td></tr><tr><td>4.c.1</td><td>All engines operating.</td><td>5(a),6,7</td><td></td><td>□</td><td>□</td><td>□</td></tr><tr><td>4.c.2</td><td>One engine inoperative.</td><td>7(t)</td><td>e.g., Autopilot, Manual (Flt. Dir. Assisted), Manual (Raw Data)</td><td>□</td><td>□</td><td>□</td></tr><tr><td>4.d.</td><td>Non-precision Instrument Approach</td><td>5(a),6,7</td><td>e.g., Manual (Flt. Dir. Assisted), Manual (Raw Data)</td><td>□</td><td>□</td><td>□</td></tr><tr><td rowspan="2">4.e.</td><td rowspan="2">Circling Approach (requires visual system)</td><td rowspan="2">6(a),7</td><td>e.g., NDB, VOR, VOR/DME, VOR/TAC,</td><td rowspan="2">□</td><td rowspan="2">□</td><td rowspan="2">□</td></tr><tr><td>RNAV, LOC, LOC/BC, ADF, and SDF.</td></tr><tr><td>4.f.</td><td>Missed Approach</td><td></td><td>Specific authorization required.</td><td>□</td><td>□</td><td>□</td></tr><tr><td>4.f.1</td><td>Normal.</td><td>5(a),6,7</td><td>None</td><td>□</td><td>□</td><td>□</td></tr><tr><td>4.f.2</td><td>One engine Inoperative.</td><td>7(t)</td><td>None</td><td>□</td><td>□</td><td>□</td></tr><tr><td>5.</td><td>Landings and Approaches to Landings.</td><td>See next</td><td>None</td><td>□</td><td>□</td><td>□</td></tr><tr><td>5.a.</td><td>Normal and Crosswind Approaches and Landings</td><td>7(t)</td><td>None</td><td>□</td><td>□</td><td>□</td></tr><tr><td>5.b.</td><td>Landing From a Precision / Non-Precision Approach</td><td>7(t)</td><td>None</td><td>□</td><td>□</td><td>□</td></tr><tr><td>5.c.</td><td>Approach and Landing with (Simulated) Engine Failure – Multiengine Airplane</td><td>7(t)</td><td>None</td><td>□</td><td>□</td><td>□</td></tr><tr><td>5.d.</td><td>Landing From Circling Approach</td><td>7(t)</td><td>None</td><td>□</td><td>□</td><td>□</td></tr><tr><td>5.e.</td><td>Rejected Landing</td><td>7(t)</td><td>None</td><td>□</td><td>□</td><td>□</td></tr><tr><td>5.f.</td><td>Landing From a No Flap or a Nonstandard Flap Configuration Approach</td><td>7(t)</td><td>None</td><td>□</td><td>□</td><td>□</td></tr><tr><td>6.</td><td>Normal and Abnormal Procedures.</td><td>See next</td><td>None</td><td>□</td><td>□</td><td>□</td></tr><tr><td>6.a.</td><td>Engine (including shutdown and restart)</td><td>4(a),5(a),6,7</td><td>None</td><td>□</td><td>□</td><td>□</td></tr><tr><td>6.b.</td><td>Fuel System</td><td>4(a),5(a),6,7</td><td>None</td><td>□</td><td>□</td><td>□</td></tr></table> GACA-AVSES-OPS-F050 Rev: 4, Date: 28 Jul 25 Page 14 of 91 GACA العامه للطيران المدني General Authority of Civil Aviation [Non-Text] FLIGHT TRAINING DEVICE (FTD) QUALIFICATION TEST CHECKLIST GACAR PART - 60 <table><tr><td>6.c.</td><td>Electrical System</td><td>4(a),5(a),6,7</td><td>None</td><td>□</td><td>□</td><td>□</td></tr><tr><td>6.d.</td><td>Hydraulic System</td><td>4(a),5(a),6,7</td><td>None</td><td>□</td><td>□</td><td>□</td></tr><tr><td>6.e.</td><td>Environmental and Pressurization Systems</td><td>4(a),5(a),6,7</td><td>None</td><td>□</td><td>□</td><td>□</td></tr><tr><td>6.f.</td><td>Fire Detection and Extinguisher Systems</td><td>4(a),5(a),6,7</td><td>None</td><td>□</td><td>□</td><td>□</td></tr><tr><td>6.g.</td><td>Navigation and Avionics Systems</td><td>4(a),5(a),6,7</td><td>None</td><td>□</td><td>□</td><td>□</td></tr><tr><td>6.h.</td><td>Automatic Flight Control System, Electronic Flight Instrument System, and Related Subsystems</td><td>4(a),5(a),6,7</td><td>None</td><td>□</td><td>□</td><td>□</td></tr><tr><td>6.i.</td><td>Flight Control Systems</td><td>4(a),5(a),6,7</td><td>None</td><td>□</td><td>□</td><td>□</td></tr><tr><td>6.j.</td><td>Anti-ice and Deice Systems</td><td>4(a),5(a),6,7</td><td>None</td><td>□</td><td>□</td><td>□</td></tr><tr><td>6.k.</td><td>Aircraft and Personal Emergency Equipment</td><td>4(a),5(a),6,7</td><td>None</td><td>□</td><td>□</td><td>□</td></tr><tr><td>7.</td><td>Emergency Procedures.</td><td>5(a),6,7</td><td>None</td><td>□</td><td>□</td><td>□</td></tr><tr><td>7.a.</td><td>Emergency Descent (Max. Rate)</td><td>5(a),6,7</td><td>None</td><td>□</td><td>□</td><td>□</td></tr><tr><td>7.b.</td><td>Inflight Fire and Smoke Removal</td><td>5(a),6,7</td><td>None</td><td>□</td><td>□</td><td>□</td></tr><tr><td>7.c.</td><td>Rapid Decompression</td><td>5(a),6,7</td><td>None</td><td>□</td><td>□</td><td>□</td></tr><tr><td>7.d.</td><td>Emergency Evacuation</td><td>4(a),5(a),6,7</td><td>None</td><td>□</td><td>□</td><td>□</td></tr><tr><td>8.</td><td>Postflight Procedures.</td><td>See next</td><td>None</td><td>□</td><td>□</td><td>□</td></tr><tr><td>8.a.</td><td>After-Landing Procedures</td><td>4(a),5(a),6,7</td><td>None</td><td>□</td><td>□</td><td>□</td></tr><tr><td>8.b.</td><td>Parking and securing</td><td>4(a),5(a),6,7</td><td>None</td><td>□</td><td>□</td><td>□</td></tr><tr><td colspan="7">Note 1: An “(a)” in the table indicates that the system, task, or procedure, although not required to be present, may be examined if the appropriate airplane system is simulated in the FTD and is working properly.Note 2: Items not installed or not functional on the FTD and not appearing on the SOQ Configuration List, are not required to be listed as exceptions on the SOQ.Note 3: A “(t)” in the table indicates that the task may only be qualified for introductory initial or recurrent qualification training. These tasks may not be qualified for proficiency testing or checking credits in a GACA approved flight training program.</td></tr></table> GACA-AVSES-OPS-F050 Rev: 4, Date: 28 Jul 25 Page 15 of 91 GACA العامه للطيران المدني General Authority of Civil Aviation [Non-Text] FLIGHT TRAINING DEVICE (FTD) QUALIFICATION TEST CHECKLIST GACAR PART – 60 QPS REQUIREMENTS <table><tr><td colspan="7">In order to be qualified at the FTD qualification level indicated, the FTD must be able to perform at least the tasks associated with that level of qualification.</td></tr><tr><td colspan="5"></td><td colspan="2">Compliance</td></tr><tr><td>Entry Number</td><td>Subjective Requirements</td><td>FTD Level</td><td>Notes/Information</td><td>Yes</td><td>No</td><td>NA</td></tr><tr><td>1.</td><td>Instructor Operating Station (IOS).</td><td>See next</td><td>NA</td><td>□</td><td>□</td><td>□</td></tr><tr><td>1.a.</td><td>Power switch(es).</td><td>4,5,6</td><td>NA</td><td>□</td><td>□</td><td>□</td></tr><tr><td>1.b.</td><td>Airplane conditions.</td><td>4(a),5,6</td><td>e.g., GW, CG, Fuel loading, Systems, Ground. Crew</td><td>□</td><td>□</td><td>□</td></tr><tr><td>1.c.</td><td>Airports / Runways.</td><td>4,5,6</td><td>e.g., Selection and Presets; Surface and Lighting controls if equipped with a visual system.</td><td>□</td><td>□</td><td>□</td></tr><tr><td>1.d.</td><td>Environmental controls.</td><td>4,5,6</td><td>e.g., Temp, Wind.</td><td>□</td><td>□</td><td>□</td></tr><tr><td>1.e.</td><td>Airplane system malfunctions (Insertion / deletion)</td><td>4(a),5,6</td><td>NA</td><td>□</td><td>□</td><td>□</td></tr><tr><td>1.f.</td><td>Locks, Freezes, and Repositioning.</td><td>4,5,6</td><td>NA</td><td>□</td><td>□</td><td>□</td></tr><tr><td>1.g.</td><td>Sound Controls. (On / off / adjustment)</td><td>4,5,6</td><td>NA</td><td>□</td><td>□</td><td>□</td></tr><tr><td>1.h.</td><td>Motion / Control Loading System, as appropriate. On / off / emergency stop</td><td>4(a),5(a),6(a)</td><td>NA</td><td>□</td><td>□</td><td>□</td></tr><tr><td>2.</td><td>Observer Seats / Stations.</td><td>See next</td><td>NA</td><td>□</td><td>□</td><td>□</td></tr><tr><td>2.a.</td><td>Position / Adjustment / Positive restraint system.</td><td>4,5,6</td><td>NA</td><td>□</td><td>□</td><td>□</td></tr><tr><td colspan="7">Note 1: An "(a)" in the table indicates that the system, task, or procedure, although not required to be present, may be examined if the appropriate system is in the FTD and is working properly</td></tr></table> GACA-AVSES-OPS-F050 Rev: 4, Date: 28 Jul 25 Page 16 of 91 GACA العامه للطيران المدني General Authority of Civil Aviation FLIGHT TRAINING DEVICE (FTD) QUALIFICATION TEST CHECKLIST GACAR PART - 60 <table><tr><td colspan="7"></td><td colspan="3">Compliance</td></tr><tr><td>Test Entry Number</td><td>Test Title</td><td>Tolerance</td><td>Flight Conditions</td><td>Test Details</td><td>FTD Level</td><td>Notes/Information</td><td>Yes</td><td>No</td><td>NA</td></tr><tr><td>1.</td><td>Performance.</td><td>See next</td><td>See next</td><td>See next</td><td>See next</td><td>None</td><td>□</td><td>□</td><td>□</td></tr><tr><td>1.a</td><td>Taxi.</td><td>See next</td><td>See next</td><td>See next</td><td>See next</td><td>None</td><td>□</td><td>□</td><td>□</td></tr><tr><td>1,a.1</td><td>Minimum radius turn.</td><td>±0.9 m (3 ft) or ±20% of airplane turn radius.</td><td>Ground</td><td>Plot both main and nose gear lock and key engine parameter(s). Data for no brakes and the minimum thrust required to maintain a steady turn except for airplanes requiring asymmetric thrust or braking to achieve the minimum radius turn.</td><td>7</td><td>None</td><td>□</td><td>□</td><td>□</td></tr><tr><td>1.a.2</td><td>Rate of turn versus nosewheel steering angle (NWA).</td><td>±10% or ±2°/s of turn rate.</td><td>Ground.</td><td>Record for a minimum of two speeds, greater than minimum turning radius speed with one at a typical taxi speed, and with a spread of at least 5 kt.</td><td>7</td><td>None</td><td>□</td><td>□</td><td>□</td></tr><tr><td>1.b</td><td>Takeoff.</td><td>See next</td><td>See next</td><td>Note: For Level 7 FTD, all airplane manufacturer commonly used certificated take-off flap settings must be demonstrated at least once either in minimum unstick speed (1.b.3), normal take-off (1.b.4), critical engine failure on take-off (1.b.5) or crosswind take-off (1.b.6).</td><td>See next</td><td>None</td><td>□</td><td>□</td><td>□</td></tr><tr><td>1.b.1</td><td>Ground acceleration time and distance.</td><td>±1.5 s or ±5% of time; and ±61 m (200 ft) or ±5% of distance. For Level 6 FTD: ±1.5 s or ±5% of time.</td><td></td><td>Acceleration time and distance must be recorded for a minimum of 80% of the total time from brake release to Vr. Preliminary aircraft certification data may be</td><td>6,7</td><td>May be combined with normal takeoff (1.b.4.) or rejected takeoff (1.b.7.). Plotted data should be shown using appropriate scales for each portion of the maneuver.</td><td>□</td><td>□</td><td>□</td></tr></table> GACA-AVSES-OPS-F050 Rev: 4, Date: 28 Jul 25 Page 17 of 91 GACA العامه للطيران المدني General Authority of Civil Aviation [Non-Text] FLIGHT TRAINING DEVICE (FTD) QUALIFICATION TEST CHECKLIST GACAR PART - 60 <table><tr><td></td><td></td><td></td><td></td><td>used.</td><td></td><td>For Level 6 FTD, this test is required only if RTO training credit is sought.</td><td></td><td></td></tr><tr><td>1.b.2</td><td>Minimum control speed, ground (Vmcg) using aerodynamic controls only per applicable airworthiness requirement or alternative engine inoperative test to demonstrate ground control characteristics.</td><td>±25% of maximum airplane lateral deviation reached or ±1.5 m (5 ft). For airplanes with reversible flight control systems: ±10% or ±2.2 daN (5 lbf) rudder pedal force.</td><td>Takeoff.</td><td>Engine failure speed must be within ±1 kt of airplane engine failure speed. Engine thrust decay must be that resulting from the mathematical model for the engine applicable to the FTD under test. If the modeled engine is not the same as the airplane manufacturer's flight test engine, a further test may be run with the same initial conditions using the thrust from the flight test data as the driving parameter.</td><td>7</td><td>If a Vmcg test is not available, an acceptable alternative is a flight test snap engine deceleration to idle at a speed between V1 and V1-10 kt, followed by control of heading using aerodynamic control only and recovery should be achieved with the main gear on the ground. To ensure only aerodynamic control, nosewheel steering must be disabled (i.e. castored) or the nosewheel held slightly off the ground.</td><td>□</td><td>□</td><td>□</td></tr><tr><td>1.b.3</td><td>Minimums unstick speed (Vmu) or equivalent test to demonstrate early rotation take-off characteristics.</td><td>±3 kt air speed. ±1.5° pitch angle.</td><td>Takeoff.</td><td>Record time history data from 10 knots before start of rotation until at least 5 seconds after the occurrence of main gear lift-off.</td><td>7</td><td>Vmu is defined as the minimum speed at which the last main landing gear leaves the ground. Main landing gear strut compression or equivalent air/ground signal should be recorded. If a Vmu test is not available, alternative acceptable flight tests are a constant high-attitude takeoff run through main gear lift-off or an early rotation takeoff. If either of these alternative solutions is selected, aft body contact/tail strike protection functionality, if present on the airplane, it should be active.</td><td>□</td><td>□</td><td>□</td></tr><tr><td>1.b.4</td><td>Normal take-off.</td><td>±3 kt air speed. ±1.5° pitch angle. ±1.5° AOA. ±6 m (20 ft) height. For airplanes with reversible flight control</td><td>Takeoff.</td><td>Data required for near maximum certificated takeoff weight at mid center of gravity location and light takeoff weight at an aft</td><td>7</td><td>The test may be used for ground acce …(181,394 more chars)