085 -atd-evaluation-and-subjective-test-criteria-part -60

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GACA
العربيه العاميه للطيران المدني
General Authority of Civil Aviation
ATD EVALUATION AND SUBJECTIVE TEST CRITERIA
GACAR PART - 60
<table><tr><td>ATD Operator Name</td><td colspan="4"></td></tr><tr><td>ATD Qualification Level</td><td colspan="2">□ Basic Aviation Training Device (BATD)</td><td colspan="2">□ Advanced Aviation Training Device (AATD)</td></tr><tr><td>ATD Qualification Type</td><td>□ Initial Qualification</td><td>□ Qualification renewal</td><td>□ Modification</td><td>□ Re-location</td></tr><tr><td>ATD Manufacturer Name</td><td colspan="4"></td></tr><tr><td>ATD Serial No</td><td colspan="4"></td></tr><tr><td>ATD Qualification Number</td><td colspan="4"></td></tr><tr><td>ATD Qualification Expiry Date</td><td colspan="4"></td></tr></table>
APPENDIX E. EVALUATION AND SUBJECTIVE TEST CRITERIA
1. General Requirements and Evaluation.
1.1 Devices eligible as an Aviation Training Device (ATD) must conform to an acceptable aircraft cockpit configuration and instrument panel design. (See Checklist B, Basic Aviation Training Device (BATD) Requirements, and Checklist C, Advanced Aviation Training Device (AATD) Requirements). The simulated systems and subsystems should be able to perform operational functions and performance maneuvers that closely mimic the represented aircraft. Specific attention should be given to ergonomic and human factors.
1.2 ATDs must be designed to readily facilitate training, practice, and improving piloting skills. This should include both the procedural and operational performance tasks specified in the Airman Certification Standards (ACS). The criteria listed in Checklists B and C and this checklist will be used to determine whether the design and performance of the training device qualifies GACA approval as an ATD. GACA will use the following checklist during the evaluation of an ATD and must be included in the Qualification and Approval Guide (QAG):
E-1. PROCEDURES AND TASKS TEST CHECKLIST
<table><tr><td colspan="2"></td><td>Maneuvers and Tasks</td><td>GACAR Reference</td><td>YES</td><td>NO</td><td>NA</td></tr><tr><td>a)</td><td>Pre-takeoff</td><td></td><td>V4 CHP 30) (AC) 61-136B</td><td>□</td><td>□</td><td>□</td></tr><tr><td>1.</td><td>Engine start</td><td></td><td>V4 CHP 30) (AC) 61-136B</td><td>□</td><td>□</td><td>□</td></tr><tr><td>2.</td><td>Taxi and brake operation</td><td></td><td>(V4 CHP 30) (AC) 61-136B</td><td>□</td><td>□</td><td>□</td></tr><tr><td>b)</td><td>Takeoff</td><td></td><td>(V4 CHP 30) (AC) 61-136B</td><td>□</td><td>□</td><td>□</td></tr><tr><td>1.</td><td>AIRPLANE Takeoff</td><td></td><td>(V4 CHP 30) (AC) 61-136B</td><td>□</td><td>□</td><td>□</td></tr><tr><td>i.</td><td>Run-up and power plant checks</td><td></td><td>(V4 CHP 30) (AC) 61-136B</td><td>□</td><td>□</td><td>□</td></tr><tr><td>ii.</td><td>Acceleration characteristics</td><td></td><td>(V4 CHP 30) (AC) 61-136B</td><td>□</td><td>□</td><td>□</td></tr><tr><td>iii.</td><td>Nose wheel and rudder steering</td><td></td><td>(V4 CHP 30) (AC) 61-136B</td><td>□</td><td>□</td><td>□</td></tr><tr><td>iv.</td><td>Effect of crosswind</td><td></td><td>(V4 CHP 30) (AC) 61-136B</td><td>□</td><td>□</td><td>□</td></tr><tr><td>v</td><td>Instrument</td><td></td><td>(V4 CHP 30) (AC) 61-136B</td><td>□</td><td>□</td><td>□</td></tr><tr><td>vi</td><td>Landing gear, wing flap operation</td><td></td><td>(V4 CHP 30) (AC) 61-136B</td><td>□</td><td>□</td><td>□</td></tr><tr><td>2.</td><td>HELICOPTER Takeoff</td><td></td><td>(V4 CHP 30) (AC) 61-136B</td><td>□</td><td>□</td><td>□</td></tr><tr><td>i.</td><td>Power plant checks</td><td></td><td>(V4 CHP 30) (AC) 61-136B</td><td>□</td><td>□</td><td>□</td></tr><tr><td>ii.</td><td>From hover</td><td></td><td>(V4 CHP 30) (AC) 61-136B</td><td>□</td><td>□</td><td>□</td></tr><tr><td>iii.</td><td>From ground</td><td></td><td>(V4 CHP 30) (AC) 61-136B</td><td>□</td><td>□</td><td>□</td></tr><tr><td>iv.</td><td>Vertical</td><td></td><td>(V4 CHP 30) (AC) 61-136B</td><td>□</td><td>□</td><td>□</td></tr><tr><td>v</td><td>Running</td><td></td><td>(V4 CHP 30) (AC) 61-136B</td><td>□</td><td>□</td><td>□</td></tr><tr><td>c)</td><td>In-Flight Operation</td><td></td><td>(V4 CHP 30) (AC) 61-136B</td><td>□</td><td>□</td><td>□</td></tr><tr><td>1.</td><td>AIRPLANE In-Flight Operation</td><td></td><td>(V4 CHP 30) (AC) 61-136B</td><td>□</td><td>□</td><td>□</td></tr><tr><td colspan="2">i. Climb</td><td></td><td>(V4 CHP 30) (AC) 61-136B</td><td>□</td><td>□</td><td>□</td></tr></table>
GACA-AVSES-OPS-F085
Rev: 3, Date: 15 Jul 25
Page 1 of 4

GACA
ال necesita للطيران المدني
General Authority of Civil Aviation
[Non-Text]
ATD EVALUATION AND SUBJECTIVE TEST CRITERIA
GACAR PART - 60
<table><tr><td>(a)</td><td>Normal and max. performance</td><td>(V4 CHP 30 (AC) 61-136B</td><td>□</td><td>□</td><td>□</td></tr><tr><td>(b)</td><td>One-engine-inoperative procedures (multiengine)</td><td>(V4 CHP 30) (AC) 61-136B</td><td>□</td><td>□</td><td>□</td></tr><tr><td>ii.</td><td>Cruise</td><td>(V4 CHP 30) (AC) 61-136B</td><td>□</td><td>□</td><td>□</td></tr><tr><td>(a)</td><td>Performance characteristics (speed vs. power)</td><td>(V4 CHP 30) (AC) 61-136B</td><td>□</td><td>□</td><td>□</td></tr><tr><td>(b)</td><td>Normal and steep turns</td><td>(V4 CHP 30) (AC) 61-136B</td><td>□</td><td>□</td><td>□</td></tr><tr><td>(c)</td><td>Approach to stalls (i.e., stall warning), stalls, and recovery. Execute from takeoff, cruise, and approach and landing configurations.</td><td>(V4 CHP 30)) (AC) 61-136B</td><td>□</td><td>□</td><td>□</td></tr><tr><td>(d)</td><td>In-flight engine shutdown (multiengine)</td><td>(V4 CHP 30) (AC) 61-136B</td><td>□</td><td>□</td><td>□</td></tr><tr><td>(e)</td><td>Fuel selector function</td><td>(V4 CHP 30) (AC) 61-136B</td><td>□</td><td>□</td><td>□</td></tr><tr><td>(f)</td><td>In-flight engine start</td><td>(V4 CHP 30) (AC) 61-136B</td><td>□</td><td>□</td><td>□</td></tr><tr><td>iii.</td><td>Approach</td><td>(V4 CHP 30) (AC) 61-136B</td><td>□</td><td>□</td><td>□</td></tr><tr><td>(a)</td><td>Normal (with and without flaps) (check gear warning, if applicable)</td><td>(V4 CHP 30) (AC) 61-136B</td><td>□</td><td>□</td><td>□</td></tr><tr><td>(b)</td><td>Best glide no power</td><td>(V4 CHP 30) (AC) 61-136B</td><td>□</td><td>□</td><td>□</td></tr><tr><td>iv.</td><td>Landings</td><td>(V4 CHP 30) (AC) 61-136B</td><td>□</td><td>□</td><td>□</td></tr><tr><td>2)</td><td>HELICOPTER In-Flight Operation</td><td>V4 CHP 30) (AC) 61-136B</td><td>□</td><td>□</td><td>□</td></tr><tr><td>i.</td><td>Hovering and air taxi</td><td>V4 CHP 30) (AC) 61-136B</td><td>□</td><td>□</td><td>□</td></tr><tr><td>(a)</td><td>Forward</td><td>V4 CHP 30) (AC) 61-136B</td><td>□</td><td>□</td><td>□</td></tr><tr><td>(b)</td><td>Rearward</td><td>V4 CHP 30) (AC) 61-136B</td><td>□</td><td>□</td><td>□</td></tr><tr><td>(c)</td><td>Sideward</td><td>V4 CHP 30) (AC) 61-136B</td><td>□</td><td>□</td><td>□</td></tr><tr><td>(d)</td><td>Turns</td><td>V4 CHP 30) (AC) 61-136B</td><td>□</td><td>□</td><td>□</td></tr><tr><td>ii.</td><td>Climb</td><td>V4 CHP 30) (AC) 61-136B</td><td>□</td><td>□</td><td>□</td></tr><tr><td>iii.</td><td>Cruise</td><td>V4 CHP 30) (AC) 61-136B</td><td>□</td><td>□</td><td>□</td></tr><tr><td>(a)</td><td>Performance characteristics (speed vs. power)</td><td>V4 CHP 30) (AC) 61-136B</td><td>□</td><td>□</td><td>□</td></tr><tr><td>(b)</td><td>Turns</td><td>V4 CHP 30) (AC) 61-136B</td><td>□</td><td>□</td><td>□</td></tr><tr><td>(i)</td><td>Recovery</td><td>V4 CHP 30) (AC) 61-136B</td><td>□</td><td>□</td><td>□</td></tr><tr><td>(ii)</td><td>Skidding</td><td>V4 CHP 30) (AC) 61-136B</td><td>□</td><td>□</td><td>□</td></tr><tr><td>(iii)</td><td>Slipping</td><td>V4 CHP 30) (AC) 61-136B</td><td>□</td><td>□</td><td>□</td></tr><tr><td>(iv)</td><td>Steep turns</td><td>V4 CHP 30) (AC) 61-136B</td><td>□</td><td>□</td><td>□</td></tr><tr><td>(c)</td><td>In-flight engine shutdown and start (multiengine)</td><td>V4 CHP 30) (AC) 61-136B</td><td>□</td><td>□</td><td>□</td></tr><tr><td>(d)</td><td>Descents</td><td>V4 CHP 30) (AC) 61-136B</td><td>□</td><td>□</td><td>□</td></tr><tr><td>(e)</td><td>Straight in and 180° autorotation</td><td>V4 CHP 30) (AC) 61-136B</td><td>□</td><td>□</td><td>□</td></tr><tr><td>(f)</td><td>Landings</td><td>V4 CHP 30) (AC) 61-136B</td><td>□</td><td>□</td><td>□</td></tr><tr><td>d)</td><td>Instrument Approaches</td><td>V4 CHP 30) (AC) 61-136B</td><td>□</td><td>□</td><td>□</td></tr><tr><td>1)</td><td>Non- precision</td><td>V4 CHP 30) (AC) 61-136B</td><td>□</td><td>□</td><td>□</td></tr><tr><td>i)</td><td>GPS and LPV</td><td>V4 CHP 30) (AC) 61-136B</td><td>□</td><td>□</td><td>□</td></tr><tr><td>ii)</td><td>GPS-WAAS (optional)</td><td>V4 CHP 30) (AC) 61-136B</td><td>□</td><td>□</td><td>□</td></tr><tr><td>iii)</td><td>All engines operating</td><td>V4 CHP 30) (AC) 61-136B</td><td>□</td><td>□</td><td>□</td></tr><tr><td>iv)</td><td>One or more engines inoperative</td><td>V4 CHP 30) (AC) 61-136B</td><td>□</td><td>□</td><td>□</td></tr><tr><td>v)</td><td>Approach procedures (VOR, VOR/DME, LOC procedures on an ILS, LDA, RNAV (RDP) or RNAV (GPS) to LNAV, LNAV/VNAV or LPV)</td><td>V4 CHP 30) (AC) 61-136B</td><td>□</td><td>□</td><td>□</td></tr><tr><td>2)</td><td>Precision</td><td>V4 CHP 30) (AC) 61-136B</td><td>□</td><td>□</td><td>□</td></tr><tr><td>i)</td><td>ILS</td><td>V4 CHP 30) (AC) 61-136B</td><td>□</td><td>□</td><td>□</td></tr></table>
GACA-AVSES-OPS-F085
Rev: 3, Date: 15 Jul 25
Page 2 of 4

GACA
المنيه العامه للطيران المدني
General Authority of Civil Aviation
[Non-Text]
ATD EVALUATION AND SUBJECTIVE TEST CRITERIA
GACAR PART – 60
<table><tr><td>ii)</td><td>GLS (optional)</td><td>V4 CHP 30) (AC) 61-136B</td><td>□</td><td>□</td><td>□</td></tr><tr><td>iii)</td><td>Effects of crosswind</td><td>V4 CHP 30) (AC) 61-136B</td><td>□</td><td>□</td><td>□</td></tr><tr><td>iv)</td><td>With engine inoperative (multiengine)</td><td>V4 CHP 30) (AC) 61-136B</td><td>□</td><td>□</td><td>□</td></tr><tr><td>v)</td><td>Missed approach</td><td>V4 CHP 30) (AC) 61-136B</td><td>□</td><td>□</td><td>□</td></tr><tr><td>(a)</td><td>Normal</td><td>V4 CHP 30) (AC) 61-136B</td><td>□</td><td>□</td><td>□</td></tr><tr><td>(b)</td><td>With engine(s) inoperative (multiengine)</td><td>V4 CHP 30) (AC) 61-136B</td><td>□</td><td>□</td><td>□</td></tr><tr><td>e)</td><td>Surface Operations</td><td>V4 CHP 30 (AC) 61-136B</td><td>□</td><td>□</td><td>□</td></tr><tr><td>1)</td><td>AIRPLANE Surface Operations (Post Landing)</td><td>V4 CHP 30 (AC) 61-136B</td><td>□</td><td>□</td><td>□</td></tr><tr><td>i)</td><td>Approach and landing roll</td><td>V4 CHP 30 (AC) 61-136B</td><td>□</td><td>□</td><td>□</td></tr><tr><td>ii)</td><td>Braking operation</td><td>V4 CHP 30 (AC) 61-136B</td><td>□</td><td>□</td><td>□</td></tr><tr><td>iii)</td><td>Reverse thrust operation, if applicable</td><td>V4 CHP 30 (AC) 61-136B</td><td>□</td><td>□</td><td>□</td></tr><tr><td>2)</td><td>HELICOPTER Surface Operations</td><td>V4 CHP 30 (AC) 61-136B</td><td>□</td><td>□</td><td>□</td></tr><tr><td>i)</td><td>Landings</td><td>V4 CHP 30 (AC) 61-136B</td><td>□</td><td>□</td><td>□</td></tr><tr><td>ii)</td><td>Landing area operations</td><td>V4 CHP 30 (AC) 61-136B</td><td>□</td><td>□</td><td>□</td></tr><tr><td>f)</td><td>HELICOPTER Emergency Operations</td><td>V4 CHP 30 (AC) 61-136B</td><td>□</td><td>□</td><td>□</td></tr><tr><td>1)</td><td>Power failure at hover</td><td>V4 CHP 30 (AC) 61-136B</td><td>□</td><td>□</td><td>□</td></tr><tr><td>2)</td><td>Power failure at altitude</td><td>V4 CHP 30 (AC) 61-136B</td><td>□</td><td>□</td><td>□</td></tr><tr><td>3)</td><td>System and equipment malfunctions</td><td>V4 CHP 30 (AC) 61-136B</td><td>□</td><td>□</td><td>□</td></tr><tr><td>4)</td><td>Settling with power (optional)</td><td>V4 CHP 30 (AC) 61-136B</td><td>□</td><td>□</td><td>□</td></tr><tr><td>5)</td><td>Low rotor RPM recovery (optional)</td><td>V4 CHP 30 (AC) 61-136B</td><td>□</td><td>□</td><td>□</td></tr><tr><td>6)</td><td>Antitorque system failure</td><td>V4 CHP 30 (AC) 61-136B</td><td>□</td><td>□</td><td>□</td></tr><tr><td>7)</td><td>Dynamic rollover (optional)</td><td>V4 CHP 30 (AC) 61-136B</td><td>□</td><td>□</td><td>□</td></tr><tr><td>g)</td><td>Any Flight Phase</td><td>V4 CHP 30 (AC) 61-136B</td><td>□</td><td>□</td><td>□</td></tr><tr><td>1)</td><td>Aircraft and Power-plant Systems</td><td>V4 CHP 30 (AC) 61-136B</td><td>□</td><td>□</td><td>□</td></tr><tr><td>i)</td><td>Electrical, mechanical, or hydraulic</td><td>V4 CHP 30 (AC) 61-136B</td><td>□</td><td>□</td><td>□</td></tr><tr><td>ii)</td><td>Flaps (airplane)</td><td>V4 CHP 30 (AC) 61-136B</td><td>□</td><td>□</td><td>□</td></tr><tr><td>iii)</td><td>Fuel selector and oil temp/pressure</td><td>V4 CHP 30 (AC) 61-136B</td><td>□</td><td>□</td><td>□</td></tr><tr><td>iv)</td><td>Landing gear (if applicable)</td><td>V4 CHP 30 (AC) 61-136B</td><td>□</td><td>□</td><td>□</td></tr><tr><td>2)</td><td>Flight Management and Guidance Systems</td><td>V4 CHP 30 (AC) 61-136B</td><td>□</td><td>□</td><td>□</td></tr><tr><td>i)</td><td>Autopilot (if standard equipment)</td><td>V4 CHP 30 (AC) 61-136B</td><td>□</td><td>□</td><td>□</td></tr><tr><td>ii)</td><td>Flight director (AATD only)/system displays (if installed)</td><td>V4 CHP 30 (AC) 61-136B</td><td>□</td><td>□</td><td>□</td></tr><tr><td>iii)</td><td>Navigation systems</td><td>V4 CHP 30 (AC) 61-136B</td><td>□</td><td>□</td><td>□</td></tr><tr><td>iv)</td><td>Stall warning systems avoidance (airplane)</td><td>V4 CHP 30 (AC) 61-136B</td><td>□</td><td>□</td><td>□</td></tr><tr><td>v)</td><td>Multi-function displays (if applicable)</td><td>V4 CHP 30 (AC) 61-136B</td><td>□</td><td>□</td><td>□</td></tr><tr><td>3)</td><td>Airborne Procedures</td><td>V4 CHP 30 (AC) 61-136B</td><td>□</td><td>□</td><td>□</td></tr><tr><td>i)</td><td>Holding</td><td>V4 CHP 30 (AC) 61-136B</td><td>□</td><td>□</td><td>□</td></tr><tr><td>ii)</td><td>Uncoordinated turns – slipping and skidding demo</td><td>V4 CHP 30 (AC) 61-136B</td><td>□</td><td>□</td><td>□</td></tr><tr><td>iii)</td><td>Configuration and power changes and resulting pitch changes</td><td>V4 CHP 30 (AC) 61-136B</td><td>□</td><td>□</td><td>□</td></tr><tr><td>iv)</td><td>Compass turns and appropriate errors (if installed)</td><td>V4 CHP 30 (AC) 61-136B</td><td>□</td><td>□</td><td>□</td></tr><tr><td>4)</td><td>Engine Shutdown and Parking</td><td>V4 CHP 30 (AC) 61-136B</td><td>□</td><td>□</td><td>□</td></tr><tr><td>i)</td><td>Systems operation</td><td>V4 CHP 30 (AC) 61-136B</td><td>□</td><td>□</td><td>□</td></tr><tr><td>ii)</td><td>Parking brake operation (if installed) (airplane)</td><td>V4 CHP 30 (AC) 61-136B</td><td>□</td><td>□</td><td>□</td></tr><tr><td>h)</td><td>Can simulate engine failure, including failures due to simulated</td><td>V4 CHP 30 (AC) 61-136B</td><td>□</td><td>□</td><td>□</td></tr></table>
GACA-AVSES-OPS-F085
Rev: 3, Date: 15 Jul 25
Page 3 of 4

GACA
ال necesita للطيران المدني
General Authority of Civil Aviation
[Non-Text]
ATD EVALUATION AND SUBJECTIVE TEST CRITERIA
GACAR PART - 60
<table><tr><td></td><td>loss of oil pressure or fuel starvation.</td><td></td><td></td><td></td><td></td></tr><tr><td>i)</td><td>Can simulate the following equipment or system failures:</td><td>V4 CHP 30 (AC) 61-136B</td><td>□</td><td>□</td><td>□</td></tr><tr><td>1)</td><td>Alternator or generator failure.</td><td>V4 CHP 30 (AC) 61-136B</td><td>□</td><td>□</td><td>□</td></tr><tr><td>2)</td><td>Vacuum pump/pressure failure and the associated flight instrument failures.</td><td>V4 CHP 30 (AC) 61-136B</td><td>□</td><td>□</td><td>□</td></tr><tr><td>3)</td><td>Gyroscopic flight instrument failures.</td><td>V4 CHP 30 (AC) 61-136B</td><td>□</td><td>□</td><td>□</td></tr><tr><td>4)</td><td>Pitot/static system malfunction and the associated flight instrument failures.</td><td>V4 CHP 30 (AC) 61-136B</td><td>□</td><td>□</td><td>□</td></tr></table>
<table><tr><td>Remarks</td></tr></table>
<table><tr><td colspan="4">Inspection Result</td></tr><tr><td colspan="2">□ Satisfactory</td><td colspan="2">□ Unsatisfactory</td></tr><tr><td>No.</td><td>Inspector Name</td><td>Signature</td><td>Date (dd/mm/yy)</td></tr><tr><td></td><td></td><td></td><td></td></tr><tr><td></td><td></td><td></td><td></td></tr></table>
GACA-AVSES-OPS-F085
Rev: 3, Date: 15 Jul 25
Page 4 of 4