# Short Bros SD-360-300 - Type: Aircraft model (FAA registry) - Registry code: 8100610 - Manufacturer (registry): SHORT BROS - Model: SD-360-300 - Aircraft type: Fixed wing multi engine - Category: Airplane - Engines: 2 · Turbo-prop - Seats: 30 - Weight class: 12,500 to 19,999 lb - Certification: Type certificated - Registered aircraft: 3 - Page: https://openairdocs.org/model/short-bros-sd-360-300 Model codes come from the FAA registry's reference file. ADs are matched to them by model name and maker. ## ADs that may apply (OpenAirDocs) Matched to this model by model name and maker. Each AD's applicability may narrow it by serial number, part number or equipment. None matched. ## Registered aircraft (3) - [N688AN](https://openairdocs.org/aircraft/N688AN): [Acc Integrated Services Inc](https://openairdocs.org/faa-owner/ACC%20INTEGRATED%20SERVICES%20INC), [Milwaukee, WI](https://openairdocs.org/faa-place/WI/Milwaukee), built 1984, S/N SH3633 - [N918GD](https://openairdocs.org/aircraft/N918GD): [Air Charter Inc DBA](https://openairdocs.org/faa-owner/AIR%20CHARTER%20INC%20DBA), [Culebra, PR](https://openairdocs.org/faa-place/PR/Culebra), S/N SH-3741 - [N970AA](https://openairdocs.org/aircraft/N970AA): [Acc Integrated Services Inc](https://openairdocs.org/faa-owner/ACC%20INTEGRATED%20SERVICES%20INC), [Milwaukee, WI](https://openairdocs.org/faa-place/WI/Milwaukee), built 1988, S/N 3737 ## NTSB investigations (3) From the NTSB's public API. Aircraft are matched to registry aircraft by N-number and event date, checked against the reported serial number, make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model. - [NTSB WPR21LA247](https://openairdocs.org/ntsb/WPR21LA247), Jun 25, 2021: Short Bros SD-360-300 (N970AA), Las Vegas, NV, substantial damage. Probable cause: The pilot’s failure to extend the landing gear during landing and the check pilot’s inadequate supervision. - [NTSB GAA15CA043](https://openairdocs.org/ntsb/GAA15CA043), Apr 16, 2015: Short Bros SD 360-300 (N688AN), Greer, SC, substantial damage. Probable cause: The fuel truck driver's inattention, which resulted in backing over a warning cone and into the horizontal stabilizer of the airplane. - [NTSB CHI06FA077](https://openairdocs.org/ntsb/CHI06FA077), Feb 5, 2006: Short Brothers SD-360-300 (N372AC), Watertown, WI, substantial damage, 3 fatal. Probable cause: The other airplane's flight crew failure to maintain clearance while maneuvering during formation flight. Contributing to the accident was the decision of both flight crews to fly in formation. ## FAA accident and incident reports (4) From the FAA Accident/Incident Data System. Reports are matched to registry aircraft by N-number and event date, checked against the reported make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model. - [Incident 20260814012059I](https://openairdocs.org/incident/20260814012059I), Aug 14, 2026: Short Bros SD-360-300 (N918GD), San Juan, PR, Minor damage. On Friday, August 14, 2026, at approximately 20:05 (l) local time (sju), [privacy data omitted] was on final approach to Luis muÑoz marÍn international… - [Accident 20210625007149A](https://openairdocs.org/incident/20210625007149A), Jun 25, 2021: Short Bros SD-360-300 (N970AA), Las Vegas, NV, Substantial damage. On June 25, 2021, at 13:37 pacific standard time (PST), a [privacy data omitted]SD3-60 (N970AA), operated by [privacy data omitted] experienced a gear-up… - [Incident 20150415004409I](https://openairdocs.org/incident/20150415004409I), Apr 15, 2015: Short Bros SD-360-300 (N688AN), Greenville, SC, Minor damage. On April 5, 2015 a stevens aviation, inc. fuel truck backed in to N688AN while pilot was on board. - [Accident 20060205004221A](https://openairdocs.org/incident/20060205004221A), Feb 5, 2006: Stbros SD360300 (N372AC), Watertown, WI, Substantial damage. (-23) Interviews with the surviving crew revealed that both aircraft were being flown for a maintenance check flight, checking fuel flow rates, prior to… ## Service difficulty reports (15) As reported by operators and repair stations, by the model named in the report. - [SDR 2026FA0000674](https://openairdocs.org/sdr/2026FA0000674), Aug 14, 2026: ACTUATOR. FAILED. AS THE PILOT AND COPILOT WERE COMING IN TO LAND, LANDING GEAR WAS LOWERED AND NOTICED THAT THE FRONT (NOSE) WHEEL LANDING GEAR INDICATION WAS RED. CREW DECIDED - [SDR DATA20220909001](https://openairdocs.org/sdr/DATA20220909001), Sep 5, 2022: FIRE LOOP. DEFECTIVE. CREW RECEIVED LEFT ENGINE FIRE WARNING AND FIRE FAULT INDICATION DURING CRUISE. CREW EXECUTED MEMORY ITEMS AND QRH PROCEDURES FOR ENGINE FIRE, DECLARED AND EMER - [SDR DATA2022040600001](https://openairdocs.org/sdr/DATA2022040600001), Apr 6, 2022: WINDSHIELD. IMPROPER PART. DURING CRUISE THE RIGHT WINDSHIELD HEAT CIRCUIT TERMINAL BOARD AT THE BASE OF THE WINDSHIELD STARTED SMOKING AND WINDSHIELD HEAT WAS INOPERATIVE. MAINTENANCE RE - [SDR DATA07092021001](https://openairdocs.org/sdr/DATA07092021001), Jul 7, 2021: GOVERNOR. INOPERATIVE. AT 10,000 MSL ON CLIMB THE NUMBER 2 PROPELLER RPM SLOWLY STARTED TO DECREASE. AN ATTEMPT TO FORWARD THE PROPELLER LEVER CAUSED THE RPM DECREASE TO CONTINUE. THE - [SDR DATA2021030901](https://openairdocs.org/sdr/DATA2021030901), Mar 8, 2021: GAS GENERATOR. LOW TORQUE. DURING CLIMB CHECKS FLIGHT CREW OBSERVED THE RIGHT PROPELLER RPM DROPPED TO THE 800 RANGE. THE MOVED THE ENGINE CONTROL LEVERS FORWARDS AND BACKWARDS ON THE AFF - [SDR DATA20180809701](https://openairdocs.org/sdr/DATA20180809701), Aug 7, 2018: HYDRAULIC SYSTEM. LEAKING. CREW OBSERVED A LT HYD LIGHT ILLUMINATED AND QUANTITY FLUCTUATED. AIRCRAFT SLOWED AND GEAR SUCCESSFULLY EXTENDED AS A PRECAUTION. HYD LT AND HYD RT INDICATORS I - [SDR DATA20180604101](https://openairdocs.org/sdr/DATA20180604101), Jun 1, 2018: ENGINE. POWER LOSS. ON A 5 MILE FINAL WITH AN RJ IN TRAIL BY 3 MILES, PULLED POWER BACK TO IDLE. RIGHT ENGINE MADE A POPPING NOISE AND STARTED FLUCTUATING IN TORQUE. P USHED BOTH P - [SDR DATA2017020301](https://openairdocs.org/sdr/DATA2017020301), Feb 3, 2017: ENGINE. OVERTEMP. AFTER TAKE OFF, DURING NORMAL CLIMB, CLIMB CHECKLIST ACCOMPLISHED, NR 1 ENGINE ITT WAS NOTED TO BE HIGH AT 840°- OIL PSI 125 - OIL TEMP 110°. POWER WAS REDUCED - [SDR DATA2015033101](https://openairdocs.org/sdr/DATA2015033101), Mar 31, 2015: WIRE. BROKEN. ON TAKEOFF ROLL RT ENG RTOP SYS FAILED TO ACTIVATE. TAKEOFF WAS ABORTED IAW ACC SOP'S. ACFT RETURNED TO BLOCK. UPON TROUBLESHOOTING IT WAS FOUND THAT A BROKEN W - [SDR TXHA2011F00184](https://openairdocs.org/sdr/TXHA2011F00184), Aug 17, 2011: HYDRAULIC SYSTEM. LOW. AFTER DEPARTURE, HYD LIGHT ILLUMINATED, WHEN GEAR WAS RETRACTED. RETURNED TO BASE. ACFT HYD SYS WAS SERVICED AND ACFT DEPARTED WITHOUT FURTHER INCIDENT. - [SDR EXDA972AA031009](https://openairdocs.org/sdr/EXDA972AA031009), Mar 8, 2009: DOWNLOCK SWITCH. OUT OF ADJUST. WHILE ON SHORT FINAL TO LAND AT AEX THE LANDING GEAR WARNING HORN SOUNDED WHEN THE FLAP LEVER WAS MOVED FROM 15 TO 30 DEGREES. ALL THREE LANDING GEAR INDICATOR - [SDR DATA200700010](https://openairdocs.org/sdr/DATA200700010), Nov 27, 2007: LINE. BROKEN. ENGINE FAILED APPROX 15 MILES SSW OF NEW HOPE VA. LEFT ENGINE INSTRUMENTS DECREASING. INFORMED FO TO CONFIRM LEFT ENGINE FAILURE. COMPLETED PROCEDURE ACCORDING - [SDR 2003FA0000771](https://openairdocs.org/sdr/2003FA0000771), Jul 18, 2003: LINE. BROKEN. AIRCRAFT WAS CROSSING THE NORTH ATLANTIC BETWEEN GREENLAND AND ICELAND AND ONCE THEY REACHED CRUSING ALTITUDE THE LEFT ENGINE SHUT DOWN. THEY STARTED LOSING ALT - [SDR CA030110002](https://openairdocs.org/sdr/CA030110002), Jan 8, 2003: CONTROL CABLE. BROKEN. (CAN) PILOT REPORTED THAT FLAPS WOULD NOT EXTEND TO SELECTED POSITION. THEY WOULD FALL 2-4 DEGREES SHORT OF SELECTED POSITION. RETRACTION WAS OKAY. INVESTIGATIO - [SDR CA011101015](https://openairdocs.org/sdr/CA011101015), Oct 29, 2001: GEARBOX. LEAKING. (CAN) DURING LAST 2 MINUTES OF APPROACH THE RT HYDRAULIC PRESSURE DROPPED OFF. AIRCRAFT LANDED UNEVENTFULLY AND WAS TOWED TO HANGAR. RT HYDRAULIC PUMP WAS REPLA --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.