# Short Bros. & Harland SD-3-60-200

- Type: Aircraft model (FAA registry)
- Registry code: 8100607
- Manufacturer (registry): SHORT BROS. & HARLAND
- Model: SD-3-60-200
- Aircraft type: Fixed wing multi engine
- Category: Airplane
- Engines: 2 · Turbo-prop
- Seats: 30
- Weight class: Up to 12,499 lb
- Certification: Type certificated
- Registered aircraft: 3
- Page: https://openairdocs.org/model/short-bros-harland-sd-3-60-200

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)

- [N368AC](https://openairdocs.org/aircraft/N368AC): [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 SH3651
- [N808TR](https://openairdocs.org/aircraft/N808TR): [Trans Executive Airlines Of Hawaii Inc DBA](https://openairdocs.org/faa-owner/TRANS%20EXECUTIVE%20AIRLINES%20OF%20HAWAII%20INC%20DBA), [Honolulu, HI](https://openairdocs.org/faa-place/HI/Honolulu), built 1987, S/N SH3718
- [N916GD](https://openairdocs.org/aircraft/N916GD): [Air Charter Inc DBA](https://openairdocs.org/faa-owner/AIR%20CHARTER%20INC%20DBA), [Culebra, PR](https://openairdocs.org/faa-place/PR/Culebra), built 1989, S/N SH3751

## NTSB investigations

None matched to aircraft with this model.

## 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 20240514007519I](https://openairdocs.org/incident/20240514007519I), May 14, 2024: Short Bros. & Harland SD-3-60-200 (N916GD), Christiansted, VI, Minor damage. The investigation revealed on approach to tisx airport, that ATC issued a vector of 150 degrees to allow an aircraft to overtake the SD3-60-200. The traffic…
- [Incident 20180120023919I](https://openairdocs.org/incident/20180120023919I), Jan 20, 2018: Short Bros. & Harland SD-3-60-200 (N808TR), Kalaeloa, HI, Minor damage. While conducting a single engine approach and landing during a training flight the crew did not extend the landing gear. The aircraft touched down and slid to…
- [Incident 20060102000279I](https://openairdocs.org/incident/20060102000279I), Jan 2, 2006: Stbros SD360 (N808TR), Kahului, HI. (-23) Smoke in cockpit reported by PIC. Mechanic found two wire terminals that had signs of arcing in the left avionics bay. Mechanic repaired and repositioned…
- [Incident 20040520010429I](https://openairdocs.org/incident/20040520010429I), May 20, 2004: Stbros SD360200 (N808TR), Honolulu, HI, No damage. (-23) Shut down #2 engine for loss of oil pressure. Operator removed power section found broken blades on power turbine. There was no indication on recent…

## Service difficulty reports (12)

As reported by operators and repair stations, by the model named in the report.

- [SDR DATA2021043001](https://openairdocs.org/sdr/DATA2021043001), Apr 30, 2021: GOVERNOR. MALFUNCTIONED. DURING A TRAINING FLIGHT, WHEN SIMULATING THE V1 CUT THE LEFT PROPELLER TRIED TO GO INTO AUTOFEATHER AND THE ENGINE SURGED. NO SUBSEQUENT POWER SETTINGS AFFECTE
- [SDR DATA2021042800087](https://openairdocs.org/sdr/DATA2021042800087), Apr 27, 2021: LINE. DAMAGED. DURING CLIMB CHECKS DUAL HYDRAULIC WARNING LIGHTS ON CWP. HYDRAULIC PANEL SHOWED DECREASING CONTENTS INDICATING A FLUID LOSS. CREW SELECTED GEAR DOWN AND RECEIV
- [SDR DATA2020031601](https://openairdocs.org/sdr/DATA2020031601), Mar 13, 2020: SWITCH. OUT OF ADJUST. IN CLIMB AT 3500 FEET WHEN PILOTS REDUCED THROTTLE THE RIGHT PROPELLER WENT INTO FEATHER. QRH PROCEDURES FOLLOWED, EMERGENCY DECLARED AND AIRCRAFT RETURNED TO B
- [SDR DATA20191220001](https://openairdocs.org/sdr/DATA20191220001), Dec 18, 2019: HYDRAULIC SYSTEM. LOW PRESSURE. ON APPROACH TO LAND THE BRAKES WERE FOUND TO BE INDICATING NO PRESSURE WHEN TESTED AFTER COMPLETION OF APPROACH CHECKS. APPROACH WAS TERMINATED TO DIAGNOSE THE 
- [SDR UOIA2019071900001](https://openairdocs.org/sdr/UOIA2019071900001), Jul 19, 2019: PUMP. INOPERATIVE. LEFT HYDRAULIC PUMP OUT.
- [SDR DATA 201805180601](https://openairdocs.org/sdr/DATA%20201805180601), May 16, 2018: DIODE. BURNED. AFTER DEPARTURE, STARTED SMELLING PLASTIC FUMES. FOUND THE AUDIO PANEL CIRCUIT BREAKER HAD TRIPPED. LOST ALL COMMS AND INTERCOM. LEVELED AT 8000 MSL. ALL COMM H
- [SDR DATA2016081601](https://openairdocs.org/sdr/DATA2016081601), Aug 16, 2016: INDICATION SYS. FALSE INDICATION. ON APPROACH, FOLLOWING APPROACH CHECKLIST AND SELECTING GEAR DOWN, F/O NOTED THE NOSE GEAR LIGHT ILLUMINATED RED, WHILE THE GEAR LEFT AND GEAR RIGHT WERE GREEN.
- [SDR TXHA20140924001](https://openairdocs.org/sdr/TXHA20140924001), Sep 24, 2014: WARNING SYSTEM. ACTIVATED. ON INITIAL EXTENSION, THE NOSE GEAR LIGHT ILLUMINATED RED. RECYCLED GEAR FOR GREEN ILLUMINATION & CONFIRMED WITH TOWER & ACFT IN TRAFFIC PATTERN ON NOSE GEAR EX
- [SDR TXH2010F00001](https://openairdocs.org/sdr/TXH2010F00001), Apr 26, 2010: OIL COOLER. LEAKING. NR 1 ENGINE OIL PRESSURE DROPPED DOWN IN FLIGHT. CHANGED OIL COOLER AND LEAK CHECKED, OK.
- [SDR TXH2010F00000](https://openairdocs.org/sdr/TXH2010F00000), Apr 24, 2010: OIL FILTER. CLOGGED. DURING CLIMB PHASE OF FLIGHT, NR 1 ENGINE OIL PRESSURE BEGAN TO FLUCUTATE BETWEEN 90-50 PSI ALL OTHER INDICATIONS WERE NORMAL. RETURNED TO DEPARTURE, MX CHECKED
- [SDR 2009F00064](https://openairdocs.org/sdr/2009F00064), Aug 26, 2009: SKIN. PUNCTURED. WHEN THE ACFT WAS ON GROUND AND PARKED, A FORKLIFT PUNCTURED THE ACFT SKIN BELOW THE MAIN CARGO DOOR DURING LOADING. ACFT WAS MX FERRIED TO MAIN BASE FOR REPAIR
- [SDR DATA200700009](https://openairdocs.org/sdr/DATA200700009), Nov 17, 2007: LINE. BROKEN. WITH ABOUT 500' TO TOUCHDOWN THE LEFT ENGINE WENT INTO FEATHER (NO INDICATION ON CWP). ALL ENGINE INSTRUMENTS WERE NORMAL EXCEPT TORQUE AT 0 LBS. TORQUE WAS SET

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