- Registered owner
- Acc Integrated Services Inc
- Location
- Milwaukee, WI
- Owner type
- Corporation
- Serial number
- SH3764
- Year built
- 1991
- Type
- Fixed wing multi engine
- Engine
- Turbo-prop
- Airworthiness
- Standard, transport
- Airworthiness date
- June 10, 2015
- Certificate issued
- April 3, 2015
- Expires
- April 30, 2028
- Mode S code
- AA513C
Short Bros SD3-60 VARIANT 200TCDS A41EUAirframe · Short Bros SD3-60 VARIANT 200TCDS E26NEEngine · Pratt & Whitney Canada PT6A-67R
From the FAA registry file of October 24, 2026.
On this page
Airworthiness directives that may apply · 2
Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
| 1997 | 1 |
|---|---|
| 2024 | 1 |
Engine · Pratt & Whitney Canada PT6A-67R
AD 2024-04-51Turbine SectionEmergency ADAD 97-04-12Compressor Bleed-off ValveInformation bulletins that may apply · 1
Advisory, not mandatory.
Engine · Pratt & Whitney Canada PT6A-67R
SAIB CE-03-24NTSB investigations
No NTSB investigations matched to N764JRMatched by N-number and event date, checked against the reported serial number, make and model. Investigations from before this aircraft carried the mark are under Earlier aircraft. Investigations on Short Bros SD3-60 VARIANT 200 aircraft
FAA incident reports
No FAA accident or incident reports matched to N764JRMatched by N-number and event date, checked against the reported make and model. Reports from before this aircraft carried the mark are under Earlier aircraft. Reports on Short Bros SD3-60 VARIANT 200 aircraft
Service difficulty reports · 5
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR DATA2022040600001Windshield · improper partDURING CRUISE THE RIGHT WINDSHIELD HEAT CIRCUIT TERMINAL BOARD AT THE BASE OF THE WINDSHIELD STARTED SMOKING AND WINDSHIELD HEAT WAS INOPERATIVE. MAINTENANCE REPLACED P2 TERMINAL BOARD HARDWARE WITH CORRECT AN508-10-5 AND MS35333-107 HARDWARE IAW WINDSHIELD MASDR DATA07092021001Governor · inoperativeAT 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 ENGINE WAS SHUT DOWN IN FLIGHT, AN EMERGENCY WAS DECLARED AND THE CREW RETURNED THE AIRCRAFT TO THESDR DATA20180604101Engine · power lossON 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 POWER LEVERS UP TO SEE IF THE TORQUE WOULD STABILIZE, THAT FAILED , DECIDED TO SECURE THE RIGHT ENGISDR DATA2017020301Engine · overtempAFTER 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 ON AFFECTED ENGINE, BUT CONDITION PERSISTED DICTATING A PRECAUTIONARY NR 1 ENGINE SHUTDOWN AND RETURSDR DATR001632Bolt · failedRT SIDE ENGINE EXPERIENCED A LOW OIL PRESSURE LIGHT 1.5 HOURS INTO MISSION AND SUBSEQUENT PRESSURE LOSS. ENGINE WAS SHUTDOWN IN FLIGHT AND ACFT DIVERTED. THE ENGINE WAS RECEIVED AT THIS FACILITY FOR INVESTIGATION. THE PROPELLER SHAFT WAS HARD TO TURN AND A
STCs that may be installed · 3
Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.