- Registered owner
- My Beaver LLC
- Location
- Seattle, WA
- Owner type
- LLC
- Serial number
- 1627
- Year built
- 1966
- Type
- Fixed wing single engine
- Engine
- Turbo-prop
- Airworthiness
- Standard, normal
- Airworthiness date
- November 6, 1975
- Certificate issued
- September 1, 2006
- Expires
- April 30, 2028
- Mode S code
- ADE605
From the FAA registry file of October 24, 2026.
On this page
Airworthiness directives that may apply · 8
Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
| 1969 | 1 |
|---|---|
| 1970 | 1 |
| 1975 | 1 |
| 1977 | 1 |
| 1980 | 1 |
| 1992 | 1 |
| 1997 | 1 |
| 2002 | 1 |
Engine · U/A Canada PT6A-6
AD 2002-23-13Turbine Exhaust DuctsAD 97-04-12Compressor Bleed-off ValveAD 92-15-11Compressor Delivery Air Line (P3) Filter AssemblyAD 80-08-12Fuel Pump Drive Coupling SplinesAD 75-06-01Gearbox DeteriorationAD 75-11-04Reduction Gearbox Engine DistressAD 70-16-01Turbo Propeller GovernorsAD 69-23-06Fuel PumpsInformation bulletins that may apply · 1
Advisory, not mandatory.
Engine · U/A Canada PT6A-6
SAIB NE-12-04Turbine/ Turboprop Engine: Reduction GearboxNTSB investigations
No NTSB investigations matched to N995JGMatched 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 Dehavilland BEAVER DHC-2 MK.3 aircraft
FAA incident reports
No FAA accident or incident reports matched to N995JGMatched 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 Dehavilland BEAVER DHC-2 MK.3 aircraft
Service difficulty reports
No reports matched to N995JGGeneral aviation reporting is voluntary. Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Reports on Dehavilland BEAVER DHC-2 MK.3 aircraft
STCs that may be installed · 11
Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.
Engine · U/A Canada PT6A-6
STC SE00014ENInstallation of the Pratt & Whitney Engine Services, Inc. CrossCheck Engine Monitor Kit P/N HUMS-K-071-1, Rev. A on the specified PT6A engine models and kit P/N HUMS-K-071-2 on the specified A250 engine models.STC SE00020ENInstallation of the Pratt & Whitney Engine Services, Inc. TrendCheck/ TrendCheck Plus Engine Monitor Kit P/N TREND-K-010-1STC SE2960SOInstallation of an oil filler cap safety adapter.STC SE615GLIncorporation of a fuel flow transducer.STC SE09257SCConvert P&W Engine Models PT6A-15AG, -27, and -28, into PT6A-34 configuration.STC SE659NEInstallation of oil tank filler neck check valve, P/N TSA-76A.STC SE1269EAStripping and recoating of compressor turbine blades, P/N 3023401, with Walbar Metals, Inc.STC SE5601SWReplacement splined end and oil mist lubrication on accessory drive gearshaft.STC SE1165EAAssembly and installation of AW10262 wet spline starter gear seal.STC SE4607SWRevise the starter-generator drive spline to provide lubrication with engine oil.STC SE4570SWRevise accessory drive spline, P/N 3008181.