N302WA2026 Piper PA-46-701TP
Safety record in brief:No NTSB accidents or incidents since 19821 AD may apply1 service difficulty report
Registration
FAA Aircraft Registry · Oct 20, 2026- Registered owner
- Western Aircraft INC
- Owner type
- Corporation
- City, state
- Boise, ID
- Airworthiness
- Standard · Normal
- Airworthiness date
- Mar 20, 2026
We never show street addresses, even though they appear in the public FAA file. Individual owners are shown by city and state only.
Airframe & engine
FAA Registry + type dataAirframe
- Manufacturer
- Piper
- Model
- PA-46-701TP
- Year
- 2026
- Serial number
- 46020102
- Aircraft type
- Fixed wing single engine
- Category
- Land
- Certification
- Type Certificated
- Seats
- 6
- Engines
- 1
- Max takeoff weight
- Up to 12,499 lb
- Type certificate data sheet
- A25SO
- Mode S code
- A328B5
Engine
- Make and model
- P&W Canada Pt6a-52
- Type
- Turbo-prop
- Power
- 898 hp
Total time and engine hours aren't public. They appear here once the owner adds logbooks.
Ownership history
Ownership history from FAA records- until nowWestern Aircraft INCBoise, ID · current
- 2010 – 2018Mec Group LLCTucson, AZ · different airframe: Boeing 737-347 S/N 23182
Individual owners are shown by city and state only.
Safety record
NTSB · Oct 15, 2026 · FAA ADs · Oct 20, 2026 · SDRs · Oct 16, 2026NTSB events (0)
No NTSB accidents or incidents found for this airframe since 1982.
Accident history for this modelADs published since 1998 that may apply (1)
These match the airframe or engine model. Whether each one applies, and whether it's been complied with, depends on serial numbers, equipment and logbook entries. Applicability must be confirmed by a mechanic against the aircraft's records.
| AD | Subject | Effective | Applies to |
|---|---|---|---|
| 2002-23-13 | Pratt & Whitney Canada PT6A Series Turboprop Engines | Dec 31, 2002 | Engine (PT6A-52)Only with: Engines with turbine exhaust ducts P/N 3012290, 3031988, 3032117, 3035784, 3035786, 3105890-01, 3112167-01, or 3111780-01 installed. |
AI-extracted — verify against original. Matched from each AD's applicability section; ADs replaced by a later AD are left out.
Service Difficulty Reports (1)
Reports of failures and defects that operators and repair stations sent to the FAA since 1995. A report describes one finding; it is not an accident.
- Flight controls · control cable · severedAug 27, 2026
DURING THE INITIAL 50 HOUR INSPECTION AT FRAME STATION 282.0 WE FOUND THE RUDDER CABLE SEVERED. PROBABLE CAUSE IS DUE TO INCORRECT ROUTING AT MANUFACTURING. IT APPEARS THAT THE CABLE WAS ROUTED UNDER THE RETAINING PIN ON THE BOTTOM OF THE PULLEY WHICH PUSHED THE CABLE INTO THE FRAME. DUE TO THIS…
From FAA Service Difficulty Reports; matched by N-number and serial number.
Sources
- FAA Aircraft RegistryRegistration, owner city and state, airframe, engineupdated Oct 20, 2026
- NTSB accident and incident databaseAccidents and incidents since 1982updated Oct 15, 2026
- FAA Airworthiness Directives (Federal Register)ADs published since 1998updated Oct 20, 2026
- FAA Service Difficulty ReportsReports since 1995updated Oct 16, 2026