N775MW1979 Partenavia S.p.a P 68 C/TC
This N-number isn't registered right now. Below is its last known registration, canceled Feb 22, 2024.
Safety record in brief:No NTSB accidents or incidents since 1982No ADs since 1998 matched1 service difficulty report
- Registration
- Deregistered
Registration
FAA Aircraft Registry · Oct 19, 2026- Last registered owner
- Gv Air INC
- Owner type
- Corporation
- City, state
- Medford, OR
- Certificate issued
- Jul 28, 2017
- Canceled
- Feb 22, 2024
- Airworthiness
- Standard · Normal
- Airworthiness date
- Apr 15, 2004
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
- Partenavia S.p.a
- Model
- P 68 C/TC
- Year
- 1979
- Serial number
- 208.01
- Aircraft type
- Fixed wing multi engine
- Category
- Land
- Certification
- Type Certificated
- Seats
- 7
- Engines
- 2
- Max takeoff weight
- Up to 12,499 lb
- Mode S code
- AA7CC2
Engine
- Make and model
- Lycoming T0-360 Ser
- Type
- Reciprocating
- Power
- 210 hp
Total time and engine hours aren't public. They appear here once the owner adds logbooks.
Ownership history
Ownership history from FAA records- 2017 – 2024Gv Air INCMedford, OR
Individual owners are shown by city and state only.
Safety record
NTSB · Oct 15, 2026 · FAA ADs · Oct 19, 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 (0)
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.
No ADs published since 1998 matched this airframe or engine model.
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.
- Wings · spar cap · corrodedDec 29, 2005
SEVERE INTERGRANULAR CORROSION OF MAIN WING SPAR WEB AND UPPER SPAR CAP AFT OF ENGINE FIREWALL. REQUIRES REMOVAL OF ENGINE, ENGINE MOUNT, FIREWALL. SUSPECT SOURCE OF CORROSION TO BE FIRE SHEATH INSTALLED OVER FUEL LINES BEHIND FIREWALL. SB 61 ADDRESSES INSPECTION OF FUEL LINES AND REMOVAL OF FIRE…
From FAA Service Difficulty Reports; matched by N-number and serial number.
Sources
- FAA Aircraft RegistryRegistration, owner city and state, airframe, engineupdated Oct 19, 2026
- NTSB accident and incident databaseAccidents and incidents since 1982updated Oct 15, 2026
- FAA Airworthiness Directives (Federal Register)ADs published since 1998updated Oct 19, 2026
- FAA Service Difficulty ReportsReports since 1995updated Oct 16, 2026