N6667V1966 Bellanca 17-30
This N-number isn't registered right now. Below is its last known registration, canceled Apr 24, 2013.
Safety record in brief:No NTSB accidents or incidents since 19822 ADs may apply2 service difficulty reports
- Registration
- Deregistered
Registration
FAA Aircraft Registry · Oct 18, 2026- Last registered owner
- Individual owner
- City, state
- Xxx, OK
- Canceled
- Apr 24, 2013
- Airworthiness
- Standard · Normal
- Airworthiness date
- Apr 11, 1967
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
- Bellanca
- Model
- 17-30
- Year
- 1966
- Serial number
- 30018
- Aircraft type
- Fixed wing single engine
- Category
- Land
- Certification
- Type Certificated
- Seats
- 4
- Engines
- 1
- Max takeoff weight
- Up to 12,499 lb
- Mode S code
- A8CDE4
Engine
- Make and model
- Cont Motor Io 520 Series
- Type
- Reciprocating
- Power
- 285 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 2013Individual ownerXxx, OK
Individual owners are shown by city and state only.
Safety record
NTSB · Oct 15, 2026 · FAA ADs · Oct 18, 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 (2)
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 |
|---|---|---|---|
| 2014-20-12 | Fuselage | Nov 12, 2014 | Airframe (17-30) |
| 2009-16-03 | Teledyne Continental Motors (TCM) IO-520, TSIO-520, and IO-550 Series Reciprocating… | Sep 9, 2009 | Engine (IO 520 SERIES)Only with: SAP investment cast cylinder assemblies P/Ns SA52000-A1, SA52000-A20P, SA52000-A21P, SA52000-A22P, SA52000-A23P, SA55000-A1, or SA55000-A20P 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 (2)
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.
- Landing gear · gear leg · failedAug 1, 1997
AIRCRAFT EXPERIENCED A FAILURE OF THE RIGHT MAIN GEAR LOWER GEAR SEGMENT. THE LOWER TUBE FAILED AT THE SCISSOR ATTACH POINT CAUSING THE WHEEL TO ROTATE 180 DEGREES.
From FAA Service Difficulty Reports; matched by N-number and serial number. - filter · blocked yokeOct 11, 1996
FILTER PREVENTED YOKE FROM FORWARD MOVEMENT. WHEN FILTER WAS INSTALLED IT WAS NOT HARD MOUNTED. HOSES WERE HOLDING FILTER. HOSE CLAMP LOOSENED ALLOWING FILTER TO MOVE. HARD MOUNTED FILTER TO AIRCRAFT FRAME USING LOCKNUT AND ADEL CLAMP. REPLACED HOSES. SUBMITTER STATED NO LOCATION FOUND IN AIRCRAFT…
From FAA Service Difficulty Reports; matched by N-number and serial number.
Sources
- FAA Aircraft RegistryRegistration, owner city and state, airframe, engineupdated Oct 18, 2026
- NTSB accident and incident databaseAccidents and incidents since 1982updated Oct 15, 2026
- FAA Airworthiness Directives (Federal Register)ADs published since 1998updated Oct 18, 2026
- FAA Service Difficulty ReportsReports since 1995updated Oct 16, 2026