Models / Bellanca / 17-30A / N93747 Aircraft record N93747 1973 Bellanca 17-30A Deregistered Unclaimed Source: FAA, updated Oct 20, 2026 This N-number isn't registered right now. Below is its last known registration, canceled Apr 9, 2015.
Safety record in brief: 2 NTSB accidents (substantial damage at worst, latest Feb 2013) · 2 ADs may apply
NTSB events 2 substantial, 2013 ADs may apply 2 confirm with A&P Service reports 0 since 1995
Registration FAA Aircraft Registry · Oct 20, 2026
Last registered owner Co-owners
City, state Colorado Springs, CO
Certificate issued Aug 7, 2012
Canceled Apr 9, 2015
Airworthiness Standard · Normal
Airworthiness date Aug 7, 1973 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 data Airframe
Manufacturer Bellanca
Model 17-30A
Year 1973
Serial number 73-30605
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 AD02AE 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 2012 – 2015 Co-owners Colorado Springs, CO 1947 – 1960 Individual owner None, OK · different airframe: Ercoupe 415-C S/N 1070 Individual owners are shown by city and state only.
Safety record NTSB · Oct 15, 2026 · FAA ADs · Oct 20, 2026 · SDRs · Oct 16, 2026 NTSB events (2)
Accident · substantial damage Feb 16, 2013 · Morris, IL The pilot's improper fuel management, which resulted in a loss of engine power due to fuel exhaustion.
Damage Substantial
Injuries None
Report CEN13LA164 From NTSB records; matched by serial number. Read NTSB report (search CAROL for CEN13LA164)
Accident · substantial damage Apr 25, 1982 · Lucerne, CA THE OWNER OF THE AIRCRAFT REPORTED THAT THERE WAS A GRADUAL LOSS OF ENGINE POWER. THE PLANE WAS LANDED ON A DIRT ROAD; HOWEVER, THERE WAS INSUFFICIENT ROOM TO STOP BEFORE REACHING THE END OF THE ROAD. THE OWNER REPORTED THAT HE SWERVED TO AVOID A DEAD END FENCE. AN INVESTIGATION REVEALED THAT A NUT BACKED OFF OF A THROTTLE LINKAGE BOLT AT THE CARBURETOR ARM. THE BOLT FELL OUT AND THE ENGINE WENT…
Damage Substantial
Injuries None
Report LAX82DUG11 From NTSB records; matched by serial number. Read NTSB report (search CAROL for LAX82DUG11)
Accident history for this model ADs 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 (17-30A) 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 (0) No Service Difficulty Reports found for this airframe since 1995.
Sources FAA Aircraft Registry Registration, owner city and state, airframe, engine updated Oct 20, 2026 NTSB accident and incident database Accidents and incidents since 1982 updated Oct 15, 2026 FAA Airworthiness Directives (Federal Register) ADs published since 1998 updated Oct 20, 2026 FAA Service Difficulty Reports Reports since 1995 updated Oct 16, 2026 Request owner name removal Report an error in this record