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Aircraft record

N83032Aeronca 7AC

Registration validNot yet verified by ownerSource: FAA, updated Oct 20, 2026

Safety record in brief:1 NTSB accident (substantial damage, Mar 2020)No ADs since 1998 matched6 service difficulty reports

Registration
Valid
expires Apr 30, 2028
Based in
Ankeny, IA
owner city / state
Engine
A&C65 SERIES · 65 hp
Cont Motor
Owners
1
since 2015
NTSB events
1
substantial, 2020
ADs may apply
0
confirm with A&P
Service reports
6
since 1995

Registration

FAA Aircraft Registry · Oct 20, 2026
Registered owner
Vintage Flying Club
Owner type
Corporation
City, state
Ankeny, IA
Certificate issued
Apr 27, 2015
Expires
Apr 30, 2028
Airworthiness
Standard
Airworthiness date
Mar 1, 1956

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
Aeronca
Model
7AC
Serial number
7AC-1688
Aircraft type
Fixed wing single engine
Category
Land
Certification
Type Certificated
Seats
2
Engines
1
Max takeoff weight
Up to 12,499 lb
Mode S code
AB5B36

Engine

Make and model
Cont Motor A&C65 Series
Type
Reciprocating
Power
65 hp

Total time and engine hours aren't public. They appear here once the owner adds logbooks.

Ownership history

Ownership history from FAA records
  1. 2015 – nowVintage Flying ClubAnkeny, IA · current

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 (1)

Accident · substantial damage

Mar 11, 2020 · Ankeny, IA

The pilot's improper starting procedure, which allowed the airplane to move forward over the wheel chocks and impact him and a hangar when he subsequently hand propped the engine.

Damage
Substantial
Injuries
Serious
Report
CEN20CA120

From NTSB records; matched by serial number.Read NTSB report (search CAROL for CEN20CA120)

Accident history for this model

ADs 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 (6)

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 · damagedMar 28, 1996

    DISMANTLED LEFT AND RIGHT WING FOR THE PURPOSE OF RECOVERING. WITH THE OLD FABRIC REMOVED, FOUND BOTH REAR SPARS HAD BEEN CHEWED BY MICE MIDWAY BETWEEN THE WING ROOT AND THE STRUT ATTACH FITTING. IT APPEARS THIS DAMAGE WAS PRESENT WHEN THE WINGS WERE LAST RECOVERED IN 1982 BECAUSE THE CHEW MARKS…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Wings · spar · crackedMar 28, 1996

    DISMANTLED BOTH LEFT AND RIGHT WINGS FOR RECOVERING. ALL SPARS WERE REMOVED FOR CLEANING, INSPECTION, AND VARNISHING. WITH THE WING SPAR FITTINGS REMOVED, FOUND THE SPAR FITTING HOLES HAD CRACKS EMANATING FROM THE TWO INBOARD HOLES THROUGH THE BUTT OF THE SPAR. ALL FOUR SPARS WERE REPLACED WITH…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Wings · fitting · crackedMar 28, 1996

    DISMANTLED LEFT WING FOR THE PURPOSE OF RECOVERING. AS A PRECAUTION, THE WING SPAR ATTACHMENT FITTINGS WERE MAGNAFLUXED. THE LEFT FRONT WING SPAR ATTACHMENT FITTING WAS FOUND TO HAVE SEVERAL IMPERFECTIONS IN THE WELDED AREA OF BOTH THE TOP AND BOTTOM GUSSETS. THE FITTING WAS REPLACED WITH A NEW…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
Show all 6 reports
  • Wings · fitting · crackedMar 28, 1996

    DISMANTLED LEFT WING FOR THE PURPOSE OF RECOVERING. AS A PRECAUTION, THE WING SPAR ATTACHMENT FITTINGS WERE MAGNAFLUXED. THE LEFT REAR SPAR ATTACHMENT FITTING WAS FOUND TO HAVE SEVERAL IMPERFECTIONS IN THE WELD AREAS OF BOTH THE TOP AND BOTTOM GUSSETS. THE FITTING WAS REPLACED WITH A NEW PART.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Wings · rib · crackedMar 28, 1996

    DISMANTLED BOTH LT AND RT WINGS FOR THE PURPOSE OF RECOVERING. IN THE PROCESS OF REMOVING OLD COVER, DETERMINED THAT ALL THE SCREWS THAT SECURE THE FABRIC TO THE RIBS FOR THE NR 2 AND NR 3 INBOARD RIBS OF EACH WING, HAD ELONGATED THE HOLES IN THE RIBS AND WAS NOT SERVING THE INTENDED PURPOSE OF…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Wings · rib · crackedMar 28, 1996

    DISMANTLED BOTH LT AND RT WINGS FOR THE PURPOSE OF RECOVERING. IN THE PROCESS OF REMOVING OLD COVER, DETERMINED THAT ALL THE SCREWS THAT SECURE THE FABRIC TO THE RIBS FOR THE NR 2 AND NR 3 INBOARD RIBS OF EACH WING, HAD ELONGATED THE HOLES IN THE RIBS AND WAS NOT SERVING THE INTENDED PURPOSE OF…

    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

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