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Aircraft record

N7698S1976 Bellanca 8KCAB

DeregisteredUnclaimedSource: FAA, updated Oct 19, 2026

This N-number isn't registered right now. Below is its last known registration, canceled Jun 26, 2017.

Safety record in brief:1 NTSB accident (substantial damage, Mar 2015)4 ADs may apply2 service difficulty reports

Registration
Deregistered
Last based in
Pearl, MS
owner city / state
Owners
1
since 2014
NTSB events
1
substantial, 2015
ADs may apply
4
confirm with A&P
Service reports
2
since 1995

Registration

FAA Aircraft Registry · Oct 19, 2026
Last registered owner
Individual owner
City, state
Pearl, MS
Certificate issued
May 28, 2014
Canceled
Jun 26, 2017
Airworthiness
Standard · Normal, Acrobatic
Airworthiness date
Jun 22, 1976

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
8KCAB
Year
1976
Serial number
262-76
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
AA6678

Engine

Type
Reciprocating

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

Ownership history

Ownership history from FAA records
  1. 2014 – 2017Individual ownerPearl, MS

Individual owners are shown by city and state only.

Safety record

NTSB · Oct 15, 2026 · FAA ADs · Oct 19, 2026 · SDRs · Oct 16, 2026

NTSB events (1)

Accident · substantial damage

Mar 8, 2015 · Kosciusko, MS

The pilot's decision to make a low pass over a lake near trees and his subsequent failure to maintain airplane control while maneuvering at a low altitude to avoid trees, which resulted in an inadvertent cross-control aerodynamic stall from which he was unable to recover.

Damage
Substantial
Injuries
Fatal
Report
ERA15FA147

From NTSB records; matched by serial number.Read NTSB report (search CAROL for ERA15FA147)

Accident history for this model

ADs published since 1998 that may apply (4)

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.

ADSubjectEffectiveApplies to
2018-14-06WingsAug 17, 2018Airframe (8KCAB)Certain serial numbers: 8KCAB 1116-2012–1120-2012; 8KCAB 1122-2012–1170-2017. Only with: Applies to airplanes in the listed serial ranges, or any airplane equipped with P/N 4-2142 exposed balance ailerons.
2009-22-02American Champion Aircraft Corp. Models 7ECA, 7GCAA, 7GCBC, 7KCAB, 8KCAB, and 8GCBC…Dec 3, 2009Airframe (8KCAB)Only with: Manufactured prior to 1989 and equipped with folding rear seat backs.
2005-24-10American Champion Aircraft Corporation Models 7AC, 7ACA, S7AC, 7BCM, 7CCM, S7CCM, 7DC…Jan 17, 2006Airframe (8KCAB)Only with: Models 7ECA, 7GCAA, 7GCBC, 8KCAB, 8GCBC manufactured before August 12, 2005 with less than 250 hours TIS; or any listed model with a flight control cable (or wing retrofit kit cable) purchased from ACAC before August 12, 2005 installed and less than 250 hours TIS since installation.
2000-25-02 R1American Champion Aircraft Corporation 7, 8, and 11 Series AirplanesJul 13, 2001Airframe (8KCAB)Only with: Airplanes equipped with wood wing spars; Group 1 vs Group 2 depends on whether the engine has been modified to greater than 90 horsepower.

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.

  • Equipment and furnishings · seat · failedSep 16, 2008

    REAR SEAT PN 7-1500 FAILED AT THE LT HINGE POINT. THE AN3 SERIES BOLT PULLED THRU THE HINGE LUGS WHICH ARE WELDED TO THE SEAT FRAME BOTTOM. THE RT HINGE HOLES SHOW ELONGATION, BUT REMAINED INTACT. THE AC WAS DOING SPIN TRAINING AT THE TIME OF THE INCIDENT. RECOMMEND THAT THE SEAT FRAME BE MODIFIED…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Reciprocating engine · crankshaft · corrodedFeb 7, 1995

    DURING OVERHAUL INSPECTION OF CRACKSHAFT, SOME CORROSION PITTING WAS NOTED ON OUTSIDE DIAMETER OF SEVERAL BEARING JOURNALS. INSPECTION OF FRONT MAIN INSIDE DIAMETER REVEALED AN AREA OF APROXIMATELY 20 CORROSION PITS. PITS WERE APPROXIMATELY .010 INCH DEEP AND WERE LOCATED APPROXIMATELY 1.50 INCHES…

    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

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