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
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.
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.
Airframe (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.
Airframe (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.
American Champion Aircraft Corporation 7, 8, and 11 Series Airplanes
Jul 13, 2001
Airframe (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.
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.