20260710009689A

Accident · Substantial damage

FAA accident report · American Champion 7GCAA · Franklin, VA · July 10, 2026

Date
July 10, 2026 · 13:15 local
Place
Franklin, VA
Phase of flight
Landing: Touchdown
Operating rules
General operating rules (Part 91)
Damage
Substantial damage
Aircraft
N67BF
Reported as
American Champion 7GCAA
Reported engine
Lycoming 0-320 series
People aboard
2
Fatal injuries
0
Other injuries
0

From the FAA’s Accident/Incident Data System (AIDS), through its Aviation Safety Information Portal, as reported. The NTSB investigates accidents separately, and its record of an accident is the fuller one. The aircraft is matched to the registry by N-number and event date, checked against the reported make and model; the registry’s history has gaps, so older matches can be wrong. Compare the reported make and model.

What happened

The FAA’s narrative, in sentence case. The FAA writes it in capitals and removes private details.

An experienced pilot was receiving instruction towards a tailwheel endorsement in this tailwheel aircraft. Runway marks showed a normal landing which appeared to be drifting slightly sideways. This drift to the left appears to have opened up a significant pre-existing metal fatigue crack in the lower portion of the right side, main landing gear spring axle. This caused what is normally a vertical compression load to be a side-load that opened the hinge point around the minimal remaining metal, and caused failure. The complete brake and wheel assembly departed the aircraft. The aircraft fell roughly 8 inches onto the broken axle stub, struck the prop, and pivoted consistent with a ground loop. Both pilots were uninjured and exited the aircraft.

As the FAA filed it

AN EXPERIENCED PILOT WAS RECEIVING INSTRUCTION TOWARDS A TAILWHEEL ENDORSEMENT IN THIS TAILWHEEL AIRCRAFT. RUNWAY MARKS SHOWED A NORMAL LANDING WHICH APPEARED TO BE DRIFTING SLIGHTLY SIDEWAYS. THIS DRIFT TO THE LEFT APPEARS TO HAVE OPENED UP A SIGNIFICANT PRE-EXISTING METAL FATIGUE CRACK IN THE LOWER PORTION OF THE RIGHT SIDE, MAIN LANDING GEAR SPRING AXLE. THIS CAUSED WHAT IS NORMALLY A VERTICAL COMPRESSION LOAD TO BE A SIDE-LOAD THAT OPENED THE HINGE POINT AROUND THE MINIMAL REMAINING METAL, AND CAUSED FAILURE. THE COMPLETE BRAKE AND WHEEL ASSEMBLY DEPARTED THE AIRCRAFT. THE AIRCRAFT FELL ROUGHLY 8 INCHES ONTO THE BROKEN AXLE STUB, STRUCK THE PROP, AND PIVOTED CONSISTENT WITH A GROUND LOOP. BOTH PILOTS WERE UNINJURED AND EXITED THE AIRCRAFT.