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CHI88DEC04

1988-07-02 · FOWLERVILLE, Michigan, United States · None · 1 aircraft · Status: Completed

Airport 65G

Aircraft involved

Probable cause & findings

THE PILOT FAILED TO MAINTAIN POSITIVE CONTROL OF HIS HOMEBUILT AIRCRAFT BY TAKING APPROPRIATE ACTIONS FOR RECOVERY FROM THE BOUNCED LANDING. THE AIRCRAFT CONTACTED THE GROUND ABRUPTLY ON THE THIRD BOUNCE AND THE UPPER WING SPAR FAILED. THE PILOT'S LACK OF TOTAL FLIGHT EXPERIENCE IN THE HOMEBUILT AIRCRAFT WAS A CONTRIBUTING FACTOR, AND THE AIRCRAFT APPEARS TO HAVE BEEN UNDERDESIGNED.

Factual narrative

THE PILOT INDICATED THAT HE HAD 3 HOURS TOTAL FLIGHT EXPERIENCE IN THE HOMEBUILT AIRCRAFT. HE STATED THAT HE ATTEMPTED A POWER-OFF LANDING AND THE AIRCRAFT BOUNCED. ON THE THIRD BOUNCE 'THE (RIGHT WING) SPAR POPPED.' THE PILOT STATED THAT 'THIS IS A LEARNING CURVE ACCIDENT' AND INDICATED THAT MORE TIME PRACTICING SLOW FLIGHT AND LANDINGS IN THE ACCIDENT AIRCRAFT WOULD HAVE HELPED PREVENT THE ACCIDENT. THE AIRCRAFT HAD SUSTAINED SUBSTANTIAL DAMAGE TO THE LEFT WING DUE TO A HARD LANDING DURING IT'S MAIDEN FLIGHT IN APRIL, 1986. THE FLIGHT DURING WHICH THIS ACCIDENT OCCURRED WAS THE AIRCRAFT'S FIRST FLIGHT SINCE THAT ACCIDENT. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12

Verbatim from NTSB's published report. Source file NTSB_1988_CHI88DEC04.txt. Findings + structured fields enriched from FAA avall.mdb. Full investigation docket on data.ntsb.gov ↗.

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