Summary
On July 05, 1994, a Pitts S1 (CGPUR) was involved in an incident near Heber City, UT. All 1 person aboard were uninjured. The aircraft sustained substantial damage.
The National Transportation Safety Board determined the probable cause of this incident to be: FAILURE OF MAIN LANDING GEAR AXLE HARDWARE. FACTORS INCLUDE COLLAPSE OF MAIN LANDING GEAR STRUT.
On July 5, 1994, approximately 1617 mountain daylight time, an experimental Pitts S-1 was substantially damaged during roll out when the right wheel/axle attachment hardware failed after landing at Heber City, Utah. The private pilot, who owned the aircraft, was uninjured. Visual meteorological conditions prevailed for the flight, which originated at Heber City at 1601. There was no fire and no report of an ELT actuating.
FAA inspectors noted that the nuts and bolts securing the axle to the aircraft were excessively worn, and indicated that the nuts had sheared their threads before separating. The pilot noted that four 1/4-20 bolts failed, causing wheel separation and subsequent gear failure, and indicated that the bolts had not been correctly torqued.
This incident is documented in NTSB report SEA94LA172. AviatorDB cross-references NTSB investigation data with FAA registry records to provide comprehensive safety information for aircraft CGPUR.
Accident Details
Probable Cause and Findings
FAILURE OF MAIN LANDING GEAR AXLE HARDWARE. FACTORS INCLUDE COLLAPSE OF MAIN LANDING GEAR STRUT.
Aircraft Information
Analysis
On July 5, 1994, approximately 1617 mountain daylight time, an experimental Pitts S-1 was substantially damaged during roll out when the right wheel/axle attachment hardware failed after landing at Heber City, Utah. The private pilot, who owned the aircraft, was uninjured. Visual meteorological conditions prevailed for the flight, which originated at Heber City at 1601. There was no fire and no report of an ELT actuating.
FAA inspectors noted that the nuts and bolts securing the axle to the aircraft were excessively worn, and indicated that the nuts had sheared their threads before separating. The pilot noted that four 1/4-20 bolts failed, causing wheel separation and subsequent gear failure, and indicated that the bolts had not been correctly torqued.
Data Source
Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# SEA94LA172