19970801026329I

Incident · Minor damage

FAA incident report · Curtis TRVAIRB94000 · Salinas, CA · August 1, 1997

Date
August 1, 1997 · 16:25 local
Place
Salinas, CA
Airport
Salinas Municipal Airport
Phase of flight
Roll-Out (Fixed Wing)
Operating rules
General operating rules (Part 91)
Damage
Minor damage
Aircraft
N8877
Reported as
Curtis TRVAIRB94000
Reported engine
WRIGHT R760*
People aboard
1
Fatal injuries
0
Pilot’s flight hours
7,350 total32 in this make and model46 in the last 90 days

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.

Narrative: upon landing at Salinas airport rwy. 26, left main landing gear wheel departed the aircraft. The aircraft departed the runway to the left, ground looped and came to rest between rwy. 26 and taxiway "b". The aircraft sustained damage to the propeller, engine, and left main landing gear. After an inspection was conducted of the left main wheel, left main wheel hub, and left main axle, it appears that the retained nut for the wheel backed itself off the axle. There was no evidence of a cotter pin being installed in the retainer nut prior to this incident. There were no injuries. This investigation is closed. Incident does not involve a pilot deviation report form 8020-17.

As the FAA filed it

NARRATIVE: UPON LANDING AT SALINAS AIRPORT RWY. 26, LEFT MAIN LANDING GEAR WHEEL DEPARTED THE AIRCRAFT. THE AIRCRAFT DEPARTED THE RUNWAY TO THE LEFT, GROUND LOOPED AND CAME TO REST BETWEEN RWY. 26 AND TAXIWAY "B". THE AIRCRAFT SUSTAINED DAMAGE TO THE PROPELLER, ENGINE, AND LEFT MAIN LANDING GEAR. AFTER AN INSPECTION WAS CONDUCTED OF THE LEFT MAIN WHEEL, LEFT MAIN WHEEL HUB, AND LEFT MAIN AXLE, IT APPEARS THAT THE RETAINED NUT FOR THE WHEEL BACKED ITSELF OFF THE AXLE. THERE WAS NO EVIDENCE OF A COTTER PIN BEING INSTALLED IN THE RETAINER NUT PRIOR TO THIS INCIDENT. THERE WERE NO INJURIES. THIS INVESTIGATION IS CLOSED. INCIDENT DOES NOT INVOLVE A PILOT DEVIATION REPORT FORM 8020-17.