Aviation Accident Summaries

Aviation Accident Summary SEA95LA056

SPOKANE, WA, USA

Aircraft #1

N49335

PITTS S-2B

Analysis

THE PILOT OF THE AEROBATIC AIRPLANE WAS PRACTICING AN INVERTED FLAT SPIN WHEN THE PROPELLER AND CRANKSHAFT FLANGE SEPARATED FROM THE ENGINE. THE PILOT RECOVERED FROM THE MANEUVER, THEN MADE A FORCED LANDING ONTO A 780 FOOT MODEL AIRPLANE RUNWAY. THE AIRCRAFT OVERRAN THE END OF THE RUNWAY, THEN THE MAIN LANDING GEAR SETTLED INTO SOFT SOIL AND THE AIRCRAFT NOSED OVER. THE PILOT STATED THAT HE HAD NOT BEEN CONDUCTING RECURRENT CRANKSHAFT FLANGE INSPECTIONS, AS RECOMMENDED BY A MANUFACTURER'S SERVICE BULLETIN.

Factual Information

On February 24, 1995, approximately 1715 Pacific standard time (PST), a Pitts S-2B, N49335, nosed over after making a forced landing about 10 miles northwest of Spokane, Washington. The commercial pilot, who was the sole occupant of the aircraft, was not injured, but the aircraft sustained substantial damage. The practice aerobatic flight, which departed Felts Field, Spokane, Washington at about 1630, was being operated in visual meteorological conditions. No flight plan had been filed, and there was no report of an ELT activation. According to the pilot, while practicing an inverted flat spin, the propeller and crankshaft flange separated from the engine. He then recovered from the maneuver, and made a forced landing at a 780 foot model airplane runway. During the landing roll, the aircraft rolled beyond the end of the runway and the main gear settled into soft soil and the aircraft nosed over. The pilot stated that he had not been conducting the recurring (each ten hours of operation) crankshaft inspections recommended by the manufacturer in Lycoming service bulletin number 482, which relates to crankshaft flange area cracking on this model engine when it is used for unlimited-style aerobatics, including inverted spins.

Probable Cause and Findings

FATIGUE FAILURE OF THE CRANKSHAFT. FACTORS WERE THE SOFT TERRAIN AND THE PILOT/OWNER'S FAILURE TO CONDUCT RECURRING CRANKSHAFT INSPECTIONS RECOMMENDED BY THE MANUFACTURER.

 

Source: NTSB Aviation Accident Database

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