No fatalities

16 Jul 2024: PIPER PA-36-375 (N2386X) — STOVE CREEK AIR LLC — Avoca, NE

Avoca, NE, United States

On 16 Jul 2024, a PIPER PA-36-375 (registration N2386X) operated by STOVE CREEK AIR LLC was involved in an aviation accident near Avoca, NE. No fatalities were reported. Investigators recorded the probable cause as: A partial loss of engine power due to the loose left magneto which resulted in erratic engine timing. This summary draws on records from NTSB; 4 related events involving the same aircraft type or operator are linked below.

SourcesNTSBPrimary reportUpdated 1778583330Data APIEditorial standards

A Piper PA-36-375 (N2386X) lost all power during an agricultural flight near Avoca, Nebraska. The pilot was uninjured; the aircraft sustained substantial damage. Examination revealed loose coil wedges in the right magneto.

Accident Overview

On July 16, 2024, about 1430 central daylight time, a Piper PA-36-375 airplane, registration N2386X, was substantially damaged in an accident near Avoca, Nebraska. The pilot, who was the sole occupant, was not injured. The airplane was operating as a Title 14 Code of Federal Regulations Part 137 aerial application flight.

Sequence of Events

The pilot reported that while maneuvering for his fourth spray pass, he had rolled the airplane level at an altitude of about 300 ft above ground level when the airplane “lost all power” and began to descend. He added full power and pushed the propeller control full forward, but did not feel the engine respond, and the airplane continued to descend. After dumping the hopper tank load, he was still unable to stop the descent. The airplane touched down in a field and continued through a cattle fence before coming to rest, resulting in substantial damage to the fuselage and left wing.

Examination Findings

The airplane was recovered to a secure facility for further examination. A crack was observed between the Nos. 1, 2, and 3 cylinders; however, no thermal distress was found within the engine. Internal continuity was confirmed throughout the engine, and a borescope examination of the cylinders revealed no anomalies. Examination of the fuel divider, injectors, servo, and pump revealed no anomalies. The oil filter was removed and contained no contamination. The air inlet and filter were free of debris.

While still attached to the engine, the left magneto flange could be rotated slightly. Both magnetos were removed and rotated by hand. The right magneto made a “clunking” sound when rotated and rattled when shaken. Both magnetos produced spark at their terminal leads.

Further examination of the magnetos found the right magneto distributor gear was timed correctly. Both coil wedges were loose in the housing. The coil wedges appeared to have been initially wedged in place, but only had minimal marring, which may not have provided enough tension to retain the wedges properly. A review of maintenance records found that the magneto was overhauled on November 27, 2023, and was installed on the airplane on April 12, 2024. The airplane had flown about 40 hours since the magneto installation.

The left magneto was in good condition and subsequently bench tested. The magneto operated as expected.

Contributing factors

Malfunction