N9892Grumman G-164A · 1974

On July 22, 2023, about 1113 central daylight time, a Grumman G-164A, N9892, was substantially damaged when it was involved in an accident near Patoka, Illinois. The pilot was not injured. The airplane was operated as a Title 14 Code of Federal Regulations Part 137 agricultural flight.

The pilot reported that during the 4th pass of the chemical spray load, the the engine lost power. Based on the airplane’s low altitude and decreasing airspeed, the pilot elected to make a forced landing into the corn field. Both wings, the fuselage, and the empennage sustained substantial damage. Flight control continuity was confirmed. The airplane was retained for further examination.

The airplane’s turboprop engine was examined at the manufacturer’s facility. The examination showed rotational scoring, hard body impact damage, and missing material throughout the CT and PT sections of the engine. Multiple CT blades were fractured above the blade platform and about 75% of the PT blades were fractured at various lengths above the blade platform. Metallurgical examination of two blades from the CT showed material necking near the fracture surfaces, microstructural rafting, creep voids, and localized alteration of the microstructure consistent with heat related material degradation.

Examination of the fuel control unit (FCU) showed the maximum Ng speed adjustment screw was found adjusted to the maximum fuel flow position and was lock wired in place.

Additionally, the FCU housing was missing a bolt and showed a fatigue fracture which created a gap between the FCU housings. Movement of the power control linkage was observed to cause a reactive open and close movement of the gap between the two housings.

The operator reported the engine’s time since new (TSN) was 14,092 hours. The time since overhaul (TBO was 6,738.5 hours and the time since inspection was 226 hours. A review of the engine logbooks showed the airplane underwent an annual inspection about two months before the accident. The recorded (TSN) at the annual was 14,217 hours. A corresponding airplane logbook entry showed the airplane TSN as 12,475 hours.

The engine manufacturer’s recommended TBO is 3,600 hours.

The pilot had serviced the airplane prior to an aerial application flight of a field during which the airplane lost engine power. The pilot performed a forced landing in a northerly direction on a hard surface road near the field, which had corn along its left side and a pole along its right side. While the pilot was trying to avoid the pole along the right side of the road, the airplane impacted the corn and terrain with its left wing resulting in substantial damage to the airplane. The left and right wings were buckled and bent from the impact. The pilot was uninjured. Examination of the airplane revealed that the oil filler cap was not installed resulting in a total loss of engine oil. The oil filler cap was found in the lower portion of the engine nacelle.