Event ERA16LA280

Factual narrative

On August 06, 2016, about 1145 eastern daylight time, a Piper PA-28R-201, N3783M, was substantially damaged during a forced landing following a partial loss of engine power near Northampton Airport (7B2), Northampton, Massachusetts. The flight instructor and pilot receiving instruction were not injured. The instructional flight was conducted under the provisions of 14 Code of Federal Regulations Part 91. Visual meteorological conditions prevailed, and no flight plan was filed for the flight, which originated from 7B2, about 1143.According to the flight instructor, during a simulated soft field take-off, the airplane's climb performance deteriorated noticeably. As the airplane reached approximately 150 feet above ground level, the engine started to lose power. He then realized that continuing the climb was not possible, and any increase in pitch resulted in an immediate decrease in airspeed. The flight instructor elected to make an emergency off airport landing in a corn field near the end of the departure runway. During the landing sequence the right wing and firewall were damaged. A post accident examination of the airplane by a Federal Aviation Administration inspector revealed that the alternate air valve plate had separated from its mounting location and was lodged in the fuel servo air intake, blocking the fuel servo. After further examination of the alternate air valve plate it was noted that the hinge pin was worn completely through the plate assembly. A review of manufacturer engineering drawings showed that the plate assembly was modified using a spring attached to the plate. A review of the logbooks did not reveal an entry of a modification, or repair of the part. The flight instructor indicated that, during a simulated soft-field takeoff on an instructional flight, the airplane's climb performance noticeably deteriorated. As the airplane reached about 150 ft above ground level, the engine started to lose power. The flight instructor chose to make an emergency off-airport landing, during which the right wing and firewall were substantially damaged. A postaccident examination of the airplane revealed that the alternate air valve plate was lodged in the air intake and blocked the fuel servo. Further examination revealed that the hinge pin that held the alternate air valve plate was worn completely through, which caused the plate assembly to separate from its mounting location and lodge in the fuel servo. This obstruction likely restricted the intake air to the engine and thus led to the loss of engine power on takeoff. Examination of the alternate air valve plate revealed that it had been altered from its original design, although there were no maintenance records documenting the alteration. The investigation could not determine whether this alteration contributed to the failure of the alternate air valve plate's mounting mechanism. Source: NTSB Aviation Accident Database Retrieved: 2026-02-12

NTSB Findings

Hierarchical cause / factor breakdown from the FAA bulk avdata database. Each finding tagged C (Cause) or F (Factor).

• C Aircraft-Aircraft power plant-Power plant-Air intake-Failure - C