No fatalities

12 Dec 2015: DEHAVILLAND TIGER MOTH DH 82A (N9410) — Modena, NY

Modena, NY, United States

On 12 Dec 2015, a DEHAVILLAND TIGER MOTH DH 82A (registration N9410) was involved in an aviation accident near Modena, NY. No fatalities were reported. Investigators recorded the probable cause as: A partial loss of engine power due to a stuck No. 1 cylinder exhaust valve. This summary draws on records from NTSB; 6 related events involving the same aircraft type or operator are linked below.

SourcesNTSBPrimary reportUpdated 1778583330Data APIEditorial standards

On December 12, 2015, a DeHavilland Tiger Moth DH-82A sustained substantial damage during a forced landing after takeoff from Old Orchard Airpark, New York. The pilot and passenger were uninjured.

Accident Summary

On December 12, 2015, at approximately 1200 eastern standard time, a DeHavilland Tiger Moth DH-82A, registration N9410, was substantially damaged during a forced landing shortly after departure from Old Orchard Airpark (2NK9) in Modena, New York. The pilot and a passenger were not injured. Visual meteorological conditions prevailed, and no flight plan had been filed for the personal flight conducted under 14 CFR Part 91.

Preflight and Takeoff

The pilot reported performing a pre-takeoff engine run that included an operational check of the magnetos, with no anomalies noted. After takeoff from runway 18, during the initial climb, the engine experienced a 200-rpm reduction in power. The pilot attempted to return to the runway, but the airplane could not maintain altitude and struck trees approximately one-quarter mile from the airport.

Aircraft and Engine Details

The airplane was manufactured in 1940 and equipped with a DeHavilland Gipsy Major 1C engine rated at 145 horsepower. Postaccident examination by a Federal Aviation Administration inspector revealed substantial damage to both wings, the empennage, and the fuselage. When the inspector rotated the engine crankshaft, continuity was observed to the accessory section, and compression was attained on all cylinders except the forward (No. 1) cylinder, which produced little to no compression. Due to the engine's disposition, the ignition system could not be checked for proper operation, and no further examination of the engine was conducted.

Postaccident Findings

The pilot subsequently reported that a teardown of the engine revealed the No. 1 cylinder exhaust valve was stuck in the open position. Additionally, disassembly of the left magneto disclosed a fractured breaker spring. The pilot stated that the loss of compression on one cylinder alone would have necessitated a forced landing, but he believed the combination of the compression loss and the magneto failure resulted in the loss of engine power experienced during the accident flight.

Contributing factors

Causes

Malfunction

Other contributing factors

Damaged/degraded