No fatalities

1988-12-31: Piper PA-60 Aerostar (Ted Smith 600) (N90393) — Albert T. Gianchiglia — Somerset, United States of America

Somerset, United States of AmericaLanding (descent or approach)

On December 31, 1988, a Piper PA-60 Aerostar (Ted Smith 600) (registration N90393) operated by Albert T. Gianchiglia was involved in an aviation accident near Somerset, United States of America during landing or approach. No fatalities were reported. Investigators recorded the probable cause as: Improper inflight decisions while approaching the airport on final approach with defective magnetos. The right fuel selector was placed in the closed position, the pilot attempted a go around, raised the landing gear and flaps, failed to maintain vmc, and… This summary draws on records from the Bureau of Aircraft Accidents Archives (B3A).

Sourcesthe Bureau of Aircraft Accidents Archives (B3A)Primary reportUpdated 1781214525Data APIEditorial standards

A multi-engine aircraft lost power in the right engine on final approach to Somerset Airport, New Jersey. The pilot raised gear and flaps, the aircraft rolled right and crashed. The fuel selector to the right wing was closed and the magnetos were defective. Four occupants were injured, two seriously.

Overview

On an unspecified date, a multi-engine aircraft was on final approach to runway 30 at Somerset Airport in Somerville, New Jersey. During the approach, the right engine experienced a loss of power. The pilot responded by raising the landing gear and flaps. Subsequently, the aircraft rolled to the right, descended toward the ground, and crashed.

Occupant Injuries

All four occupants on board were injured in the accident, with two sustaining serious injuries.

Aircraft Condition

Post-accident examination revealed that the fuel selector valve for the right wing tank was found in the closed position. Additionally, the magnetos on the right engine were defective, exhibiting signs of being burned and worn.

Sequence of Events

The accident occurred in three phases. First, during the final approach in visual flight rules (VFR) pattern, the right engine lost power. The pilot then initiated a go-around, during which the landing gear and flaps were raised. The aircraft failed to maintain minimum control speed (Vmc), resulting in a loss of control in flight. Finally, the aircraft descended uncontrolled and collided with wooded terrain.

Investigation Findings

The official investigation identified several findings. The ignition system magnetos were burned and worn. The fuel selector/valve was in the closed position. The pilot's improper fuel tank selector position was noted. During the go-around, the pilot attempted a go-around, raised the flaps, and diverted attention. The pilot failed to maintain Vmc, leading to a loss of control.

Probable Cause

As stated in the official report: Improper inflight decisions while approaching the airport on final approach with defective magnetos. The right fuel selector was placed in the closed position, the pilot attempted a go around, raised the landing gear and flaps, failed to maintain vmc, and crashed into wooded terrain.