2 fatalities

1996-06-10: Beechcraft 90 King Air (N916PA) — Ruma Advisory Company — Wiscasset, United States of America

Wiscasset, United States of AmericaTakeoff (climb)

On June 10, 1996, a Beechcraft 90 King Air (registration N916PA) operated by Ruma Advisory Company was involved in an aviation accident near Wiscasset, United States of America during takeoff. 2 people were killed. Investigators recorded the probable cause as: Failure of the pilot to maintain control of the airplane while climbing after takeoff, due to spatial disorientation, which resulted in an uncontrolled descent and subsequent collision with terrain. This summary draws on records from the Bureau of Aircraft Accidents Archives (B3A).

Sourcesthe Bureau of Aircraft Accidents Archives (B3A)Primary reportUpdated 1781206971Data APIEditorial standards

A Beech E90 veered left after takeoff and crashed in an uncontrolled descent 1.6 miles north of the airport. Investigation revealed a 840-pound fuel imbalance from a partial refueling three days earlier, and the pilot was not informed. No preimpact malfunctions were found.

Accident Overview

A pilot took off on runway 07 and was cleared direct to the Wiscasset NDB, located east of the airport. Shortly after takeoff, the airplane began turning to the left. The pilot then asked the controller, "...can you tell if I'm in a turn? I have a problem here." Soon thereafter, the airplane collided with terrain in an uncontrolled descent, approximately 1.6 miles north of the airport.

Fueling and Imbalance

Investigation revealed that three days before the accident, a refueler had added 840 pounds of fuel to the airplane's left wing. The fuel farm then ran out of fuel, and no further fueling was accomplished. The pilot was not advised of the uneven fuel load. During the preflight, procedures in the Beech E90 Pilot's Operating Manual (POM) included a check of the fuel tanks. The Beech C90 POM specified a maximum fuel imbalance of 200 pounds, but the E90 POM did not specify a maximum fuel imbalance. Examination of the wreckage found no preimpact malfunction or failure.

Probable Cause

The official probable cause was stated as: Failure of the pilot to maintain control of the airplane while climbing after takeoff, due to spatial disorientation, which resulted in an uncontrolled descent and subsequent collision with terrain. Factors relating to the accident were: the improper refueling (servicing of the aircraft) by FBO personnel, and failure of the pilot to note the excessive lateral imbalance of the airplane during preflight.