Casualties unknown

1992-06-13: Piper PA-30 (N7958Y) — Professional Flight Service — Indian Head, MD

Indian Head, MD, US

On June 13, 1992, a Piper PA-30 (registration N7958Y) operated by Professional Flight Service was involved in an aviation accident near Indian Head, MD. Investigators recorded the probable cause as: The pilot's failure to maintain directional control during a simulated engine-out landing due to asymmetric thrust application in a right crosswind, resulting in a runway excursion. This summary draws on records from the U.S. National Transportation Safety Board (NTSB) historical archive.

Sourcesthe U.S. National Transportation Safety Board (NTSB) historical archivePrimary reportUpdated 1781061362Data APIEditorial standards

During a simulated engine-out approach, the pilot added power to one engine at touchdown to soften the landing. A right crosswind caused the aircraft to veer off the runway and strike three parked planes.

What happened

The pilot was conducting a flight that included a simulated engine-out procedure. As part of this training or operational maneuver, the pilot executed an approach and landing with one engine assumed to be inoperative. The objective was to demonstrate proficiency in handling the aircraft under these specific failure conditions.

As the airplane approached the runway threshold for Runway 17, the pilot initiated the flare and touchdown sequence. Upon contact with the pavement, the aircraft encountered a right crosswind component. To manage the descent rate and "soften the touchdown," the pilot applied power to the left engine, which was functioning normally, while maintaining the right engine at simulated zero thrust.

The application of asymmetric thrust during the critical ground roll phase, combined with the lateral wind force, resulted in a loss of directional control. The aircraft veered sharply to the right side of the runway. Unable to correct the trajectory, the airplane departed the paved surface and continued its path into an area where other aircraft were stationary. The out-of-control aircraft collided with three parked airplanes.

The investigation

Post-accident examination focused on the sequence of events leading to the loss of control. Investigators reviewed the pilot's account of the maneuver, specifically the timing of power application relative to touchdown and wind conditions. The physical damage sustained by the involved aircraft was documented to confirm the point of departure from the runway and the nature of the subsequent impacts.

Findings

The primary factor contributing to the accident was the pilot's decision to apply asymmetric power during the touchdown roll while dealing with a crosswind. This action created a yawing moment that, without sufficient rudder correction or differential braking, caused the aircraft to leave the runway environment. The presence of parked aircraft in the overrun area exacerbated the damage but did not cause the initial excursion.

Safety message

Pilots conducting simulated engine-out landings must be aware that asymmetric thrust at or near touchdown can significantly affect directional control, especially in crosswind conditions. Careful management of power settings and rudder input is essential to maintain runway centerline alignment during this vulnerable phase of flight.

Probable cause

The pilot's failure to maintain directional control during a simulated engine-out landing due to asymmetric thrust application in a right crosswind, resulting in a runway excursion.

Investigation report by the U.S. National Transportation Safety Board (NTSB) historical archive. Original record: https://carol.ntsb.gov/event/20001211X14971. This page is a structured re-presentation; facts and quotes are in the National Transportation Safety Board (NTSB), United States.