No fatalities

Total Electrical Failure During Night Climb Leads to Runway Excursion at Chester County Airport (N821LG)

Coatesville-Chester County-G. O. Carlson, United States of AmericaLanding (descent or approach)

On February 27, 1986, a Dassault Falcon 10 (registration N821LG) operated by Seneca Sawmill Company was involved in an aviation accident near Coatesville-Chester County-G. O. Carlson, United States of America during landing or approach. No fatalities were reported. Investigators recorded the probable cause as: Occurrence #1: airframe/component/system failure/malfunction due to inadequate maintenance, worn generator, generator failure, battery exhaustion, electrical system inoperative, comm/nav inoperative, stabilator trim inoperative, flap inoperative, steering… This summary draws on records from the Bureau of Aircraft Accidents Archives (B3A).

Sourcesthe Bureau of Aircraft Accidents Archives (B3A)Source recordUpdated 2026-07-04Data APIEditorial standards

While climbing through 19,000 feet at night, generator failures caused total electrical loss. The crew diverted to Chester County Airport; after landing, inoperative systems led to an overrun and collision with objects.

Accident Summary

At night, a climbing aircraft experienced a generator failure at 19,000 feet. The #2 generator light illuminated, indicating no output and the generator could not be reset. The #1 generator voltage was observed at 14–15 volts. The crew reduced the electrical load, but the batteries discharged within about five minutes, resulting in a total loss of electrical power.

Sequence of Events

Using a flashlight for illumination, the crew diverted to Chester County Airport, which has a 4,600-foot runway. The landing gear was extended using the emergency system. The elevator trim was inoperative, requiring both pilots to apply back pressure on the yoke to counteract a nose-down tendency. The aircraft touched down approximately one-quarter of the way down the runway. The crew attempted to use thrust reversers, but they were inoperative. The aircraft continued off the side and beyond the end of the runway, striking a wooden beam and a snowbank before coming to rest in a ditch.

Investigation Findings

The investigation revealed a shaft failure of the #2 generator (starter/generator) and worn brushes in the #1 generator. The total electrical failure rendered several systems inoperative, including wing flaps, anti-skid brakes, the captain's airspeed indicator and altimeter, nose wheel steering, and cockpit lighting.

Probable Cause

The official findings attribute the accident to multiple factors: Occurrence #1 (airframe/component/system failure/malfunction) due to inadequate maintenance, a worn generator, generator failure, battery exhaustion, and inoperative electrical, communication/navigation, stabilator trim, flap, steering, anti-skid, and thrust reverser systems. Occurrence #2 (loss of control on ground) resulted from dark night conditions and failure to maintain directional control. Occurrence #3 (overrun) was due to improper use of powerplant controls. Occurrences #4 and #5 involved collision with an object and encounter with terrain.

Frequently asked questions

What happened in the 27 Feb 1986 Dassault Falcon 10 accident near Coatesville-Chester County-G. O. Carlson, United States of America?

While climbing through 19,000 feet at night, generator failures caused total electrical loss. The crew diverted to Chester County Airport; after landing, inoperative systems led to an overrun and collision with objects.

Were there any fatalities in the 27 Feb 1986 Dassault Falcon 10 accident?

No fatalities were recorded in this accident.

What aircraft was involved and where did it happen?

The accident on 27 Feb 1986 involved a Dassault Falcon 10, registration N821LG, operated by Seneca Sawmill Company, at Coatesville-Chester County-G. O. Carlson, United States of America.

What was the probable cause of the accident?

Occurrence #1: airframe/component/system failure/malfunction due to inadequate maintenance, worn generator, generator failure, battery exhaustion, electrical system inoperative, comm/nav inoperative, stabilator trim inoperative, flap inoperative, steering inoperative, anti-skid inoperative, thrust reverser…