17 fatalities

Skydiving Flight Crash Kills All 17 After Engine Failure Due to Fuel Contamination (N551CC)

Jenkinsburg, United States of AmericaTakeoff (climb)

On September 29, 1985, a Cessna 208A Caravan (registration N551CC) operated by Air Carriers Express Services was involved in an aviation accident near Jenkinsburg, United States of America during takeoff. 17 people were killed. Investigators recorded the probable cause as: Loss of engine power due to fuel contamination (water and algae) leading to blocked filters; loss of control due to pilot's failure to maintain airspeed resulting in inadvertent stall and spiral; contributing factors: improper maintenance/service, operation… This summary draws on records from the Bureau of Aircraft Accidents Archives (B3A); 8 related events involving the same aircraft type or operator are linked below.

Sourcesthe Bureau of Aircraft Accidents Archives (B3A)Primary reportUpdated 2026-06-11Data APIEditorial standards

A skydiving flight crashed shortly after takeoff when the engine lost power due to contaminated fuel. The aircraft was overweight, had a disabled stall warning, and all 17 occupants were killed.

Accident Overview

A skydiving flight carrying a pilot and 16 jumpers lost engine power at approximately 300 feet above ground level during initial climb. The aircraft banked steeply left, entered a steep nose-down spiral, and crashed. All 17 occupants were killed.

Fuel Contamination

Post-crash examination revealed that the fuel tanks contained water and foreign material resembling brown algae. The engine fuel control unit held a milky fluid composed of approximately 65% jet fuel and 34% water, along with iron contaminants. Fuel filters contained dark stringy material. The aircraft had been refueled from 55-gallon drums that were stored upright; rain water could leak through the filler caps. The aircraft, registration N551CC, had a history of fuel contamination that occasionally triggered the fuel bypass indicator.

Weight and Balance Issues

The aircraft was estimated to be 370 pounds over its maximum weight limit and 1 foot forward of the center of gravity limit. Nine passenger seats had been removed to accommodate up to 18 jumpers, and seat belts were not used by the occupants.

Disabled Warning System

According to reports, the stall warning circuit breaker had been disengaged on previous flights to avoid startling the jumpers. Due to impact damage, its pre-impact position could not be verified.

Lack of FAA Surveillance

The investigation noted a lack of Federal Aviation Administration (FAA) surveillance of the operator.

Official Findings

The official findings attributed the accident to three occurrences: loss of engine power (total) due to fuel contamination and blocked filters; loss of control in flight due to pilot's failure to maintain airspeed resulting in inadvertent stall and spiral, compounded by the aircraft being overweight and forward of CG, and a disabled stall warning; and in-flight collision with terrain. Contributing factors included improper maintenance, operation with known deficiencies, and inadequate FAA surveillance.

Probable cause

Loss of engine power due to fuel contamination (water and algae) leading to blocked filters; loss of control due to pilot's failure to maintain airspeed resulting in inadvertent stall and spiral; contributing factors: improper maintenance/service, operation with known deficiencies, inadequate FAA surveillance, aircraft overweight and forward of CG, disabled stall warning circuit breaker, and lack of seat belt use.