Fort Lauderdale - Fernandina Beach
Flight / Schedule
Fort Lauderdale - Fernandina Beach
Aircraft
Cessna 421B Golden Eagle IIRegistration
N1935G
MSN
421B-0836
Year of Manufacture
1974
Operator
Sebring Air CharterDate
April 17, 2009 at 11:15 AM
Type
CRASHFlight Type
Positioning
Flight Phase
Takeoff (climb)
Crash Site
City
Crash Location
Fort Lauderdale-Executive Florida
Region
North America • United States of America
Coordinates
26.1960°, -80.1808°
Crash Cause
Technical failure
Narrative Report
On April 17, 2009 at 11:15 AM, Fort Lauderdale - Fernandina Beach experienced a crash involving Cessna 421B Golden Eagle II, operated by Sebring Air Charter, with the event recorded near Fort Lauderdale-Executive Florida.
The flight was categorized as positioning and the reported phase was takeoff (climb) at a city crash site.
1 people were known to be on board, 1 fatalities were recorded, 0 survivors were identified or estimated. This corresponds to an estimated fatality rate of 100.0%.
Crew on board: 1, crew fatalities: 1, passengers on board: 0, passenger fatalities: 0, other fatalities: 0.
The listed crash cause is technical failure. Prior to the accident flight witnesses observed the pilot "haphazardly" pouring oil into the right engine. The pilot then ran the engines at mid-range power for approximately 20 minutes. The airplane subsequently taxied out of the ramp area and departed. Fire was observed emanating from the right engine after rotation. The airplane continued in a shallow climb from the runway, flying low, with the right engine on fire. The airplane then banked right to return to the airport and descended into a residential area. Examination of the right engine revealed an exhaust leak at the No. 4 cylinder exhaust riser flange. Additionally, one of the flange boltholes was elongated, most likely from the resulting vibration. The fuel nozzle and B-nut were secure in the No. 4 cylinder; however, its respective fuel line was separated about 8 inches from the nozzle. No determination could be made as to when the fuel line separated (preimpact or postimpact) due to the impact and postcrash fire damage. Examination of the right engine turbocharger revealed that the compressor wheel exhibited uniform deposits of an aluminum alloy mixture, consistent with ingestion during operation, and most likely from the melting of the aluminum fresh air duct. Additionally, the right propeller was found near the low pitch position, which was contrary to the owner's manual emergency procedure to secure the engine and feather the propeller in the event of an engine fire.
Aircraft reference details include registration N1935G, MSN 421B-0836, year of manufacture 1974.
Geospatial coordinates for this crash are approximately 26.1960°, -80.1808°.
Fatalities
Total
1
Crew
1
Passengers
0
Other
0
Crash Summary
Prior to the accident flight witnesses observed the pilot "haphazardly" pouring oil into the right engine. The pilot then ran the engines at mid-range power for approximately 20 minutes. The airplane subsequently taxied out of the ramp area and departed. Fire was observed emanating from the right engine after rotation. The airplane continued in a shallow climb from the runway, flying low, with the right engine on fire. The airplane then banked right to return to the airport and descended into a residential area. Examination of the right engine revealed an exhaust leak at the No. 4 cylinder exhaust riser flange. Additionally, one of the flange boltholes was elongated, most likely from the resulting vibration. The fuel nozzle and B-nut were secure in the No. 4 cylinder; however, its respective fuel line was separated about 8 inches from the nozzle. No determination could be made as to when the fuel line separated (preimpact or postimpact) due to the impact and postcrash fire damage. Examination of the right engine turbocharger revealed that the compressor wheel exhibited uniform deposits of an aluminum alloy mixture, consistent with ingestion during operation, and most likely from the melting of the aluminum fresh air duct. Additionally, the right propeller was found near the low pitch position, which was contrary to the owner's manual emergency procedure to secure the engine and feather the propeller in the event of an engine fire.
Cause: Technical failure
Occupants & Outcome
Crew On Board
1
Passengers On Board
0
Estimated Survivors
0
Fatality Rate
100.0%
Known people on board: 1
Operational Details
Schedule / Flight
Fort Lauderdale - Fernandina Beach
Operator
Sebring Air CharterFlight Type
Positioning
Flight Phase
Takeoff (climb)
Crash Site
City
Region / Country
North America • United States of America
