ASN Wikibase Occurrence # 29988
This information is added by users of ASN. Neither ASN nor the Flight Safety Foundation are responsible for the completeness or correctness of this information.
If you feel this information is incomplete or incorrect, you can
submit corrected information.
Date: | Thursday 19 October 2000 |
Time: | 10:15 |
Type: | Beechcraft C55 Baron |
Owner/operator: | Jetsun Aviation |
Registration: | N782B |
MSN: | TE-247 |
Total airframe hrs: | 3745 hours |
Fatalities: | Fatalities: 2 / Occupants: 2 |
Aircraft damage: | Destroyed |
Category: | Accident |
Location: | 5 miles NW of Homer, Dakota County, Nebraska -
United States of America
|
Phase: | Initial climb |
Nature: | Training |
Departure airport: | Sioux City, IA (SUX) |
Destination airport: | |
Investigating agency: | NTSB |
Confidence Rating: | Accident investigation report completed and information captured |
Narrative:The airplane was destroyed following an uncontrolled descent, and impact with terrain. A witness said that he heard sounds like stall and recovery sounds where power was reduced and power was added. He stated that he observed the airplane fly in stair step like maneuver. He said that during the last step, he observed the airplane in a flat attitude. He estimated that he observed the airplane there to be about 150 to 200 yards above the ground. He stated he saw the airplane in a counter clockwise spin with a nose down attitude. He said that he did not hear any sounds during the airplane's spiral. The instructor pilot had given 5.2 hours of dual instruction since he obtained his multi-engine flight instructor certificate. An on-scene investigation revealed the landing gear selector was down and the landing gear actuator was extended. The flap actuator was found extended to 15 degrees. Control continuity was established to all flight control surfaces. Control continuity was established to both engines. A thumb compression was found at all cylinders of both engines. All magnetos produced spark. Removed spark plugs were gray in color with a carbon colored coating. Both propellers exhibited an aft bend on one of their blades. The propellers exhibited chordwise abrasion. All four fuel tanks were found compromised. No preimpact anomalies were found.
Probable Cause: The inadequate remedial action the flightcrew had during the stall recovery maneuver and the flight instructor's inadequate supervision. A factor was the intentional stall the flightcrew was performing.
Accident investigation:
|
| |
Investigating agency: | NTSB |
Report number: | CHI01FA017 |
Status: | Investigation completed |
Duration: | |
Download report: | Final report |
|
Sources:
NTSB:
https://www.ntsb.gov/_layouts/ntsb.aviation/brief.aspx?ev_id=20001212X22112&key=1 FAA register: 2.
http://registry.faa.gov/aircraftinquiry/NNum_Results.aspx?nNumberTxt=782B Revision history:
Date/time | Contributor | Updates |
27-Sep-2008 01:00 |
ASN archive |
Added |
01-Jun-2014 18:44 |
Dr. John Smith |
Updated [Time, Operator, Total fatalities, Total occupants, Other fatalities, Location, Country, Phase, Nature, Departure airport, Destination airport, Source, Damage, Narrative] |
21-Dec-2016 19:16 |
ASN Update Bot |
Updated [Time, Damage, Category, Investigating agency] |
21-Dec-2016 19:20 |
ASN Update Bot |
Updated [Time, Damage, Category, Investigating agency] |
12-Dec-2017 19:14 |
ASN Update Bot |
Updated [Operator, Departure airport, Destination airport, Source, Narrative] |
07-Jun-2023 12:04 |
Ron Averes |
Updated [[Operator, Departure airport, Destination airport, Source, Narrative]] |
The Aviation Safety Network is an exclusive service provided by:
CONNECT WITH US:
©2024 Flight Safety Foundation