CESSNA 501 near Franklin, NC — 2012-03-15
- Date
- 2012-03-15
- Location
- Franklin, NC, USA
- Airport
- 1A5
- Aircraft
- CESSNA 501
- Registration
- N7700T
- Category
- Airplane
- Highest injury
- Fatal
- Fatalities
- 5
- Phase of flight
- Approach
Probable cause
The pilot's failure to achieve a stabilized approach, resulting in a nose-first, bounced landing. Contributing to the accident was the pilot's activation of only one thrust reverser, resulting in asymmetrical thrust.
Contributing factors
Contributing to the accident was the pilot's activation of only one thrust reverser, resulting in asymmetrical thrust.
NTSB narrative
The pilot was not familiar with the mountain airport. The airplane was high during the first visual approach to the runway. The pilot performed a go-around and the airplane was again high for the second approach. During the second approach, the approach angle steepened, and the airplane pitched nose-down toward the runway. The nosegear touched down about halfway down the runway followed by main gear touchdown. The airplane then bounced and the sound of engine noise increased as the airplane banked right and the right wing contacted the ground. The airplane subsequently flipped over and off the right side of the runway, and a postcrash fire ensued. Examination of the airframe and engines did not reveal any preimpact mechanical malfunctions. The examination also revealed that the right engine thrust reverser was deployed during the impact sequence, and the left engine thrust reverser was stowed. Although manufacturer data revealed single-engine reversing has been demonstrated during normal landings and is easily controllable, the airplane had already porpoised and bounced during the landing. The pilot’s subsequent activation of only the right engine’s thrust reverser would have created an asymmetrical thrust and most likely exacerbated an already uncontrolled touchdown. Had the touchdown been controlled, the airplane could have stopped on the remaining runway or the pilot could have performed a go-around uneventfully.
Analysis
- Primary failure mode
- Loss of control
- First missed decision gate
- Pilot could have executed a go-around earlier during the second approach.
NTSB coding
Evidence available
- Photos
- 23 docket documents
Docket documents23
- ATC Dataatc
- Evidence Control Formform
- Release of Aircraft Wreckage, NTSB Form 6120.15form
- Interview Summaryinterview
- Statement of Party Representatives to NTSB Investigationinterview
- Witness Statementsinterview
- Correspondence From Lockheed Martinother
- Excerpt From Maintenance Recordsother
- Excerpts From Cessna 500/501 Operation Manualother
- Excerpts From Cessna 501 Flight Manualother
- Excerpts From Pilot Logbookother
- Fuel Receiptother
- Photograph # 1: First Skid Marksphotos
- Photograph # 2: Second Skid Marksphotos
- Photograph # 3: View of Main Wreckage From Left Sidephotos
- Photograph # 4: View of Main Wreckage From Frontphotos
- Photograph # 5: View of Main Wreckage From Right Sidephotos
- Photograph # 6: Aft View of Main Wreckagephotos
- Photograph # 7: Right Engine Thrust Reverserphotos
- Manufacturer Report of Engine Examinationsreport
- Toxicological Reportreport
- Weather Reportreport
- GPS Plot of Skid Marks and Wreckagewreckage
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