CESSNA 172S near New Smyrna Beach, FL — 2011-02-16
- Date
- 2011-02-16
- Location
- New Smyrna Beach, FL, USA
- Aircraft
- CESSNA 172S
- Registration
- N6345L
- Category
- Airplane
- Highest injury
- Fatal
- Fatalities
- 2
- Phase of flight
- Descent
Probable cause
The flight instructor's failure to recognize or implement adequate remedial action to counter the effects of spatial disorientation. Contributing to the accident was the spatial disorientation experienced by one or both pilots.
Contributing factors
Contributing to the accident was the spatial disorientation experienced by one or both pilots.
NTSB narrative
With sunset approaching and nearing coastal water, the flight instructor and the private pilot under instruction were completing a cross-country instrument training flight. One of the pilots contacted air traffic control and reported the airplane's altitude at 7,000 feet. The controller told the pilots to expect vectors for a visual approach to the destination airport. They cancelled their instrument flight rules flight plan, angled the airplane offshore, and completed a right-turning pattern before returning to the shoreline. About 13 minutes after sunset, the airplane again proceeded offshore and appeared to make a general, one and one-half, circle-like pattern to the left, with the last full circle much tighter than the first half circle. During the last full circle, the airplane's altitude decreased from 3,100 feet to 1,700 feet in 14 seconds, a rate of descent of about a 6,000 feet per minute. Witnesses stated that they saw the airplane descending at a high rate, not in a spin, but in a nearly vertical, extreme nose-low attitude before it impacted the water. Wreckage examination confirmed that the airplane impacted the water nose low, left wing down, and slightly inverted. No preexisting mechanical malfunctions or failures were noted with the airplane that would have precluded normal operation, and radar returns did not indicate that any objects detached from the airplane in flight. Weather observations recorded about 2 nm inland and about 10 minutes before the accident indicated visibility of 5 statute miles in light mist, scattered clouds at 800 feet above ground level (agl), and a broken cloud layer at 1,900 feet agl. With diminished lighting conditions, cloudy conditions inland, and a mostly overwater sight picture, it is likely that there was little or no discernible horizon. A loss of horizon reference is conducive to the onset of spatial disorientation. The pilot at the controls was likely not using or believing his instruments, instead, relying on his senses to determine airplane orientation. He then likely attempted to level the airplane by feel and by pulling back on the yoke while in the left turn, which made the turn tighter and lowered the airplane's nose until the airplane was in a vertical descent. It could not be determined which pilot was at the controls or whether both may have been at some point; however, the flight instructor had the ultimate responsibility to maintain safety of flight.
Analysis
- Primary failure mode
- Spatial disorientation
- First missed decision gate
- Cancellation of IFR flight plan without adequate visual references.
NTSB coding
Evidence available
- ATC audio
- ADS-B / radar
- Photos
- 24 docket documents
Docket documents24
- ATC 3 - Attachment 1 - Radar Plotatc
- ATC 3 - Attachment 2 - ATC Radar Data PPB Fileatc
- Partial FAA Air Traffic Control Transcriptatc
- Pilot/Operator Aircraft Accident Report, NTSB Form 6120.1form
- Release of Aircraft Wreckage, NTSB Form 6120.15form
- Statement of Party Representatives to NTSB Investigationinterview
- Flight Instructor Pre-Hire Resumeother
- Memorandum of Record (Change of Investigator in Charge)other
- Memorandum of Record - Correction to Flight Instructor Simulated Flight Timeother
- Photo 1 - Wreckage Overview Less Enginephotos
- Photo 10 - Second Propeller Blade; Some Aft-facing Chordwise Scratchingphotos
- Photo 11 - Overhead View of the Engine from Aftphotos
- Photo 12 - Subsequently-Recovered Left Wing Fragmentphotos
- Photo 13 - Wing Fragment Upper Skin (In Storage Facility Amid Wreckage from other Aircraft)photos
- Photo 2 - Recovered Tail Parts with Vertical Stabilizer Leading Edge Crushed Aft and Rightphotos
- Photo 3 - Seats From Aft Perspective and Left Landing Gear Bent Aftphotos
- Photo 4 - Instrument Panelphotos
- Photo 5 - Airspeed Indicatorphotos
- Photo 6 - Propeller/Engine Combinationphotos
- Photo 7 - Propeller Blade Leading Edge Burnishingphotos
- Photo 8 - Propeller Blade; Some Aft-facing Chordwise Scratchingphotos
- Photo 9 - Second Propeller Blade Leading Edge Burnishingphotos
- Toxicological Report - Flight Instructorreport
- Toxicological Report - Private Pilotreport
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