CIRRUS DESIGN CORP SR22 near Columbus, OH — 2011-06-19
- Date
- 2011-06-19
- Location
- Columbus, OH, USA
- Airport
- LCK
- Aircraft
- CIRRUS DESIGN CORP SR22
- Registration
- N526PG
- Category
- Airplane
- Highest injury
- Fatal
- Fatalities
- 2
- Phase of flight
- Initial climb
Probable cause
The pilot's spatial disorientation during the takeoff into instrument meteorological conditions, which resulted in his failure to maintain control of the airplane.
NTSB narrative
After takeoff in instrument meteorological conditions, the airplane was cleared for a left turn. Shortly thereafter, the airplane entered a left climbing turn, and the pilot engaged the autopilot. The flight director subsequently commanded a right roll and a decrease in pitch attitude. (The GPS steering command was set to navigate to a waypoint, and the shortest way to get there was a turn to the right.) The airspeed decreased to 105 knots and the bank angle was over 45 degrees left-wing low, so the aural underspeed alert activated because of the risk of stall. The nose-up pitch attitude decreased through level flight and entered a nose-down attitude; the left bank angle continued to increase. The underspeed alert ceased when the airplane reached an airspeed of 141 knots; the airplane was at a maximum left bank angle of 72 degrees and a maximum nose-down attitude of 24 degrees. Recorded data showed the engine was producing power throughout the flight and the autopilot was operating normally. An examination of the engine and airplane revealed no evidence of mechanical malfunctions or failures that would have precluded normal operations. Given that the autopilot was set such that it would command a right turn when engaged, yet the pilot was instructed by the air traffic controller to turn left, it is likely that the pilot was overpowering the autopilot system to comply with the instructions. According to the airplane manufacturer, it would only take 17 pounds of force to override the autopilot in pitch and 3 to 5 pounds to override the roll. Further, given the instrument conditions that were present at the time, it is likely that the pilot experience spatial disorientation and did not recognize the effects of his inputs. oxicological results indicated the pilot had taken a sedating medication at some point before the accident; however, the levels were such that a determination of the level of impairment was not possible.
Analysis
- Primary failure mode
- Loss of control
- First missed decision gate
- Pilot could have aborted takeoff or maintained control after engaging autopilot.
NTSB coding
Evidence available
- FDR / data
- Photos
- 32 docket documents
Docket documents32
- Air Traffic Control Informationatc
- Cockpit Display(s) - Recorded Flight Data - Attachment 1 Tabular Data for Figures 9 through 14fdr
- Cockpit Display(s) - Recorded Flight Data - Attachment 2 Tabular Data - MFDfdr
- Cockpit Display(s) - Recorded Flight Data - Attachment 3 Tabular Data - RDMfdr
- Cockpit Display(s) - Recorded Flight Data - Factual Reportfdr
- Release of Aircraft Wreckage, NTSB Form 146120.15form
- Record of Interviewinterview
- Statement of Party Representatives to NTSB Investigationinterview
- Statement of Party Representatives to NTSB Investigationinterview
- Witness Statementsinterview
- Fuel Invoiceother
- Low Altitude En Route Chartother
- Total Station Site Mapother
- Photo 01. Aerial View of Accident Site. Ohio State Highway Patrol Photo.photos
- Photo 02. Aerial View of Accident Site. Ohio State Highway Patrol Photo.photos
- Photo 03. Wreckage Path. Ohio State Highway Patrol Photo.photos
- Photo 04. Main Wreckage Ohio State Highway Patrol Photo.photos
- Photo 05. Main Wreckage. Ohio State Highway Patrol Photo.photos
- Photo 06. Main Wreckage. Ohio State Highway Patrol Photo.photos
- Photo 07. Main Wreckage.photos
- Photo 08. Main Wreckage. Ohio State Highway Patrol Photo.photos
- Photo 09. Main Wreckage. Ohio State Highway Patrol Photo.photos
- Photo 10. Empennage.photos
- Photo 11. Main Wreckage.photos
- Photo 12. Outboard Section of Right Wing.photos
- Photo 13. Outboard Section of Left Wing.photos
- Photo 14. Propellerphotos
- Photo 15. Cylinders 2, 4, and 6.photos
- Photo 16. Cylinders 1, 3, and 5.photos
- Photo 17. View of Wreckage in Hangar. FAA Photo.photos
- Toxicological Reportreport
- Wreckage Examinationwreckage
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