PIPER PA-46-310P near Milaca, MN — 2010-12-30
- Date
- 2010-12-30
- Location
- Milaca, MN, USA
- Aircraft
- PIPER PA-46-310P
- Registration
- N9103N
- Category
- Airplane
- Highest injury
- Fatal
- Fatalities
- 2
- Phase of flight
- Climb
Probable cause
The pilot did not recover from an unusual attitude while operating in instrument meteorological conditions following a disconnect of the autopilot system for undetermined reasons. Contributing to the accident were the pilot’s lack of recent flight experience and impairment due to diphenhydramine.
Contributing factors
Contributing to the accident were the pilot’s lack of recent flight experience and impairment due to diphenhydramine.
NTSB narrative
About 20 minutes after departing on a cross-country flight, the pilot acknowledged the air traffic controller’s clearance to climb to 17,000 feet mean sea level (msl). Radar data indicated that the airplane reached a maximum altitude of 16,800 feet msl. The airplane then entered a right descending turn followed by a left descending turn. While in the left turn, the pilot informed the controller, “I lost my autopilot; I’m in an unusual attitude.” The pilot stated this same information two more times in response to transmissions by the controller. The pilot’s last transmission was that he was busy trying to recover the airplane. Witnesses heard the airplane flying overhead for several minutes, but they could not see it due to the low ceiling. A postaccident examination of the airplane did not reveal any preaccident mechanical malfunctions or failures with the engine that would have precluded normal operation. Examination of the autopilot system revealed a loose screw inside the pitch servo housing. The screw was one of two that secured the high wattage resistor to the solenoid housing. Observed corrosion within the screw threads was consistent with the threads not being engaged in a nut or other internally threaded feature. No mechanical damage or arcing was visible on the screw. The operational impact of the loose screw is unknown. The pilot’s instrument flying proficiency could not be determined. According to log records, the pilot last flew 4.5 months before the accident. The airplane was in instrument meteorological conditions when the pilot stated that he was trying to recover from the unusual attitude. The pilot did not follow prescribed procedures for an autopilot malfunction. Weather data indicates that the airplane most likely encountered turbulence and icing conditions during the flight; however, the airplane was equipped with an ice protection system. Although ethanol was found during the toxicology tests, the levels varied greatly among the tissue/fluid samples. The investigation was unable to determine if the presence of ethanol was from ingestion or from postmortem production or contamination. The detected level of diphenhydramine, an over-the-counter sedating antihistamine used to treat allergies, was above therapeutic levels and likely contributed to the pilot’s inability to recover from the unusual attitude.
Analysis
- Primary failure mode
- Automation / mode confusion
- First missed decision gate
- Pilot could have opted to hand-fly the aircraft instead of relying on autopilot.
NTSB coding
Evidence available
- Photos
- 41 docket documents
Docket documents41
- ATC 3 - Air Traffic Control Specialists Reportatc
- ATC 3 - Attachment 1 - Flight Progress Stripatc
- Air Traffic Control Communicationsatc
- Autopilot Maintenance Informationform
- Release of Aircraft Wreckage, NTSB Form 6120.15form
- Record of Interview - Marianiinterview
- Record of Interview - P. Eberhardtinterview
- Statement of Party Representatives to NTSB Investigationinterview
- Aircraft Flight Logother
- Autopilot Component Examinationother
- Evidence Control Documentationother
- Flight Manual Section 4.49other
- Flight Manual Supplement - Autopilot (Excerpt)other
- Flight Manual Supplement - Ice Protection (Excerpt)other
- JPI Engine Dataother
- Meteorology 5 - Attachment 1other
- Meteorology 5 - Attachment 2other
- Meteorology 5 - Attachment 3other
- Meteorology 5 - Weather Studyother
- Training Recordother
- Materials Laboratory Factual Report 11-069 (with 2 embedded images)photos
- Photo 01. Initial Impact and Main Wreckagephotos
- Photo 02. Left Side of Main Wreckagephotos
- Photo 03. Left Front View of the Main Wreckagephotos
- Photo 04. Left Side of Main Wreckagephotos
- Photo 05. Right Wingphotos
- Photo 06. Rear View of Main Wreckagephotos
- Photo 07. Forward Right View of Main Wreckagephotos
- Photo 08. Propellerphotos
- Photo 09. Accessory Section of the Enginephotos
- Photo 10. Left Side of Enginephotos
- Photo 11. Right Side of Enginephotos
- Photo 12. Left Turbochargerphotos
- Photo 13. Left Turbochargerphotos
- Photo 14. Right Turbochargerphotos
- Photo 15. Right Turbochargerphotos
- Photo 16. Pitch Servophotos
- Photo 17. Pitch Servophotos
- Photo 18. Pitch Servo Screwphotos
- Mille Lacs County Sheriff's Reportreport
- Toxicological Reportreport
Related mishaps
- PIPER PA-28-151
2024-06-24 · Fire Island, NY
- CESSNA A185F
2023-07-09 · La Mesa, CA
- CESSNA 560
2023-06-04 · Montebello, VA · 4 fatalities
- CESSNA 182Q
2022-08-09 · Centennial, CO · 1 fatality
- Siebel Auriga
2020-08-14 · Rockford, IL
- SOCATA TB 30 EPSILON
2019-11-01 · Kalamazoo, MI