PIPER PA-32R-301T near Groveland, CA — 2010-02-20
- Date
- 2010-02-20
- Location
- Groveland, CA, USA
- Airport
- E45
- Aircraft
- PIPER PA-32R-301T
- Registration
- N4175A
- Category
- Airplane
- Highest injury
- Fatal
- Fatalities
- 2
- Phase of flight
- Approach
Probable cause
The pilot's continued flight into night instrument meteorological conditions during the landing approach, which resulted in an in-flight loss of aircraft control due to spatial disorientation.
NTSB narrative
The instrument-rated pilot departed at night without obtaining a weather briefing or filing an instrument flight plan. Radar track data revealed no deviations of heading or altitude for the en route segment, indicative of consistent autopilot usage. For a portion of the flight, the pilot was in communication with air traffic control (ATC) and was receiving flight following. As he approached the airport he reported to ATC that the airport was not in sight and that he would return if it was covered in a fog layer. The radar data indicated that the airplane continued to overfly the runway and begin a series of rapid altitude and heading changes. Multiple witnesses reported hearing an airplane flying with high engine speeds in the vicinity of the airport subsequent to its collision with the ground. The wreckage path, instrument indications, and damage to surrounding trees were indicative of a high-speed, 80-degree-right-bank, and 45-degree-nose-down collision with terrain. The pilot, having flown only two instrument approaches in the preceding 6 months, was not current to fly an instrument approach. He had limited experience landing at the accident airport at night and had never performed an instrument approach into the airport in actual instrument meteorological conditions (IMC). The airplane was equipped with an autopilot and instruments suitable for flight in IMC. Impact damage and postaccident fire prevented a determination of the operational status of these systems. Examination of the remaining wreckage revealed no evidence of premishap or mechanical malfunctions of the engine and airframe. An hour prior to the accident, another pilot reported performing a missed approach at the arrival airport due to limited visibility, followed by a diversion to an alternate airport. Witnesses and en route weather reporting facilities reported low clouds, fog, and precipitation in the vicinity of the airport. The weather conditions and operation at night were conducive to the onset of pilot spatial disorientation as indicated by the airplane's multiple rapid descents, ascents, and heading changes after the airplane passed over the airport.
Analysis
- Primary failure mode
- Spatial disorientation
- First missed decision gate
- Pilot could have diverted to alternate airport instead of attempting to land.
NTSB coding
Evidence available
- ATC audio
- ADS-B / radar
- Photos
- 34 docket documents
Docket documents34
- FAA Air Traffic Control Audioatc
- Release of Aircraft Wreckage, NTSB Form 6120.15 - Evidence Controlform
- Statement of Party Representatives to NTSB Investigationinterview
- Witness Statementsinterview
- Airframe Maintenance Logbook Excerptsother
- Engine Maintenance Logbook Excerptsother
- N4175A Original Equipment List Excerptsother
- NTSB Airframe Examination Notesother
- NTSB Engine Examination Notesother
- Pilot Logbook Excerptsother
- Pilot Weather Access and Work Scheduleother
- Propeller Maintenance Logbook Excerptsother
- U.S. Naval Observatory Sun and Moon Dataother
- Image 1 - Route of Flight Radar Dataphotos
- Image 2 - Radar Data for Last 2 Minutes of Flightphotos
- Photograph 1 - Pine Mountain Lake Airport Webcam Image-Downloaded 3/10/2010 from http://wallacecompany.com/E45/index.htmlphotos
- Photograph 10 - Engine Underside Viewphotos
- Photograph 11 - Engine Right Side Viewphotos
- Photograph 12 - Engine Aft Viewphotos
- Photograph 13 - Airspeed Indicatorphotos
- Photograph 14 Attitude Indicator Vanesphotos
- Photograph 15 - Turbocharger Assemblyphotos
- Photograph 2 - Tree Swath - View To The Southwest From The Impact Craterphotos
- Photograph 3 - Crater and Debris Field View To The Northphotos
- Photograph 5 - Main Cabin Wrecakge View Facing Northphotos
- Photograph 6 - Forward Cabinphotos
- Photograph 7 - Engine At Accident Sitephotos
- Photograph 8 - Forward Enginephotos
- Photograph 9 - Propeller Blade 3 Located In Craterphotos
- Photogrpah 4 - Green Lens Fragments And Wing Tip Navigation Lamp Casing Located At Initial Impact Fencephotos
- FAA Radar Data 1200 Beacon Code (.kml format)radar
- FAA Radar Data 4530 Beacon Code (.kml format)radar
- Weather Radar Data With Radar Track Overlay: WSR-88D KDAXradar
- Toxicological Report: Pilotreport
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