PIPER PA-32R-300 near Tulsa, OK — 2009-09-05
- Date
- 2009-09-05
- Location
- Tulsa, OK, USA
- Aircraft
- PIPER PA-32R-300
- Registration
- N1228H
- Category
- Airplane
- Highest injury
- Fatal
- Fatalities
- 5
- Phase of flight
- Initial climb
Probable cause
The non-instrument-rated pilot’s decision to attempt flight in instrument meteorological conditions, which resulted in spatial disorientation and an in-flight collision with a radio tower guy wire.
NTSB narrative
The non-instrument-rated private pilot obtained a standard weather briefing for a cross-country flight and was advised that a visual flight rules (VFR) flight was not recommended. The ceiling was 600 feet overcast with 4 miles visibility. Approximately 4 hours later, the pilot radioed ground control for taxi and a VFR clearance. The controller informed the pilot that the airport was in instrument flight rules (IFR) conditions. The pilot then requested and received an IFR clearance. The pilot departed and had to be reminded by the local and departure controllers to make several course and altitude changes. The pilot acknowledged the changes but took no action. The pilot was also warned of antennas near his position. Review of radar data revealed the pilot's altitude varied from 1,100 feet mean sea level (msl) to 1,600 feet (msl). The last radar target was at 1,200 feet msl in a left descending turn although the pilot had been instructed to climb to 4,000 feet 2 minutes before the accident. During periods of low visibility, a pilot is particularly vulnerable to spatial disorientation. Further, the pilot's descending turn when he was supposed to be climbing is indicative of spatial disorientation. The airplane then collided with a guy wire on a 600-foot radio transmission tower at a terrain elevation of 860 feet msl. Postaccident examination of the airframe, flight controls, engine assembly, and accessories revealed no anomalies. The altimeter, transponder, and transponder automatic altitude reporting system test was current. The gyroscopic instruments were destroyed and could not be examined.
Analysis
- Primary failure mode
- VFR into IMC
- First missed decision gate
- Pilot should have aborted takeoff due to IMC conditions.
NTSB coding
Evidence available
- ADS-B / radar
- Photos
- 32 docket documents
Docket documents32
- ATC IFR Stripatc
- ATC Report Extractsatc
- FAA Form 7230 4form
- Radio Transmission Tower Informationform
- Release of Aircraft Wreckage, NTSB Form 6120.15form
- Controller Statementsinterview
- Statement of Party Representatives to NTSB Investigationinterview
- Witness Refuel Statementinterview
- Witness Statementinterview
- Champion Check A Plugother
- Extract Logbooksother
- Extract Pilot's Burned Logbookother
- FAA Advisory Circular Spatial Disorientationother
- Sectional With Flight Pathother
- Weatherother
- Photo 1 Panoramic view of crash site. Photo Piperphotos
- Photo 10 View of right side of airplane. Photo Piperphotos
- Photo 11 View of left Horizontal stabilizer. Photo Piperphotos
- Photo 12 View of separted left wing. Photo Piperphotos
- Photo 2 View of engine and propeller assembly. Note guy wire wrapped around cabin area. Photo Piperphotos
- Photo 3 Another view of engine and propeller assembly. Photo Piperphotos
- Photo 4 View of separated steel guy wire cable. Photo Piperphotos
- Photo 5 View of forward and aft cabin area. Photo Piperphotos
- Photo 6 View of fragmented instrument panel. Photo Piperphotos
- Photo 7 Left front side view of cabin area. Photo Piperphotos
- Photo 8 View of separated inboard right wing section. Photo Piperphotos
- Photo 9 View of separated outboard right wing section. Photo Piperphotos
- Radar Plots N1228Hradar
- Police Reportreport
- Toxicology Reportreport
- Transcriptstranscript
- Wreckage Diagramwreckage
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