PIPER PA-28R-201T near Kalispell, MT — 2012-02-04
- Date
- 2012-02-04
- Location
- Kalispell, MT, USA
- Airport
- KS27
- Aircraft
- PIPER PA-28R-201T
- Registration
- N38906
- Category
- Airplane
- Highest injury
- Minor
- Fatalities
- 0
- Phase of flight
- Initial climb
Probable cause
The partial loss of engine power due to magneto malfunction. Contributing to the accident was the lack of adherence to the manufacturer’s recommended magneto overhaul schedule.
NTSB narrative
After takeoff, between 300 and 500 feet above ground level over a residential area, the airplane's engine started to sputter and lose power. The pilot selected the longest street on which to make a forced landing, lowered the flaps, and slowed the airplane to a minimum controllable airspeed. The airplane collided with a number of vehicles and trees, and, in the process, the left wing separated from the fuselage. The airplane rotated inverted and embedded itself into the front of a residential house. Postaccident examination and testing of the left magneto revealed that the magneto’s distributor block bushing was worn to an extent that it provided significant radial play between the bushing and distributor block. The bushing, which holds the distributor gear axle in place, would permit the distributor gear to intermittently disengage from the drive gear. Once the distributor gear had disengaged from the drive gear, the internal timing of the magneto would be off, which could disrupt the normal ignition sequence and operation of the engine. If the pilot had switched to the right magneto, engine power would have likely been restored. The most recent magneto overhaul was performed in 1989. The engine manufacturer recommends that magnetos be overhauled or replaced 5 years after the date of manufacture or last overhaul, or 4 years after the date placed in service, whichever occurs first, without regard to accumulated operating hours since new or last overhaul.
Analysis
- Primary failure mode
- Engine power loss
- First missed decision gate
- Pilot could have aborted takeoff after engine started to sputter.
NTSB coding
Evidence available
- Video
- Photos
- 14 docket documents
Docket documents14
- Evidence Control Formform
- Pilot/Operator Aircraft Accident Report, NTSB Form 6120.1form
- Release of Aircraft Wreckage, NTSB Form 6120.15form
- Statement of Party Representatives to NTSB Investigationinterview
- Witness Statementinterview
- Engine Logbook (extract)other
- Piper PA-28R-201T Emergency Procedures (extract)other
- Record of Conversation with the Pilotother
- S-20 Service Manual (extract)other
- Photo 1 - On scene photo showing airplane and house.photos
- Reports from Parties to the Investigation - CMI Field Inspection Reportreport
- Reports from Parties to the Investigation - CMI Magneto Analytical Reportreport
- FAA Video Emailvideo
- Video Filevideo
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