PIPER PA 28R-201T near Nipton, CA — 2017-11-17
- Date
- 2017-11-17
- Location
- Nipton, CA, USA
- Aircraft
- PIPER PA 28R-201T
- Registration
- N5966V
- Category
- Airplane
- Highest injury
- None
- Fatalities
- 0
- Phase of flight
- Cruise
Probable cause
A loss of engine power due to the detonation of the No. 5 cylinder due to excessive leaning at high power settings, which resulted in a forced landing and the subsequent hard touchdown.
NTSB narrative
About 40 minutes after takeoff and while the airplane was at a cruise altitude of 10,000 ft mean sea level, the pilot began leaning the engine mixture. After about 5 minutes, the pilot observed that the engine was running roughly, the No. 5 cylinder head temperature had spiked, and the airplane was unable to maintain altitude. The pilot could not restore engine power and subsequently made a forced landing on a highway. The airplane touched down hard, which resulted in substantial damage to both wings. A postaccident engine examination confirmed continuity to the accessory section. Spark was produced on all six top spark plug leads, and thumb compression was obtained on all cylinders except the No. 5 cylinder. The top spark plugs were removed, and all except the No. 5 spark plug exhibited dark-colored combustion deposits; the No. 5 spark plug exhibited a molten, metal-like substance around the electrode. Cylinder Nos. 1 and 3 exhibited minor signs of detonation. The No. 5 cylinder exhibited signs of detonation/preignition with material missing from around the circumference of the piston face, and the No. 5 cylinder exhaust and intake valves showed signs of mechanical damage. The detonation was consistent with excessive leaning at high power settings.
Analysis
- Primary failure mode
- Mechanical failure
- First missed decision gate
- Pilot could have diverted to alternate airport instead of attempting highway landing.
NTSB coding
Evidence available
- 6 docket documents
Docket documents6
- EVIDENCE CONTROL FORMform
- PILOT/OPERATOR AIRCRAFT ACCIDENT REPORT, NTSB FORM 6120.1form
- RELEASE OF AIRCRAFT WRECKAGE, NTSB FORM 6120.15form
- SUMMARY OF ENGINE EXAMINATIONother
- ENGINE DATA MONITOR (EDM) - SPECIALIST'S FACTUAL REPORTreport
- ENGINE DATA MONITOR (EDM) - SPECIALIST'S FACTUAL REPORT - ATTACHMENT 1report
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