CESSNA P337H near Kona, HI — 2023-02-14
- Date
- 2023-02-14
- Location
- Kona, HI, USA
- Airport
- KOA
- Aircraft
- CESSNA P337H
- Registration
- N5KR
- Category
- Airplane
- Highest injury
- Minor
- Fatalities
- 0
- Phase of flight
- Takeoff roll
Probable cause
The failure of the pilot to recognize that the rear engine was not operating during takeoff, which resulted in an attempted single-engine takeoff and the airplane’s subsequent descent and impact with terrain. Contributing to the accident was a loss of rear engine power for reasons that could not be determined.
Contributing factors
Contributing to the accident was a loss of rear engine power for reasons that could not be determined.
NTSB narrative
The pilot reported that during the preflight inspection and engine run-up, he noted no anomalies with the airplane. Then, on departure, the airplane lost partial power. The pilot performed an emergency landing to the runway overrun area with the landing gear retracted, and the airplane sustained substantial damage to the fuselage. Postaccident examination of the engines revealed no evidence of any preimpact mechanical malfunctions or failures that would have precluded normal operation. During the examination the rear engine started normally, accelerated smoothly, and ran continuously without interruption. Review of recorded engine monitoring data revealed that the rear engine lost total engine power during the engine run-up. Although the reason for the rear engine’s total loss of power during the engine run-up could not be determined, the pilot should have recognized that the rear engine was not operating during the takeoff roll and aborted the takeoff. Placards on the instrument panel and the owner’s manual stated, “Do not initiate single engine take-off,” The continuation of the takeoff in this condition resulted in the airplane’s inability to climb and its subsequent descent and impact with terrain.
Analysis
- Primary failure mode
- Loss of control
- First missed decision gate
- Pilot should have aborted takeoff when performance decreased after gear retraction.
NTSB coding
Evidence available
- Photos
- 10 docket documents
Docket documents10
- PILOT/OPERATOR AIRCRAFT ACCIDENT REPORT, NTSB FORM 6120.1form
- RELEASE OF AIRCRAFT WRECKAGE, NTSB FORM 6120.15form
- PILOT'S STATEMENTinterview
- AIRPLANE WEIGHT AND BALANCEother
- ENGINE EXAM NOTESother
- EXCERPTS FROM THE OWNER'S MANUALother
- MAINTENANCE LOGBOOKother
- INVESTIGATIVE PHOTOGRAPHSphotos
- ATTACHMENT 1 TO ENGINE DATA MONITOR - SPECIALIST'S FACTUAL REPORTreport
- ENGINE DATA MONITOR - SPECIALIST'S FACTUAL REPORTreport
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