BEECH A36TC near Erwin, NC — 2012-05-12
- Date
- 2012-05-12
- Location
- Erwin, NC, USA
- Airport
- HRJ
- Aircraft
- BEECH A36TC
- Registration
- N2WZ
- Category
- Airplane
- Highest injury
- Minor
- Fatalities
- 0
- Phase of flight
- Takeoff roll
Probable cause
The partial loss of engine power shortly after takeoff due to fatigue-fractured exhaust valve springs. Contributing to the accident was the mechanic’s decision to install exhaust valve springs with an unknown service history in the engine’s No. 4 cylinder.
Contributing factors
Contributing to the accident was the mechanic’s decision to install exhaust valve springs with an unknown service history in the engine’s No. 4 cylinder.
NTSB narrative
After what he described as an uneventful engine run-up, the pilot took off from the 5,000-foot-long runway. The pilot stated that when the airplane reached an altitude of about 50 feet, he retracted the landing gear; the engine lost partial power. The airplane yawed to the left and touched down again, impacting a thicket. According to a witness who observed the takeoff, the engine power never decreased until the engine stopped suddenly upon impacting the ground. Postaccident examination of the engine revealed that the No. 4 cylinder exhaust valve springs had fractured in fatigue. Detailed examination of the springs showed that the fatigue cracking likely originated from one or more of the iron oxide (rust) pits present on the surface of the springs. The springs had been installed in the engine about 1 year before the accident flight. According to the mechanic who installed the springs, he had retrieved them from a similar engine’s cylinder that was removed from another airplane; there was no documentation of the springs’ service history or serviceability.
Analysis
- Primary failure mode
- Engine power loss
- First missed decision gate
- Pilot could have aborted takeoff when engine began to lose power.
NTSB coding
Evidence available
- Photos
- 13 docket documents
Docket documents13
- Pilot/Operator Aircraft Accident Report, NTSB Form 6120.1form
- Release of Aircraft Wreckage, NTSB Form 6120.15form
- Memorandum for Record - Telephone Interview, Mechanicinterview
- Statement of Party Representatives to NTSB Investigationinterview
- Witness Statementsinterview
- Engine Log (Excerpt)other
- Laboratory Component Analysis (Courtesy of Continental Motors Inc.)other
- Pilot's Weight and Balance Calculationsother
- Engine Log (Excerpt, FAA Photo)photos
- Photo 1 - Airplane from Aft Right (Photo Courtesy of FAA)photos
- Photo 2 - Damage to Lower Fuselage (Photo Courtesy of FAA)photos
- Photo 3 - Photo of Number 4 Cylinder Exhaust Valve Spring Installedphotos
- Photo 4 - Photo of Broken Number 4 Exhaust Valve Springsphotos
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