ATL07CA084 · Rotorway Rotorway INTL 162F
Rotorway Rotorway INTL 162F · Accident: total loss of engine power (mechanical failure) en route
From Private strip, NY to Mountain Top Airport (NY02)
Event
- NTSB case
- ATL07CA084
- Event typeAccident: someone killed or seriously injured, or the aircraft substantially damaged (NTSB definition). Incident: an occurrence that affected or could have affected safety, short of that. Glossary
- Accident
- InvestigationHow far the investigation had got when the record was published: preliminary, ongoing, final or completed. Unknown where the source does not say. Glossary
- Completed
- API-reported fatalities
- 0 · all aircraft and ground
- Ground fatalities
- Unknown
- OperationWhat kind of flying it was, grouped by the rules it flew under: airline (US Part 121), air taxi and commuter (Part 135), general aviation (Part 91 and similar), military or government. Glossary
- General aviation
- WeatherVisual meteorological conditions (VMC): good enough to fly by looking outside. Instrument conditions (IMC): cloud or low visibility, flying by instruments. Glossary
- Visual Meteorological Cond
Rotorway Rotorway INTL 162F
- Aircraft type
- Rotorway INTL 162
- Category
- Helicopter
- RegistrationThe aircraft's tail number, such as N12345 or G-ABCD. Registrations are reissued, so the same one years apart can be a different aircraft. Glossary
- N636PB
- Operator
- Paul Breton
- Onboard fatalities
- Unknown
- Route
- From Private strip, NYTo Mountain Top Airport (NY02), ARGYLE, NY
- Aircraft age
- Not recorded
- Flight rulesThe regulations the flight operated under: in the US, Part 91 (general aviation), Part 121 (airlines), Part 135 (air taxi and commuter) and others; for flights abroad, the NTSB's coarser commercial or non-commercial code. Glossary
- Part 91: General Aviation
- Phase of flightThe stage of the flight when things started to go wrong: standing, taxi, takeoff, initial climb, en route, maneuvering, approach or landing. Glossary
- En route · cruise
- First occurrenceThe single coded event the NTSB judges best describes what happened (records from 2008 on). Older records name the first occurrence in the sequence instead. Glossary
- Total loss of engine power (mechanical failure)
- DamageDestroyed: beyond practical repair. Substantial: damage that affects the structure, performance or handling and normally needs major repair. Minor: less than that. Glossary
- Substantial
Cause areas
- Engine assembly, valve, exhaust › Contamination
- Engine assembly, valve, exhaust › Movement restricted
Approximate · Coordinates from the NTSB case API, which marks them as estimated or does not say; no uncertainty radius is established.
NTSB narrative
The certified flight instructor (CFI) stated that the purpose of the flight was instruction. He conducted a preflight of the helicopter and did not note any problems with the helicopter. Start up and run up was completed by the checklist with no problems. They lifted off, hovered for a few minutes and landed again. Shortly thereafter they departed an airport for training. The takeoff and climb were normal, and they leveled off at 1,500 feet. Approximately 3 miles from the airport, the engine began to run rough and there was a drop in power. The dual student transferred the flight controls to the CFI. The CFI decided not to continue the flight to the airport, and initiated an approach to a field behind a house. On approach the engine stopped, and an autorotation was initiated to the field. The touchdown was "smooth" and level, with a slow forward speed. The helicopter slid approximately 10 feet and rolled over onto the left side. Examination of the helicopter by an FAA inspector revealed no flight control anomalies. The pilot reported that the helicopter was fine until the engine power began decrease. The examination of the engine revealed that the number 4 rocker arm was unsecured and the spring retainer was damaged. Further examination revealed that the number 4 exhaust valve had stuck in the open position. In a review of the logbook it was discovered that the mechanic had made valve lash adjustments to all the cylinders on September 16, 2006, at an engine tachometer time of 17.4 hours. The engine tachometer time at the accident site was 18.1 hours. The engine had .7 hours before the exhaust valve failed. The cylinder heads were sent to Rotorway International for examination of the exhaust and intake valves. According to Rotorway, examination of the heads revealed that the exhaust valves were found to be "sticky in their guides". The guide size measured at the low side of the tolerance before cleaning. After cleaning with a wire brush, the fit of the valves in the cylinder heads and the tolerance of sizes were acceptable.
Probable cause
The loss of engine power due to the sticking of the exhaust valves that resulted from carbon buildup.
Verbatim NTSB analysis and probable cause from the NTSB dataset
Sources
NTSB record ATL07CA084
- Event ID
- 20070828X01253
- Case number
- ATL07CA084
- Dataset
- historical-pre2008
- Source SHA-256
- 89e2df6d848e7ab3b42e7d7c7a03ff403303057a26ca04c95b3ea67201c3ce74
Source notes (4)
- Unreviewed is an editorial label, not an investigation status. API-sourced is not report-checked or human-reviewed. Explicit event totals are used without summing aircraft injury tables; onboard allocation is withheld. Unknown values remain unknown. The operation category is mapped from the NTSB-reported FAR part and has not been reviewed.
- Filled from the NTSB case API where the bulk record had no value: investigation status, coordinates. Values present in the bulk record are kept.
- The date is the local date, which is the same as the UTC date the NTSB stores.
- API snapshot SHA-256: 9fd8f199914ae6346b75c83e0f48c991c5b02fb8f66cbe91d9a87acd50d7ca4d; retrieved 2026-09-22T03:48:39.380Z.