ERA09LA460 · McDonnell Douglas Helicopter 369E
Rotorworks McDonnell Douglas Helicopter 369E · Accident: loss of engine power (total) en route
From Cobb County International Airport-McCollum Field (RYY) to Cobb County International Airport-McCollum Field (RYY)
Event
- NTSB case
- ERA09LA460
- 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
McDonnell Douglas Helicopter 369E
- Aircraft type
- McDonnell Douglas 369
- 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
- N527BB
- Operator
- Rotorworks
- Onboard fatalities
- Unknown
- Route
- From Cobb County International Airport-McCollum Field (RYY), Acworth, GATo Cobb County International Airport-McCollum Field (RYY), Acworth, GA
- 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 · descent
- Defining eventThe 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
- Loss of engine power (total)
- 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
- Aircraft › Aircraft power plant
Approximate · Coordinates from the NTSB case API, which marks them as estimated or does not say; no uncertainty radius is established.
NTSB narrative
The pilot stated that he and an observer were conducting an aerial observation when during the descent he heard a loud noise. Subsequently, he received an "ENG OUT" audio and caution lights, and made an emergency autorotation into a field. An examination of the engine’s turbine section revealed rub marks throughout the turbine section consistent with an out-of-balance condition caused by a third-stage turbine airfoil release. The third-stage wheel airfoil fractured in fatigue near the root of the airfoil and no anomalies were found at the fatigue origin. The fracture surface of the failed third-stage blade revealed high-cycle fatigue failure over an extended period of time. The crack propagation is estimated to be greater than 2000 cycles. No additional cracks were found on the other third-stage wheel airfoils.
Review of the logbook revealed that the airframe engine total time was 3,820 hours and the engine had gone through a 100- and 300-hour inspection at 3,809.6 engine hours. All airworthiness directives and applicable service bulletins as well as all instructions for continued airworthiness were complied with. The hot section and turbine inspection was completed on February 21, 2008, at 2,958 hours. The third-stage turbine wheel was overhauled on February 3, 2004, at 1210.6 hours and 1633.0 cycles and was due to be replaced at 4,710.6 hours. At the time of the accident the wheel had 2609.7 hours and 2412.0 cycles.
Probable cause
The loss of engine power due to the fatigue failure of the third-stage turbine wheel airfoil.
Verbatim NTSB analysis and probable cause from the NTSB dataset
Sources
NTSB record ERA09LA460
- Event ID
- 20090812X15132
- Case number
- ERA09LA460
- Dataset
- full-current
- Source SHA-256
- 5cf380f0061817c0331a6b2d8cc7e0ee3a79bea469a1001dc5c10e56f35f5ab3
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: e5a56e8f5bcc3aaa52e0ae49a6bf3c80f6cc56f94c23b37c50130b0188dc0756; retrieved 2026-09-15T12:47:30.922Z.