NYC03FA008 · Pilatus PC-12/45
The Nielsen-Wurster Group Pilatus PC-12/45 · Accident: total loss of engine power (mechanical failure) during initial climb
From Trenton Mercer Airport (TTN) to Washington Dulles International Airport (IAD)
Event
- NTSB case
- NYC03FA008
- 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
- Instrument Meteorological Cond
Pilatus PC-12/45
- Aircraft type
- Pilatus PC-12
- Category
- Airplane
- 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
- N96WF
- Operator
- The Nielsen-Wurster Group
- Onboard fatalities
- Unknown
- Route
- From Trenton Mercer Airport (TTN), Trenton, NJTo Washington Dulles International Airport (IAD), Washington, VA
- 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
- Initial climb
- 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
- Electrical system, generator › Shorted
- Engine assembly, bearing › Failure
Approximate · Coordinates from the NTSB case API, which marks them as estimated or does not say; no uncertainty radius is established.
NTSB narrative
The Pilatus PC-12/45 departed into instrument meteorological conditions. Just as the airplane entered clouds, loud bangs were heard from the engine and flame was observed coming the left side engine exhaust. The pilot in command pushed the nose over, aimed the airplane to where he thought the airport was, and the second pilot initiated engine shutdown. The airplane touched down long and fast, on a wet runway. The pilot intentionally yawed the airplane, and it departed the runway in a nose right 60-degree skid, and struck a chain link fence about 300 feet beyond the departure end of the runway. Examination of the engine revealed the #1 bearing had failed. Electrical pitting was found on the gears in the accessory drive between the starter-generator (SG) attach point, and the # 1 bearing. About 704 hour earlier, the SG had an unscheduled replacement. Records indicated that the SG had burn marks on the stator vanes and armature; however, the initiating event for the SG failure was not determined. Other engines were identified as having experienced electrical discharge damage (EDD), all of which preceded the accident. Each event occurred on a multi-engine airplane and resulted in an in-flight shutdown, followed by a single engine landing. None of the starter generators that were identified as the source of the EDD were original equipment manufacturer (OEM), and all had been previously overhauled. Additional engines were identified as having experienced EDD; however, the records on the engines were incomplete, and there was no starter generator history to review. Goodrich published an overhaul manual for the starter-generator. In the manual they stated that only Goodrich replacement parts should be used, and the use of non-Goodrich parts would void their warranty. However, there was no FAA requirement that the overhaul be conducted by an FAA approved repair station, or that only Goodrich parts be used as replacement items
Probable cause
A power loss, due to failure of the No. 1 bearing, which was a result of previous electrical discharge damage (EDD). Factors were the low ceiling and a wet runway.
Verbatim NTSB analysis and probable cause from the NTSB dataset
Sources
NTSB record NYC03FA008
- Event ID
- 20021101X05421
- Case number
- NYC03FA008
- 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: cae3586fd47e6edac0622faf939e22a4b43fbcc9dfbaaf1b2800a09db3fdf1cc; retrieved 2026-09-21T19:35:46.133Z.