NYC07LA125 · Cessna 172E
Cessna 172E · Accident: partial loss of engine power (mechanical failure) en route
From Leesburg Executive Airport (JYO) to Culpeper Regional Airport (CJR)
Event
- NTSB case
- NYC07LA125
- 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
Cessna 172E
- Aircraft type
- Cessna 172
- 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
- N3982S
- Operator
- Unknown
- Onboard fatalities
- Unknown
- Route
- From Leesburg Executive Airport (JYO), Leesburg, VATo Culpeper Regional Airport (CJR), Culpeper, 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
- 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
- Partial 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, rocker arm/tappet › Failure
Approximate · Coordinates as recorded by the NTSB; no uncertainty radius is established.
NTSB narrative
The pilot was relocating a Cessna 172E for the airplane's annual maintenance inspection. During the flight, the engine suffered a partial loss of power and began to "shake and misfire violently." The pilot then attempted to control the engine by adjusting the throttle and mixture controls, without result. As the airplane descended, the pilot looked for a place to land and spotted an open field. After turning final, he extended his wing flaps to the 40-degree position and touched down. During the emergency landing the airplane approached a ditch. The pilot attempted to get over the ditch by raising the flaps, but the airplane struck the far side of the ditch. During a postaccident examination of the engine, it was discovered that the No.2 cylinder's exhaust valve rocker arm was fractured and had separated into two parts. The initial fracture on the exhaust valve rocker arm was on the push rod side of the arm. This fracture had features indicative of overstress. The fracture on the valve side of the arm was secondary to the overstress fracture on the push rod side. The fatigue cracking at this location appeared to be the result of bending loads generated after the fracture on the push rod side was created. The fracture on the push rod side of the arm was generated from some type of high load event, possibly during an overhaul 34.8 hours prior to the accident. The pilot/owner had purchased one of the cylinders on "eBay," and there were discrepancies in the engine maintenance records.
Probable cause
The loss of engine power that resulted from the failure of an exhaust valve rocker arm during cruise.
Verbatim NTSB analysis and probable cause from the NTSB dataset
Sources
NTSB record NYC07LA125
- Event ID
- 20070624X00785
- Case number
- NYC07LA125
- 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. 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: cad136767856e0bedaaf46e476c07cb4474358fa7ce229e33e9d328e4231a288; retrieved 2026-09-21T18:30:45.125Z.