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ERA18LA072 · Cessna P210N N

29 Jan 2018 · Farmington, PA, United States

Romag Air Services Cessna P210N N · Accident: loss of engine power (total) en route

From Montgomery County Airpark (GAI) to Wheeling Ohio County Airport (HLG)

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Event

NTSB case
ERA18LA072
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

Cessna P210N N

Aircraft type
Cessna 210
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
N34VF
Onboard fatalities
Unknown
Route
From Montgomery County Airpark (GAI), Gaithersburg, MDTo Wheeling Ohio County Airport (HLG), Wheeling, WV
Aircraft age
About 39 years (built 1979)
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
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 as recorded by the NTSB; no uncertainty radius is established.

NTSB narrative

During cruise flight in instrument meteorological conditions, the engine lost total power and the commercial pilot performed a forced landing to a field after emerging from the clouds about 300 ft above ground level; the airplane struck trees and a power line, resulting in a loss of control, impact with the ground, and subsequent post-impact fire. Examination of the engine revealed that the crankshaft drive gear was missing teeth, the camshaft gears were damaged, and each of the six pistons displayed valve impact damage. It is likely that the missing teeth from the drive gear caused an out-of-alignment condition that led to a cascade of additional damage to the mating timing gear on the camshaft. The improper engagement of the crankshaft drive gear to the camshaft compromised the timing of the entire valvetrain, which resulted in the loss of engine power. Review of the five most recent oil analysis results conducted during the 13 months before the accident revealed elevated levels of iron, chromium, silicon and nickel; elements present in the alloy steel drive gear. These levels were considered elevated relative to the initial oil analysis sample taken about 15 months before the accident. It is likely that the fatigue cracking had begun or become severe enough to alter the composition of the oil; however, there were no material anomalies or significant findings to indicate the gear was deficient. In addition, there were no irregularities discovered with the maintenance history, tolerances, or timing that would preclude eventual failure of the gear, therefore, no definitive cause of the gear failure could be determined.

Probable cause

A total loss of engine power due to fatigue failure of the crankshaft drive gear teeth.

Verbatim NTSB analysis and probable cause from the NTSB dataset

Sources

NTSB record ERA18LA072
Event ID
20180129X74948
Case number
ERA18LA072
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. 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: 8574a8a0cf7a264972575871ad8c12bb1726b753ef2c90ba6c994ff220dbaec5; retrieved 2026-09-16T06:24:00.235Z.