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ERA12FA143 · Cessna 150G

11 Jan 2012 · Fitchburg, MA, United States

TENLE Aviation Cessna 150G · Accident: loss of engine power (partial) during initial climb

From Fitchburg Municipal Airport (FIT) to Fitchburg Municipal Airport (FIT)

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Event

NTSB case
ERA12FA143
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 150G

Aircraft type
Cessna 150
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
N4041J
Onboard fatalities
Unknown
Route
From Fitchburg Municipal Airport (FIT), Fitchburg, MATo Fitchburg Municipal Airport (FIT), Fitchburg, MA
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
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 (partial)
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
  • Environmental issues › Conditions/weather/phenomena
  • Personnel issues › Task performance

Approximate · Coordinates as recorded by the NTSB; no uncertainty radius is established.

NTSB narrative

On the day of the accident, the student pilot conducted a touch-and-go landing and then entered the traffic pattern to perform another one. While on the downwind leg of the traffic pattern, the engine began to run roughly, so the student applied carburetor heat and kept it on until touchdown. During climb after the second touch-and-go landing, the engine began running roughly again. Subsequently, the flight instructor took control of the airplane, lowered the angle-of-attack, and reapplied carburetor heat. According to the flight instructor, the engine subsequently ran more roughly, so he immediately placed the carburetor heat to “off.” He stated that, although the engine then ran less roughly, it still ran roughly. The flight instructor decided that there was not sufficient remaining runway to “land.” He was not sure how much power the engine was producing or if he could maintain level flight. He stated that he thought about turning back but decided against it. He said that the airplane was low and slow, so he decided to continue straight ahead. He tried to keep the airplane flying and was successful for about 15 to 20 seconds, but then he observed a warehouse ahead and banked to the right to avoid it. The airplane then settled and struck trees, substantially damaging the airplane and seriously injuring the student pilot.

Examination of the airplane and engine revealed no evidence of any preimpact mechanical failure or malfunction that would have precluded normal operation. However, a postaccident review of weather data and a carburetor icing probability chart also revealed that, at the time of the accident, the ambient temperature and dew point favored serious icing. Industry and Federal Aviation Administration guidance advised pilots to be aware of the warning signs of carburetor ice, including loss of rpm (with a fixed-pitch propeller) and rough running (both of which occurred before the accident), and advised that the pilot should respond to these warning signs by immediately applying full carburetor heat, and that the engine may initially run roughly for a short time while the ice melts. Therefore, the flight instructor should not have turned off the carburetor heat when the engine was still running roughly after he turned it on.

Probable cause

A partial loss of engine power due to the formation of carburetor ice and the flight instructor's improper application of carburetor heat.

Verbatim NTSB analysis and probable cause from the NTSB dataset

Sources

NTSB record ERA12FA143
Event ID
20120111X05220
Case number
ERA12FA143
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: 7f529e3106ec9b0ccc303e4fe3a846cbf8df0383e628ebe63c3339719438c213; retrieved 2026-09-15T17:03:31.311Z.