CEN15LA215 · Cessna 172 - H
Cessna 172 - H · Accident: loss of engine power (total) during an emergency descent
From Austin Bergstrom International Airport (AUS) to Austin Bergstrom International Airport (AUS)
Event
- NTSB case
- CEN15LA215
- 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 172 - H
- 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
- N8282L
- Operator
- Student Pilot
- Onboard fatalities
- Unknown
- Route
- From Austin Bergstrom International Airport (AUS), Austin, TXTo Austin Bergstrom International Airport (AUS), Austin, TX
- Aircraft age
- About 48 years (built 1967)
- 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
- Emergency 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
- Environmental issues › Conditions/weather/phenomena
Approximate · Coordinates as recorded by the NTSB; no uncertainty radius is established.
NTSB narrative
The flight instructor was conducting an instructional flight with a student pilot. The student reported that the preflight engine run-up was normal and that, before takeoff for the flight, there was a small wait because they were the fourth airplane in line for takeoff. At takeoff, the engine power was not normal, but leaning the mixture returned the engine performance to normal. After performing several flight maneuvers at 4,500 ft mean sea level (msl), the flight instructor simulated an engine failure by applying carburetor heat and retarding the throttle to idle. After descending the airplane to 2,500 ft msl, the flight instructor attempted to clear the engine and pushed the throttle control to full power, but the engine power was not restored. Subsequent attempts to restart the engine were unsuccessful, and the student then transferred the flight controls to the flight instructor, who then conducted a forced landing to muddy terrain, which resulted in the airplane nosing over.
The weather conditions at the time of the accident were conductive to moderate carburetor icing at cruise power and serious carburetor icing at descent power. Given the delayed takeoff, during which the engine would have been at an idle power setting, and that the mixture needed to be leaned at higher engine power to return to normal, it is likely that carburetor icing had accumulated. Although the flight instructor applied carburetor heat for the simulated engine failure to prevent carburetor icing, there would have been reduced heat output by the engine at the idle power setting, which would not have been effective in preventing carburetor icing.
Probable cause
The failure of the engine to regain normal power after a simulated engine failure due to carburetor icing, which resulted in a forced landing on muddy terrain and a subsequent nose-over.
Verbatim NTSB analysis and probable cause from the NTSB dataset
Sources
NTSB record CEN15LA215
- Event ID
- 20150504X31324
- Case number
- CEN15LA215
- 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: a11e8d0e21246fb1e946f3d74f78cb1534b063f00d363355754cb735e10d66f3; retrieved 2026-09-16T02:16:54.244Z.