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IAD05LA090 · Aeronca 11CC

3 Jul 2005 · Charlotte, VT, United States

Aeronca 11CC · Accident: partial loss of engine power (mechanical failure) during initial climb

From Charlotte, VT (no airport) to No airport

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Event

NTSB case
IAD05LA090
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

Aeronca 11CC

Aircraft type
Aeronca 11
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
N4337E
Operator
Unknown
Onboard fatalities
Unknown
Route
From Charlotte, VT (no airport)To No airport
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
Partial loss of engine power (mechanical failure)
Also codedOther events the NTSB coded in the sequence, such as a wire strike after a loss of power. Flight Findings uses them for its kinds of event. Glossary
Stall
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

  • Pilot in command › Airspeed, inadequate

Approximate · Coordinates from the NTSB case API, which marks them as estimated or does not say; no uncertainty radius is established.

NTSB narrative

A witness observed the airplane as it appeared from between trees traveling northbound, below the treetops, and out over a field about 50 feet above the ground. The engine sound was "slow," the airspeed was "real slow," and the wings rocked from side to side. The pitch attitude continued to increase to about 45 degrees, but the airplane did not climb. The nose of the airplane then lowered, the engine noise stopped, and the airplane disappeared from view behind a line of trees. The airplane crashed in a "big" field that was suitable for a forced landing. The engine was started and ran to partial power in a test cell after the accident. Oil-soaked spark plugs were cleaned and reinstalled, and impact-damaged ignition leads were replaced and the engine was restarted. The engine started immediately, accelerated smoothly, and ran to full operating rpm without interruption. Prior to the engine run, the carburetor bowl drain plug was removed, and approximately one-half ounce of fluid was drained. The fluid was absent of water and debris. The fluid was dark yellow in color, with an odor of automotive gasoline and lacquer thinner. The engine was modified in accordance with an FAA supplemental type certificate to run on unleaded automotive gasoline. Interpolation of a carburetor icing probability chart revealed that atmospheric conditions at the time of the accident were conducive to "serious icing at glide power."

Probable cause

The pilot's failure to maintain adequate airspeed, which resulted in an inadvertent stall, and impact with terrain. A factor in the accident was the partial loss of engine power for undetermined reasons.

Verbatim NTSB analysis and probable cause from the NTSB dataset

Sources

NTSB record IAD05LA090
Event ID
20050714X01025
Case number
IAD05LA090
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: 75ad74ccfbf0588a9ca9529cfbbd56a7adb5f567240247ac51ee6e0b31d9ec84; retrieved 2026-09-21T09:05:46.243Z.