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CEN25LA054 · American Aviation AA-1B

1 Dec 2024 · Brenham, TX, United States

American Aviation AA-1B · Accident: loss of engine power (partial) during initial climb

From Brenham Municipal Airport (11R) to an unrecorded destination

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Event

NTSB case
CEN25LA054
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
Ongoing
Event fatalities
Unknown
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

American Aviation AA-1B

Aircraft type
American AA-1
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
N6242L
Operator
Unknown
Onboard fatalities
Unknown
Route
From Brenham Municipal Airport (11R), Brenham, TXTo not recorded
Aircraft age
About 52 years (built 1972)
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

No findings designated as a cause are recorded in the NTSB data yet.

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

NTSB narrative

On December 1, 2024, about 1438 central daylight time, an American Aviation AA-1B airplane, N6242L, sustained substantial damage when it was involved in an accident near Brenham, Texas. The pilot had his passenger were not injured. The airplane was operated as a Title 14 Code of Federal Regulations (CFR) Part 91 personal flight.

The pilot reported that there was a partial loss of engine power shortly after takeoff from runway 34 at Brenham Municipal Airport (11R), Brenham, Texas. The partial loss of engine power occurred about 500 ft above the ground as the airplane crossed over the departure end of the runway. The engine, which appeared to be running at idle power, was unable to sustain level flight and a forced landing was made in a grass field north of the airport. The airplane’s nose landing gear separated during the forced landing.

The airplane’s left wing leading edge was substantially damaged during the forced landing. The left wing exhibited a large semicircular impact likely due to a collision with the separated nose gear and/or with an anthill in the grass field. However, the leading edge damage did not exhibit evidence of tire rubber transfer or scratching, nor did it contain anything resembling dirt/sand.

Examination of the engine did not reveal any evidence of a mechanical failure that would prevented normal operation. A visual examination of the engine’s exterior revealed that all four engine cylinders had evidence of mud dauber nests within their respective cooling fins. Additionally, a roughly 1.5-inch diameter mud dauber nest was found in the airbox between the air filter and the throat of the carburetor, as shown in Figure 1. Additionally, dirt with the same color as the mud dauber nest was observed within the carburetor throat and on the clean side of the air filter. The recovered mud dauber nest exhibited impressions consistent with the spacing of the wire coil that supported the flexible ducting associated with the carburetor heat system. The flexible ducting also contained various-sized fragments of mud dauber nest debris.

The accident occurred about 4.7 hours since the last annual inspection completed on November 17, 2024, during which the air filter was replaced. Based on maintenance logbook documentation, the engine had accumulated 531.7 hours since the last major overhaul that was completed on May 1, 1999.

Figure 1. Mud dauber nest found in the airbox between the air filter and the throat of the carburetor. Red arrows point to the mud dauber nest. (Photos courtesy of Lycoming Engines and edited by NTSB)

Verbatim NTSB factual narrative from the NTSB dataset

Sources

NTSB record CEN25LA054
Event ID
20241203195575
Case number
CEN25LA054
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, 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: 4f7b5e36271bcb8d59220ae63ba8dc268ab83c2d1f4d8e26c81f609707364ce0; retrieved 2026-09-16T19:31:05.858Z.