AMERICAN AVIATION AA-1B
Brenham, TX, December 1, 2024
Event Information
| Date | December 1, 2024 |
| Event Type | ACC |
| Location | Brenham, TX |
| Country | USA |
| Coordinates | 30.23509, -96.37445 |
| Airport | Brenham Municipal Airport |
| Highest Injury | NONE |
| NTSB Number | CEN25LA054 |
| Event ID | 20241203195575 |
Aircraft
| Make | AMERICAN AVIATION |
| Model | AA-1B |
| Registration # | N6242L |
| Category | AIR |
| FAR Part | 091 |
| Aircraft Damage | SUBS |
Conditions
| Light Condition | DAYL |
| Weather | VMC |
Injuries
| Fatal | 0 |
| Serious | 0 |
| Minor | 0 |
| None | 2 |
| Total Injured | 0 |
Event Location
Probable Cause
A partial loss of engine power due to an obstructed induction system from a mud dauber nest.
Full 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 and his passenger were not injured. The airplane was operated as a Title 14 Code of Federal Regulations 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 flew over the departure end of the runway. The pilot reported that the engine appeared to be running at idle power and he was unable to maintain altitude, so he conducted a forced landing into 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 prevent 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 airplane had flown 4.7 hours since the last annual inspection that was completed on November 17, 2024. The air filter was replaced during the annual inspection. At the time of the accident, 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)
About This NTSB Record
This aviation event was investigated by the National Transportation Safety Board (NTSB). NTSB investigates all U.S. civil aviation accidents to determine probable cause and issue safety recommendations to prevent future accidents.