Probable cause
A partial loss of engine power for reasons that could not be determined.
NTSB analysis
The pilot and five passengers departed from a remote lake in the float-equipped airplane. The pilot reported that, shortly after takeoff, he felt the manifold pressure decrease, and he advanced the propeller and throttle controls. The engine initially responded with an increase in rpm and manifold pressure but subsequently lost total power. The pilot performed a forced landing into a heavily wooded area, and the airplane sustained substantial damage to the fuselage and wings.
A postaccident examination of the engine revealed no evidence of preimpact mechanical malfunctions or failures that would have precluded normal engine operation. Passengers reported that the pilot made an aggressive steep turn at low altitude with no change in engine noise from takeoff to impact with terrain. Based on available evidence, it is likely that the engine sustained a partial loss of engine power for reasons that could not be determined.
Text from the NTSB. Open the NTSB docket for ANC24LA049 for the full record.
Event
- Date
- Jun 11, 2024
- Type
- Accident
- Place
- Port Alsworth, Alaska
- Highest injury
- Serious
- Serious injuries
- 1
- Weather
- Visual (VMC)
- Light
- Day
Dehavilland BEAVER L-20A (DHC-2)
- N-number
- N4957
- Category
- Airplane
- Year built
- 1953
- Damage
- Substantial
- Operating rule
- Part 91 (general aviation)
- Purpose of flight
- Other work use
From the NTSB aviation accident database: N-registered aircraft, events since 2008, data through Oct 28, 2026. The file is published monthly, so the latest weeks are incomplete and recent records can change. The official source is the NTSB aviation investigation search. CheckAero is independent and not affiliated with the NTSB.