Accident Overview
The pilot of a float-equipped airplane reported that immediately after takeoff, he experienced difficulty lowering the aircraft's nose. The airplane subsequently stalled and impacted the water. The pilot stated that he thought the elevator trim did not function. He also noted that a large moose rack was tied to the left float.
Postaccident Inspection
Two FAA inspectors conducted a postaccident inspection of the aircraft. The inspection revealed that the stabilizer rear trim mechanism was in the neutral position and rotated freely. The rear stabilizer hinge was also free to rotate. The stabilizer trim actuator handle in the cockpit was missing, and the actuator would only partially engage. The inspectors could not determine whether the observed damage was preaccident or postaccident.
Aircraft Details
The source does not specify the aircraft type, registration, engine count, date, operator, location, or number of occupants. No information is provided regarding injuries or damage items. The time of day, weather conditions, and ATC involvement are not mentioned.
Probable Cause
No probable cause is stated in the source.