Accident Aviat A-1 N623KD, Saturday 29 May 2004
ASN logo
This information is added by users of ASN. Neither ASN nor the Flight Safety Foundation are responsible for the completeness or correctness of this information. If you feel this information is incomplete or incorrect, you can submit corrected information.

Date:Saturday 29 May 2004
Type:Silhouette image of generic HUSK model; specific model in this crash may look slightly different    
Aviat A-1
Registration: N623KD
MSN: 1274
Total airframe hrs:451 hours
Engine model:Lycoming O-360-A1P
Fatalities:Fatalities: 2 / Occupants: 2
Other fatalities:0
Aircraft damage: Substantial
Location:Harwood, TX -   United States of America
Phase: Take off
Departure airport:Harwood, TX (PVT)
Destination airport:
Investigating agency: NTSB
Confidence Rating: Accident investigation report completed and information captured
During takeoff, a witness observed the airplane depart to the south and climbed vertically at an approximate 85 degree angle, with the rudder deflected to the right. When it reached the apex of the climb, approximately 200-250 feet above ground level, it began to "fly backwards like a kite," and the engine was "throttled back." The airplane then made a descending left hand turn in an approximate 45-50 degree nose down attitude. While in the descent, the elevator was deflected to the full up position. The witness then observed the left wing "drop" and the upward deflection on the elevator decreased. At this point, and while still in the descent, the right aileron was deflected to the full up position, and the airplane's wings leveled out, while the engine "throttled back up to full power." The right aileron stayed deflected, and the airplane turned to the right and contacted the ground with the right wing tip first followed by the engine. Another witness reported that the 410-hour pilot "almost always" performed this type of take-off, and he has observed the pilot perform this maneuver "recently and frequently." Flight control continuity was established throughout the airplane at the accident site. No mechanical anomalies were noted with the engine or airframe. The airplane was found to be within weight and balance limits.
Probable Cause: The pilot's failure to maintain airspeed sufficient for flight resulting in an inadvertent stall/spin during takeoff.

Accident investigation:
Investigating agency: NTSB
Report number: FTW04FA144
Status: Investigation completed
Download report: Final report




Revision history:

28-Oct-2008 00:45 ASN archive Added
21-Dec-2016 19:24 ASN Update Bot Updated [Time, Damage, Category, Investigating agency]
07-Dec-2017 18:00 ASN Update Bot Updated [Operator, Source, Narrative]

Corrections or additions? ... Edit this accident description

The Aviation Safety Network is an exclusive service provided by:
Quick Links:

CONNECT WITH US: FSF on social media FSF Facebook FSF Twitter FSF Youtube FSF LinkedIn FSF Instagram

©2024 Flight Safety Foundation

1920 Ballenger Av, 4th Fl.
Alexandria, Virginia 22314