ASN logo
ASN Wikibase Occurrence # 41134
Last updated: 1 August 2020
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.

Type:Silhouette image of generic SPIT model; specific model in this crash may look slightly different
Time Warp Spitfire 9
Registration: N355DE
C/n / msn: 201
Fatalities:Fatalities: 1 / Occupants: 1
Other fatalities:0
Aircraft damage: Written off (damaged beyond repair)
Location:Lakeland, FL -   United States of America
Phase: Take off
Departure airport:LAL
Destination airport:
Investigating agency: NTSB
This was the first flight of this airplane after being built. The airplane was seen departing from runway 9, climb at a steep nose high attitude to an altitude of about 150 to 200 feet above the ground; fall flat to the ground, impacting right side up, and flat. Videotape, made by a relative of the pilot, revealed that the pilot was heard saying he was having difficulty in getting the tail up. He told the people present, ''s a bugger back there,' referring to the tail coming up. In addition, he said, '...I should have more elevator authority.' He said that he had the speed up to 70 knots, the stick full forward, the tail would not come up, and '...that the aircraft may need a larger horizontal stabilizer and elevator to attain sufficient elevator authority.' No work to correct this problem was accomplished prior to the attempted flight. The videotape indicated that the airplane might have been overweight or tail heavy, or perhaps both. Inspection of the wreckage revealed no apparent airframe failure. The control surfaces were heavily coated with bondo to smooth them out. A piece of bondo was chipped from the aileron that measured 3/16 of an inch thick. The listed empty weight was 1,300 pounds, and the gross weight was 2,000 pounds. The actual weight shown for certification was empty weight 1,779 pounds, and gross weight 2,400 pounds. Continuity was established through the elevator cables, but the tail section and cables were cut to extract the pilot from the wreckage. Control continuity was established to all the flight controls.
Probable Cause: a loss of control which resulted in an inadvertent stall at too low an altitude to allow recovery. Factors in this accident were, the pilot/owner did not verify that the airplane was balanced before the flight, and he did not perform any weight or balance checks.



Related books:

Revision history:

24-Oct-2008 10:30 ASN archive Added
21-Dec-2016 19:23 ASN Update Bot Updated [Time, Damage, Category, Investigating agency]
12-Dec-2017 19:02 ASN Update Bot Updated [Operator, Departure airport, Source, Narrative]

Corrections or additions? ... Edit this accident description