WIMAUMA, FL, USA
UNREG
MAXAIR AVR-582
THE INSTRUCTOR PILOT STATED THEY DESCENDED FROM 600 FEET TO 200 FEET AND LEVELED OFF. SHORTLY AFTER THAT THE ENGINE SEIZED. WHILE MAKING A FORCED LANDING IN A FIELD THE AIRSPEED DECREASED RAPIDLY AND THE AIRCRAFT STALLED 20 FEET ABOVE THE FIELD. THE AIRCRAFT DESCENDED RAPIDLY AND CRASHED. POSTCRASH EXAMINATION OF THE ENGINE INDICATED THE NUMBER 1 PISTON HAD SEIZED IN THE CYLINDER DUE TO RAPID COOLING. THE AIRCRAFT WAS NOT REGISTERED WITH FAA. THE PILOT/OWNER HAD APPLIED FOR USUA EXEMPTION TO FAA REGISTRY REQUIREMENTS; HOWEVER, AT THE TIME OF THE ACCIDENT THE EXEMPTION HAD NOT BEEN ISSUED. NEITHER THE INSTRUCTOR PILOT OR DUAL STUDENT HELD FAA PILOT CERTIFICATES OR MEDICAL CERTIFICATES.
On July 25, 1993, at 1510 eastern daylight time, an unregistered Maxair two-seat ultralight aircraft, owned and operated by Rufus E. Hinton, crashed while making a forced landing, following loss of engine power near Wimauma, Florida, while on a 14 CFR Part 91, instructional flight. Visual meteorological conditions prevailed at the time and no flight plan was filed. The aircraft received substantial damage and the nonrated pilot/instructor and nonrated dual student received serious injuries. The flight originated at Wimauma, Florida, on July 25, 1993, at 1440. The nonrated flight instructor stated he was giving an orientation flight to the student. After about 30 minutes of flying they preceded back to the airport. They descended from 600 feet to 200 feet and leveled off. Suddenly, the engine seized. He initiated a forced landing to a field. At an altitude of 20 feet above the field the airspeed decreased rapidly and the aircraft stalled. The aircraft then descended uncontrolled and crashed. Postcrash examination of the engine revealed the no. 1 cylinder spark plug to be fouled by unknown matter. The no. 1 piston had score marks on each corner. According to the mechanic who inspected the engine, the score marks are typical of a seizure of the piston in the cylinder caused by rapid cooling of the engine due to a rapid descent at idle power. (See attached FAA inspector statement and mechanic statement.) The aircraft was not registered with the FAA at the time of the accident. The aircraft was qualified to receive a United States Ultralight Association exemption to FAA registry requirements. The pilot had applied for the exemption from USUA; however, at the time of the accident the exemption had not been issued.
THE PILOT-IN-COMMANDS FAILURE TO MAINTAIN AIRSPEED WHILE MAKING A FORCED LANDING FOLLOWING LOSS OF ENGINE POWER RESULTING IN THE AIRCRAFT STALLING AND DESCENDING UNCONTROLLED TO THE GROUND.
Source: NTSB Aviation Accident Database
Aviation Accidents App
In-Depth Access to Aviation Accident Reports
