NTSB Identification: MIA83FU002.
The docket is stored on NTSB microfiche number 21454.
Accident occurred Wednesday, April 13, 1983 in PALM BAY, FL
Aircraft: ROTEC RALLY 2B ULTRALIGHT, registration: NONE
Injuries: 1 Fatal.

NTSB investigators either traveled in support of this investigation or conducted a significant amount of investigative work without any travel, and used data obtained from various sources to prepare this aircraft accident report.

THE ROTEC RALLY 2B WAS AN UNREGISTERED ULTRALIGHT VEHICLE THAT HAD BEEN ASSEMBLED FROM A KIT. THE PLTS OF TWO OTHER ULTRALIGHT VEHICLES STATED THAT THEY WERE IN A VERY LOOSE FORMATION WITH THE ONE THAT HAD CRASHED. ACCORDING TO THEM, THEY WERE FLYING AT ABOUT 600 FT AGL WHEN THEY SAW THE RALLY 2B ENTER A LEFT TURN, THEN GO INTO A STEEP DIVE & CRASH. THEY OBSERVED THE WINGS FOLD UPWARD AFTER THE VEHICLE HAD LOST 100 TO 200 FT OF ALTITUDE. AN INVESTIGATION REVEALED THAT THE VEHICLE WAS WITHIN ITS AUTHORIZED GROSS WT LIMITATION. THE FUEL CAPACITY WAS 3.5 GAL, BUT THE PLT HAD STRAPPED A 6 GAL AUXILIARY TANK ADJACENT TO HIS SEAT. IT WAS FOUND WITH APRX 4.5 GAL REMAINING. AN EXAM OF THE WRECKAGE REVEALED THAT THE NOSE WIRE UPPER KING POST TANG HAD FAILED FROM FATIGUE. THE FATIGUE CRACK HAD INITIATED NEXT TO A HOLE & HAD PROGRESSED ALMOST ENTIRELY THRU THE TANG. ALSO, THE UPPER RUDDER CLEVIS HAD FAILED WHERE A CRACK FROM HIGH STRESS FATIGUE HAD PROGRESSED THRU 20% OF THE PART.

The National Transportation Safety Board determines the probable cause(s) of this accident to be:

FUSELAGE,ATTACHMENT..FATIGUE

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