ATL93LA023

Factual narrative

AFTER LIFT OFF FROM THE RUNWAY, AT ABOUT SIX TO EIGHT FEET, THE LANDING GEAR WAS RETRACTED & THE NOSE OF THE AIRPLANE PITCHED DOWN. THE AIRPLANE IS EQUIPPED WITH A SIDE STICK CONTROLLER & A MANUALLY ACTUATED LANDING GEAR. THE LANDING GEAR HANDLE IS LOCATED FORWARD OF THE PILOT IN THE CENTER OF THE FLOOR, BETWEEN THE PILOT'S LEGS, & IS PULLED AFT TO RETRACT THE GEAR. THE BOTTOM OF THE AIRPLANE CONTACTED THE RUNWAY WHICH SEPARATED THE OIL COOLER SCOOP. THE PILOT THEN ENTERED A RIGHT HAND TRAFFIC PATTERN. ACCORDING TO WITNESSES, AS THE AIRPLANE WAS TURNED FROM THE BASE TO FINAL LEG IT STALLED ABRUPTLY, ROLLED LEFT MORE THAN ONCE, AND BEGAN A VERTICAL DIVE TO IMPACT. POST CRASH EXAMINATION OF THE AIRPLANE REVEALED FIRE DAMAGE AND CONTINUITY OF THE FLIGHT CONTROLS. THE PILOT'S HANDBOOK INDICATES THAT AN ACCELERATED STALL WILL RESULT IN A LEFT ROLL. IT ALSO STATES THAT A STALL BUFFET WILL OCCUR ABOUT 72 MPH. THE LOG BOOK FOR N84EJ NOTED THAT THE AIRPLANE HAD A CLEAN STALL SPEED OF 80 MPH, & A STALL SPEED OF 85 MPH IN A 60 DEGREE ONE 'G' RIGHT TURN. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12