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Printed page 1. PDF page 1.
ft above ground level (agl), the autopilot was disconnected. Shortly thereafter, the pitch trim was moved in the aircraft nose down (AND) direction, while the captain pulled aft on the control column to maintain an aircraft nose up (ANU) attitude.Open official document at PDF page 1JSX Flight 284: hard landing at Houston - NTSB DCA24FA179
Printed page 2. PDF page 2.
vertical speed. About 17 seconds before touchdown, AND inputs were made and at touchdown, pitch trim was at -2.86 and continued to about -4°, full AND. In the previous flight flown by the accident captain, the captain made similar ANDOpen official document at PDF page 2JSX Flight 284: hard landing at Houston - NTSB DCA24FA179
Printed page 3. PDF page 3.
the autopilot. Flight data showed that at the time the autopilot was disconnected the pitch trim was 3.72° ANU. About 25 seconds later, the pitch trim moved in the AND direction and aft pressure was applied to the control columnOpen official document at PDF page 3JSX Flight 284: hard landing at Houston - NTSB DCA24FA179
Printed page 4. PDF page 4.
data showed an increase in engine power and aft control column position, however, AND pitch trim inputs continued. The FDR indicated that the vertical load factor during the touchdown was 3.9 gravitational constants (g). As the aircraft continued down theOpen official document at PDF page 4JSX Flight 284: hard landing at Houston - NTSB DCA24FA179
Printed page 12. PDF page 12.
17:57:48, at about 1,300 ft and 145 kts. At the time the autopilot was disengaged, the pitch trim was at 3.72° ANU. Page 12 of 17 DCA24FA179Open official document at PDF page 12JSX Flight 284: hard landing at Houston - NTSB DCA24FA179
Printed page 13. PDF page 13.
About 17:58:13, the pitch trim began to move in the nose down direction. Control column and elevator position increased (ANU) as the trim position decreased (AND). At about 250 ft agl pitch trim was at aboOpen official document at PDF page 13JSX Flight 284: hard landing at Houston - NTSB DCA24FA179