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IAD97LA044

1997-01-18 · UNIVERSITY PARK, Pennsylvania, United States · None · 1 aircraft · Status: Completed

Airport UNV

Current FAA registration · N2803A

Make / Model
SOCATA TB-20 TRINIDAD
Engine
LYCOMING IO-540 SER (300 hp)
Seats / Engines
4 seats · 1 engine
Last airworthiness date
19900508
ADS-B equipped
Yes — Mode-S A2D0BD

Source: FAA Aircraft Registry (releasable master file).

Aircraft involved

Probable cause & findings

the pilot's inability to control the airplane due to a damaged/bent elevator control lever and resultant lack of elevator authority.

Factual narrative

On January 18, 1997, at about 1635 eastern standard time, a Aerospatiale Trinidad TB-20, N2803A, crashed shortly after takeoff when the pilot, after rotation, experienced elevator control problems. The pilot returned to runway 24 and crashed while attempting an emergency landing at the University Park Airport, State College, Pennsylvania. The pilot and passenger were not injured, however, the airplane sustained substantial damage. Visual Flight Rules prevailed, however an IFR flight plan was filed. The flight was conducted under 14 CFR Part 91. The pilot stated that during preflight the elevator controls "seemed normal with full travel forward and aft". After takeoff, the pilot noticed that he could not maintain normal takeoff pitch attitude and the airplane continued an excessive climb rate out of his control. The pilot state that to control the airplane, power adjustments were needed to keep the nose down. The pilot stalled the airplane on final approach just above the runway numbers. Examination of the wreckage revealed bending of the elevator control lever due to overload from an undetermined source. The pilot stated that during preflight, the elevator controls 'seemed normal with full travel forward and aft.' After takeoff, the pilot noticed that he could not maintain normal takeoff pitch attitude. The airplane continued an excessive climb rate out of his control, even with full forward yoke. The pilot stated that to control the airplane, power adjustments were needed to keep the nose down. He maneuvered to land on the airport; however, on final approach to land, the airplane stalled just above the runway numbers. Post-accident examination of the airplane revealed bending of the elevator control lever due to overload from an undetermined source. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12

Verbatim from NTSB's published report. Source file NTSB_1997_IAD97LA044.txt. Findings + structured fields enriched from FAA avall.mdb. Full investigation docket on data.ntsb.gov ↗.

Related research

Matched on aircraft type or causal vocabulary (stall). All research papers