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Atlas / NTSB / FTW93LA273

NTSB CAROL · Event

Event FTW93LA273

1993-09-30 HURST, Texas, United States Airport · 2F2 None 1 aircraft Status: Completed

Registry · N2064J

FAA Aircraft Registry record.

Make / Model

AIR TRACTOR INC AT-802

Engine

P&W CANADA PT6A-67AG (1350 hp)

Seats / Engines

2 seats · 1 engine

Last airworthiness date

20120409

ADS-B equipped

Yes — Mode-S A1AB3A

Registrant of record

PADGETT AG ROTORS LLC

Source: FAA Aircraft Registry (releasable master file).

Aircraft involved

Probable cause & findings

THE EXCESSIVE FLARE AND THE CONTROL INTERFERENCE BY THE PILOT UNDERGOING INSTRUCTION AND INADEQUATE SUPERVISION BY THE CFI. FACTORS WERE THE PILOT'S FAILURE TO UNDERSTAND THE INSTRUCTOR'S DIRECTIONS DUE TO HIS LIMITED KNOWLEDGE OF THE ENGLISH LANGUAGE.

Factual narrative

On September 30, 1993, at 1450 central daylight time, a Bell 206-L4, N2064J, was substantially damaged during a simulated autorotative landing near Hurst, Texas. Neither the airline transport rated pilot, nor the foreign airline transport rated pilot undergoing instruction were injured. Visual meteorological conditions prevailed for the instructional flight. According to the instructor, the pilot flared in an excessively nose high attitude following a simulated engine failure during takeoff. The instructor pilot announced to the pilot receiving instruction that he was taking the controls of the aircraft, but the pilot did not understand his command and stayed on the controls. The instructor stated that he had to forcibly overcome the other pilot's control inputs while he attempted to level the attitude of the helicopter to a landing attitude. The pilot said that he was attempting to keep the helicopter airborne. In the enclosed instructor pilot's statement he reported that "due to language problem with the Japanese student the student did not recognize or acknowledge my stating, "I have it." The instructor further stated that the helicopter did not touch down hard, but the rotor RPM decayed to the point that pylon rock was encountered during touchdown, resulting in substantial damage to the tailboom. A PILOT RECEIVING INSTRUCTION FLARED EXCESSIVELY DURING AN AUTOROTATIVE LANDING FOLLOWING A SIMULATED ENGINE FAILURE DURING TAKEOFF. THE INSTRUCTOR PILOT ANNOUNCED THAT HE WAS TAKING THE CONTROLS TO LEVEL THE AIRCRAFT PRIOR TO TOUCHDOWN. THERE WERE LANGUAGE DIFFICULTIES BETWEEN THE JAPANESE PILOT RECEIVING INSTRUCTION AND THE INSTRUCTOR. THE PILOT RECEIVING INSTRUCTION FAILED TO RELINQUISH THE CONTROLS AND TRIED TO KEEP THE AIRCRAFT AIRBORNE WHILE THE INSTRUCTOR WAS TRYING TO LAND. THE LOW ROTOR RPM DURING TOUCHDOWN RESULTED IN DAMAGE TO THE TAILBOOM. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12

Verbatim from NTSB's published report. Source file NTSB_1993_FTW93LA273.txt. Findings + structured fields enriched from FAA avall.mdb. Full investigation docket on data.ntsb.gov ↗.

Related research

What the literature says.

Academic papers and agency reports matching this event's aircraft type or causal vocabulary (engine failure). Sourced from NASA NTRS, NTSB Safety Studies, FAA CAMI, AOPA Air Safety Institute, Embry-Riddle Scholarly Commons, arXiv, and the Semantic Scholar academic graph.

Browse the full corpus — academia portal ↗