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Atlas / NTSB / FTW84FA244

NTSB CAROL · Event

Event FTW84FA244

1984-05-27 SAN ANTONIO, Texas, United States Serious 1 aircraft Status: Completed

Registry · N102CD

FAA Aircraft Registry record.

Make / Model

CIRRUS DESIGN SR20

Year of manufacture

2000

Engine

CONT MOTOR IO-360 SER (300 hp)

Seats / Engines

4 seats · 1 engine

Last airworthiness date

20000125

ADS-B equipped

Yes — Mode-S A00C58

Registrant of record

SCH AVIATION INC TRUSTEE

Source: FAA Aircraft Registry (releasable master file).

Aircraft involved

Factual narrative

IN A LEFT ORBIT THE HELICOPTER YAWED RIGHT AND CONTINUED THE RIGHT ROTATION TO IMPACT. AT THE TIME OF THE LOSS OF CONTROL THE ACFT WAS OPERATING OUT OF GROUND EFFECT AT 250 FT AGL WITH A DENSITY ALT OF 3751 FT AND AN INDICATED AIRSPEED OF 20 TO 25 KTS. THE PLT'S ATTEMPTS TO REGAIN CONTROL WERE UNSUCCESSFUL. EXAM OF THE WRECKAGE REVEALED NO MECHANICAL MALFUNCTIONS. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12

Verbatim from NTSB's published report. Source file NTSB_1984_FTW84FA244.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 (loss of control). 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 ↗