NTSB CAROL · Event
Event FTW01LA202
Registry · N2770
FAA Aircraft Registry record.
Make / Model
HILLER UH-12D
TCDS
4H10 · SIAM HILLER HOLDINGS INC
Engine
LYCOMING VO-435 SERIES (260 hp)
Seats / Engines
4 seats · 1 engine
Last airworthiness date
20010831
ADS-B equipped
Yes — Mode-S A2C2D5
Registrant of record
LIL DAWG AVIATION
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
the failure of the tail rotor drive shaft hanger bearing, which resulted in the separation of the tail rotor drive shaft. A contributing factor was the lack of suitable terrain for the forced landing.
Factual narrative
On September 3, 2001, at 1610 central daylight time, a Hiller UH-12D agricultural helicopter, N2770, was substantially damaged during a forced landing following a loss of directional control near Lubbock, Texas. The helicopter was registered to the pilot and operated by Aero Management, Inc., of Olton, Texas. The commercial pilot, sole occupant, was not injured. Visual meteorological conditions prevailed, and a flight plan was not filed for the 14 Code of Federal Regulations Part 137 aerial application flight. The local flight originated from the Town and Country Airpark Airport, Lubbock, Texas, at 1515. The pilot reported to the FAA inspector that while spraying a cotton field, at 4 feet agl, he felt a vibration followed by a "pop" with a loss of tail rotor control. Subsequently, during the forced landing to the cotton field, the main rotor blades struck the tailboom separating it from the fuselage. Examination of the helicopter by the FAA inspector, who responded to the accident site, revealed that a tail rotor drive shaft hanger bearing had failed, and the tail rotor drive shaft had separated. The helicopter pilot was spraying a cotton field at 4 feet agl, when he felt a vibration followed by a "pop" with a loss of tail rotor control. Subsequently, during the forced landing to the cotton field, the main rotor blades struck the tailboom separating it from the fuselage. Examination of the helicopter, by an FAA inspector revealed that a tail rotor drive shaft hanger bearing had failed, and the tail rotor drive shaft had separated. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_2001_FTW01LA202.txt.
Findings + structured fields enriched from FAA avall.mdb.
Full investigation docket on
data.ntsb.gov ↗.
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