NTSB CAROL · Event
Event LAX03TA229
Registry · N6979R
FAA Aircraft Registry record.
Make / Model
SIKORSKY S-64E
Year of manufacture
1968 · 35 years old at event
Engine
P & W JFTD12A SER (4500 hp)
Seats / Engines
3 seats · 2 engines
Last airworthiness date
20010731
ADS-B equipped
Yes — Mode-S A9485A
Registrant of record
U S LEASECO INC
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
the pilot's failure to maintain tail rotor clearance while hovering resulting in a tail rotor blade strike.
Factual narrative
On July 7, 2003, at 1834 mountain standard time, a Sikorsky S-64E, N6979R, impacted trees with the tail rotor while hovering near Tucson, Arizona. The U.S. Forest Service was operating the helicopter as a public-use flight under the provisions of 14 CFR Part 133 for firefighting operations. The airline transport pilot and copilot were not injured; the helicopter sustained substantial damage. The flight departed Tucson International Airport (TUS), Tucson, about 1715. Visual meteorological conditions existed during the flight and a company visual flight rules (VFR) flight plan was in effect. In a written statement, the operator reported that the helicopter was equipped with a 2,000 gallon fixed tank with snorkel hover fill capability. After a series of water drops, the crew refilled the tank from a dip tank. The dip tank was located in mountainous terrain and there were two mesquite trees near it. During the refilling operation, the tail rotor made contact with the mesquite trees, but the pilots were unaware of the strike. When the helicopter returned to Tucson, it was refueled. During the refueling operations, damage was discovered to the number one exhaust stack. The helicopter was shutdown and examined. The tail rotor blade damage was discovered and initially thought to be a result of debris from the exhaust stack coming into contact with the tail rotor blades. In a telephone interview with a representative of the operator, he stated that closer inspection of the helicopter revealed that a portion of the exhaust stack was collapsed, but no portions were missing. The pilot reported to him that, when dipping the tank, he flew perpendicular to the road, into the wind with the tail of the helicopter in the trees. A tail rotor blade tip cap and small section of a mesquite tree were found at the dip tank site. A Federal Aviation Admininstration designated repair station inspected three of the tail rotor blades and found spar damage on the leading edge of one blade approximately 14.5 inches from the tip end. The two other blades examined were noted to have minor damage. After a series of water drops were conducted on a forest fire, the helicopter's crew refilled the fixed tank with water from a dip tank via a snorkel. The dip tank was located in mountainous terrain and there were two mesquite trees near the tank. During the refilling operation, the tail rotor blades contacted the trees; however, the flight crew was unaware of the strike. The tail rotor blade damage was noticed when ground personnel detected damage to the number one exhaust stack, and the helicopter was inspected further. One of the four tail rotor blades incurred spar damage on the leading edge, approximately 14.5 inches from the tip end. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_2003_LAX03TA229.txt.
Findings + structured fields enriched from FAA avall.mdb.
Full investigation docket on
data.ntsb.gov ↗.
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