NTSB CAROL · Event
Event BFO94LA159
Registry · N204JB
FAA Aircraft Registry record.
Make / Model
BELL UH-1B
Year of manufacture
1963 · 31 years old at event
Engine
LYCOMING T-53 SERIES (1150 hp)
Seats / Engines
6 seats · 1 engine
Last airworthiness date
19920302
ADS-B equipped
Yes — Mode-S A1A1A9
Registrant of record
PREMIER AIRCRAFT SERVICES LLC
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
Fracture failure of the tail rotor drive intermediate gearbox.
Factual narrative
On August 31, 1994, at 1430 eastern daylight time, N204JB, a Bell UH-18, owned and operated by Joseph Brigham of Pembroke, New Hampshire, crashed during takeoff at Carrabasset, Maine. The certificated airline transport pilot, the sole occupant, was not injured. The helicopter was substantially damaged. Visual meteorological conditions prevailed and a flight plan was not filed. The helicopter was being operated under 14 CFR 133. According to an FAA Aviation Safety Inspector, this was an external load operation. The pilot reported that a foundation for the ski lift in Sugarloaf Mountain was being constructed, and the helicopter was being used to lift buckets of cement to pour into the foundation. The pilot stated that as the helicopter was lifting the bucket of cement, "...he heard a loud "bang" noise, followed by a growling noise and the aircraft nose attempting to turn right." He stated that he entered autorotation, flared hitting the tail stinger on the upslope, and landed hard with the aircraft still spinning, and broke off the skid landing gear. The helicopter was examined by an FAA Safety Inspector. The examination revealed the tail rotor gear box (42 deg) had separated from the tail boom due to overload. THE PILOT REPORTED THAT HE WAS ENGAGED IN AN EXTERNAL LOAD OPERATION POURING CONCRETE FROM BUCKETS FOR A NEW SKI LIFT WHEN HE HEARD A LOUD 'BANG' NOISE FOLLOWED BY A GROWLING NOISE AND THE AIRCRAFT NOSE ATTEMPTING TO TURN RIGHT. HE STATED THAT HE ENTERED AUTOROTATION AND LANDED HARD ON UPSLOPING TERRAIN, COLLAPSING THE LANDING SKID. EXAMINATION OF THE AIRCRAFT REVEALED FRACTURE FAILURE OF THE TAIL ROTOR DRIVE SYSTEM INTERMEDIDATE GEAR BOX (42 DEGS). Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_1994_BFO94LA159.txt.
Findings + structured fields enriched from FAA avall.mdb.
Full investigation docket on
data.ntsb.gov ↗.
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