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Aviation safety reports, made easier to study

NTSB Reports is an independent research and search tool for public aviation accident and incident records. It brings NTSB aviation reports, structured fields, docket files, extracted figures, photos, videos, and update history into one searchable interface.

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NTSB Report

March 7, 1995 · Hiller UH-12C · N222TE

Bonners Ferry, ID

Overview

Report Status
Final with probable cause
Event Type
Accident
Date
March 7, 1995
Injury Outcomes
No injuries (1 uninjured)
Location
Bonners Ferry, ID
Aircraft
Hiller UH-12C
Tail Number
N222TE
Injuries
None
Aircraft Damage
Substantial
NTSB Number
SEA95LA063

THE PILOT REPORTED THAT DURING A STUDENT SOLO INSTRUCTIONAL FLIGHT, HE PERFORMED AN APPROACH TO A PINNACLE AND HELD A HOVER APPROXIMATELY THREE FEET ABOVE THE GROUND. THE PILOT THEN TRANSITIONED TO FORWARD FLIGHT AND STATED THAT THE ROTOR RPM BEGAN TO DECREASE. SUITABLE TERRAIN WAS NOT AVAILABLE, THEREFORE THE PILOT INITIATED A RIGHT 180 DEGREE TURN. DURING THE TURN, THE ROTOR RPM CONTINUED TO DECAY UNTIL TAIL ROTOR AUTHORITY WAS LOST. THE PILOT THEN SIDE SLIPPED THE HELICOPTER TO THE RIVER BANK, WHERE THE HELICOPTER LANDED HARD AND ROLLED ONTO ITS RIGHT SIDE. THE PILOT REPORTED THAT THERE WERE NO MECHANICAL FAILURES OR MALFUNCTIONS WITH THE HELICOPTER AT THE TIME OF THE ACCIDENT.

NTSB Probable Cause

ROTOR RPM WAS NOT MAINTAINED. FACTORS TO THE ACCIDENT WERE: INADEQUATE IN FLIGHT PLANNING/DECISION AND SUITABLE TERRAIN WAS NOT AVAILABLE.

Full Narrative

On March 7, 1995, at 1430 Pacific standard time, N222TE, a Hiller UH-12C helicopter, operated by Wilderness Helicopter, Inc., Billings, Montana, impacted terrain while maneuvering near Bonners Ferry, Idaho, and was substantially damaged. The student pilot, the sole occupant, was not injured. Visual meteorological conditions prevailed and a flight plan was not filed. The local instructional flight was conducted under 14 CFR 91. In a written statement, the pilot reported that he performed an approach to a pinnacle which was approximately 25 feet higher than the surrounding terrain. The pilot maintained the hover approximately three feet above the ground for 15 to 20 seconds, then transitioned to forward flight. During the transition, the rotor rpm began to decay. The pilot stated that he did not feel that he would make his planned departure and began a right 180 degree turn and lowered the collective before flying over the edge of the river. Approximately 90 degrees into the turn, the rotor rpm decayed enough that tail rotor authority was lost. The pilot stated that he attempted to side slip the helicopter to a landing spot, however, the helicopter "stalled" just as it reached the edge of a gravel bar. The helicopter landed hard, breaking the right skid and rolling onto its right side. The pilot reported that there were no mechanical failures or malfunctions with the helicopter at the time of the accident.

Flight

Event TypeAccident
Event Time14:30 PST
Nearest Airport0nm
Runway0
Flight Plan FiledNone
Aircraft FireNo
Aircraft ExplosionNo

Aircraft

AircraftHiller UH-12C
Tail NumberN222TE
Aircraft CategoryHeli
DamageSubstantial
Operating RulePart 91
Engines1
Engine TypeReciprocating
Engine DetailsFranklin · 6V-335-D · Reciprocating · 210
Seats4

People & Injuries

Injury SummaryNo injuries (1 uninjured)
Fatal0
Serious0
Minor0
Uninjured1
Total1
Crew 1Age 26 · Second Class

Conditions

ConditionsVMC
LightDaylight
Wind45° @ 5 kt
Visibility10 sm
CeilingNone
Temperature / Dew Point36 C / 0 C
Altimeter0
Weather SourcePILO

Appendix: Source Data