SEA86FA039

NTSB accident investigation · Hiller-Soloy UH-12E · Horton, OR · January 16, 1986

Accident · FatalField investigationFinal report
Date
January 16, 1986, 12:38 local (20:38 UTC)
Place
Horton, OR
Injuries
1 fatal
Damage
Destroyed
Phase of flight
Maneuvering
Aircraft
N40290Hiller-Soloy UH-12E
Weather
Instrument (IMC) · Day
Status
Completed
Report
Approved by Office Director
FAA report
19860116000729A
Case key
40264

From the NTSB’s public API. By law, NTSB reports can’t be used as evidence in lawsuits over the accident.

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Sequence of events

NTSB’s coding before 2008: each occurrence and phase of flight, and the causes and factors under it. The codes are defined in NTSB’s coding manual.

Airframe/component/system failure/malfunctionManeuvering
Rotor system,main rotor hub grip(sleeve) - fatigueCause
Maintenance,inspection - inadequateCompany maintenance personnelFactor
Information insufficientCompany maintenance personnelFactor
Insufficient standards/requirementsFaa(organization)Factor
Maintenance,recordkeeping - poorManufacturerFactor
Weather condition - gustsFactor
Loss of control - in flightDescent - uncontrolled
In flight collision with terrain/waterDescent - uncontrolled

Analysis

The fork connecting the rotorcraft's blue blade to the main rotor hub separated after a long term fatigue crack had spread through more than 60% of the fork circumference. The operator failed to carry out the appropriate inspection of the fork unit as delineated in the FAA airworthiness directive due in part to confusion over the wording of the AD coupled with the misperception that the fork required only a visual inspection rather than a dye penetrant check. The misperception of the type of inspection was born out of a belief that the original blade fork with its ten thousand series serial number required only a visual check. The installed blade fork serial number was no longer evident on the part and manufacturer records had been lost thus preventing the operator from verifying the serial number and instituting the necessary inspection. Strong gusty winds existed at the accident site associated with frontal passage at the time of the accident.

Aircraft

Registration
N40290
Reported as
Hiller-Soloy UH-12E
Category
Helicopter
Serial number
HA3081
Airframe hours
2,288
Engine
Allison 250-020, 305 horsepower, turbo shaft
Damage
Destroyed
Flight
Aerial application · Part 137
Registered owner
Western Helicopter Services
Airworthiness certificate
Special, Restricted (Special)
Last inspection
AAIP · December 19, 1985 · 28 hours before
Departed
Horton, OR

Matched to the registry by N-number and the event date; the registry’s history has gaps, so older matches can be wrong. Compare the reported make and model.

Flight crew

As NTSB recorded them. NTSB leaves out names.

Role
Pilot
Age
37
Certificate
Commercial
Airplane ratings
Single-engine land
Medical
Class 2, Valid Medical--no waivers/lim.
Seat
Left
Toxicology
Performed
Flight hours
4,733 total · 3,100 in this make and model · 4,733 as pilot in command · 120 in the last 90 days · 4 in the last 24 hours

Weather

Conditions
Instrument (IMC) · Day
Wind
160° at 19 knots, gusting 23
Visibility
2 statute miles
Lowest ceiling
1,200 ft broken
Temperature
54 °F, dew point 52 °F
Altimeter
29.00 inHg
Observed at
EUG, 10 nm away

FAA reports on this event · 1

The FAA’s own accident and incident reports, matched to the aircraft by N-number and date.