DEN88LA046

NTSB accident investigation · Hiller UH-12E · Vernal, UT · January 2, 1988

Accident · No injuriesLimited investigationFinal report
Date
January 2, 1988, 15:30 local (22:30 UTC)
Place
Vernal, UT
Injuries
3 uninjured
Damage
Substantial damage
Phase of flight
Enroute
Aircraft
N400AHHiller UH-12E
Weather
Visual (VMC) · Day
Status
Completed · report March 30, 1989
Report
Approved by Office Director
FAA report
19880102000119A
Case key
17432

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.

Loss of engine power(total) - mech failure/malfCruise - normal
Engine assembly,connecting rod - fatigueCause
Maintenance,rebuild/remanufacture - poorOther maintenance personnelCause
Engine assembly,connecting rod bolt - stripped threadCause
Engine assembly,connecting rod cap - failure,totalCause
Forced landingDescent - emergency
Autorotation - initiated
Hard landingLanding - flare/touchdown
Altitude - misjudgedPilot in commandCause
Flare - improperPilot in commandCause
Misc rotorcraft,tail boom - sheared

Analysis

The commercial plt and two passengers were surveying a road route in mountainous terrain. At cruise, the pilot noticed a drop in manifold pressure, followed by a loss of oil pressure. The plt reported that the engine quit. An autorotation to a snow covered road resulted in a hard landing. The main rotor blades severed the tail boom and the landing skids collapsed. A post accident engine tear down revealed evidence consistent with connecting rod failure. The number five rod bearing had disintegrated and the rod end cap had broken in service. The damaged rod end cap and connecting rod were examined for failure mode determination. The metallurgist's factual report states that the rod shows fracture details characteristics of high cycle fatigue.

Aircraft

Registration
N400AH
Reported as
Hiller UH-12E
Category
Helicopter
Serial number
1177
Airframe hours
6,732
Engine
Lycoming TIVO-540-A2A, 315 horsepower, reciprocating
Damage
Substantial damage
Flight
Business · Part 91
Registered owner
Ben J. Richards
Airworthiness certificate
Standard, Normal
Last inspection
Annual · August 29, 1987 · 9 hours before
Departed
VEL · Vernal, UT

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
35
Certificate
Commercial
Airplane ratings
Single-engine land
Medical
Class 2, Valid Medical--no waivers/lim.
Seat
Center
Flight hours
5,450 total · 5,100 in this make and model · 5,100 as pilot in command · 30 in the last 30 days · 1 in the last 24 hours

Weather

Conditions
Visual (VMC) · Day
Wind
Calm
Visibility
50 statute miles
Lowest ceiling
None
Temperature
5 °F
Observed at
RKS

FAA reports on this event · 1

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

Other investigations on N400AH · 4

Matched to the same aircraft by N-number and date.