LAX91LA249

NTSB accident investigation · Hiller UH-12E · Huron, CA · June 7, 1991

Accident · No injuriesLimited investigationFinal report
Date
June 6, 1991, 20:45 local (Jun 7, 1991, 03:45 UTC)
Place
Huron, CA
Injuries
1 uninjured
Damage
Substantial damage
Phase of flight
Enroute
Aircraft
N507HAHiller UH-12E
Weather
Visual (VMC) · Night/bright
Status
Completed · report May 27, 1993
Report
Approved by Office Director
FAA report
19910606020509A
Case key
27237

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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Probable cause

That unknown pilot(s) impoperly used the throttle control which caused an overspeed condition. Contributing to this accident was the connecting rod bolt fatigue failure.

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 powerCruise
Single engine aircraft
Engine assembly,connecting rod bolt - failure,totalFactor
Engine assembly,connecting rod bolt - fatigueFactor
Powerplant - overspeedCause
Throttle/power control - improper use ofUnknownCause
Forced landingDescent - emergency
Autorotation - performedPilot in command
In flight collision with objectDescent - emergency
Object - tree(s)

Analysis

The pilot completed an aerial application flight and was returning to the loading area when the helicopter sustained a total loss of power. During the subsequent autorotation the pilot attempted to sideslip the helicopter between the almond trees but was unable to do so. The engine and subsequent metallurgical examination disclosed the no. 3 cylinder connecting rod bolt failed due to fatigue. Company maintenance personnel reported that the fatigue was caused by consistent engine overspeed power settings by the pilots flying the helicopter.

Aircraft

Registration
N507HA
Reported as
Hiller UH-12E
Category
Helicopter
Serial number
5007
Airframe hours
3,112
Engine
Lycoming VO-540-C2A, 305 horsepower, reciprocating
Damage
Substantial damage
Flight
Aerial application · Part 137
Operator
San Joaquin Helicopters
Registered owner
San Joaquin Helicopters
Airworthiness certificate
Standard, Normal
Last inspection
Annual · February 25, 1991 · 114 hours before

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
43
Certificate
Commercial
Airplane ratings
Multi-engine land, Single-engine land
Medical
Class 2, Valid Medical--no waivers/lim.
Seat
Center
Flight hours
15,000 total · 15,000 as pilot in command

Weather

Conditions
Visual (VMC) · Night/bright
Visibility
20 statute miles
Lowest ceiling
None
Temperature
70 °F

FAA reports on this event · 1

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