LAX86FVM05

NTSB accident investigation · Hiller UH12E · Castroville, CA · April 27, 1986

Accident · Minor injuriesFinal report
Date
April 27, 1986, 05:30 local (12:30 UTC)
Place
Castroville, CA
Injuries
1 minor
Damage
Destroyed
Phase of flight
Enroute
Aircraft
N5374VHiller UH12E
Weather
Visual (VMC) · Night/dark
Status
Completed
Report
Approved by Office Director
FAA report
19860427016079A
Case key
24985

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/malfunctionCruise - normal
Rotor system,tail rotor blade - overloadCause
Rotor system,tail rotor blade - failure,totalCause
Rotor system,tail rotor blade - separationCause
Forced landingDescent - emergency
Hard landingLanding - flare/touchdown
Roll overLanding - flare/touchdown
Landing gear,main gear strut - failure,totalCause

Analysis

The acft landed hard and rolled over after the lndg skid failed in a forced lndg. The plt said he was crusing at 500 ft AGL over an open field when he heard a loud bang. The helicopter began to vibrate severely and spiral to the right. The plt lost ground reference in the pre-dawn darkness when he turned on the lights. Not wanting to land too hard he elected to leave the eng running and not auto-rotate. Investigation indicated that one tail rotor blade had separated at the tension torsion strap attach bolt hole. This is the transition area where the blade root casting and sheet metal blade skin are joined. The fracture surface of the casting appeared to be overloaded with no apparent indication of fatigue. The outboard blade section showed no indication of foreign object contact. All components of the helicopter were located in the impact area except one tail rotor blade.

Aircraft

Registration
N5374V
Reported as
Hiller UH12E
Category
Helicopter
Serial number
2073
Airframe hours
7,563
Engine
Allison 250-C20, 385 horsepower, turbo shaft
Damage
Destroyed
Flight
Aerial application · Part 137
Operator
Douglas E. Walker, doing business as Pilot Civilian
Registered owner
Verticare Inc.
Airworthiness certificate
Special, Restricted (Special)
Last inspection
100 hour · July 1, 1985 · 42 hours before
Departed
Castroville, CA
Destination
Salinas, CA
Airport
SNS · Salinas

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
31
Certificate
Commercial
Airplane ratings
Multi-engine land
Instrument ratings
Airplane
Medical
Class 2, Valid Medical--no waivers/lim.
Seat
Center
Flight hours
2,000 in this make and model

Weather

Conditions
Visual (VMC) · Night/dark
Wind
Calm
Visibility
25 statute miles
Lowest ceiling
None
Temperature
45 °F, dew point 39 °F
Altimeter
30.00 inHg
Observed at
SNS

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 N5374V · 2

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