LAX86MA238

NTSB accident investigation · Aerospatiale AS-355F-1 · Kameula, HI · May 31, 1986

Accident · Minor injuriesMajor investigationFinal report
Date
May 31, 1986, 12:30 local (22:30 UTC)
Place
Kameula, HI
Injuries
1 minor, 4 uninjured
Damage
Substantial damage
Phase of flight
Maneuvering
Aircraft
N909CHAerospatiale AS-355F-1
Weather
Visual (VMC) · Day
Status
Completed · report May 27, 1988
Report
Approved by Office Director
FAA report
19860531087019A
Case key
25282

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.

Miscellaneous/otherHover
Fuselage - vibration
Precautionary landing - performed
Airframe/component/system failure/malfunctionLanding
Reason for occurrence undeterminedCause
Fuselage,attachment - fatigue
Rotor system,main rotor hub flapping hinge/stop(s) - failure,total
Landing gear,skid assembly - overload

Analysis

The plt rprtd that as he 'hovered' the helicopter btn 5 & 10 ft after lift-off, he noted a 'slight lateral vibration.' He lndd immediately, but the vibration/ground resonance (vib) increased in severity, so he 'shut-off' both throttles. The vib contd to the extent that he couldn't hold onto the cyclic ctl stick. The transmission sepd fm its attach point &the main rotor blades contacted the gnd bfr the eng stopped. An exam revealed the transmission support bars (tsb's) had failed drg the acdnt. There was evidence of overload failure of the tsb's, except the left fwd tsb had evidence of fa- tigue on either side of the buckled area. A striation count indcd the crack had progressed ovr an estd time of at least 1 hr & 15 min. Also, an arm of the starflex assy (s/a) had failed. The s/a had 323 hrs since rplcmnt. Craze cracks were fnd on the s/a, but an exam failed to verify whether they had formed bfr or drg the acdnt. The s/a was aprx 3% porous & holes in the enamel barrier allowed environmental blackening of its edges. Lndg skid shock absorbers were badly dmg.

Aircraft

Registration
N909CH
Reported as
Aerospatiale AS-355F-1
Category
Helicopter
Serial number
5123
Airframe hours
731
Engine
Allison 250-C20F, 450 horsepower, turbo shaft
Damage
Substantial damage
Flight
Personal · Part 91
Operator
Hemmeter Aviation, Inc.
Registered owner
Hemmeter Investment Company
Airworthiness certificate
Standard, Normal
Last inspection
Annual · December 5, 1985 · 78 hours before
Destination
Maui, HI

Flight crew

As NTSB recorded them. NTSB leaves out names.

Role
Pilot
Age
37
Certificates
Commercial, Airline transport
Airplane ratings
Multi-engine land, Single-engine land
Instrument ratings
Airplane
Medical
Class 1, Valid Medical--no waivers/lim.
Seat
Right
Flight hours
2,657 total · 200 in this make and model · 2,040 as pilot in command · 50 in the last 90 days · 22 in the last 30 days · 2 in the last 24 hours

Weather

Conditions
Visual (VMC) · Day
Wind
60° at 5 knots
Visibility
25 statute miles
Lowest ceiling
None
Temperature
93 °F

FAA reports on this event · 1

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