LAX88LA212

NTSB accident investigation · Fairchild Hiller FH-1100 · Lihue, HI · June 4, 1988

Accident · No injuriesLimited investigationFinal report
Date
June 4, 1988, 12:00 local (22:00 UTC)
Place
Lihue, HI
Injuries
5 uninjured
Damage
Substantial damage
Phase of flight
Enroute
Aircraft
N53EPFairchild Hiller FH-1100
Weather
Visual (VMC) · Day
Status
Completed · report October 16, 1990
Report
Approved by Office Director
FAA report
19880604071489A
Case key
26024

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

Fatigue failure of the engine to transmission drive shaft engine coupling due to an angular misalignment of the drive shaft.

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
Rotor drive system,engine to transmission drive - fatigueCause
Maintenance,alignment - improperCause
Rotor drive system,engine to transmission drive - failure,totalCause
Rotor drive system,engine to transmission drive - disengagedCause
Forced landingDescent - emergency
Terrain condition - waterFactor
Autorotation - attemptedPilot in command
Terrain condition - none suitableFactor
Hard landingLanding - flare/touchdown

Analysis

The pilot said that the aircraft was in normal cruise flight when he noticed that the engine was no longer driving the rotor system. The pilot entered an autorotation and had to stretch the glide slightly to a suitable landing area on an off shore reef. The helicopter made a hard landing on the reef in about one foot of water. On site examination of the helicopter by FAA airworthiness inspectors revealed that the bendix coupling on the engine to transmission shaft had ruptured on the engine end of the shaft. Metallurgical examination of the failed coupling revealed a fatigue fracture in a circumferential orientation on the coupling disk. The drive shaft couplings are the subject of a recurring AD which mandates alignment measurements of the drive shaft every 100 hours. The last alignment check was done about 60 hours prior to the accident.

Aircraft

Registration
N53EP
Reported as
Fairchild Hiller FH-1100
Category
Helicopter
Serial number
182
Airframe hours
2,023
Engine
Allison 250-C18C, 274 horsepower, turbo shaft
Damage
Substantial damage
Flight
Part 91
Registered owner
Preston S. Myers
Airworthiness certificate
Standard, Normal
Last inspection
100 hour · May 13, 1988 · 62 hours before
Departed
LIH · Lihue, HI
Destination
LIH

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
40
Certificates
Commercial, Private
Airplane ratings
Single-engine land
Medical
Class 2, Valid Medical--no waivers/lim.
Seat
Right
Flight hours
6,032 total · 134 in this make and model · 5,846 as pilot in command · 123 in the last 90 days · 47 in the last 30 days · 5 in the last 24 hours

Weather

Conditions
Visual (VMC) · Day
Wind
90° at 14 knots
Visibility
15 statute miles
Lowest ceiling
None
Temperature
79 °F

FAA reports on this event · 1

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