LAX92LA175

NTSB accident investigation · Hughes 369C · Pacific Ocean (Pacific Ocean) · April 10, 1992

Accident · Minor injuriesLimited investigationFinal report
Date
April 9, 1992, 17:00 local (Apr 10, 1992, 00:00 UTC)
Place
Pacific Ocean (Pacific Ocean)
Injuries
2 minor
Damage
Substantial damage
Phase of flight
Landing
Aircraft
N8311FHughes 369C
Weather
Visual (VMC) · Day
Status
Completed · report May 26, 1993
Report
Approved by Office Director
FAA report
19920409010029A
Case key
27597

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

An undetermined failure in the rotor system.

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/malfunctionLanding - flare/touchdown
Rotor system - undeterminedCause
Rotor system - separation

Analysis

The helicopter was completing an aerial observation flight (fish spotting) over the Pacific Ocean near the island of canton and was landing on the ship's helipad. When the skids touched down, the rotor mast assembly separated from the rotor mast base causing the helicopter to turn to the left 90 degrees. The rotor mast assembly and all its components fell into the Ocean and were not recovered. The helicopter sustained substantial damage. The pilot reported that the helicopter did not experience any abnormal cyclic movements or any unusual vibrations before the occurrence. The helicopter had accrued 328.5 hours since the last annual inspection. A 300-hour and a 100-hour inspection had recently been completed. Metallurgical examination of the rotor mast base fracture surfaces revealed overload characteristics with some post fracture mechanical smearing and damage. No evidence of any corrosion or fatigue was found. The hardness measurements complied with the material specifications.

Aircraft

Registration
N8311F
Reported as
Hughes 369C
Category
Helicopter
Serial number
460806S
Airframe hours
11,013
Engine
Allison 250-C20, 425 horsepower, turbo shaft
Damage
Substantial damage
Flight
Aerial observation · Part 91
Operator
Voyager, Inc
Registered owner
Voyager, Inc
Airworthiness certificate
Standard, Normal
Last inspection
100 hour · April 1, 1992 · 42 hours before

Flight crew

As NTSB recorded them. NTSB leaves out names.

Role
Pilot
Age
42
Certificate
Commercial
Medical
Class 2, Valid Medical--no waivers/lim.
Seat
Left

Weather

Conditions
Visual (VMC) · Day
Visibility
20 statute miles
Lowest ceiling
None

FAA reports on this event · 1

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