Plane Crash List

Eurocopter AS-350D N5771L

24 October 1994 · Kaupo, Hawaii, United States · Minor injuries

Summary

On 24 October 1994 at about 18:30 local time, a Eurocopter AS-350D registered N5771L was involved in an accident near Kaupo, Hawaii, United States. 4 people were on board and 4 had minor injuries. The aircraft was substantially damaged. The NTSB has published a probable cause for this accident; it is quoted in full below.

The record

Date
at 18:30
Classification
Accident
Location
Kaupo, Hawaii, United States
Coordinates
20.7698, -155.9901
Aircraft
Eurocopter AS-350D
Registration
N5771L
Category
Helicopter
Engines
1
Operator
Not recorded
Operating rule
Part 135: Air Taxi & Commuter
Purpose of flight
Unknown
Phase of flight
Not recorded
Route
Kahului → Unknown
Aircraft damage
Substantial
Weather
VMC
Light
Day
NTSB number
LAX95LA019

People

4 people had minor injuries.

On board Died Serious Minor Uninjured
4 0 0 4 0

Probable cause

a total loss of engine power by the corrosion fatigue failure of the compressor impeller due to the failure of company maintenance personnel to perform the prescribed daily compressor wash procedures and the inadequate maintenance inspections, which failed to detect the corrosion and subsequent pitting, that led to the fatigue initiation.

Quoted verbatim from the NTSB record. This site does not paraphrase or interpret it.

Read the full NTSB narrative

AN EUROCOPTER AS-350D COLLIDED WITH TREES AFTER A LOSS OF POWER WHILE OPERATING IN A MARINE ENVIRONMENT. THE PILOT REPORTED HE HEARD AN EXPLOSION FOLLOWED BY THE ENGINE OUT HORN. THE ENGINE TEMPERATURE (T4) GAUGE WAS NOTED AT 900 DEGREES CELSIUS AND THE ENGINE CHIP DETECTOR LIGHT ILLUMINATED. EXAMINATION REVEALED THAT THE ENGINE HAD SUSTAINED DAMAGE TO THE AXIAL COMPRESSOR, COMPRESSOR STATOR VANES, AND THE IMPELLER. PORTIONS OF THE IMPELLER BLADES WERE EXAMINED MICROSCOPICALLY REVEALING EVIDENCE OF METAL FATIGUE, WITH PITTING EVIDENT THROUGHOUT THE BLADES. ENERGY DISPERSIVE X RAY SHOWED THE PRESENCE OF SULFUR AND CHLORINE IN CORROSION DEPOSITS IN THE PITS. THE ENGINE WAS INSPECTED TWICE IN THE MONTH PRECEDING THE ACCIDENT. THE INSPECTION CRITERIA OUTLINED IN THE ENGINE MAINTENANCE MANUAL DETAILS A VISUAL INSPECTION PROCEDURE OF THE COMPRESSOR SECTION FOR CRACKS. THE MAINTENANCE MANUAL ALSO PRESCRIBES A DAILY COMPRESSOR WATER RINSE TO REMOVE SALT DEPOSITS, FOLLOWED BY INSPECTING THE COMPRESSOR FOR CLEANLINESS.

Quoted verbatim from the NTSB record.

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no coordinates
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