ANC92FA164

NTSB accident investigation · Mcdonnell Douglas 369D · Eagle, AK · September 11, 1992

Accident · FatalField investigationFinal report
Date
September 11, 1992, 09:10 local (17:10 UTC)
Place
Eagle, AK
Injuries
3 fatal
Damage
Destroyed
Phase of flight
Approach
Aircraft
N1096XMcdonnell Douglas 369D
Weather
Visual (VMC) · Day
Status
Completed · report September 17, 1993
Report
Approved by Office Director
NTSB office
Alaska Regional Office
FAA report
19920911036509A
Case key
5651

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 inflight fatigue failure and separation of a main rotor blade, inadequate operator maintenance and inspection, and material defect.

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/malfunctionApproach
Rotor system,main rotor blade - fatigueCause
Inadequate quality controlManufacturerCause
Rotor system,main rotor blade - separationCause
Maintenance,compliance with ad - not performedCompany maintenance personnelCause
Loss of control - in flightApproach
In flight collision with terrain/waterApproach

Analysis

Shortly after takeoff the pilot radioed he was returning due to poor visual flight conditions, and was last seen circling the Eagle runway. The wreckage was found aprx 7 hrs later 150 yds north of the runway. The blue m/r blade was found separated; the trailing attachment lugs of both the upper and lower blade root fittings were fractured through the holes, and the lead lag dampener lug was also fractured. Metallurgical examination revealed fatigue progression on all four root fractures. Operator maintenance personnel stated that they were not aware of AD91-17-04 requirement to remove & inspect the m/r blades at 100-HR intervals.

Aircraft

Registration
N1096X
Reported as
Mcdonnell Douglas 369D
Category
Helicopter
Serial number
110836D
Airframe hours
3,023
Engine
Allison 250-C20B, 420 horsepower, turbo shaft
Damage
Destroyed
Flight
Part 135
Operator
Tundra Copters Inc.
Registered owner
Tundra Copters Inc.
Airworthiness certificate
Standard, Normal
Last inspection
100 hour · August 14, 1992 · 57 hours before
Flight plan
Company VFR

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
36
Certificates
Flight instructor, Commercial
Airplane ratings
Multi-engine land, Single-engine land, Single-engine sea
Instrument ratings
Airplane, Helicopter
Medical
Class 2, Valid Medical--no waivers/lim.
Seat
Left
Toxicology
Performed
Flight hours
3,779 total · 281 in this make and model · 3,644 as pilot in command · 205 in the last 90 days · 61 in the last 30 days · 1 in the last 24 hours

Weather

Conditions
Visual (VMC) · Day
Visibility
1 statute miles
Temperature
34 °F, dew point -0 °F

FAA reports on this event · 1

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