SEA86LA026

NTSB accident investigation · Hughes 269C · Brooks, OR · November 24, 1985

Accident · No injuriesLimited investigationFinal report
Date
November 24, 1985, 14:00 local (22:00 UTC)
Place
Brooks, OR
Injuries
2 uninjured
Damage
Substantial damage
Phase of flight
Enroute
Aircraft
N58181Hughes 269C
Weather
Visual (VMC) · Day
Status
Completed
Report
Approved by Office Director
FAA report
19851124058099A
Case key
40336

From the NTSB’s public API. By law, NTSB reports can’t be used as evidence in lawsuits over the accident.

On this page

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.

Loss of engine power(total) - mech failure/malfCruise - normal
Engine assembly,cylinder - failure,totalCause
Hard landingLanding - flare/touchdown
In flight collision with terrain/waterLanding - flare/touchdown

Analysis

A total loss of power occurred due to the number 4 cylinder failing. A tail boom strike occurred during a hard landing in a parking lot, severing the tail boom.

Aircraft

Registration
N58181
Reported as
Hughes 269C
Category
Helicopter
Serial number
480682
Airframe hours
4,650
Engine
Lycoming HIO-360 SER, 190 horsepower, reciprocating
Damage
Substantial damage
Flight
Personal · Part 91
Registered owner
Ronnie T. Walters
Airworthiness certificate
Standard, Normal
Last inspection
100 hour · August 29, 1985 · 15 hours before
Departed
RBG · Roseburg, OR
Destination
PDX · Portlande, OR

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
46
Certificates
Flight instructor, Commercial
Medical
Class 2, Valid Medical--no waivers/lim.
Seat
Left
Flight hours
785 total · 500 in this make and model · 680 as pilot in command · 120 in the last 90 days · 8 in the last 24 hours

Weather

Conditions
Visual (VMC) · Day
Wind
360° at 7 knots
Visibility
20 statute miles
Lowest ceiling
4,000 ft broken
Temperature
25 °F

FAA reports on this event · 1

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