SEA99LA092

NTSB accident investigation · Hughes 369D · Shelton, WA · June 22, 1999

Accident · No injuriesLimited investigationFinal report
Date
June 22, 1999, 14:30 local (21:30 UTC)
Place
Shelton, WA
Injuries
1 uninjured
Damage
Substantial damage
Phase of flight
Landing
Aircraft
N1089YHughes 369D
Weather
Visual (VMC) · Day
Status
Completed · report August 3, 2000
Report
Approved by Office Director
FAA report
19990622007449A
Case key
46656

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

On this page

Probable cause

The NTSB’s determination of the probable cause, and any contributing factors.

The pilot's failure to maintain rotor RPM during an autorotation.

Analysis

The pilot was practicing autorotations from an altitude of approximately 200 feet above ground level (AGL) and an airspeed of approximately 50 knots. During the second practice autorotation, the pilot reduced power with throttle and used collective to adjust rotor speed to 410 RPM (minimum RPM for practice autorotations). The rotor RPM decreased below 410 RPM and the aircraft rapidly started to descend. Before the pilot was able to recover, the aircraft collided with the ground and rolled over. The aircraft sustained substantial damage to the main rotor blades, tail rotor, tail boom and fuselage. The pilot reported no mechanical failures or malfunctions with the aircraft at the time of the accident.

Factual narrative

On June 22, 1999, about 1430 Pacific daylight time, a Hughes 369D, N1089Y, registered to and operated by Olympic Air, Incorporated, was substantially damaged during landing following a practice autorotation. The accident occurred at Shelton Airport, Shelton, Washington. The commercial pilot, the sole occupant of the aircraft, was not injured. A company VFR flight plan was filed and visual meteorological conditions prevailed for this 14CFR91 flight. The flight originated from Rockaway, Oregon, approximately one hour prior to the accident.

The pilot stated he was practicing autorotations from an altitude of approximately 200 feet above ground level (AGL) and an airspeed of approximately 50 knots. During the second practice autorotation, the pilot reduced power with throttle and used collective to adjust rotor speed to 410 RPM (minimum RPM for practice autorotations). The pilot stated the rotor RPM "quickly" decayed and the aircraft rapidly started to descend. Before the pilot was able to recover, the aircraft collided with the ground and rolled over. The aircraft sustained substantial damage to the main rotor blades, tail rotor, tail boom and fuselage.

The pilot reported no mechanical failures or malfunctions with the aircraft at the time of the accident.

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.

Hard landingLanding - flare/touchdown
Autorotation - performedPilot in command
Rotor rpm - inadequatePilot in commandCause

Aircraft

Registration
N1089Y
Reported as
Hughes 369D
Category
Helicopter
Serial number
510962D
Airframe hours
15,399
Engine
Allison C20-B, 420 horsepower, turbo shaft
Damage
Substantial damage
Flight
Business · Part 91
Registered owner
Olympic Air Inc.
Airworthiness certificate
Standard, Normal
Last inspection
Annual · June 10, 1999 · 59 hours before
Departed
Rockaway, OR
Destination
SHN · WA
Flight plan
Company VFR
Airport
SHN · Sanderson Field

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
41
Certificates
Commercial, Private
Airplane ratings
Single-engine land
Medical
Class 2, Valid Medical--no waivers/lim.
Seat
Left
Toxicology
Performed
Flight hours
8,000 total · 5,000 in this make and model · 7,900 as pilot in command · 160 in the last 90 days · 91 in the last 30 days · 1 in the last 24 hours

Weather

Conditions
Visual (VMC) · Day
Wind
220° at 17 knots, gusting 24
Visibility
10 statute miles
Lowest ceiling
None
Temperature
63 °F
Altimeter
30.00 inHg
Observed at
KLS

FAA reports on this event · 1

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