SEA02LA150

NTSB accident investigation · Hughes 269A · Covington, WA · August 10, 2002

Accident · No injuriesLimited investigationFinal report
Date
August 10, 2002, 09:45 local (16:45 UTC)
Place
Covington, WA
Injuries
1 uninjured
Damage
Substantial damage
Phase of flight
Takeoff
Aircraft
N90271Hughes 269A
Weather
Visual (VMC) · Day
Status
Completed · report April 18, 2003
Report
Approved by Office Director
Parties
FAA-FSDO
FAA report
20020810023529A
Case key
55473

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

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

Aircraft control not maintained while hovering.

Analysis

In a written statement the student pilot reported that the accident flight was his first attempt to hover the helicopter, solo. He reported that after his instructor exited the helicopter, and as he raised the collective in preparation for takeoff "The helicopter jumped into the air and moved to the right." He said that he inadvertently over corrected for the situation, and the helicopter started to move toward where his instructor was standing. In an effort to control the movement of the helicopter he "...immediately pulled the cyclic to rear." The helicopter's tail rotor subsequently struck the ground, and sustained substantial damage.

Factual narrative

On August 10, 2002, approximately 0945 Pacific daylight time, a Hughes 269A helicopter, N90271, registered to Seaquest Expeditions Inc. of Eugene, Oregon, and being flown by a student pilot on his first solo flight, was substantially damaged when its tail rotor contacted terrain during liftoff from Crest Airpark (S36), Covington, Washington. The solo student pilot was not injured in the accident. Visual flight rules (VFR) weather conditions (ceiling 2,200 feet broken, visibility 10 statute miles), with winds from 290 degrees true at 4 knots, were reported at Seattle-Tacoma International Airport, Seattle, Washington, at 0956, and no flight plan had been filed for the 14 CFR 91 local instructional flight.

In a written statement the student pilot reported that the accident flight was his first attempt to hover the helicopter, solo. He reported that after his instructor exited the helicopter, and as he raised the collective in preparation for takeoff "The helicopter jumped into the air and moved to the right." He said that he inadvertently over corrected for the situation, and the helicopter started to move toward where his instructor was standing. In an effort to control the movement of the helicopter he "...immediately pulled the cyclic to rear." The helicopter's tail rotor subsequently struck the ground, and sustained substantial damage.

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 control - in flightTakeoff
Aircraft control - not maintainedPilot in commandCause
In flight collision with terrain/waterTakeoff
Terrain condition - ground

Aircraft

Registration
N90271
Reported as
Hughes 269A
Category
Helicopter
Serial number
65-18261
Airframe hours
5,309
Engine
Lycoming HIO-360, 180 horsepower, reciprocating
Damage
Substantial damage
Flight
Instructional · Part 91
Operator
Charles Douglas
Registered owner
Seaquest Expeditions Inc
Airworthiness certificate
Standard, Normal
Last inspection
Annual · October 10, 2001 · 61 hours before
Departed
S36 · Covington, WA
Destination
S36
Airport
S36 · Crest Airpark

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
Student pilot
Age
60
Injuries
None
Certificate
Student
Medical
Class 3, Unknown
Seat
Right
Flight hours
28 total · 27 in this make and model · 15 in the last 90 days · 12 in the last 30 days

Weather

Conditions
Visual (VMC) · Day
Wind
270° at 4 knots
Visibility
10 statute miles
Lowest ceiling
2,200 ft broken
Temperature
63 °F, dew point 57 °F
Altimeter
30.12 inHg
Observed at
SEA, 10 nm away

FAA reports on this event · 1

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