SEA02LA176

NTSB accident investigation · Eells Air Command 503 · Prineville, OR · September 15, 2002

Accident · No injuriesLimited investigationFinal report
Date
September 15, 2002, 09:30 local (16:30 UTC)
Place
Prineville, OR
Injuries
1 uninjured
Damage
Substantial damage
Phase of flight
Landing
Aircraft
N25069Eells Air Command 503
Weather
Visual (VMC) · Day
Status
Completed · report April 8, 2003
Report
Approved by Office Director
Parties
FAA-FSDO
FAA report
20020915023549A
Case key
55705

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 student pilot's failure to maintain airspeed resulting in a hard landing.

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
Airspeed - not maintainedPilot in commandCause

Analysis

The student pilot reported that he flew the gyroplane down to about 11 feet above the runway surface for landing. He then pulled the control stick back to level the aircraft. The student pilot stated that the aircraft ballooned a little so he pushed the stick forward. At this point, the aircraft was about 12 feet above the runway and it began to rapidly descend. The student pilot applied power to arrest the sink rate, however, the rotor speed had decayed and the aircraft landed hard with no forward airspeed. After touchdown, the aircraft bounced and tilted to the left. The rotors contacted the runway surface and the aircraft came to rest on its left side. The student pilot reported no mechanical failures or malfunctions with the aircraft at the time.

Factual narrative

On September 15, 2002, about 0930 Pacific daylight time, an experimental Air Command 503 gyrocopter, N25069, registered to a private individual and operated by a student pilot as a 14 CFR Part 91 instructional flight, landed hard and bounced at the Prineville Airport, Prineville, Oregon. Visual meteorological conditions prevailed at the time and no flight plan was filed for the local flight. The gyrocopter was substantially damaged and the student pilot, the sole occupant, was not injured.

The student pilot reported that he flew the aircraft down to about 11 feet above ground level over the runway for landing. He then pulled the control stick back to level the aircraft. The student pilot stated that the aircraft ballooned a little so he pushed the stick forward. At this point, the aircraft was about 12 feet above the runway and began to rapidly descend. The student pilot applied power to arrest the sink rate, however, the rotor speed had decayed and the aircraft landed hard with no forward airspeed. After touchdown, the aircraft bounced and tilted to the left. The rotors contacted the runway surface and the aircraft came to rest on its left side.

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

The student pilot reported a total flight time in all aircraft (gyrocopter) of 46.2 hours. A total of 19.8 hours were accumulated as pilot-in command.

Aircraft

Registration
N25069
Reported as
Eells Air Command 503
Category
Gyroplane, amateur-built
Serial number
1D188
Airframe hours
92
Engine
Rotax 503 ULDCDI, 52 horsepower, reciprocating
Damage
Substantial damage
Flight
Instructional · Part 91
Registered owner
Belinda C. Eells
Airworthiness certificate
Special, Experimental (Special)
Last inspection
Annual · March 1, 2002 · 14 hours before
Departed
S39 · Prineville, OR
Destination
S39
Airport
S39 · Prineville, runway 28, 5,000 × 60 ft, asphalt

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
53
Injuries
None
Certificate
Student
Medical
Class 3, Valid Medical--w/ waivers/lim
Seat
Front
Flight hours
46 total · 2 in the last 90 days · 1 in the last 30 days

Weather

Conditions
Visual (VMC) · Day
Wind
Variable at 3 knots
Visibility
10 statute miles
Lowest ceiling
None
Temperature
55 °F

FAA reports on this event · 1

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