FTW95LA031

NTSB accident investigation · Herron Little Wing Autogyro · Little Rock, AR · October 21, 1994

Accident · No injuriesLimited investigationFinal report
Date
October 21, 1994, 15:00 local (20:00 UTC)
Place
Little Rock, AR
Injuries
1 uninjured
Damage
Substantial damage
Phase of flight
Landing
Aircraft
N45LWHerron Little Wing Autogyro
Weather
Visual (VMC) · Day
Status
Completed · report May 9, 1995
Report
Approved by Office Director
Case key
19293

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 fractured tail wheel mounting bracket and loose tailwheel. A factor was the pilot's continued flight testing after experiencing tail wheel shimmy on the prior test flight.

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/malfunctionLanding - roll
Landing gear,tailwheel assembly - fracturedCause
Landing gear,tailwheel - looseCause
Operation with known deficiencies in equipment - performedPilot in commandFactor
Loss of control - on ground/waterLanding - roll
Directional control - not possiblePilot in command
Roll overLanding - roll

Analysis

A homebuilt gyroplane rolled inverted during landing on a concrete runway. The initial touchdown was on the two front main landing gear, and as the tail wheel came into contact with the ground, the tail of the aircraft turned sharply to the right. The aircraft then swerved to the left and rolled inverted to the right causing structural damage. Examination of the aircraft revealed a fractured tail wheel assembly mounting bracket and loose tail wheel. The pilot experienced 'tail wheel shimmy' during ground taxi testing the previous day.

Factual narrative

On October 21, 1994, at 1500 central daylight time, a Herron Little Wing Autogyro, N45LW, was substantially damaged while landing near Little Rock, Arkansas. The private pilot was not injured. Visual meteorological conditions prevailed for the local test flight.

The pilot, and builder of the gyroplane, was conducting initial low level flight and taxi tests at North Little Rock Municipal Airport. He stated that the "initial flight tests" consisted of climbs, descents, and S-turns conducted at low altitude over the runway surface. Both hovering and roll-on landings were conducted with power on. These were accomplished by taking off from the approach end of the runway, flying the length of the runway at low altitude, and landing the airplane at the departure end. This sequence was accomplished 10 or 12 times with no problems. The pilot stated that, during the last landing, he attempted to land the gyroplane with power off and 10 to 15 knots of forward airspeed. The initial touchdown was on the two front main landing gear, and as the tail wheel came in contact with the ground, the tail turned sharply to the right. The aircraft then swerved to the left and rolled inverted to the right causing structural damage.

After the accident, the pilot reported that the aircraft had a "tail wheel shimmy" during ground taxi testing the day prior to the accident. Examination of the aircraft after the accident revealed that the mounting bracket for the tail wheel assembly was fractured for undetermined reasons, and the tail wheel was loose.

Aircraft

Registration
N45LW
Reported as
Herron Little Wing Autogyro (LITTLE WIN)
Category
Gyroplane, amateur-built
Serial number
LW-1
Engine
Continental O-200-A, 100 horsepower, reciprocating
Damage
Substantial damage
Flight
Part 91
Registered owner
Herron, Ronald L.
Airworthiness certificate
Special, Experimental (Special)
Airport
1M1 · North Little Rock Muni, runway 5, 3,000 × 150 ft, concrete

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
45
Certificate
Private
Airplane ratings
Single-engine land
Medical
Class 3, Valid Medical--no waivers/lim.
Seat
Front
Flight hours
1,400 total · 2 in this make and model · 1,400 as pilot in command · 40 in the last 90 days · 23 in the last 30 days · 7 in the last 24 hours

Weather

Conditions
Visual (VMC) · Day
Wind
210° at 4 knots
Visibility
7 statute miles
Lowest ceiling
1,400 ft broken
Temperature
72 °F, dew point 66 °F
Altimeter
29.00 inHg
Observed at
LIT, 5 nm away