20060906018049I

Incident · Minor damage

FAA incident report · Rans SL7S · Kansas City, MO · September 6, 2006

Date
September 6, 2006 · 12:15 local
Place
Kansas City, MO
Airport
Kansas City International
Phase of flight
Roll-Out (Fixed Wing)
Operating rules
General operating rules (Part 91)
Damage
Minor damage
Aircraft
N2506A
Reported as
Rans SL7S
Reported engine
ROTAX ROTAX*
People aboard
1
Fatal injuries
0
Pilot’s flight hours
6,100 total6 in this make and model80 in the last 90 days

From the FAA’s Accident/Incident Data System (AIDS), through its Aviation Safety Information Portal, as reported. The NTSB investigates accidents separately, and its record of an accident is the fuller one. The aircraft is matched to the registry by N-number and event date, checked against the reported make and model; the registry’s history has gaps, so older matches can be wrong. Compare the reported make and model.

What happened

The FAA’s narrative, in sentence case. The FAA writes it in capitals and removes private details.

(-23) Light-sport airplane on a VFR flight from hayes, Kansas (hys) to Kansas City, Missouri international airport (mci). Surface wind 360 degrees @ 8 knots and the pilot made a three point landing on runway 1L. After touch down, aircraft veered to left and did not respond to input on the rudder controls. Pilot attempted to control ground roll by use of brakes and aircraft tail raised up resulting in a propeller strike. Investigation of the incident found that the tail wheel unit failed due to metal fatigue. Incident privacy data omitted closed.

As the FAA filed it

(-23) LIGHT-SPORT AIRPLANE ON A VFR FLIGHT FROM HAYES, KANSAS (HYS) TO KANSAS CITY, MISSOURI INTERNATIONAL AIRPORT (MCI). SURFACE WIND 360 DEGREES @ 8 KNOTS AND THE PILOT MADE A THREE POINT LANDING ON RUNWAY 1L. AFTER TOUCH DOWN, AIRCRAFT VEERED TO LEFT AND DID NOT RESPOND TO INPUT ON THE RUDDER CONTROLS. PILOT ATTEMPTED TO CONTROL GROUND ROLL BY USE OF BRAKES AND AIRCRAFT TAIL RAISED UP RESULTING IN A PROPELLER STRIKE. INVESTIGATION OF THE INCIDENT FOUND THAT THE TAIL WHEEL UNIT FAILED DUE TO METAL FATIGUE. INCIDENT ^PRIVACY DATA OMITTED^ CLOSED.