20090428006599I

Incident · Minor damage

FAA incident report · Amtr Velocityxlrg · Joplin, MO · April 28, 2009

Date
April 28, 2009 · 15:05 local
Place
Joplin, MO
Airport
Joplin Regional
Phase of flight
Landing
Operating rules
General operating rules (Part 91)
Damage
Minor damage
Aircraft
N568Y
Reported as
Amtr Velocityxlrg
People aboard
2
Fatal injuries
0
Other injuries
0
Pilot’s flight hours
800 total85 in this make and model20 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) During climb-out from kjln, the pilot reported that the landing gear "in transient" light remained on after selecting gear-up. Returning to kjln for landing, the nose gear strut and wheel assembly departed the aircraft after touchdown. The aircraft nose lowered to the runway and skidded approximately 800 feet. Post-incident inspection of the nose gear strut assembly by the owner/operator showed indications of stress overload and the possibility of pre-existing crack. This may have caused gear retract and nose door alignment problems, resulting in abnormal gear indications. Nose-gear shimmy problems, well known to velocity aircraft owners and the manufacturer, may have precipitated these conditions. Incident number ICE052009014 is closed with this report.

As the FAA filed it

(-23) DURING CLIMB-OUT FROM KJLN, THE PILOT REPORTED THAT THE LANDING GEAR "IN TRANSIENT" LIGHT REMAINED ON AFTER SELECTING GEAR-UP. RETURNING TO KJLN FOR LANDING, THE NOSE GEAR STRUT AND WHEEL ASSEMBLY DEPARTED THE AIRCRAFT AFTER TOUCHDOWN. THE AIRCRAFT NOSE LOWERED TO THE RUNWAY AND SKIDDED APPROXIMATELY 800 FEET. POST-INCIDENT INSPECTION OF THE NOSE GEAR STRUT ASSEMBLY BY THE OWNER/OPERATOR SHOWED INDICATIONS OF STRESS OVERLOAD AND THE POSSIBILITY OF PRE-EXISTING CRACK. THIS MAY HAVE CAUSED GEAR RETRACT AND NOSE DOOR ALIGNMENT PROBLEMS, RESULTING IN ABNORMAL GEAR INDICATIONS. NOSE-GEAR SHIMMY PROBLEMS, WELL KNOWN TO VELOCITY AIRCRAFT OWNERS AND THE MANUFACTURER, MAY HAVE PRECIPITATED THESE CONDITIONS. INCIDENT NUMBER ICE052009014 IS CLOSED WITH THIS REPORT.

Other reports on N568Y · 1

Matched to the same aircraft by N-number and date.