What happened
The FAA’s narrative, in sentence case. The FAA writes it in capitals and removes private details.
(-23) On July 24, 2003, at 0750 MDT, N500EA. An experimental (r&d) eclipse 500 business jet, registered to eclipse aviation, corporation Albuquerque, NM, experienced a right main landing gear failure shortly after touching down at the conclusion of a production test flight. Visual meteorological conditions prevailed at the time and weather was not a factor. The company had an approved test flight area arranged with ATC but no IFR flight plan was filed. Aircraft damage was minor and the ATP certificated pilot was not injured. The flight had originated one hour earlier from the same airport. Examination of the aircraft revealed a cast fitting on the main gear actuator had failed at the airframe attach point. It was the second failure of this type actuator and the aircraft manufacturer had recently decided to change actuator manufacturers due to production problems. Additionally, as a result of this incident, the aircraft manufacturer is considering a landing gear design change to compensate for actuator failure.
As the FAA filed it
(-23) ON JULY 24, 2003, AT 0750 MDT, N500EA. AN EXPERIMENTAL (R&D) ECLIPSE 500 BUSINESS JET, REGISTERED TO ECLIPSE AVIATION, CORPORATION ALBUQUERQUE, NM, EXPERIENCED A RIGHT MAIN LANDING GEAR FAILURE SHORTLY AFTER TOUCHING DOWN AT THE CONCLUSION OF A PRODUCTION TEST FLIGHT. VISUAL METEOROLOGICAL CONDITIONS PREVAILED AT THE TIME AND WEATHER WAS NOT A FACTOR. THE COMPANY HAD AN APPROVED TEST FLIGHT AREA ARRANGED WITH ATC BUT NO IFR FLIGHT PLAN WAS FILED. AIRCRAFT DAMAGE WAS MINOR AND THE ATP CERTIFICATED PILOT WAS NOT INJURED. THE FLIGHT HAD ORIGINATED ONE HOUR EARLIER FROM THE SAME AIRPORT. EXAMINATION OF THE AIRCRAFT REVEALED A CAST FITTING ON THE MAIN GEAR ACTUATOR HAD FAILED AT THE AIRFRAME ATTACH POINT. IT WAS THE SECOND FAILURE OF THIS TYPE ACTUATOR AND THE AIRCRAFT MANUFACTURER HAD RECENTLY DECIDED TO CHANGE ACTUATOR MANUFACTURERS DUE TO PRODUCTION PROBLEMS. ADDITIONALLY, AS A RESULT OF THIS INCIDENT, THE AIRCRAFT MANUFACTURER IS CONSIDERING A LANDING GEAR DESIGN CHANGE TO COMPENSATE FOR ACTUATOR FAILURE.
Other reports on N500EA · 1
Matched to the same aircraft by N-number and date.