What happened
The FAA’s narrative, in sentence case. The FAA writes it in capitals and removes private details.
(-23) On 07/20/2003 at approximately 1930 EDT, PA-24 N5611P was engaged in a training flight. Mr. R. Edwards was the pilot under instruction (pui) and Mr. F. Puglia was the instructor (ip). Their 8th landing of the training event ended in a gear up landing. The landing gear system had, apparently, failed. Neither pilot recognized the failure or took steps to mitigate it. After a thorough inspection of the aircraft, inspector observed landing gear jackscrew assembly detached from its mounting support. Further, support assembly was observed with ten sheared rivets. Also, bulkhead for jackscrew was severely damaged. Inspection of the right main landing gear revealed landing gear control rod assembly bent at approximately 20 degrees, with slight damage to the rear side of forward spar and wheel axle cover. Fuselage undercarriage was observed with substantial damage to skin, and antenna's. nose wheel, and lower cowling also exhibited damage. Extensive damage was sustained to the propeller. As a result, there was sudden stoppage to the engine. privacy data omitted This incident is closed.
As the FAA filed it
(-23) ON 07/20/2003 AT APPROXIMATELY 1930 EDT, PA-24 N5611P WAS ENGAGED IN A TRAINING FLIGHT. MR. R. EDWARDS WAS THE PILOT UNDER INSTRUCTION (PUI) AND MR. F. PUGLIA WAS THE INSTRUCTOR (IP). THEIR 8TH LANDING OF THE TRAINING EVENT ENDED IN A GEAR UP LANDING. THE LANDING GEAR SYSTEM HAD, APPARENTLY, FAILED. NEITHER PILOT RECOGNIZED THE FAILURE OR TOOK STEPS TO MITIGATE IT. AFTER A THOROUGH INSPECTION OF THE AIRCRAFT, INSPECTOR OBSERVED LANDING GEAR JACKSCREW ASSEMBLY DETACHED FROM ITS MOUNTING SUPPORT. FURTHER, SUPPORT ASSEMBLY WAS OBSERVED WITH TEN SHEARED RIVETS. ALSO, BULKHEAD FOR JACKSCREW WAS SEVERELY DAMAGED. INSPECTION OF THE RIGHT MAIN LANDING GEAR REVEALED LANDING GEAR CONTROL ROD ASSEMBLY BENT AT APPROXIMATELY 20 DEGREES, WITH SLIGHT DAMAGE TO THE REAR SIDE OF FORWARD SPAR AND WHEEL AXLE COVER. FUSELAGE UNDERCARRIAGE WAS OBSERVED WITH SUBSTANTIAL DAMAGE TO SKIN, AND ANTENNA'S. NOSE WHEEL, AND LOWER COWLING ALSO EXHIBITED DAMAGE. EXTENSIVE DAMAGE WAS SUSTAINED TO THE PROPELLER. AS A RESULT, THERE WAS SUDDEN STOPPAGE TO THE ENGINE. ^PRIVACY DATA OMITTED^ THIS INCIDENT IS CLOSED.
Other reports on N5611P · 1
Matched to the same aircraft by N-number and date.