What happened
The FAA’s narrative, in sentence case. The FAA writes it in capitals and removes private details.
(-23) On may 12, 2007, at approximately 0650 MST, at Glendale Municipal Airport, AZ (geu), Aeronca 11AC, N85835, veered off geu runway 19 and struck a runway sign and taxiway light. N85835 was being operated by a certificated pilot receiving a tailwheel aircraft endorsement by a flight instructor. The certified flight instructor (CFI) stated that the landing was a good three point landing. After the landing, the CFI noted that the aircraft slowly went right. The CFI took over control and verified that the yoke was full up elevator and applied full left rudder. The aircraft continued to turn right through the dirt, striking a taxi light and a taxiway sign. The aircraft came to rest on a taxiway. The extent of the damage was to the fuselage midsection on the lower left side. The lower left longeron was damaged as well as the cluster assemble that it attached to. The fabric covering the longeron was also damaged. The CFI was unable to correct the situation that the student induced as the student failed to maintain directional control. The situation was difficult for the CFI to correct as the aircraft does not have pilot brake controls on the right side where the CFI was located.
As the FAA filed it
(-23) ON MAY 12, 2007, AT APPROXIMATELY 0650 MST, AT GLENDALE MUNICIPAL AIRPORT, AZ (GEU), AERONCA 11AC, N85835, VEERED OFF GEU RUNWAY 19 AND STRUCK A RUNWAY SIGN AND TAXIWAY LIGHT. N85835 WAS BEING OPERATED BY A CERTIFICATED PILOT RECEIVING A TAILWHEEL AIRCRAFT ENDORSEMENT BY A FLIGHT INSTRUCTOR. THE CERTIFIED FLIGHT INSTRUCTOR (CFI) STATED THAT THE LANDING WAS A GOOD THREE POINT LANDING. AFTER THE LANDING, THE CFI NOTED THAT THE AIRCRAFT SLOWLY WENT RIGHT. THE CFI TOOK OVER CONTROL AND VERIFIED THAT THE YOKE WAS FULL UP ELEVATOR AND APPLIED FULL LEFT RUDDER. THE AIRCRAFT CONTINUED TO TURN RIGHT THROUGH THE DIRT, STRIKING A TAXI LIGHT AND A TAXIWAY SIGN. THE AIRCRAFT CAME TO REST ON A TAXIWAY. THE EXTENT OF THE DAMAGE WAS TO THE FUSELAGE MIDSECTION ON THE LOWER LEFT SIDE. THE LOWER LEFT LONGERON WAS DAMAGED AS WELL AS THE CLUSTER ASSEMBLE THAT IT ATTACHED TO. THE FABRIC COVERING THE LONGERON WAS ALSO DAMAGED. THE CFI WAS UNABLE TO CORRECT THE SITUATION THAT THE STUDENT INDUCED AS THE STUDENT FAILED TO MAINTAIN DIRECTIONAL CONTROL. THE SITUATION WAS DIFFICULT FOR THE CFI TO CORRECT AS THE AIRCRAFT DOES NOT HAVE PILOT BRAKE CONTROLS ON THE RIGHT SIDE WHERE THE CFI WAS LOCATED.
NTSB investigation
The NTSB’s investigation of this event, with its probable cause and findings. Matched to this report by N-number and date.