Service difficulty reports · 5
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR ULX2004F00007Housing · crackedCRACKED AT DRIVE FLANGE WELD. POSSIBLE CAUSE- AERODYNAMIC AND MECHANICAL FORCES AT DRIVE FLANGE. RECOMMENDATION- USE OF STRONGER BASE MATERIAL AND STRICTER CONTROL OF WELDING PROCESS.SDR ULX2004F00018Flyweight · malfunctionedN2 RPM UNSTABLE. WILL NOT HOLD N2 RPM STABILIZED. PROBABLE CAUSE: FLYWHEEL WEIGHT MALFUNCTION.SDR 98ZZZX1266Doubler · corrodedFUEL BOOST PUMP MOUNTING FLANGE BECAME DEBONDED ALLOWING THE BOOST PUMPS TO FLEX WITH THE FUEL CELL. REMOVAL OF THE FUEL CELL REVEALED EXTENSIVE CORROSION OF THE ALUMINUM MOUNTING FLANGE. SUBMITTER SUGGESTED A POSSIBLE CAUSE OF FAILURE WAS MOISTURE TRAPPED SDR 97ZZZX4708Blade · bearing bindingACFT TT: 13,497.8 HOURS. 104.2 HR. TWO NEW T/R BLADES P/N 206-016-201-131, SN CS-2814 AND SN CS-2815 WERE INSTALLED. PILOT'S COMPLAINT ABOUT T/R PEDAL PROBLEM. HELICOPTER WAS INSPECTED AND THE FOUR BEARINGS (2 EACH ON BLADES) ON T/R BLADES WERE FOUND BINSDR 97ZZZX4707Bearing · bindingACFT TT: 13,497.8 HOURS. 104.2 HR. TWO NEW T/R BLADES P/N 206-016-201-131, SN CS-2814 AND SN CS-2815 WERE INSTALLED. PILOT'S COMPLAINT ABOUT T/R PEDAL PROBLEM. HELICOPTER WAS INSPECTED AND THE FOUR BEARINGS (2 EACH ON BLADES) ON T/R BLADES WERE FOUND BIN
Other aircraft with N212LA · 1
The FAA can assign a mark to another aircraft once a registration is cancelled. N212LA is registered now to the first aircraft listed.