Service difficulty reports · 9
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR QMLA2010031510006Engine · out of rigUPON DEPARTURE FROM ROOFTOP PAD, NR 1 ENGINE TORQUE EXCEEDED 86.4 PERCENT AND NR 2 ENGINE TORQUE WAS NEAR ZERO WITH DECREASING RPM. ENDED UP THE ENG RIGGING NEEDED TO BE ADJUSTED.SDR HAIW6HR0087Panel Assy · crackedPANEL ASSY IS CRACKED. APPROX. 10 INCH CRACK STARTING @ R/H AFT CORNER GOING FOWARD AND TOWARDS THE LEFT. THIS CRACK HAPPENED DUE TO STA. 233 FRAME ASSY. P/N: 222-031-503-101 CRACKING. PERFORMED BHT FIELD REPAIR PROCEDURE 96R1-037, D.O.Y. S.O.C. SERIAL # ASDR HAIW6HR0086Roof · crackedPART IS CRACKED. ROOF WAS CRACKED DUE TO FRAME ASSY P/N: 222-031-503-101 (STA 233) CRACKING. INSTALLED STRAP DOUBLER P/N: 222-031-517-179 I/A/W BHT TB 222U-91-56, DATED 1-15-91.SDR HAIW6HR0085Frame Assy · crackedFRAME ASSY IS CRACKED. CRACKED @ R/H CORNER THRU FASTNER HOLES. PERFORMED REPAIR I/A/W BHT FIELD REPAIR PROCEDURE 96R1-036 REV. A D.O.T. S.O.C. SERIAL # A4753, DATED 3-19-97.SDR HAIW6HR0056Flexure · brokenPART IS BROKEN. RUBBER IS SEPERATED FROM END FITTINGS. RETURNED TO MANU FOR CREDIT ( REQUEST REPLACEMENT PART)SDR HAIW6HR0055Flexure · brokenPART IS BROKEN. RUBBER IS SEPERATED FROM END FITTINGS.SDR HAIW6HR0050Pump · worn excessivelyPUMP IS WORN EXCESSIVELY. PUMP LEAKS AT SHAFT SEAL. PUMP HAS ONLY BEEN INSTALLED 1 MONTH. BHT P/N: 222-380-009-103. . REPLACED WITH SERVICEABLE UNIT.SDR 96ZZZX826Torque Sensor · failedMAST TORQUE METER FAILED AFTER 604.9 HOURS IN SERVICE. SUBMITTER STATES EXPERIENCING FREQUENT SENSOR FAILURES.SDR 96ZZZX1766Isolation Mount · brokenISOLATION MOUNT IS BROKEN. THREADED BUSHING THAT ROD END ASSY THREADS INTO IS SEPARATED FROM ELASTOMERIC MATERIAL. DATE OF MANUFACTURE OF THIS PART WAS 5-29-93.
Other aircraft with N415MA · 2
The FAA can assign a mark to another aircraft once a registration is cancelled. N415MA is registered now to the first aircraft listed.