FAA incident reports · 1
FAA accident and incident reports matched to this aircraft by N419MA and the event date: after October 4, 1997, when the previous aircraft’s registration ended, through this one’s cancellation.
Service difficulty reports · 5
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR QMLA2013061613079Unknown · odorON FINAL, CREW SENSED THE ODOR OF BURNED ELECTRICAL. THERE NO VISUAL INDICATIONS (SMOKE, FIRE OR SPARKS) OF ANY ELECTRICAL ISSUES. ALL COCKPIT INDICATIONS WERE NORMAL. ACFT WAS LANDED AND SHUTDOWN NORMALLY WITH NO FURTHER INDICATIONS. AIRCRAFT WAS THROUGHLSDR QMLA2012092512159Longeron · crackedDURING INSPECTION OF TAIL ROTOR ACTUATOR AND SURROUNDING AREA FOUND CRACK ON LONGERON ABOVE AND TO THE LT OF THE ACTUATOR.SDR QMLA2011092111094Engine · making metalNR 2 ENG CHIP LIGHT ILLUMINATED, FOUND MINOR DEBRIS ON GEARBOX CHIP DETECTOR AT 13137 ACFT TT. CLEANED DETECTOR IAW LTS 101 2.2MM CHAP 72-00-00, RETURNED ACFT TO SERVICE. NR 2 ENG CHIP LIGHT ILLUMINATED 2ND TIME INTERMITTENTLY WITH TURBINE CHIP LIGHT ALSO ILLSDR 47518022205Flexure · delaminatedSHORTLY AFTER TAKEOFF WHILE ACCELERATING THROUGH 40-50 KTS A MODERATE 1/1 WAS NOTED. IT CONTINUED TO WORSEN WITH AIR SPEED. I TURNED AROUND AT ABOUT 100 KTS. LOWERED COLLECTIVE, AND RETURNED TO BASE. THE SEVERITY OF THE VIBRATION LESSENED WITH LOWER COLLECTIVESDR 47518011705Line · rupturedTHE NR 1 HYD SYSTEM CAUTION LIGHT CAME ON. PRESSURE CHECKED AND WAS CONFIRMED TO BE AT ZERO. CYCLED SWITCH, MOVED PEDALS AND VERIFIED ACTUAL FAILURE, SO TURNED HYD SYSTEM #1 OFF, PROCEEDED TO FULLERTON AIRPORT AND MADE LANDING FROM A HOVER TO HELIPAD, NO PROBL
Other aircraft with N419MA · 2
The FAA can assign a mark to another aircraft once a registration is cancelled. N419MA is registered now to the first aircraft listed.