Service difficulty reports · 7
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR BUEA20160219001Fadec · faultyWHILE AT CRUISE ALTITUDE FL34 & MACH .76, THE NR 2 ENG LOST POWER & N1 ROLLED BACK. LOST APPROX 10% N1 POWER & NO EICAS MSGS DISPLAYED. THE LOSS OF POWER LASTED APPROX 3 - 4 SECONDS. N1 POWER WAS SET AT APPROX 86%. ACFT CONTINUED ON AS FILED, LANDING WAS USDR BUEA20160205002Retaining Nut · unsecureAIRCRAFT DEPART AFTER RTS & FLEW ONE SUCCESSFUL LEG & ON THE SECOND LEG THE CAPTAIN REPORT EICAS MSG E2 CTL FAIL, WHILE IN FLIGHT & AFTER LANDING EICAS MSG E2 NO DISP. FIM WAS PERFORMED & THE TECHNICIAN DISCOVERED THE PMA ROTOR RETAINING NUT CAME OFF & DESTROSDR BUEA20160205001Fadec · malfunctionedAIRCRAFT DEPARTED DURING DAYLIGHT HOURS & WAS CLIMBING THROUGH 6500 FT, ACCELERATING THROUGH 21KTS, WHEN THE NR 2 ENG ROLLED BACK & FAILED. THE CREW DECLARED AN EMER & RETURNED BACK. ACFT HAD AN OVERWEIGHT LANDING & LANDING WAS ALSO UNEVENTFUL WITH 37 PAXS OSDR BUEA20150227001Transducer · failedDURING CLIMB TO FL32, NOTICE A REDUCTION IN AIRSPEED AT FL 30. NOTICED A FLUX IN NR 1 ENG ITT, N1 & N2, 91 TO 88%. PILOT LEVELED OFF AT FL32 & REDUCED POWER SETTING, POWER BACK & NOTICED A LARGER ITT, N1, N2 FLUX. WEATHER WAS VFR CLEAR WITH NO ICING. PILOSDR CHQA20140506130Light · brokenDURING INSPECTION, THE EMERGENCY FLOOR LIGHT STRIP AT THE EMERGENCY EXIT WAS FOUND TO BE BROKEN. REPLACED THE EMERGENCY LIGHT FLOOR STRIP AT THE EMERGENCY EXIT. OPERATIONAL CHECKS WERE GOOD WITH NO FURTHER DEFECTS NOTED.SDR CHQA20140314084Switch · faultyCREW REPORTED THAT THEY RECEIVED A PITCH TRIM MAIN INOPERATIVE MSG IN FLIGHT. THE CREW RETURNED TO FIELD & LANDED WITHOUT INCIDENT. MX REPLACED THE AUTO PILOT DISCONNECT SWITCH. OPERATIONAL CHECKS WERE GOOD WITH NO FURTHER DEFECTS NOTED.SDR CHQA200500055Static Inverter · inoperativeEMERGENCY LIGHT ON COCKPIT PARTITION EXIT MARKER IS INOP. REMOVED AND REPLACED STATIC INVERTER NR 1 IAW EMB 145 AMM 33-50-11. OPS CHECK GOOD.