Service difficulty reports · 15
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR ASMF201608008Window · crackedCAPTAIN REPORTED THAT DURING CRUISE, THE RT SIDE WINDOW HEAT WITH FAULT CODE 304 022 42 DUE TO A CRACK ON THE LOWER RT CORNER WITH CORRECT CABIN PRESSURE. MAINTENANCE REPLACED THE RIDE SIDE OPERABLE WINDOW IAW AMM 56-11-02, TESTED CORRECT.SDR ASMF201501011Generator · failedCAPTAIN REPORTED THAT AFTER START ENGS APPEARED THE EICAS MSG LT BACK UP GEN OUT OF SERVICE. PERFORMED FIM 24-20 TASK 811 PROCEDURE, SHOWING FAILURE CODE 24-46000. THE BACK GEN WAS DEFERRED IAW MEL 24-25-01A CAT C. REPLACED THE BACK GEN IAW AMM 24-25-01, TESDR ASMF201311223002Warning System · false activationAIRCRAFT PERFORMED AN UNSCHEDULED LANDING AT LIM DUE TO EICAS MESSAGE WXR SYS. MX PERSONNEL PERFORMED THE AIR, GND INTERFACE TEST IAW AMM 34-43-00, NOT CONFIRMING THE FAILURE & DELETING FAILURE MESSAGE, THE WXR SYS TEST WAS PERFORMED IAW AMM 34-43-00, TESTED SDR ASMF201312005Engine · malfunctionedCAPTAIN REPORTED THAT DURING TAKEOFF, THE RT ENG REACHED 1031 CELSIUS DEGREES OF EGT FOR AROUND 2 SECONDS. PERFORMED RT ENG INSPECTION WITH EGT PARAMETERS WITHIN OPERATION LIMITS IAW AMM 71-00-00 & ENG EXCEEDANCE CHECK IAW AMM 71-00-00, TESTED CORRECT.SDR ASMF201308016Fairing · damagedCAPTAIN REPORTED THAT DURING LANDING ROLL, ACFT HAD A BIRD STRIKE ON RT ENGINE. MX PERSONNEL PERFORMED A BIRD STRIKE CONDITIONAL INSPECTION IAW MM 05-51-18, DETECTING RT ENGINE REVERSER CASCADE SEGMENT NR 8 DAMAGED AND OGV FAIRING WITH SCRATCHES. INSPECTIONSDR ASMF201308006Structure · damagedDURING ROUTINE CHECK, LIGHTNING STRIKE IN NOSE AND MLG. MAINTENANCE PERSONNEL PERFORMED A LIGHTNING STRIKE INSPECTION IAW MM 05-51-19, DETECTING VHF ANTENNA NR 2 WITH DAMAGE OUT OF LIMIT, THREE BURNS IN THE FWD LEFT NLG DOOR AND TWENTY BURNS IN THE LT MLG DOOSDR ASMF201303017Actuator · leakingDURING TRANSIT CHECK, A HYD LEAK WAS DETECTED ON AFT REAR SPAR OF LT WING. MX PERSONNEL PERFORMED AN INSPECTION DETECTING HYD LEAK IN SPOILER ACTUATOR NR 3, SO THE ACTUATOR WAS REPLACED IAW AMM 27-61-08 AND ADJUSTMENT AND TEST WERE PERFORMED IAW AMM 27-61-00,SDR ASMF201207001Skin · puncturedDURING PUSH BACK, THE LT WING L/E WAS HIT BY A MOBILE STAIRWAY CAUSING A HOLE OF 8.0" LONG, 4.0" WIDE. INSPECTION PERSONNEL EVALUATED THE DAMAGED AND FOUND OUT LIMITS IAW SRM 57-41-00. MX ISSUED THE NON ROUTINE CARDS A0190507 AND A019506. THE MID FAIRING ASSDR ASMF201012005Sensor · damagedACFT PERFORMED AN UNSCHEDULED LANDING, DURING CRUISE THE ENG OIL FILTER RT LIGHT TURNED ON WITH AN OIL TEMP INDICATION OF 60 CENTIGRADE DEGREES AND OIL PRESSURE INDICATION OF 60 PSI; THE EICAS MESSAGES ENG OIL FILT R AND MX MESSAGES 79-31452, 79-31-31462 AND 7SDR ASMF201008002Pressure Sensor · damagedACFT RETURNED OF FLIGHT DUE TO DURING CLIMB, EICAS MESSAGE AND LIGHT TURNED ON OF ENG OIL FILTER L WAS SHOWN. THE FLIGHT CREW PERFORMED THE QRH ENG OIL FILTER L, R PROCEDURE, CONFIRMING THE FAILURE. MX PERSONNEL REPLACED THE LT OIL DIFFERENTIAL PRESSURE SENSORSDR ASMF20100405Compressor · damagedDURING A BORESCOPE INSP OF THE HPC AND HPT MODULES OF RT ENGINE WERE DETECTED 41 BLADES OF HPC 8TH STAGE AND 23 BLADES OF 9TH STAGE WITH TEARS, NICKS, BENDS AND MISSING MATERIAL FROM THE LEADING TO THE T/E. OPENSDR ASM2008F00000Warning System · malfunctionedACFT REJECTED TAKEOFF AT 80 KNOTS DUE TO THE E/E COMPARTMENT LIGHT TURNED ON. MAINTENANCE PERSONNEL PERFORMED DOOR LIGHT TEST IAW MM 62-71-00, ALL CORRECT. THE HIGH ENERGY STOP INSPECTION WAS PERFORMED IAW MM 05-51-14, ALL CORRECT. (S)SDR ASMF200801003Slat · damagedDURING TAXING, AC HIT WITH LT SLAT NR 1 ON THE LT WING OF THE AIRCRAFT REGISTRATION N774AM. DETAILED INSPECTION WAS PERFORMED ON LT WING TIP DETECTING A STRUCTURAL DAMAGE ON SLAT NR 1 OF 17 INCHES LENGTH AND 11 INCHES WIDTH, OUT OF LIMITS, LOCATED BETWEEN STATSDR ASMF200711004Engine · damagedCAPTAIN REPORTED THAT AT 39,000 FEET, LEFT ENGINE STALLED, DESCENDING TO 27,000 FEET WITH OSCILLATIONS IN N1 AND N2 WITH ENG CONTROL L AND ENG EEC C1 L MESSAGES, LANDING AT GRU. AT GRU, TECHNICAL PERSONNEL CONFIRMED THE MESSAGES AND PERFORMED FIM 71-05 TASK 8SDR ASMF200710005Engine · overtempCAPTAIN REPORTED THAT DURING TAKEOFF RUN THE LT ENGINE EGTS INDICATION EXCEEDED RED DIAL; CAPTAIN REDUCED THE THRUST RECOVERING NORMAL INDICATIONS. AT CDG, MAINTENANCE DETERMINED THAT EXCEED WAS WITHIN LIMITS IAW MM 71-00-00-613, REQUIRING BOROSCOPIC INSPECTIO
Other aircraft with N746AM · 1
The FAA can assign a mark to another aircraft once a registration is cancelled. N746AM is registered now to the first aircraft listed.