Boeing 747-47UF

Service difficulty reports · 3,116

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duckdb -csv -c "SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy
  FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet'
  WHERE aircraft_model_key = '74747UF'
  ORDER BY difficulty_date DESC"

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SDR UIEA200600126Terminal · looseRIGHT WINDSHIELD ELEC CONNECTION ON LOWER RIGHT CORNER SMOKING. SHUT OFF PER NON NORMAL CHECK LIST. FOUND LOWER TERMINAL LOOSE WITH SIGN OF ARCHING ON INSULATION. RE-TORQUE IAW MM 56-11-01. PERFORMED INTERIM REPAIR ON WIRE INSULATION IAW SWP 20-10-13 (AIRWJun 3, 2006 · N418MC · Boeing 74747UF · Windshield/Door Rain/Ice RemovalSDR UIEA200600118Lever · brokenSEVERE COMPRESSOR STALL ON ENGINE NR 4 WITH FULL CLIMB POWER AT 6000 FEET ON CLIMBOUT FROM DXB. ENGINE NR 4 ROLLED BACK TO IDLE, OVERTEMP EGT INDICATION. NR 4 ENGINE SHUT DOWN. FUEL JETTISON ACCOMPLISHED. UNEVENTFUL SMOOTH AUTO LAND RWY 30R AT 299.0 TONS. May 22, 2006 · N415MC · Boeing 74747UF · Turbine Engine Compressor SectionSDR UIEA200600117Skin · crackedDURING WALKAROUND, FOUND DAMAGE ON LEFT INBOARD TRAILING EDGE ELEVATOR AS PER XEO NR 55-052106. TEMP REPAIR ACCOMPLISHED. REPEAT INSPECTION SCHEDULED EVERY FLIGHT. PERMANENT REPAIR TO BE ACCOMPLISHED AFTER 10 FLIGHT CYCLES. TRANSFERRED TO DMI PAGE 71072, DMay 22, 2006 · N498MC · Boeing 74747UF · Elevator, Plate/SkinSDR UIEA200600116Seat Track · tornMAIN DECK SEAT TRACK BETWEEN STATION 1430 AND 1442, LBL 99, 12 INCH SECTION OF SEAT TRACK WAS TORN AND DAMAGED. SEAT TRACK WAS PERMANENT REPAIRED PER SRM 53-00-52 FIG 201, REPAIR 6 AND REFERENCE XEO 53-051206.May 12, 2006 · N496MC · Boeing 74747UF · Fuselage, Seat/Cargo Attach FittingsSDR UIEA200600070Engine · damagedNR 1 ENGINE HAD EGT SPIKE TO 943* AT 5,000 MSL POWER REMAINED LOW THROUGHOUT CLIMB AND CRUISE. NR 1 N1- 20% BELOW 2-3-4. N2- 8-10% BELOW 2-3-4, EGT 50*-80* HOTTER THAN 2-3-4. N2 VIB 5.0 2-3-4 WERE 1.1-1.2. JFK NOTIFIED. NR 1 ENGINE SHUT DOWN AS PER JFK INSTApr 8, 2006 · N408MC · Boeing 74747UF · Engine (Turbine/Turboprop)SDR UIEA200600069Cooling Fan · odorELECTRICAL BURNING SMELL ON TAXI IN, E/E BAY. AFTER DEBRIEF, STS EE CLNG SUP FAN APPEARED. NIL STOCK. ITEM TRANSFERRED TO DEFERRED DMI M06-032 PAGE 63427 PER MEL 21-58-06. CAT "C", PART ON ORDER.Apr 6, 2006 · N499MC · Boeing 74747UF · Air Distribution FanSDR UIEA200600020Cooling Fan · contaminatedON TRANSIT FLIGHT CREW AND ENGINEERING CREW REPORT BURNING SMELL THROUGHOUT FLIGHT DECK AND NOTICEABLE IN MAIN EQUIPMENT CENTER AND FORWARD CARGO. DEFECT INVESTIGATED, SMELL ISOLATED TO EQUIPMENT COOLING SUPPLY FAN/CENTER RISER FILTER OIL CONTAMINATION. BOTHMar 9, 2006 · N412MC · Boeing 74747UF · Air Distribution FanSDR UIEA200600018Skin · delaminatedDURING A-4 CHECK, LEFT HAND INBOARD T/E MID FLAP HAS IMPACT DAMAGE WITH DELAM ON LOWER AFT INBOARD SURFACE AS MARKED. REPAIR CARRIED OUT IAW SRM 51-70-06 AND SRM 57-53-01.Mar 7, 2006 · N416MC · Boeing 74747UF · Trailing Edge FlapsSDR UIEA200600015Tire · failedNR 4 MAIN WHEEL BLOWN OUT. REPLACED NR 3 AND NR 4 WHEEL ASSY IAW MM 32-42-01. PERFORMED CHAPTER 5-51-25 AND 5-51-20 INSPECTION. ALSO PERFORMED 5-51-34 AND DEACTIVATED NR 4 BRAKE AS A PRECAUTION.Mar 3, 2006 · N498MC · Boeing 74747UF · TireSDR UIEA200600014Tire · separatedON ARRIVAL FOUND NR 4 MAIN WHEEL TIRE TREAD CAP MISSING. DUE TO EXTENSIVE DAMAGE TO THE LEFT INBOARD AFT FLAP MID FLAP AND FORE FLAP PERFORMED XEO 57-022706-1 57-022706-1 AND 5722706-2.Mar 1, 2006 · N497MC · Boeing 74747UF · TireSDR UIEA200600013Window · crackedPRIOR TO DEPARTURE L1 WINDOW OVERHEATED AND CRACKED.Mar 1, 2006 · N497MC · Boeing 74747UF · Flight Compartment WindowsSDR UIEA200600011Tire · tornFOUND ON ARRIVAL AT GOT LOSS OF NR 4 TIRE THREAD. INSPECTION OF A/C REVEALED DENTS TO THE L/E OF THE FORE, MID AND AFT FLAPS DIRECTLY BEHIND THE THREAD LOSS OF THE TIRE AND OTHER RELATED DENTS TO THE LOWER WING T/E FIBERGLASS PANEL AND UNDERSIDE OF FLAP PANELFeb 22, 2006 · N497MC · Boeing 74747UF · TireSDR UIEA200500167Skin · damagedDURING TRANSIT CHECK, FOUND AIRCRAFT DAMAGE AT AFT FUSELAGE NEAR STA 2577.75. REPAIR SCHEME FROM SRM 53-00-01 REPAIR 1 AND 2 , H/F EDDY CURRENT INSPECTION, SIGNED ON WORK PERFORMANCE STATEMENT. REPAIR TO CAT B STANDARD, TO BE INSPECTED EVERY 1500 HOURS. REPOct 19, 2005 · N493MC · Boeing 74747UF · Fuselage Main, Plate/SkinSDR UIEA200500118Pin · migratedDAILY CHECK, ON WALK AROUND, FOUND LT BODY GEAR JURY STRUT UPPER ATTACHMENT PIN FOUND MIGRATED. RETENTION BOLT AND UPPER CAP STILL WITH CONDUIT. LOWER CAP AND NUT FOUND IN ADJACENT STRUCTURE. ON WALKAROUND, FOUND RT BODY GEAR JURY STRUT UPPER ATTACHMENT RETAug 25, 2005 · N409MC · Boeing 74747UF · Main Landing GearSDR P5CA0501378Fmc · failedCREW REPORTED RT FMC INOP. REPLACED RT FMC- MM 34-61-01. ALL OPS NORMAL.Jul 10, 2005 · N496MC · Boeing 74747UF · Flight Management Computing Hardware SystemSDR UIEA200500058Hmu · unserviceableAFTER ROTATION UP TO 1000 FT, NR3 ENGINE N1 WOULD SURGE (ROLL BACK) BETWEEN 101.5 AND 98.0 N1. AT THRUST REDUCTION ALTITUDE, THE SURGE WOULD STOP. ALL PHASES OF FLIGHT WERE NORMAL. AFTER LANDING, DID A POWER RUN UP AND THE SAME AS ABOVE OCCURRED, NO EICAS OApr 26, 2005 · N409MC · Boeing 74747UF · Fuel Controlling SystemSDR UIEA200500059Fuel Filter · unserviceableAIR TURN BACK. STATUS MESSAGE: ENG 3 FUEL FILTER. THE AIRCRAFT RETURNED TO DEPARTURE. REMOVED AND REPLACED FUEL FILTER IAW MM, LEAK CHECKED SATISFACTORY. (K)Apr 25, 2005 · N499MC · Boeing 74747UF · Engine Fuel DistributionSDR UIEA200500060Connector · contaminatedON TAXI OUT NR2 ENGINE OIL PRESSURE DROPPED BELOW RED LINE-ENGINE SHUTDOWN. T/S IAW MM. CLEANED OIL PRESSURE TRANSMITTER CONNECTOR. ENGINE GROUND RUN PERFORMED ALL WORKING NORMAL. (K)Apr 22, 2005 · N496MC · Boeing 74747UF · Engine Oil PressureSDR UIEA200500062Seat Track · damagedMAIN DECK SEAT TRACK DAMAGED AT SAT 1810 NEXT TO SIDE CARGO DOOR. SEAT TRACK REPAIRED IAW SRM. (K)Apr 21, 2005 · N493MC · Boeing 74747UF · Fuselage, Seat/Cargo Attach FittingsSDR UIEA200500061Support Beam · damagedSTA 1810 SIDE CARGO DOOR SILL SUPPORT BEAM DAMAGED AT ROLLOUT SAFETY STOPS. FORM 8100-9 SHOWS THAT THE DAMAGED AREA WAS TRIMMED OUT AND A REPAIR ANGLE IS INSTALLED. (K)Apr 21, 2005 · N493MC · Boeing 74747UF · Fuselage Main, StructureSDR UIEA200500054Nose Cowl · dentedENGINE 1 NOSE COWL AT 4 O`CLOCK POSITION DENT AT LIP 5.6 INCHES X 4.2 INCHES X 0.224 INCH. DENTED AREA TRIMMED OUT AND SRM WAS PERFORMED. INSTALLED DOUBLER AND FILLER IAW SRM USING BLIND .1562 FASTENERS. (K)Apr 21, 2005 · N412MC · Boeing 74747UF · Nacelle/Pylon, Plate/SkinSDR UIEA200500053Skin · dentedSTA 2660-2680, 2 DENTS FOUND ON EXT SKIN. REPORTED DENT WAS REPAIRED IAW SRM. PERFORMED HFEC INSP, NO CRACKS WERE FOUND. AFTER SECONDARY INSP FOUND DENT, CREASE, AND CHAFING 2.5 INCH X 1.5 INCH X 0.050 INCH. DOUBLER REPAIR PERFORMED IAW SRM. (K)Apr 21, 2005 · N412MC · Boeing 74747UF · Fuselage Main, Plate/SkinSDR UIEA200500052Skin · dentedSTA 1980-2000, STR 42-44, RT (2 EA) DENT (A) AND (B) WERE FOUND ON THE EXT FUSELAGE. DENT (A) STA 1980-2000, STR 42-43, RT D=0.09, W=1.15 INCH, L=3.8 INCH. DENT (B) STAT 1980-2000, STR 43-44, RT D=0.051, W=1.18, L=1.54. THE DAMAGED AREA TRIMMED OUT. A REPApr 20, 2005 · N412MC · Boeing 74747UF · Fuselage Main, Plate/SkinSDR UIEA200500051Door · malfunctionedRT BODY GEAR DOOR OPENED AFTER RETRACTION WHEN GEAR LEVER PLACED IN OFF POSITION. STATUS MSG GEAR DOOR GEAR MONITOR. GEAR PINS INSTALLED. PRESSURIZED HYD SYSTEM. OPS CHECKED DOOR IAW MM. ALL INDICATIONS OK IN ALL HANDLE POSITIONS. RT BODY GEAR DOOR DID NApr 13, 2005 · N416MC · Boeing 74747UF · Landing Gear Door Retract SectionSDR UIEA200500050Brake · damagedEICAS MESSAGE BRAKE TEMP AFTER LANDING ROLLOUT IN MEL, SMALL FIRE NOTICED ON NR 7 BRAKE AFTER AIRCRAFT WAS PARKED. IT WAS QUICKLY EXTINGUISHED WITH A DRY FIRE EXTINGUISHER AGENT. INSPECTION CARRIED OUT. MAX TEMP INDICATION 5, CMC MSG 32127. NO ITEMS NOTED.Apr 12, 2005 · N409MC · Boeing 74747UF · Landing Gear Brake SystemSDR UIEA200500044Tire · blownFLIGHT (90 K FUEL DUMPED). AT ABOUT V1 SPEED, DURING T/O GOT BRAKE LIMITER AND ANTI SKID EICAS FOLLOWED BY GEAR CONFIG AND BODY GEAR STEERING WARNING, AND AFTER LIFT OFF GEAR TILT EICAS. LANDED BACK IN TPE AFTER DUMPING FUEL AND COORDINATING WITH GCC. NR 11Mar 31, 2005 · N493MC · Boeing 74747UF · TireSDR UIEA200500032Module · failedAFTER TAKEOFF GEAR LEVER WOULD NOT GO PAST OFF POSITION. GEAR MONITOR STATUS MESSAGE. NO FUEL DUMPED. REMOVED AND REPLACED LANDING GEAR MODULE PER AMM 32-31-01 P/N OFF 257U0002-15 S/N OFF D00574. AIRCRAFT IN AIR MODE PER 32-09-02. PERFORMED ALL TESTS PER Mar 22, 2005 · N497MC · Boeing 74747UF · Landing Gear Retraction/Extension SystemSDR UIEA200500031Sequence Valve · malfunctionedFLT 862 - AFTER TAKEOFF GEAR LEVER WOULD NOT GO PAST OFF. LOCK OVERRIDE WOULD NOT RELEASE. EICAS MESSAGE GEAR DISAGREE, EICAS MESSAGE GEAR MONITOR, STATUS MESSAGE GEAR DISAGREE, STATUS MESSAGE GEAR MONITOR. NO FUEL DUMPED. LUBRICATED LANDING GEAR LEVER LOCMar 22, 2005 · N497MC · Boeing 74747UF · Landing Gear Retraction/Extension SystemSDR UIEA200500020Proximity Sensor · malfunctionedAFTER TAKEOFF GEAR CLOSED NORMALLY; INDICATED CLOSED GEAR LEVER SELECTED TO OFF; VIBRATION FELT, EICAS MSG (GEAR DOOR) AND SYNOPTIC INDICATED LT BODY GEAR DOOR NOT CLOSED. NNC 14.5 ACCOMPLISHED AND FLIGHT CONTINUED WITH GEAR LEVER IN UP POSITION. PERFORMED VMar 15, 2005 · N493MC · Boeing 74747UF · Landing Gear Position and WarningSDR UIEA200500012B-Nut · looseSHORTLY AFTER TAKEOFF OIL QTY DROPPED TO ZERO. DURING CLIMB-OUT, OIL PRESSURE DROPPED EVENTUALLY TO SIX PSI. NR 4 ENGINE WAS SHUT DOWN AS OIL PRESSURE TO 10 PSI. OIL PRESSURE REMAINED AT 6 PSI, N1 AT 25 PERCENT AND N2 BETWEEN 17 AND 21 PERCENT FOR DURATION Mar 3, 2005 · N409MC · Boeing 74747UF · Turbine Engine Oil SystemSDR UIEA200500013Hmu · malfunctionedPVG/ANC - NR 2 ENGINE FAILED DURING CRUISE. EICAS AND STATUS MSG. ENGINE 2 FUEL VALVE, ENGINE 2 CONTROL. WITH NO ACTION ENGINE RESTARTED IN APPROX 90 SECONDS. FOUND ACTIVE FAULT 72417 PERFORMED WIRING CHECKS PER CMCS MESSAGE INDEX. REPLACED ECU NR 2 (P/N Feb 24, 2005 · N492MC · Boeing 74747UF · Fuel Controlling SystemSDR UIEA200500009Engine · vibrationFLT GT 9991 - ENGINE NR 2 VIBRATION OCCURRED DURING CLIMB-OUT AND INTERMITTENTLY DURING FLIGHT. AFTER 4 HOURS FLIGHT TIME THE LEVEL OCCASIONALLY EXCEEDED 5.0, NR 3 EGT AVERAGED ABOUT 18 DEG HIGHER THAN THE OTHER THREE. REMOVED AND REPLACED NR 3 ENGINE IAW ATFeb 22, 2005 · N498MC · Boeing 74747UF · Engine (Turbine/Turboprop)SDR UIEA200500010Flap · damagedDURING WALK AROUND, MAINTENANCE FOUND DAMAGED TO LEFT OUTBOARD MIDFLAP T/E. REMOVED AND REPLACED LEFT OUTBOARD MIDFLAP IAW TASK CARD 27-51-04-404-025 REV 17 OCT 2003 S/N OFF, 000484. (M)Feb 22, 2005 · N493MC · Boeing 74747UF · Trailing Edge FlapsSDR UIEA200500003Skin · delaminatedFLIGHT CT 603, PIK-LUX 08 JAN, 2005 - IB LOG ITEM, LT OB MID FLAP PANEL DELAMINATED. MAINTENANCE PICK-UP ITEM. DURING FLAP REPLACEMENT FOUND IB CARRIAGE ASSY CORRODED. (LEVEL 1) REPLACED LT OB MID-FLAP, MM 27-51-04, REF LOG PAGE 544103. REPLACED IB CARRIAJan 19, 2005 · N499MC · Boeing 74747UF · Trailing Edge FlapsSDR UIEA200400208Arm · brokenDURING ACCOMPLISHMENT OF ENGINE CONDITION MONITORING ALERT ITEM NR 2004P093. ENGINE NR 1 VISUAL INSPECTION OF STG 5 ACTUATION HARDWEAR, FOUND ONE VSV LEVER ARM MISSING AT 11 OCLOCK POSITION AMM. REPLACED ENGINE NR 1 IAW WORK CARD NR A717101GT1 AND MM. PERFODec 28, 2004 · N409MC · Boeing 74747UF · Compressor Bleed ControlSDR UIEA200400207Windshield · crackedMAINTENANCE PICKED UP ITEM. CAPTAINS WINDSHIELD CRACKED (L1). REPLACED L1 WINDSHIELD MM. CHECKS OK. (K)Dec 27, 2004 · N497MC · Boeing 74747UF · Flight Compartment WindowsSDR UIEA200400199B-Nut · looseEICAS MESG; ENGINE NR 1 OIL PRESSURE. CONFIRMED OIL PRESSURE BELOW 10 PSI. SHUTDOWN NR 1 ENGINE. CONFIRMED NR 1 ENGINE OIL QTY LOW, AND ON INSPECTION FOUND B-NUT LOOSE FROM OIL TUBE CONNECTED TO FRONT OF MAIN GEAR BOX AT 6 O’CLOCK POSITION. SERVICED ENGINEDec 7, 2004 · N412MC · Boeing 74747UF · Turbine Engine Oil SystemSDR UIEA200400188Transmitter · failedNR 3 ENGINE OIL PRESSURE DROPPED TO RED LINE 30 MINUTES FROM DEPARTURE. ENGINE SHUTDOWN IAW CHECK LIST. REMOVED AND REPLACED THE OIL PRESSURE TRANSMITTER IAW AMM 79-32-01 AND REPLACED THE OIL PRESSURE SWITCH IAW AMM 79-33-01.Nov 8, 2004 · N498MC · Boeing 74747UF · Engine Oil PressureSDR UIEA200400185Engine · malfunctionedNR 4 ENGINE NOT MAKING TO THRUST. (RTO) REJECTED TAKE OFF DUE TO NR 4 ENGINE NOT MAKING TAKE OFF THRUST. PERFORMED POWER ASSURANCE CHEDK (TEST 10), ALL WITHIN LIMITS IAW MM 71-00-00.Oct 16, 2004 · N408MC · Boeing 74747UF · Engine (Turbine/Turboprop)SDR UIEA200400183Anti-Ice Valve · contaminatedGT9012 TLV/CAI: AUTO NACELLE ANTI-ICE. (ATB) APPROX 8,000 CLEAR, TEMP +27C, AUTO NACELLE ANTI-ICE COMMANDED ANTI-ICE ON. ICING WING ALSO DISPLAYED. WHEN NAC ANTI-ICE VALVE IN OFF, NAI VALVE 1,2,3 AND 4 CAME ON. ALL FOUR VALVES WERE STUCK OPEN BY CHECKLIST. Oct 9, 2004 · N498MC · Boeing 74747UF · Air Intake Anti/De-Ice SystemSDR UIEA2004118Skin · dentedDENT FOUND IN THE FUSELAGE SKIN RT SIDE AT STATION 2596. ACCOMPLISHED DENT REPAIR ON FUSELAGE SKIN RT SIDE STATION 2596 STRINGER 42 AREA IAW SRM 53-00-01 FIG 215 DETAIL I. (M)Oct 6, 2004 · N498MC · Boeing 74747UF · Fuselage Main, Plate/SkinSDR P5CA0401229Connector · dirtyNR 2 ENGINE OIL ITEM INDICATION. CLEANED ELECTRICAL CONNECTOR ON OIL TEMPRATURE SENSOR, NR 2 ENGINE INDICATION OK, IAW AMM 71-00-00.Sep 28, 2004 · N496MC · Boeing 74747UF · Electrical ConnectorsSDR UIEA200400170Smoke Detector · malfunctionedIMMEDIATELY AFTER TAKEOFF 'EICAS MSG'. WITH SMOKE DETECTOR MAKING LOUD BEEPING NOISE. AFTER 1 HOUR EICAS MSG WENT AWAY AND SMOKE DETECTOR STOPPED BEEPING, NO SMOKE DETECTED. ALL ASSOCIATED DUCTING CHECKED FROM CREW REST AREA TO STATION 950. NIL ABNORMALITISep 20, 2004 · N492MC · Boeing 74747UF · Smoke DetectionSDR UIEA200400158Limiter · malfunctionedILLUMINATION OF EICAS ANTI-SKID INTERMITTENT CAUTION WITH LONG HISTORY. REMAINS ILLUMINATED FOR PERIODS OF ONE MINUTE AND MORE UP TO TEN MINUTES PERIODS STATUS MSG. ANTI-SKID BRAKE LIMITER EXTINGUISHED DURING DESCENT, BUT INTERMITTENT EICAS REMAIN THROUGH ROSep 17, 2004 · N497MC · Boeing 74747UF · Brake Anti-Skid SectionSDR P5CA0401185Transmitter · failedLOSS OF ENGINE NR 1 OIL PSI INDICATION ON LWR EICAS DURING CLIMB, NO EICAS MSG RECD OIL INDICATION HAD BEEN NORMAL THROUGHOUT TAXI. REPLACED NR 1 OIL PRESSURE TRANSMITTER PER MM 79-32-01. OPS CHECK ON RUN OK.Sep 5, 2004 · N496MC · Boeing 74747UF · Engine Oil PressureSDR UIEA200400153Control Panel · dirtyHKG/ICN - AFTER TAKEOFF CLIMBING THROUGH 13,000 FEET, HAD INDICATION OF MAIN DECK CARGO FIRE. NO EICAS, NO WARNING BELL, JUST OVERHEAD SWITCH. IT WAS RAINING VERY HARD AND HIGH MOISTURE CONTENT IN AIRCRAFT. DEEP CLEANED MAIN DECK CARGO FIRE SWITCH. PERFORMAug 28, 2004 · N409MC · Boeing 74747UF · Fire DetectionSDR UIEA200400151Turbine Blades · missingON TAKEOFF ROTATION, ENGINE NR 3 HAD 2 COMPRESSOR STALLS. N1 ROLLED BACK AND RECOVERED, EGT REACHED 950 DEGREES CELSIUS. ON CLIMB-OUT AND CRUISE ENGINE OPERATED NORMAL. PERFORMED TEST 72-00-00-206-050-020. STALL INSPECTION, FOUND HPC STAGE 6, THREE BLADES Aug 24, 2004 · N409MC · Boeing 74747UF · Turbine SectionSDR UIEA200400146Actuator · malfunctioned- REJECTED TAKEOFF DUE TO WARNING BODY GEAR STEERING CONFIGURATION. GEAR CONTROL ON TAKEOFF ROLL AT 30 KNOTS. PERFORMED RECHECK FOR CORRECT DE-ACTIVATION, ALL CHECK OK. REMOVED BLANKS ON DE-ACTIVATED ACTUATOR. FOUND TRAPPED PRESSURE IN ACTUATOR. RELEASED Aug 12, 2004 · N497MC · Boeing 74747UF · Steering UnitSDR UIEA200400142Wheel · damagedHOT BRAKES ON LEFT WING GEAR AND LEFT BODY GEAR. INSPECTION OF AFFECTED WHEELS AND BRAKES CARRIED OUT TASK, 5-51-10-202-001. NR 1 AND NR 6 AXLE INSPECTED FOR HEAT DAMAGE, NONE EVIDENT TASK 05-51-10-202-001. (M)Aug 4, 2004 · N418MC · Boeing 74747UF · Wheel/Ski/FloatSDR P5CA0401129Warning Light · illuminatedAFTER PUSHBACK APU DUCT LEAIL STATUS MESSAGE DISPLAYED. OPENED MEL 49-11-1-1.Jul 28, 2004 · N496MC · Boeing 74747UF · Central Warning
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