Boeing 747-87UF

Service difficulty reports · 1,102

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Query with SQL
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 = '74787UF'
  ORDER BY difficulty_date DESC"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR P5CA2015031700018Fire Warning · false activationDURING CLIMB, APPROXIMATELY 11,000', FIRE BELL SOUNDED FOR 2 SECONDS. NO FIRE OR SMOKE INDICATIONS. NO EICAS WARNINGS, ALERTS OR FIRE LIGHTS. REPEAT WRITE UP. FIRE BELL SOUNDED REPEATEDLY EVERY 30 SECONDS FOR 3 SECONDS WITH WHEEL WELL EICAS MESSAGE AND MASMar 12, 2015 · N857GT · Boeing 74787UF · Fire DetectionSDR P5CA2015031100016Fire Warning · false activationTWO TIMES DURING CRUISE FIRE BELL SOUNDED 1-2 SECONDS; NO FIRE OR SMOKE INDICATIONS, NO EICAS WARNING, ALERT OR FIRE LIGHTS. NO FAULTS NOTED IN CMC. RAN CMC GROUND TEST FIRE PROTECTION. TEST PASSED AND OPS CHECK NORMAL. REF AMM 26-11-00.Mar 10, 2015 · N857GT · Boeing 74787UF · Fire DetectionSDR P5CA2015030900014Unknown · unknownLOW SPEED RTO, ICN DEPT 33L AFTER T/O THRUST SET ACFT VEERED SHARPLY TO THE RT. EICAS MASTER WARNING CONFIGURATION GEAR CTR, MESSAGE. CHECKED PRESENT LEG, EXISTING FAULTS. NO MESSAGE FOUND. TESTED CONFIDENCE T/O WARNING, BODY GEAR STEERING. MAIN & NOSE TIREMar 7, 2015 · N857GT · Boeing 74787UF · Landing Gear SystemSDR UIEA2015030300160Skin · dentedDENT ON FUSELAGE SKIN AT STATION 516 BETWEEN STRINGER 35R - 36R. REPAIRED DAMAGE AREA IAW EI NO T2015A53B-390 REV 1. JOB COMPLETED & CONDITION CHECKED NORMAL.Mar 3, 2015 · N855GT · Boeing 74787UF · Fuselage Main, Plate/SkinSDR P5CA2015022300012Fire Warning · false activationDURING CLIMB OUT, FIRE BELL AURAL SOUNDED TWICE WITHOUT OTHER VISUAL WARNINGS. ENTRY 689531-3, 22FEB15. CHECKED CMC. NO MESSAGE FOUND IN PRESENT LEG, EXISTING FAULT HISTORY. C/W FIRE TEST IAW AMM 26-10-00 AND TEST PASSED.Feb 23, 2015 · N857GT · Boeing 74787UF · Fire DetectionSDR P5CA2015022300011Fire Warning · false activationAFTER LANDING FIRE BELL OF UNKNOWN ORIGIN. NO CURRENT FAULTS AT THIS TIME COMPLIED WITH CMC TEST IAW AMM 26-10-00. OPS CHECK GOOD.Feb 22, 2015 · N857GT · Boeing 74787UF · Fire DetectionSDR P5CA2015021300010Fire Warning · false activationON TAKEOFF WHEN FLAPS 1 SELECTED MOMENTARY FIRE BELL WITH MASTER WARNING LIGHT. NO CMC MESSAGE PRESENT. PERFORMED FIRE SYSTEM TEST PER AMM 26-10-00. TEST PASSED.Feb 11, 2015 · N857GT · Boeing 74787UF · Fire DetectionSDR P5CA2015021100009Fire Warning · false activationINTERMITTENT FIRE BELL WARNING WITH NO EICAS MESSAGE. NO CURRENT FAULTS AT THIS TIME. COMPLIED WITH CMC GROUND TEST IAW AMM 26-10-00. TEST GOOD.Feb 11, 2015 · N857GT · Boeing 74787UF · Fire DetectionSDR UIEA2015020100060Fan · defectiveNUMBER 1 PACK PRODUCES AN ODD SMELL AS IF THERE IS ELEC BURNING. VISUAL INSPECTION AT PACKS INLET & OUTLET AT PACK 1 BAY, NO ABNORMALITIES NOTED. REF ITEM 3 DETAILED INSPECTION ACCOMPLISHED & FOUND EE SUPPLY FAN AT FAULT. FAN DEACTIVATED & OPERATIONS CHECKFeb 1, 2015 · N855GT · Boeing 74787UF · Air Distribution FanSDR P5CA2015012000003Warning Message · illuminatedLOW SPEED AIR TURNBACK DUE TO MASTER CAUTION WITH VISUAL AND AURAL WARNING AT 35KTS. AFTER FOLLOWING COMPANY PROCEDURES NO LATCHED OR INDICATED EICAS MESSAGE. DEPARTURE NORMAL. NO CMC MESSAGES. PERFORMED TAKE OFF WARNING TEST AND PASSED IAW AMM 31-52-00.Jan 19, 2015 · N853GT · Boeing 74787UF · Central WarningSDR UIEA2015011400007Frame · brokenBROKEN CONDITION ON THE STATION 1600 LOWER FRAME UPPER CAP NEAR RBL 9. REPAIR DAMAGE IAW EI NO T2015A53B044.Jan 9, 2015 · N854GT · Boeing 74787UF · Fuselage Main, FrameSDR P5CA2014122600063Warning Message · illuminatedSTATUS MESSAGE GEAR TILT. EICAS MESSAGE GEAR TILT AFTER TAKEOFF, THEN EICAS MESSAGE GEAR TILT NO LONGER DISPLAYED, ATTENPTED GEAR RETRACTION, EICAS MESSAGE GEAR TILT RETURNED TO DOWN POSITION. PERFORMED PSEU CMC GROUND TEST IAW AMM 32-09-03 ALL TEST PASS, C/WDec 24, 2014 · N853GT · Boeing 74787UF · Landing Gear Retraction/Extension SystemSDR P5CA2014122000059Proximity Sensor · malfunctionedGEAR TILT EICAS MESSAGE. FOUND CMC CODE 32723 AND 32724; ACCOMPLISHED WIRING CHECK OF WIRES FROM PSEU TO THE SENSOR S2653 AND S2654 IAW WDM 32-61-15 AND WDM 32-61-16. NO FAULTS FOUND. SENSOR, S2653 AND S2654, REPLACED IAW AMM 32-61-12. OPS CHECK WAS GOOD.Dec 19, 2014 · N857GT · Boeing 74787UF · Landing Gear Position and WarningSDR P5CA2014111100053Structure · damagedDURING WALK AROUND CHECK, FOUND LOWER FORWARD CARGO DOOR DAMAGED AT LOWER FORWARD CORNER. INSPECTED AND FOUND CORNER BENT AND CRACKED. REPAIRED IAW SRM 52-30-01-2R-1, REPAIR 1.Nov 11, 2014 · N853GT · Boeing 74787UF · Cargo/Baggage DoorsSDR P5CA2014111100054Structure · damagedDURING WALK-AROUND CHECK, FOUND LOWER FORWARD CARGO DOOR DAMAGED AT AFT SIDE LOWER EDGE. INSPECTED AND FOUND LOWER AFT CORNER BENT. REPAIRED IAW SRM 52-30-01-2R-1, REPAIR 1.Nov 11, 2014 · N853GT · Boeing 74787UF · Cargo/Baggage DoorsSDR P5CA2014110900051B-Nut · looseOIL QUANTITY NR 2 ENGINE DECREASED TO ZERO OVER A 2 HOUR PERIOD, DIVERTED. PRESSURE AND TEMPERATURE STAYED NORMAL. FOUND NR 5 BEARING SCAVENGE TUBE B-NUT LOOSE. TORQUED B-NUT IAW AMM 79-21-09. PERFORMED GROUND RUN AND NO LEAKS NOTED.Nov 9, 2014 · N858GT · Boeing 74787UF · Turbine Engine Oil SystemSDR UIEA2014102400504Proximity Sensor · faultyGEAR TILT STATUS MSG, GEAR WOULD NOT RETRACT AFTER TAKE TAKEOFF, QRH CHECKLIST ACCOMPLISHED. R & R L/B TRUCK TILT LEVER LOCK PROX SENSOR S2653 IAW AMM 32-61-12. ADJUSTED SENSOR IAW AMM 32-61-12. OPERATIONS NORMAL IAW AMM 32-61-00 & 32-31-00.Oct 22, 2014 · N855GT · Boeing 74787UF · Landing Gear Position and WarningSDR P5CA2014093000041Tire · failedAFTER LANDING, FOUND TIRE MISSING CAP ON RT LANDING WING GEAR AFT INBD TIRE. REPLACED THE TIRE ASSY IAW AMM 32-45-04. ACCOMPLISHED CONDITIONAL INSPECTION IAW AMM 05-51-34. MULTIPLE DAMAGE FOUND.Sep 30, 2014 · N857GT · Boeing 74787UF · TireSDR P5CA2014091200040Warning Message · false activationREJECTED TAKEOFF, AT 35 KNOTS DUE TO A MASTER CAUTION SPLIT IRS OPERATION WENT AWAY AFTER 30 SECONDS. FOUNDINGS CMC MESSAGE. PERFORMED THE OPS TEST; GROUND TEST OF ALL ADIRS SYSTEM AND THEN OPS CHECKED NORMAL. GROUND TEST PASSED, NOT DUPLICATED FAULTS IAW ASep 11, 2014 · N853GT · Boeing 74787UF · Central WarningSDR P5CA2014090700038Unknown · unknownLOW SPEED RTO; 20 KTS FOR A MASTER CAUTION MESSAGE. A/T DISCONNECTED. ENTERED RUNWAY, MESSAGE GONE. BRAKE TEMP & LT; 1.0, TAXI BACK NORMAL T/O BUT SLIGHT VARIANCE IN AIRSPEED. ACFT TRYING TO FLY AT V1. AIRSPEED INDICATION JUMPED DURING CLIMBOUT. INFO NOTSep 7, 2014 · N858GT · Boeing 74787UF · Auto Throttle SystemSDR P5CA2014090500033Skin · corrodedNR 4 PYLON AFT FAIRING INBD EXTERNAL SURFACE CORROSION, ACCOMPLISHED IAW EI NR T2014A54B-3022, REV 2.Sep 5, 2014 · N853GT · Boeing 74787UF · Nacelle/Pylon, Plate/SkinSDR P5CA2014090500034Skin · corrodedNR 3 PYLON AFT FAIRING INBD EXTERNAL SURFACE CORROSION, ACCOMPLISHED IAW EI NR T2014A54B-3020, REV 2.Sep 5, 2014 · N853GT · Boeing 74787UF · Nacelle/Pylon, Plate/SkinSDR P5CA2014090500035Skin · corrodedNR 1 PYLON AFT FAIRING INBD EXTERNAL SURFACE CORROSION, ACCOMPLISHED IAW EI NR T2014A54B-3018, REV 2.Sep 5, 2014 · N853GT · Boeing 74787UF · Nacelle/Pylon, Plate/SkinSDR P5CA2014090500036Skin · corrodedNR 2 PYLON AFT FAIRING INBD EXTERNAL SURFACE CORROSION, ACCOMPLISHED IAW EI NR T2014A54B-3019, REV 2.Sep 5, 2014 · N853GT · Boeing 74787UF · Nacelle/Pylon, Plate/SkinSDR P5CA2014081300028Skin · damagedLIGHTNING STRIKE ON RT SIDE AND FORWARD OF COCKPIT SKIN. DESCENDING THROUGH 19,500 FEET. LIGHTING STRIKE INSPECTION CARRIED OUT IAW AMM 05-51-13. FOUND BURN MARK AT FUSELAGE BS 360 BETWEEN STRINGERS 23 - 24R. FOUND WITHIN SRM 53-00-01 ALLOWABLE DAMAGE LIMAug 13, 2014 · N852GT · Boeing 74787UF · Fuselage Main, Plate/SkinSDR P5CA2014081300029Skin · damagedLIGHTNING STRIKE ON RT SIDE AND FWD OF COCKPIT SKIN. DESCENDING THROUGH 19,500 FEET. FASTENER AT BS 320, STRINGER S25R FOUND DAMAGED. TEMPORARY REPAIR ACCOMPLISHED IAW SRM 53-00-01-2R-9, REPAIR 9, PARA 5.Aug 13, 2014 · N852GT · Boeing 74787UF · Fuselage Main, Plate/SkinSDR P5CA2014081100027Iru · out of alignmentECIAS MESSAGE, FMC AND AUTOTHROTTLE DISCONNECTED BEFORE TAKEOFF, NO PLF MESSAGE NOTED BOTH FMC & IRS SYS; ALL 3 IRU REALIGNED AND FMC LT & RT; GROUND TESTED GOOD. FMC LT & RT SERVO LOOP GROUND TEST ALSO PASSENGER IAW AMM 34-01-00.Aug 11, 2014 · N858GT · Boeing 74787UF · Flight Management Computing Hardware SystemSDR P5CA2014080500024Ball Screw · nickedDURING NR 5 BALLSCREW LUBRICATION, FOUND A NICK ON NR 5 BALLSCREW. REPLACED NR 5 BALLSCREW ASSY AND OPS CHECK NORMAL IAW AMM 27-51-41.Aug 5, 2014 · N858GT · Boeing 74787UF · Trailing Edge Flap Control SystemSDR P5CA2014072500022Fairing · crackedLEFT WING NR 4 FIXED FAIRING PANEL NR 571AB INBD SUPPORT BEAM AFT & END FOUND CRACKED, SUPPORT BEAM REPAIR CARRIED OUT IAW RI-57-51-10611.Jul 25, 2014 · N852GT · Boeing 74787UF · Wing Main, Frame StructureSDR UIEA2014072300341Rivet · damagedSDR UIEA2014071800338. LIGHTNING STRIKE AT 12 O'CLOCK POSITION. EO4853A013 DOCUMENTS & APPROVES THE CAT. A PERMANENT REPAIR TO THE PSE & FCBS STRUCTURE DAMAGED BY THIS EVENT. THIS EO DOCUMENTS & APPROVES THE RIVET REPAIRS ACCOMPLISHED WHETHER THEY ARE REPLJul 23, 2014 · N856GT · Boeing 74787UF · Fuselage Main, Plate/SkinSDR UIEA2014071800338Antenna · damagedLIGHTNING STRIKE AT 12 O'CLOCK POSITION. PRELIMINARY INSPECTION IAW AMM 05-51-13 201 FOUND MULTIPLE BURN MARKS AROUND RIVETS, DAMAGED VHF, GPS, ELT, ADF & HF ANTENNAS. REPLACEMENT OF DAMAGED PARTS & REPAIRS ARE CURRENTLY IN PROGRESS & REMAINDER OF CONDITIONAJul 18, 2014 · N856GT · Boeing 74787UF · UHF Communications SystemSDR P5CA2014070200019Window · delaminatedF/O FORWARD WINDOW DELAMINATING 11" X 3" AREA NEXT TO WINDOW HEAT ELEMENTS. R X R R1 WINDOW IAW AMM 56-11-01.Jul 2, 2014 · N857GT · Boeing 74787UF · Flight Compartment WindowsSDR UIEA2014061200233Control Cable · out of adjustLEFT AILERON FLIGHT CONTROL CHECK. PRONOUNCED BUMP COMING BACK TO NEUTRAL. FOUND LOST MOTION DRUM OUT OF RIG. AILERON BUS CABLES ACBA & ACBB ADJUSTED IAW MM 27-11-00. AILERON SYS FUNCTIONAL CHECK OK IAW MM 27-11-00.Jun 12, 2014 · N850GT · Boeing 74787UF · Aileron Control SystemSDR P5CA2014060400018Warning Horn · false activationREJECTED TAKEOFF AT 65 KNOTS DUE TO TAKEOFF WARNING HORN. NO RECORDED FAULT MESSAGES AND NOT RECENT HISTORY; BITE CHECK CARRIED OUT AND SATISFACTORY IAW AMM 31-51-00. TAKEOFF WARNING TEST CARRIED OUT AND SATISFACTORY AMM 31-52-00. FUNCTIONS CHECKED, CONFIG FJun 4, 2014 · N858GT · Boeing 74787UF · Central WarningSDR UIEA2014060200222Engine · power lossINADVERTENT ENCOUNTER WITH ICE CRYSTALS, NR 2 ENG ROLLED BACK. PERFORMED BORESCOPE INSPECTION OF ALL HIGH PRESS COMPRESSOR BLADE AIRFOILS OF THE NR 2 ENG IAW AMM TASK 71-00-00-200-816-G00, AWL 30-099-01 & AD 2013-24-01 PARA J I & SATISFACTORY.Jun 2, 2014 · N855GT · Boeing 74787UF · Engine (Turbine/Turboprop)SDR P5CA2014053100017Brake · delaminatedDURING WALKAROUND FOUND NR 4 AND NR 8 BRAKES HOT. FOUND BRAKE TEMP EICAS MESSAGE, COMPLIED WITH BRAKE INSPECTION IAW MM 05-51-10 NR 4 BRAKE OK AND FOUND NR 8 BRAKE DELAMINATED.May 31, 2014 · N853GT · Boeing 74787UF · Landing Gear Brake SystemSDR UIEA2014021200053Engine · power lossDURING TAKEOFF ROLL AT VERY LOW SPEED, NR 4 ENG ROLLED BACK TO IDLE. DURING TAKEOFF REJECTION THERE WAS A BURNING ODOR FOR APPROXIMATELY 20 SECONDS IN THE AIR CONDITIONING SYS & THEN THE ODOR DISSIPATED COMPLETELY. ACCOMPLISHED INLET & EXHAUST INSPECTION, NOFeb 12, 2014 · N851GT · Boeing 74787UF · Engine (Turbine/Turboprop)SDR UIEA2013121600605Fmc · malfunctionedEICAS MESSAGE, FMC RUNWAY DIS, DISPLAYED DURING TAKEOFF ROLL. RESET FMC LT & FMC RT IAW 34-51-00.Dec 16, 2013 · N854GT · Boeing 74787UF · Flight Management Computing Hardware SystemSDR UIEA2013112200569Warning Message · illuminatedLOW SPEED REJECT (40-50KTS) DUE TO EICAS MESSAGE "FMC RUNWAY DIS" CONFIRMED POSITION THEN NORMAL TAKE OFF,Nov 21, 2013 · N854GT · Boeing 74787UF · Flight Management Computing Hardware SystemSDR UIEA2013111900563Engine · damagedNR 2 ENGINE, REQUIRES REPLACEMENT DUE TO HIGH PRESSURE COMPRESSOR ROTOR DAMAGED BEYOND SERVICEABLE LIMITS. REPLACED NR 2 ENGINE IAW AMM 71-00-00 AND REMOVAL AND INSTALLATION LIST 1039.Nov 19, 2013 · N854GT · Boeing 74787UF · Engine (Turbine/Turboprop)SDR UIEA2013111900562Wire · chafedREF: SPOILER PCU NR 7 PROBLEM HISTORY. DURING TROUBLESHOOTING CABLE W27R4-30-20R, CHAFED UNDER P-CLIP REF WDM 27-61-31 PAGE 1;SAME WIRE TEMPORARILY REPAIRED IAW EO 4827A014, REV 0, PART 1, PART 2, PERMANENT REPAIR TO BE ACCOMPLISHED PRIOR TO 10 FLIGHT CYCLES.Nov 19, 2013 · N850GT · Boeing 74787UF · Flight Control System WiringSDR UIEA2013110500550Engine · power lossUNCOMMANDED ROLLBACK OF NR 2 AND NR 4 ENGINES IN ICE CONDITIONS, ENG X THRUST, MASTER CAUTION. ENGINES RETURNED TO NORMAL AFTER EXITING ICE CRYSTALS, NOTIFIED MCC, INSPECTED ENGINES IAW FIM 73-21-00 STEP 1 THROUGH 9, NFF, OK FOR CONTINUED SERVICE.Nov 5, 2013 · N854GT · Boeing 74787UF · Engine (Turbine/Turboprop)SDR UIEA2013062600343Controller · inoperative"CARGO DET AFT 28" STATUS MESSAGE APPEARED 40 MINUTES INTO FLIGHT FOLLOWED BY "FIRE CARGO AFT" & 20 MINUTES LATER. QRH EMERGENCY CHECKLIST FOLLOWED AND FLIGHT DIVERTED TO IAD. ON ARRIVAL, THE LOWER AFT CARGO BAY WAS INSPECTED AND FOUND THAT THERE WAS NO EVIDJun 26, 2013 · N850GT · Boeing 74787UF · Fire DetectionSDR UIEA2013022800107Circuit Card · malfunctionedWHEEL WELL FIRE MASTER WARNING ON TAKEOFF ROLL (WHEEL WELLS INSPECTED FOR PNEUMATIC LEAKS, NONE FOUND. INSPECTED FIRE LOOPS, ALL OK. WHEEL WELL FIRE DETECTION CARD REPLACED AS A PRECAUTION, SYSTEM TESTED NORMAL).Feb 28, 2013 · N853GT · Boeing 74787UF · Fire DetectionSDR UIEA2012121200545Structure · puncturedDURING WALKAROUND INSPECTION, MX FOUND THE NR 9 VARIABLE CAMBER FLAP - BULL NOSE PUNCTURE AND EDGE DAMAGE REF FIG 1. THE DAMAGE EXCEEDS THE LIMITS OF SRM 57-43-02, FIG 101, ALLOWABLE DAMAGE 3 - L/E FLAP SKIN. DISPOSITION WAS MADE TO PERFORM A TIME LIMITED REDec 12, 2012 · N850GT · Boeing 74787UF · Leading Edge DevicesSDR UIEA2012113000537Warning Light · false activationFIRE WHEEL WELL EICAS MESSAGE DISPLAYED IMMEDIATELY AFTER LIFT OFF. MESSAGE CLEARED BY ITSELF IN APPROX 10 SECONDS. LT THE GEAR DOWN AND ACCOMPLISHED NON NORMAL PROCEDURES EXCEPT GEAR RAISED AFTER APPROX 4 MINUTES. ALL INDICATIONS NORMAL INCLUDING VISUAL INNov 30, 2012 · N852GT · Boeing 74787UF · Fire DetectionSDR UIEA2012110500514Actuator · inoperativeMESSAGE REPORTED THAT THE GEAR DISAGREE MESSAGE FOR RT WING GEAR EXPERIENCED, REPLACED RT WING LANDING GEAR DOOR ACTUATOR IAW MM 32-32-07 HYD LEAK CHECKED OPS AND ADJUSTMENT CARRIED OUT SATISFACTORY IAW MM 32-12-00, NIL MESSAGE NOTED DURING DOOR OPERATION.Nov 5, 2012 · N850GT · Boeing 74787UF · Landing Gear ActuatorSDR UIEA2012110500512Proximity Switch · failedRT WING GEAR HAD AN UP INDICATION AFTER LOWERING GEAR FOR LANDING. QRH COMPLETED WITH ALL GEAR DOWN. CMC REPORTED FAILURE OF PRI AND ALT PROXIMITY SWITCHES FOR RT WING GEAR UP, DOWN AND DOORS. CYCLED GEAR SWITCHES BACK TO NORMAL, RUN CMC TEST IAW AMM 32-09-Nov 5, 2012 · N850GT · Boeing 74787UF · Landing Gear Position and WarningSDR UIEA2012101400472Nut Plate · damagedNR 3 PYLON T/E FAIRING HAS TWO NUTPLATES DAMAGED. PERFORM A TIME LIMITED REPAIR.Oct 14, 2012 · N852GT · Boeing 74787UF · Nacelle/Pylon, Main FrameSDR UIEA2012100700455Pump · leakingHYD QTY LOW 2 & HYD PRESSURE ENG 2 EICAS MESSAGES. ON INSPECTION IT WAS FOUND THAT THERE WAS HYD FLUID LEAKING FROM ENG 2 DRAIN MAST, FOR THE ENGINE DRIVEN HYD PUMP. NR 2 EDP REPLACED IAW AMM 29-11-05. DURING LEAK CHECK, A LEAK WAS ALSO FOUND AT THE RT INOct 7, 2012 · N852GT · Boeing 74787UF · Hydraulic Pump (Electric/Engine), Main
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