N754CX
Service difficulty reports · 204
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.
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 n_number = 'N754CX' AND registry_match = 'registration' 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.
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 n_number = 'N754CX' AND registry_match = 'registration' ORDER BY difficulty_date DESC
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR IXXA20221001136Hose · leakingLEFT HYDRAULIC SYSTEM TOTAL LOSS OF QUANTITY AND PRESSURE PUMPS SHUTOFF PRIOR TO ZERO QUANTITY 27%. RIGHT ENGINE HYDRAULIC OVERHEAT-PUMP SHUT OFF. RIGHT ENGINE HYDRAULIC ELECTRIC-PUMP SHUT OFF. BOTH PUMPS SHUTOFF IMMEDIATELY. STATUS MESSAGE 8 RIGHT HYDRAULIC SSDR IXXA202201287003None · noneON POST FLIGHT INSPECTION INBOUND FROM KNGU LINE MAINTENANCE IDENTIFIED DAMAGE ON THE LEFT INBOUND LEADING SLAT PANEL. GROUNDED FOR UNSCHEDULED MAINTENANCE. WORK IN PROGRESS.SDR IXXA20210124002Light · inoperativeDURING THE COURSE OF SCHEDULED MAINTENANCE CHECKS, TECHNICIAN IDENTIFIES EMERGENCY EXIT SIGN NEXT TO R1 DOOR INOPERATIVE. AIRCRAFT OUT OF SERVICE, WORK IN PROGRESS. CORRECTIVE ACTION PENDING.SDR 6PMR202012270001Spar · corrodedLT WING UPPER SKIN, FRONT SPAR, APPROXIMATELY WING STA 285 HAS CORROSION AROUND FASTENERS. CORRECTIVE ACTION: COMPLIED WITH EO 20495-6.SDR 6PMR2020122408318Skin · corrodedLEFT WING UPPER SKIN, FRONT SPAR APPROXIMATELY WING STA 238 HAS CORROSION AROUND FASTENER. CORRECTIVE ACTION: REMOVED CORROSION, BLENDED AREA, ACCOMPLISHED NDT AND SHOT PEEN. REAPPLIED SURFACE PROTECTION, IAW EO 20495-6. PEMCO NON-ROUTINE 10248-0318.SDR 6PMR2020122480315Spar · corrodedLT WING UPPER SKIN, FRONT SPAR, APPROXIMATELY WING STA 170 HAS CORROSION AROUND FASTENER. CORRECTIVE ACTION: REMOVED CORROSION AND BLENDED AREA. ACCOMPLISHED NDT, SHOT PEEN. REAPPLIED CORROSION PROTECTION, IAW EO 20495-6. PEMCO NON-ROUTINE 10248-0315.SDR 6PMR202012230002Stringer · corrodedRIGHT WING FUEL TANK, CORROSION ON UPPER STRINGER BETWEEN WS 719 AND WS 743. CORRECTIVE ACTION: REMOVED AND REPLACED STRINGER SECTION BETWEEN STA 719 AND STA 743, IAW B-757 SRM 57-00-03, REPAIR 1 AND B-757 SRM 51-40-02. PEMCO NON-ROUTINE 10248-0549.SDR 6PMR2020122131223Skin · corrodedAREAS WITH CORROSION ON UPPER LEFT AFT SKIN SURFACE OF CENTER HORIZONTAL STABILIZER BOX, BETWEEN HYDRAULIC LINES CONNECTION AND LEFT ATTACH MOUNT PLATE AROUND FASTENERS AND ALONG EDGE. CORRECTIVE ACTION: ACCOMPLISHED EO 20495-3, REV IR. REMOVED CORROSION, ACSDR 6PMR202012170001Skin · corrodedLEFT WING UPPER SKIN, FRONT SPAR, APPROXIMATELY WING STA 660 HAS CORROSION AROUND VORTEX GENERATOR. CORRECTIVE ACTION: BLENDED AREA, IAW EO 20495-6, REV IR PEMCO NON-ROUTINE 10248-0320.SDR 6PMR202012164551Skin · dentedFUSELAGE SKIN DENTED AND SCRATCHED ON TOP OF EXISTING DOT AT LAP SEAQM ON TOP OF FASTENER AT STA 1714 AND STR 14AL. CORRECTIVE ACTION: REPAIRED FUSELAGE SKIN WITH CUTOUT, FILLER AND DOUBLER, TRIPLER, IAW EO 20492-1 REV IR. PEMCO NON-ROUTINE10248-0045.SDR 6PMR1024804661210Seat Track · gougedMAIN DECK SEAT TRACK AT STA 905 AND RBL 24075 HAS DEEP GOUGES ON SCALLOP TABS. CORRECTIVE ACTION: REPLACED AND REPAIRED SEAT TRACK IN ACCORDANCE B757-200 SRM 53-00-52 REPAIR 4. PEMCO NON-ROUTINE 10248-0466.SDR 6PMR1024806201210Strap · crackedFOUND OVERHEAD STABILIZER STRAP AT BS 1380 LT CRACKED. MANUFACTURED LAP PATCH AND FILLER, IAW B-757-200 SRM 53-00-51 REPAIR 12.SDR 6PMR1024802981210Skin · corrodedNR 2 PYLON, CORROSION ON PYLON SKIN OUTBOARD SIDE JUST AFT OF 441AL. CORRECTIVE ACTION: INSTALLED REPAIR, IAW EO 20495-4 REV IR. PEMCO NON/ROUTINE 10248-0298.SDR 6PMR1024800441210Skin · gougedEXT FUSELAGE SKIN HAS GOUGES AT STA 1680-1690 AT STR 17L. CORRECTIVE ACTION: BLENDED GOUGES, IAW EA PD 57-53-350 PEMCO NON-ROUTINE 10248-0044.SDR 6PMR1024803260812Skin · corrodedDISCREPANCY: PEMCO NON-ROUTINE 10248-0326: LEFT WING UPPER SKIN REAR SPAR, APPROXIMATELY WING STATION 600 HAS CORROSION UNDER PANEL AND AROUND FASTENER. CORRECTIVE ACTION: REMOVED CORROSION AND EVALUATED LT WING UPPER SKIN. REAR SPAR FOUND TO BE OUT OF LIMITSDR 6PMR202012090466Seat Track · damagedAIRBORNE/PEMCO N/R 10248.0466 DISCREPANCY: MAIN DECK SEAT TRACK AT STA 905 AND RBL 24.75 HAS DEEP GOUGES ON SCALLOP TABS WHERE LOADING SYSTEM COMPONENT LOCKS DOWN. CORRECTIVE ACTION: REPAIRED MAIN DECK SEAT TRACK AT STA 905 RBL 24.75, IAW B757-200 SRM 53-00-5SDR 6PMR202012160327Skin · corrodedAIRBORNE/PEMCO N/R 10248.0327 DISCREPANCY: LT WING UPPER SKIN, FRONT SPAR, APPROXIMATELY WING STA 660 HAS CORROSION AROUND VORTEX GEN. CORRECTIVE ACTION: COMPLIED WITH RES 15402 FOR LT WING SKIN, FRONT SPAR WING STA 660 AROUND VORTEX GEN AREA, IAW EO 20495-6 SDR 6PMR202012160321Skin · corrodedAIRBORNE/PEMCO N/R 10248.0321 DISCREPANCY: LT WING UPPER SKIN, FRONT SPAR, APPROXIMATELY WING STA 342 HAS CORROSION AROUND FASTENER. CORRECTIVE ACTION: COMPLIED WITH RES 15402 FOR LT WING UPPER SKIN FRONT SPAR, WING STA 342 AREA, IAW EO 20495-6 REV IR.SDR 6PMR202012160322Skin · corrodedAIRBORNE/PEMCO N/R 10248.0322 DISCREPANCY: LT WING UPPER SKIN, FRONT SPAR, APPROXIMATELY WING STA 395 HAS CORROSION AROUND VORTEX GEN. CORRECTIVE ACTION: COMPLIED WITH RES NR 15402 FOR LT WING UPPER SKIN FRONT SPAR W/S 395 AROUND VORTEX GEN AREA (RES SEE COPYSDR 6PMR202012160324Skin · corrodedAIRBORNE/PEMCO N/R 10248.0324 DISCREPANCY: LT WING UPPER SKIN, FRONT SPAR, APPROXIMATELY WING STA 460 HAS CORROSION AROUND VORTEX GEN. CORRECTIVE ACTION: COMPLIED WITH RES 15402 FOR LT WING UPPER SKIN, FRONT SPAR WING STA-460 AROUND VORTEX GEN AREA, IAW EO 20SDR 6PMR10248.0325Skin · corrodedAIRBORNE/PEMCO N/R 10248.0325 DISCREPANCY: LT WING UPPER SKIN, FRONT SPAR, APPROXIMATELY WING STA 565 HAS CORROSION AROUND VORTEX GEN. CORRECTIVE ACTION: COMPLIED WITH RES 15402 FOR LT WING UPPER SKIN, FRONT SPAR WING. STA 565, AROUND VORTEX GEN AREA, IAW EOSDR 6PMR202012160323Skin · corrodedAIRBORNE/PEMCO N/R 10248.0323 DISCREPANCY: LT WING UPPER SKIN, FRONT SPAR, APPROXIMATELY WING STA 425 HAS CORROSION AROUND VORTEX GEN. CORRECTIVE ACTION: COMPLIED WITH EA NR RESRES 15402, FOR LT WING UPPER SKIN, FRONT SPAR, STA 425 AROUND VORTEX GEN AREA, IAWSDR 6PMR202012090298Skin · corrodedAIRBORNE/PEMCO N/R DISCREPANCY: NR 2 PYLON. CORROSION ON PYLON SKIN OUTBOARD SIDE JUST AFT OF 444AL. CORRECTIVE ACTION: INSTALLED REPAIR, IAW FVCI CONTROL NR 20495-4 REV IR AT NR 2 PYLON SKIN OUTBOARD SIDE JUST AFT OF 441AL.SDR 6PMR202012090217Skin · corrodedAIRBORNE/PEMCO N/R 10248.0217 DISCREPANCY: TWO (2) AREAS WITH CORROSION ON UPPER SKIN SURFACE OF LEFT HORIZ STAB AFT SKIN PLANK NEAR SEAMAT APPROX. LOCATION ON AT APPROX. 35 INCHES AFT OF LOGO LIGHT AND APPROX. 81 AND 1/4 INCHES OUTBOARD OF UPPER MOVEABLE FAIRSDR 6PMR10248.0009Window Frame · damagedAIRBORNE/PEMCO N/R 10248.0009 DISCREPANCY: LOGBOOK: 514118, REF DMI 56096: TIME LIMITED REPAIR TO WINDOW FRAMES IN PAX CABIN, PER DER 47285 REA 04 MAY NOT EXCEED 24 MONTHS OR 3000 CYCLES WHICHEVER COMES FIRST, REF TASK TRMZ2000TYX2. CORRECTIVE ACTION: FABRICASDR 6PMR202012094844Skin · dentedAIRBORNE/PEMCON N/R 10248.0044 DISCREPANCY: EXT FUSELAGE SKIN HAS GOUGES AT STA 1680-1690 AT STR 17L. CORRECTIVE ACTION: BLENDED GOUGES ON EXT FUSELAGE SKIN STA 1680-1690 BELOW STR 17L, IAW B757-200 SRM 51-10-02. CUT GAUGED BLENDED AREAS LOWEST READING OF .1SDR IXXA20201021500Light · inoperativePRE-DEPARTURE: R4 DOOR EXTERIOR EMERGENCY LIGHT INOPERABLE. RELAMPED R4 DOOR EXTERIOR EMERGENCY LIGHT (ESCAPE SLIDE LIGHT), IAW B757 AMM 33-51-06. OPERATIONAL CHECK SATISTFACTORY. FAULT NOT DUPLICATED. AIRCRAFT RELEASED TO SERVICE.SDR IXXA20200925037Bottle · low pressureL4 DOOR ESCAPE SLIDE PRESSURE IS LOW. AIRCRAFT GROUNDED FOR UNSCHEDULED MAINTENANCE. REMOVED AND REPLACED L4 DOOR EVACUATION SLIDE, IAW B767 AMM 25-66-01. AIRCRAFT RELEASED TO SERVICE.SDR IXXA20191024017Battery Pack · inoperativePILOT REPORT: R1 DOOR EMERGENCY EXIT LIGHT AND EXTERNAL LIGHT INOPERATIVE. REMOVED AND REPLACED BATTERY IAW AMM 33-51-07. OPERATIONAL CHECK SATISFACTORY. FAULT NOT DUPLICATED. AIRCRAFT RELEASED TO SERVICE.SDR IXXA20191024016Battery Pack · inoperativePRE DEPARTURE CHECK: R-4 EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY IAW AMM 33-51-07. OPERATIONAL CHECK SATISFACTORY. FAULT NOT DUPLICATED. AIRCRAFT RELEASED TO SERVICE.SDR IXXA201908310001Structure · corrodedLEFT MAIN LANDING GEAR HAS CORROSION ON CEILING AFT OF THE LEFT HYDRAULIC RESERVOIR. CORROSION OUT OF LIMITS. ORIGINAL MATERIAL 140", MATERIAL REMOVED .040, MATERIAL REMAINING .100. ALL REPAIRS PER FVCI ENGINEERING ORDER 19158.SDR IXXA2019062029012Skin · corrodedAIRCRAFT GROUNDED FOR HEAVY MAINTENANCE C-17. IN COMPLIANCE OF GENERAL VISUAL INSPECTION-CORROSION PREVENTION TASK CARD 53-800-10-01, THE FOLLOWING FINDINGS WERE NOTED: BULGED SKIN AT STA 1400 BETWEEN STRINGER 26L AND 27L. WORK IN PROGRESS. REPAIRED BULGED SKISDR IXXA20181113888Hydraulic Line · damagedON APPROACH TO DESTINATION STATION WSAP, LOSS OF LEFT SYSTEM HYDRAULIC QUANTITY AND SYSTEM PRESSURE. LOSS WAS NOTED AFTER SELECTING LANDING DOWN FOR LANDING. FLAPS CONFIGURED TO 20 BEFORE LOSS OF PRESSURE. APPROACH WAS ABANDONED. HYDRAULIC SYSTEM PRESSURE (LEFSDR IXXA20180621030Battery · weakF/O'S EMERGENCY BATTERY IS WEAK. REMOVED AND REPLACE F/O'S FLASHLIGHT BATTERY P/N P2-07-001-2015.SDR IXXA20171113343Skin · corrodedTHE RIGHT INBOARD FLAP LOWER SKIN HAS SURFACE CORROSION. REMOVED AND REPLACED THE LOWER SKIN PANEL IAW SRM 51-40-08, AND 51-40-05.SDR IXXA20171113342Strap · corrodedCORROSION AROUND THE PERIMETER OF THE APU AIR INLET DOOR PANEL, AND AT THE BS 1787 LAP SEAM IN THE AREA BELOW THE DOOR. REMOVED AND REPLACEDTHE CORRODED FWD FRAME STRAP. REMOVED AND REPLACED THE ANGLES IAW SRM 51-40-02, PAR 4, 7, 9, AND DWG 148N3152.SDR IXXA20171109341Skin · corrodedFOUND CORROSION ON THE LT WING UPPER SURFACE VORTEX GENERATORS NR 10, & 14. REMOVED THE CORROSION, AND FOUND OUT OF LIMITS. REPAIRED IAW REA 47285REA07.SDR IXXA20171113344Skin · corrodedRIGHT WING INBD FLAP UPPER SURFACE HAS BUBBLED PAINT. CLEANED THE AREA, REMOVED CORROSION IAW SRM 57-53-01. FABRICATED AND INSTALLED A REPAIR IAW SRM 51-70-10, AND SRM 57-53-01.SDR IXXA20171109334Web · corrodedMULTIPLE SPOTS OF CORROSION FOUND IN RT MLG WW VERTICAL WEB BETWEEN BS 1080 - 1100 BL 0. KEEL VERTICAL WEB REPLACED IAW TIN-RE-1705379.SDR IXXA20171109333Web · corrodedMULTIPLE SPOTS OF CORROSION IN THE RT MLG WW ON VERTICAL WEB BETWEEN BS 1160 - 1170, BL 0. THE WEB WAS REPLACED IAW TIN-RE-1705379.SDR IXXA20171109328Stiffener · corrodedRT MLG WW PRESSURE DECK LONGITUDINAL STIFFENER BS 1150, RBL 9 CORRODED. REPAIRED THE STIFFENER IAW TIN-RE-1705379.SDR IXXA20171109327Stiffener · corrodedRT MLG WW PRESSURE BULKHEAD LONGITUDINAL STIFFENER BS 1156 - 1170, RBL 39 CORRODED IN SEVERAL AREAS, INCLUDING LOWER FLANGE UPPER SIDE. REPAIRED THE STIFFENER.SDR IXXA20171107324Stiffener · corrodedRT MLG WW PRESSURE DECK, LONGITUDINAL STIFFENER, BS 1104 - 1112, RBL 46 CORRODED. ALSO CORRODED ON THE OTBD SIDE OF VERTICAL LEG. THE PRESSURE DECK LONGITUDAL STIFFENER WAS REPAIRED.SDR IXXA20171109337Pressure Deck · corrodedRT MLG WW PRESSURE DECK WEB HAS CORROSION AT BS 1072, RBL 11. REPAIRED IAW TIN-RE-1705379.SDR IXXA20171109332Pressure Deck · corrodedCORROSION IN THE RT MLG WW UPPER WEB BS 1170 - 1178, RBL 54. REPAIRED IAW TIN-RE-1705379.SDR IXXA20171109326Bulkhead Web · corrodedRT MLG WW PRESSURE BULKHEAD WEB BS 1070 - 1178, RBL 54 CORRODED. REPAIRED.SDR IXXA20171107325Bulkhead Web · corrodedRIGHT MLG WW PRESSURE BULKHEAD WEB BS 1077 - 1079, RBL 27 - 32 CORRODED. REPAIRED THE BULKHEAD WEB.SDR IXXA20171109331Stiffener · corrodedLT MLG WW PRESSURE DECK LONGITUDINAL STIFFENER CORRODED BS 1112, LBL 17. THE STIFFENER WAS REPAIRED IAW TIN-RE-1705379.SDR IXXA20171109339Fitting · corrodedRT MLG WW BS 1180, RBL 25 AFT BULKHEAD FLAP ASSEMBLY ATTACH FITTING HAS CORROSION AROUND FASTENER. THE FITTING ASSEMBLY WAS REPLACED IAW TIN-RE-1705379.SDR IXXA20171109338Fitting · corrodedRIGHT MLG WW BS 1180, RBL 39, AFT BULKHEAD FLAP ASSEMBLY ATTACH FITTING HAS CORROSION AROUND THE FASTENER. THE FITTING ASSEMBLY WAS REPLACED IAW TIN-RE-1705379.
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