N752CX

Service difficulty reports · 226

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 = 'N752CX' 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.

SDR IXXA2022112901Skin · corrodedLEFT WING LOWER WING PNL STA. 822-829 IS CORRODED AT FUEL PNLJun 10, 2022 · N752CX · Boeing 7572G5 · Wing, Plate/SkinSDR IXXA2022072601Stiffener · corrodedLWW UPPER WEB STIFFENER AT STA 1144 LBL 16.5 CORRODEDJun 5, 2022 · N752CX · Boeing 757200 · Fuselage Main, StructureSDR IXXA20220100201Bracket · corrodedREF AMES NR 147534-0100-0150 LWW FS1180 35" OTBD KEEL CENTER WEB AT CEILING ISOLATION VALVE STAND OFF MOUNTING WEB CORROSION ON AFT SIDE.May 26, 2022 · N752CX · Boeing 7572G5 · Fuselage Main, Attach FittingsSDR IXXA2022061701Flap System · crackedFOUND CRACK IN THE RIGHT O/B AFT FLAP T/E LOWER SURFACE BY THE O/B SUPPORT FITTINGMay 23, 2022 · N752CX · Boeing 757200 · Trailing Edge Flap Control SystemSDR IXXA2022072604Skin Panel · corrodedLEFT WING UPPER SURFACE L/E CORRODEDMay 20, 2022 · N752CX · Boeing 757200 · Wing StructureSDR IXXA2022072203Skin Panel · corrodedLEFT WING TE EXTERNAL SKIN CORRODED AT WS 717.5 TO 775.5May 20, 2022 · N752CX · Boeing 757200 · Crew Oxygen SystemSDR IXXA2022111103Web · corrodedKEEL WEB IN LEFT WHEEL WELL AT STA 1175 SHOWS SIGNS CORROSION AROUND HYDRAULIC LINESMay 19, 2022 · N752CX · Boeing 7572G5 · Fuselage Miscellaneous StructureSDR IXXA2022072602Stiffener · corrodedLONGITUDINAL STIFFENER IN LEFT WHEEL WELL AT LWS 38 FROM STA 1100-1110 CORRODEDMay 19, 2022 · N752CX · Boeing 757200 · Fuselage Structure (General)SDR IXXA2022072204Skin Panel · corrodedLEFT WING LOWER SKIN CORRODED FROM WS 150-177.5 AT AFT SPARMay 19, 2022 · N752CX · Boeing 757200 · Crew Oxygen SystemSDR IXXA20220100102Web · corrodedREF AMES NR 147534-0100-0077 AFT SIDE OF STA 900 WEB IS CORRODED AROUND PNEUMATIC DUCT AND HYDRAULIC LINE RBL 12May 17, 2022 · N752CX · Boeing 7572G5 · Fuselage Miscellaneous StructureSDR IXXA2022100101Skin · corrodedCORROSION ON UPPER SURFACE LWING 60" FROM FUSELAGE 18" FROM L/E. REF AMES NR 147534-0500-0030May 16, 2022 · N752CX · Boeing 7572G5 · Wing, Plate/SkinSDR IXXA2022072603Pressure Deck · corrodedRT WHEEL WELL PRESSURE DECK CORRODEDMay 16, 2022 · N752CX · Boeing 757200 · Fuselage Main, StructureSDR IXXA2022072206Floorbeam · corrodedLOWER FLANGE OF ANGLE IN THE KEEL AREA AT STA 1168 CORRODEDMay 16, 2022 · N752CX · Boeing 757200 · Fuselage Main, StructureSDR IXXA2022072205Skin · corrodedRT WHEEL WELL PRESSUER DECK CORRODED STA 100 RBL 49May 16, 2022 · N752CX · Boeing 757200 · Fuselage Main, StructureSDR IXXA2022072202Door · corrodedRT WEHEEL WELL PRESSURE DECK CORRODED STA 1100 RBL 64-58May 16, 2022 · N752CX · Boeing 757200 · Fuselage Main, StructureSDR IXXA2022070001Door · corrodedRT WHEEL WELL PRESSURE DECK CORRDED STA 1094 RBL 47May 16, 2022 · N752CX · Boeing 757200 · Fuselage Main, StructureSDR IXXA2022062302Pressure Deck · corrodedLT WHEEL WELL PRESSURE DECK CORRODEDMay 16, 2022 · N752CX · Boeing 757200 · Fuselage Main, StructureSDR IXXA2022062301Pressure Deck · corrodedLT WHEEL WELL PRESSURE DECK CORRODEDMay 16, 2022 · N752CX · Boeing 757200 · Fuselage Structure (General)SDR IXXA2022072207Skin Panel · corrodedUPPER SURFACE LEFT WING ABOVE PYLON AREA CORRODEDMay 14, 2022 · N752CX · Boeing 757200 · Crew Oxygen SystemSDR IXXA2022093001Skin · corrodedCORROSION ON EXTERNAL SURFACE OF LEFT WING LOWER SKIN AT WS 74.5 AND APPROXIMATELY SIX INCHES AFT OF STRINGER L8 REF AMES NR 147534-0500-0018May 11, 2022 · N752CX · Boeing 7572G5 · Wing, Longeron/StringerSDR IXXA2022072208Skin Panel · corrodedLEFT WING EXTERNAL LOWER SURFACE SKIN STR L6 AT WS 150.5 TO 177.5 CORRODEDMay 10, 2022 · N752CX · Boeing 757200 · Fuselage Main, StructureSDR IXXA202262304Skin Panel · corrodedCORROSION ON EXTERNAL SIDE OF RIGHT WING REAR SPAR LOWER CHORD IN RIGHT WHEEL WELL WHERE SPAR ATTACHES TO CENTER WING BOXMay 10, 2022 · N752CX · Boeing 757200 · Fuselage Main, StructureSDR IXXA20220929002Roller Tray · cutUPPER CARGO ROLLER TRAY AT RBL 30.0 IS CUT REF AMES N/R 147534-0200-0042May 7, 2022 · N752CX · Boeing 7572G5 · Fuselage Floor PanelSDR IXXA20210225013Battery · inoperativeAIRCRAFT GROUNDED FOR UNSCHEDULED POWER PLANT MAINTENANCE, IDENTIFIED R1 DOOR EMERGENCY EXIT DOORS LIGHT INOPERATIVE. REMOVED AND REPLACED REMOVED AND REPLACED R1 EMERGENCY EXIT LIGHTS POWER SUPPLY IAW AMM 33-51-07. OPERATIONAL CHECK SATISFACTORY. NO FURTHEFeb 21, 2021 · N752CX · Boeing 7572G5 · Emergency LightingSDR 2020F00333Battery Pack · dischargedDURING EMERGENCY LIGHT OPS CHECKS MULTIPLE LIGHTS FAILED TO COME ON. REMOVED AND REPLACED TWO BATTERY PACKS AT M736 AND M737 IAW AMM 33-51-07. REMOVED AND REPLACED 5 AMP FUSE IAW AMM 33-51-07. PERFORMED OPS CHECK OF EMERGENCY LIGHTS IAW 33-51-00 OPS CHECK GJul 13, 2020 · N752CX · Boeing 7572G5 · Emergency LightingSDR 2020F00334Switch · faultyDURING EMERGENCY LIGHT OPS CHECKS MULTIPLE LIGHTS FAILED TO COME ON. REMOVED AND REPLACED TWO BATTERY PACKS AT M736 AND M737 IAW AMM 33-51-07. REMOVED AND REPLACED 5 AMP FUSE IAW AMM 33-51-07. PERFORMED OPS CHECK OF EMERGENCY LIGHTS IAW AMM 33-51-00. OPS CJul 13, 2020 · N752CX · Boeing 7572G5 · Emergency LightingSDR 2020F00335Stringer · corrodedRIGHT WING STA 718 STRINGER U12 WAS CORRODED. REMOVED AND ELVAUATED CORROSION, ORIGNAL MATERIAL .100 IN., MATERIAL LOSS .068 IN., MATERIAL REMAINING .022., MATERIAL LOSS ALLOWABLE 10%. FOUND TO BE OUT OF LIMITS. REMOVED DAMAGE AND PERFORMED STRINGER REPAIR Jul 12, 2020 · N752CX · Boeing 7572G5 · Wing, Longeron/StringerSDR 2020F00301Doubler · corrodedNR 2 NACELLE STRUT DOOR (443LL) HAS CORROSION ON FWD BOTTOM CORNER ON DOOR LANDING. ACCOMPLISHED REPAIR IAW ENGINEERING ORDER CONTROL 20191, TITLED REPAIR-DOUBLER, INBOARD NACELLE SIDE SKIN PANEL ASSEMBLY NR 2 ENG, PPS 176.25.Jun 3, 2020 · N752CX · Boeing 7572G5 · Nacelle/Pylon, Plate/SkinSDR 2020F00289Support Beam · corrodedNON-ROUTINE 2832N248 DISCREPANCY. LMWW, CORROSION ON FWD LOWER FLANGE OF LT MAIN GEAR DOOR ACTUATOR SUPPORT BEAM STA 1120. CORRECTIVE ACTION, LT WHEEL WELL MAIN GEAR DOOR ACTUATOR SUPPORT REPAIRED IAW FVCI EO CONTROL 20184.May 29, 2020 · N752CX · Boeing 7572G5 · Fuselage, Landing Gear Attach FittingsSDR 2020F00275Keelbeam · corrodedAIRBORNE/PEMCO NON-ROUTINE 2832N241 DISCREPANCY: CORROSION ON KEEL BEAM LOWER SURFACE NLEFT CHORD AT STA 1170 CORRECTIVE ACTION: REPAIRED PER FVCI E.O. #20174May 21, 2020 · N752CX · Boeing 7572G5 · Fuselage Main, KeelSDR 2020F00319Floor Support · corrodedFWD WET AREA, FLOOR SUPPORT BETWEEN BS 324 AND 345 CORRODED AT RBL 40. ACCOMPLISHED EO 20215, REPAIR OF SEC. 41 WITHOUT ANY DEVIATIONS.May 20, 2020 · N752CX · Boeing 7572G5 · Fuselage Miscellaneous StructureSDR 2020F00302Doubler · corrodedNR 2 NACELLE STRUT DOOR (443LL) HAS CORROSION ON FWD BOTTOM CORNER ON DOOR LANDING. ACCOMPLISHED REPAIR IAW ENGINEERING ORDER CONTROL 20191, TITLED REPAIR-DOUBLER, INBOARD NACELLE SIDE SKIN PANEL ASSEMBLY NR 2 ENG, PPS. 176.25.May 16, 2020 · N752CX · Boeing 7572G5 · Nacelle/Pylon, Plate/SkinSDR 2020F00330Service Panel · corrodedFWD LAV SVC PANEL INSIDE ALL FASTENER ARE CORRODED AND 2EA COVER PLATES HAVE CORROSION. REMOVED AND REPLACED FASTENERS AND FABRICATED 2EA COVER PLATES ON 2832N1011, ACCOMPLISHED EO 20195 ON N/R 2832N245 WITHOUT ANY DEVIATIONS.May 2, 2020 · N752CX · Boeing 7572G5 · Service DoorsSDR 2020F00328Panel · corrodedNON-ROUTINE 2832N283, NR 1 ENG ZONE 433 NACELLE STRUT MID STRUCTURE O/B PANEL, LWR AFT CORNER; FOUND EXCESSIVE CORROSION. REPAIRED NR 1 ENGINE NACELLE STRUT MID STRUCTURE O/B PANEL, ACCOMPLISHED REPAIR ON ENGINEERING ORDER 20192, WITHOUT ANY DEVIATIONS.May 2, 2020 · N752CX · Boeing 7572G5 · Nacelle/Pylon Miscellaneous StructureSDR 2020F00299Keelbeam · corrodedNON-ROUTINE 2832N258 DISCREPANCY. RMWW, CORROSION ON KEEL BEAM RIGHT CHORD UPPER SURFACE IN RADIUS OF TAB THAT ATTACHES TO STA 1120 GEAR DOOR ACTUATOR SUPPORT BEAM. CORROSION RUNS UNDER SUPPORT BEAM. CORRECTIVE ACTION. REMOVED CORROSION ON RT KEEL BEAM CHOMay 2, 2020 · N752CX · Boeing 7572G5 · Fuselage Main, KeelSDR 2020F00297Structure · corrodedNWW LOWER CHORD HAS CORROSION BETWEEN RT AFT GEAR DOOR AND HINGE FITTINGS. REMOVED CORROSION ON NWW LWR CHORD RT AFT AREA IAW-B757-200-SRM-53-10-14. GRID MAP LWR CHORD AREA 2 EA AREA ON LWR CHORD, IAW- PRELIMINARY-E.O. CONTROL 20613. HFEC ACCOMPLISHED IAW-NTMMay 2, 2020 · N752CX · Boeing 7572G5 · Fuselage Miscellaneous StructureSDR 2020F00298Bulkhead · corrodedNON-ROUTINE 2832N271 DISCREPANCY, NWW, STA 263 BLKHD AFT FACE, LOWER CHORD HAS CORROSION FROM STR 26L TO STR 26R. CORRECTIVE ACTION: REPAIRED NWW STA 263 BULKHEAD LOWR CHORD PER EO CONTROL 20172 + 20181.May 2, 2020 · N752CX · Boeing 7572G5 · Fuselage Main, BulkheadSDR IXXA20180405015Spar Cap · corrodedCORRODED UPPER AFT SPAR CAP AT LEFT WS 180. REPAIRED THE SPAR CAP IAW 47313REA05.Mar 15, 2018 · N752CX · Boeing 7572G5 · Wing SparSDR IXXA20180403014Support Beam · corrodedPANEL SUPPORT BEAM INBD OF PANEL 197BL IS CORRODED. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM 53-00-04. REMOVED AND REPLACED IAW DWG 149N7550, AND SRM 51-40-02, PARA 7. AIRCRAFT GROUNDEDMar 9, 2018 · N752CX · Boeing 7572G5 · Fuselage Main, Plate/SkinSDR IXXA20180423019Stiffener · corrodedRIGHT MLG WW BS 1040 BULKHEAD ABOVE ECS DUCT,STIFFENER IS CORRODED AT FASTENER. REMOVED & REPLACED THE CHANNEL STIFFENER IAW SRM 51-40-02 & 58-757-35-0024.Mar 8, 2018 · N752CX · Boeing 7572G5 · Fuselage Miscellaneous StructureSDR IXXA20180409017Tube · crackedNR 1 PYLON AFT MOUNT BARREL NUT FWD GUIDE TUBE IS CRACKED, LANYARDS ARE NOT SECURE. REPAIRED THE MOUNT BARREL NUT FWD GUIDE TUBE IAW AMES 47313REA01 AND SECURED THE LANYARDS IAW AMM 71-21-03.Mar 8, 2018 · N752CX · Boeing 7572G5 · Nacelle/Pylon, Main FrameSDR IXXA20180409016Web · corrodedLWR KEEL WEB HAS AREA OF CORROSION AROUND HYD LINE BULKHEAD FITTING JUST FWD AND ABOVE LANDING GEAR DOOR ACTUATOR. REPAIRED THE VERTICAL LWR KEEL WEB IAW REA47313 REA 03.REINSTALLED ABOVE THE GEAR DOOR ACTUATOR. LEAK CHECKED IAW IAW AMM 29-11-00. ACFT GROUNMar 7, 2018 · N752CX · Boeing 7572G5 · Fuselage Miscellaneous StructureSDR IXXA20180403013Skin · corrodedRT OTBD FORE FLAP LOWER SURFACE HAS 2 SMALL AREAS OF CORROSION OTBD OF THE OTBD SUPPORT MECHANISM. REPAIRED THE AREAS OF CORROSION ON THE RT WING OTBD FORE FLAP LOWER SURFACE IAW SRM 57-53-01, REPAIR 5, FIG 201. AIRCRAFT GROUNDED FOR HEAVY MAINTENANCE.Mar 7, 2018 · N752CX · Boeing 7572G5 · Trailing Edge FlapsSDR IXXA2017ATN254Battery · inoperativeL4 INBOUND FLASHLIGHT BATTERY DEAD. REMOVED AND REPLACED THE BATTERY IAW AMM 25-60-00.Aug 24, 2017 · N752CX · Boeing 7572G5 · Emergency EquipmentSDR IXXA20170807268Battery · inoperativeCAPTAIN'S EMERGENCY FLASHLIGHT INOPERATIVE. REMOVED AND REPLACED THE FLASHLIGHT BATTERIES IAW AMM 25-64-00. OPS CHECKED SATISFACTORY. AIRCRAFT RELEASED TO SERVICE.Aug 2, 2017 · N752CX · Boeing 7572G5 · Emergency EquipmentSDR IXXA20170310155Compressor · stalledIN FLIGHT EMERGENCY DECLARATION. AIR TURN BACK. 5 COMPRESSOR STALLS/SURGES WITH ENGINE EXCEEDANCE VALUES RECORDED. INDICATIONS RETURNED TO NORMAL THEREAFTER AND PRIOR TO LANDING. AIRCRAFT GROUNDED FOR BORESCOPE INSPECTION AND FURTHER ANALYSIS. WORK IN PROGRESSFeb 28, 2017 · N752CX · Boeing 7572G5 · Turbine Engine Compressor SectionSDR IXXA20170217153Skin · dentedSKIN DENTED BETWEEN BS 1701 AND 1720, STRINGER 11 TO 16L. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-01, FIGURE 101. REPAIRED THE AREA IAW ENGINEERING DOCUMENT 47255REA01.Feb 14, 2017 · N752CX · Boeing 7572G5 · Fuselage Main, Plate/SkinSDR IXXA20160610040Battery Pack · inoperativeL3 AND R3 EMERGENCY EXIT DOOR LIGHTS INOPERATIVE. R & R BATTERY POWER PACK AT MID/AFT IAW AMM 33-51-07. OPS CHECK SATISFACTORY. ADDITIONAL FAULTS NOT NOTED. ACFT RELEASED TO SERVICE.Jun 5, 2016 · N752CX · Boeing 7572G5 · Emergency LightingSDR IXXA20160513027Liner · defectiveR4 DOOR WILL NOT DISARM. RETRACTABLE DOOR MECHANISM STICKING DUE TO EXCESSIVE CONTACT WITH DOOR LINERS. TRIMMED DOOR LINER ON L4 DOOR. OPERATIONAL CHECKED SATISFACTORY IAW AMM 52-11-20. ACFT RELEASED TO SERVICE.May 6, 2016 · N752CX · Boeing 7572G5 · Passenger/Crew DoorsSDR IXXA20160513024Liner · defectiveL4 DOOR WILL NOT DISARM. UPON TROUBLESHOOTING FOUND RETRACTABLE DOOR MECHANISM STICKING DUE TO EXCESSIVE CONTACT WITH DOOR LINERS. TRIMMED DOOR LINER ON L4 DOOR. OPERATIONAL CHECK SATISFACTORY. ACFT RELEASED TO SERVICE ETOPS 180.May 6, 2016 · N752CX · Boeing 7572G5 · Passenger/Crew Doors
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