N952CA
Service difficulty reports · 268
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 = 'N952CA' 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 = 'N952CA' 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 U2RA2026091100059Bottle · low pressureUPPER DECK DOOR SLIDE INFLATION CYLINDER PRESSURE LOW. REMOVED AND REPLACED DOOR SLIDE ASSEMBLY.SDR U2RA2026081700049Circuit Card · faultedON GROUND - ERRONEOUS FIRE WARNINGS - CLEANED AND RESEATED AFOLTS INTERFACE CARD. SYSTEM OPERATION NORMAL PER AIRCRAFT MAINTENANCE MANUAL 26-10-01.SDR U2RA2026051200028Longeron · cracked2EA CRACK INDICATON FOUND AT BS2598 BULKHEAD R/H S-11R LONGERON P/N 65B02522-4 PER BOEING SR MUA-MUA-26-0026-22B REPAIR CARRIED OUT PER BOEING 8100-9 DATED MAY 12-2026 AND PER BCS 202603210023-0016SDR U2RA2026051200027Frame · cracked1EA CRACK FOUND AT BS2598 BULKHEAD RHS OUTER CHORD HOLE C PER BOEING SR MUA-MUA-26-0022-07B REPAIR CARRIED OUT PER BOEING 8100-9 DATEED MAY, 12,2026.REFF BOEING BCS 202603210023-0016SDR U2RA2026051200019Stringer · crackedFCD 744-53-0025 OPEN HOLE NDI INSPECTION FOUND CRACK SIGNALS WHILE PERFORMING STA R/H 1160 AND STRINGER 10R REPAIR CARRIED OUT PER 8100-9 DATED 04/28/2026 REF BOEING COMMUNICATION SYSTEM
MESSAGE NUMBERS FOR CASE # 06320986SDR U2RA2026051200024Frame · crackedONE CRACK FOUND AT FRAME SUPPORT OF 747 SSID REV. H ITEMS F49G ON THE RHS AREA OF THE HINGE FITTING. PER BOEING SR MUAMUA26002603B. REPAIR CARRIED OUT PER BOEING 81009 DATED MAY 13 2026 AND REF BCS 202603130057009SDR U2RA2026051200025Stringer · crackedFCD 744-53-0025 OPEN HOLE NDI INSPECTION FOUND CRACK SIGNALS WHILE PERFORMING STA L/H 1160 AND STRINGER 10L REPAIR CARRIED OUT PER BOEING 8100-9 DATED MAY 12, 2026 REF BCS 0632095SDR U2RA2026051200018Tension Tie · crackedOPEN HOLE NDI INSPECTION FOUND CRACK SIGNALS AT 1120 R/H TENSION TIE. REPAIR CARRIED OUT PER 8100=9 DATED 05/08/2026 REFF BOEING COMMUNICATION CASE 063200880SDR U2RA202605000011Fastener · brokenLOCK FASTENER HEAD BROKEN AT TENSION TIE ATTACH FRAME LOCATED AT BS 1220 RT AND STRINGER 10RSDR U2RA2026051200017Doubler · crackedFINDING 002002 DOCUMENT FCD 744-53-0057-DURING C-CHECK 0.7" CRACK HAS EXTENDED FROM THE STOP HOLE OF THE PREVIOUS CRACK AT R/H STABILIZER UPPER LOBE DOUBLER. REPAIR WAS COMPLTED PER FAA 8100-9 DATED 0/21/2006 ON BOEING SERVICE REQUEST 202603060065-0011.SDR U2RA202604110007Doubler · cracked0.7" CRACK HAS EXTENDED FROM THE STOP HOLE OF THE PREVIOUS CRACK AT R/H STABILIZER UPPER LOBE DOUBLER. REPAIR COMPLETED PER :CASTLE ID: 202603060065: BOEING 8100-9 ISSUED DATED 04/21/2026. REF ID 202603060065-0011SDR U2RA202604110006Web · crackedCRACK FOUND ON FORWARD FUSELAGE WEB OF THE NOSE GEAR WELL AT STRINGER 26, BS 160-180 CORRECTIVE ACTION: CAT B. REPAIR PER SRM. REINSPECT DUE AT 33,018 CYCLESSDR U2RA2026033100003Floor Support · crackedAFT CARGO INTERCOSTAL CRACK AT STA 1940 TO STA 1960, LBL77 PERFORMED REPAIR IAW SRM 51-70-13 R1SDR U2RA202604280010Tension Tie · crackedOPEN-HOLE NDI INSPECTION FOUND DEFECT SIGNALS WHILE PERFORMING BS 1180LT - 1140 RT.SDR U2RA2020405000005Web · crackedCRACK FOUND ON FORWARD FUSELAGE WEB OF NOSE GEAR WELL AT STRINGER S-26 STA 140-160 WL 205 R&R WEB PART NUMBER 65B01870U243 IAW SRM 51-40-02SDR U2RA2026051100015Tension Tie · crackedOPEN-HOLE NDI INSPECTION FOUND DEFECT SIGNALS WHILE PERFORMING STA 1180 L/H STA 1140 R/H. REPAIR COMPLETED PER BCS MESSAGE NUMBER 06316150 INSPECTION THRESHOLD 21,108 TOTAL FLIGHT CYCLESSDR U2RA2026051100014Frame · crackedWHILE IN C CHECK - PERFORMED SURFACE HFEC INSPECTION OF FCD 744-53-0017 R2 A 1 INCH CRACK WAS FOUND ON CHORD BETWEEN S-37R AND S-38R. REPAIR PERFORMED PER BOEING BCS MUA N952CA / 25238 FRAME CRACK BS 1140 RH, RBL 80 / WL 330.SDR U2RA2025102600023Bottle · low pressureLH EMERGENCY SLIDE RESERVOIR PRESSURE IS BELOW GREEN BAND.SDR U2RA2025021900012Unknown · odorON DESCENT ELECTRICAL BURNING SMELL. STATUS: EE CLNG EXH FAN. PERFORMED EE CLNG EXT FAN GROUND TEST PER AMM 21-58-00, TEST OF. INSPECTED ELECTRONIC EQUIPMENT COMPARTMENT FOR SUSPECTED BURNING AND CHECKED FOR ALL CBS, ALL OK. NO VISIBLE BURNS OR BURNING SMELLSDR U2RA2025020300002Fuel Panel · misinstalledFUEL PANEL WAS INCORRECTLY SET AND CAUSED FUEL TO OVERBOARD THROUGH THE FUEL TANK VENT R/H. PANEL TESTED AND NO DEFECTS NOTED.SDR U2RA2025011300070Wire Harness · chafedDURING A-CHECK AT LEVEL 5 KCNW, IT WAS DISCOVERED THAT A WIRE BUNDLE WAS CHAFFING WITH POST P/N: 65B14087-3 LOCATED AT FRAME STA. 460, LBL 87. THE DAMAGE WAS MEASURED AS 4MM X 5MM, WHICH IS OUT OF LIMITS. PERMANENT REPAIR ACCOMPLISHED IN ACCORDANCE WITH FVCI ESDR U2RA2025011100069Reservoir · low pressureDURING A-CHECK INSPECTION AT LEVEL 5 AEROSPACE KCNW, IT WAS FOUND THAT EMERGENCY POWER RESERVOIR P/N: 1270156-4 S/N: ALT183-3683 HAS LOW PRESSURE. EMERGENCY POWER RESERVOIR P/N: 1270156-4 S/N: ALT183-3683 WAS REMOVED AND REPLACED ON NR 0072 UNDER LEVEL 5 AEROSSDR U2RA2024081500023Pressure Deck · crackedDURING C CHECK IN GMF, FOUND CRACK ON SKIN AT LH WLG W/W CANTED PRESSURE DECK STA 1241LBL 11.33 CATEGORY B REPAIR WAS ACCOMPLISED IN ACCORDANCE WITH BOEING MESSAGE BOE MUA-MUA 24-0122SDR U2RA202406040146Skin · crackedDURING C CHECK IN GMF FOUND CRACK ON SKIN AT LH WLG CANTED PRESSURE DECT STA 1241 LBL 11.33. CATEGORY B REPAIR WAS ACCOMPLISHED IN ACCORDANCE WITH BOEING MESSAGE NUMBER- BOE-MUA-24-0122SDR U2RA2024081500040Skin · damagedFOUND RIVET HOLES ELOGATED ON SKIN 2700 LH SIDE AFTER MEASURMENT RIVET HOLES DIAMETER BETWEEN .280 INCH UP TO .320 INCHSDR U2RA2024081500039Support Frame · corrodedDURING MAINTENANCE C CHECK AT GMF FOUND LOWER FUSALAGE STA 1000 CENTER TO RH SIDE SUPPORT FRAME FOR BODY FAIRING CORRISON . REAPIR ACCOMPLISHED IN ACCORDANCE WITH SRM 51-70-12 (REV59/20FEB2024) AND WAS A CAT A REPAIR.SDR U2RA2024081500038Fairing · crackedWHILE PERFORMING C CHECK RH WING O/B AILERON UPPERSURFACE L/E FAIRING CRACK POS O/B SIDE REPAIR WAS ACCOMPLISHED IN ACCORDANCE WITH SRM 57-60-01 REPAIR 1 (REV59 20FEB2024)SDR U2RA2024082100022Fairing · corrodedWHILE PERFORMING C CHECK RH WING O/B AILERON UPPER SURFACE LE FAIRING CRACK POS CENTER REPAIR WAS ACCOMPLISHED IN ACCORDANCE WITH SRM 57-60-01 REPAIR 1 (REV 59 20FEB2024.SDR U2RA2024081500036Bracket · crackedWHILE PERFORMING C CHECK RH WING O/B AILERON UPPER SURFACCE BRACKET FE FAIRING CRACK POS I/B SIDE. REPAIR WAS ACCOMPLISED IN ACCORDANCE WITH SRM 57-60-01 REPAIR 1 (REV 59 20FEB2024)SDR U2RA2024081500035Bracket · corrodedWHILE PERFOMING C CHECK IN GMF RH WING O/B AILERON BRACKET BALLAST CORROSION POS #1 FROM O/B. REPAIR WAS ACCOMPLISHED IN ACCORDANCE WITH SRM 57-56-02 REPAIR 1 (REV 59 20FEB2024)SDR U2RA2024081500034Structure · corrodedWHILE PERFOMING C CHECK IN GMF FOUND CORROSION ON LH WING L/E CHORD OLES 1530. THIS REPAIR IS CATEGORY A. REPAIR WAS ACCOMPLISHED IN ACCORDANCE WITH SRM 57-41-13 REPAIR 1 & 51-70-11 (REV 59 20FEB 2024)SDR U2RA2024081500033Cargo Track · chafedWHILE PERFORMING C CHECK IN GMF FOUND CHAFING ON FWD CARGO COMPARTMENT SEAT TRACK AT STA 570 RBL 45.5 THIS REPAIR IS CATEGORY A REPAIR WAS ACCOMPLICHED IN ACCORDANCE WITH SRM 53-00-52 REPAIR 10 (RREV 59 20FEB2024)SDR U2RA2024081500032Bracket · crackedWHILE PERFORMING C CHECK RH WING O/B AILRERON UPPER SURFACE BRAKET LE FAIRING CRACK POS I/B SIDE. REPAIR WAS ACCOMPLISED IN ACCORDANCE WITH SRM 57-60-01 REPAIR 1 (REV 59/20FEB2024)SDR U2RA2024081500031Support Frame · corrodedWHILE PERFORMING C CHECK IN GMF FOUND CORRISION OUT OF LIMTS ON STA 1000 LBL 11.33-37.50 SUPPORT FRAME FOR BODY FAIRING THIS REPAIR IS CATIGORY A REPAIR WAS ACCOMPLISHE IN ACCORDANCE WITH THE SRM 51-70-12 (REV 59,20 FEB/2024SDR U2RA2024081500030Skin · corrodedRT SIDE FUSELAGE INNER WINDOW BELT CORROSION AT STA 1000 STR 15-STR 23SDR U2RA2024081500029Skin · damagedFOUND RIVET HOLES ELOGATED ON SKIN RH SIDE AFTER MEASURMENT RIVET HOLES DIAMETER IS BETWEEN .280 TO .320 INCHSDR U2RA2024081500028Skin · temp repairDURING CHECK AT GMF FOUND TEMPERARY REPAIR AT LH WING LEADING EDGE WS 1000 THAT NEEDS REPLACED TO PERMANET REPAIR CATEGORY A REPAIR WAS ACCOMPLISHED IN ACCORDANCE WITH SRM 57-41-01 REPAIR 6 (REV 59/20 FEB 2023SDR U2RA2024081500027Skin · puncturedWHILE PERFORMING C CHECK IN GMF RH WING AILERON LOWER SURFACE PUNCTURE REPAIR WAS ACCOMPLISHED IN ACCORDANCE WITH SRM 57-60-01 REPAIR 1 (REV 59/20FEB 2024SDR U2RA2024081500026Web · crackedDURING C CHECK IN GMF FOUND CRACK AT MED#1 RH UPPER SILL WEB CRACK AT STA 480 STR 16R CATEGORY B REPAIR WAS ACCOMPISHED IN ACCORDANCE WITH SRM 53-10-15 REPAIR 1 (REV 59/20 FEB 2024SDR U2RA2024081500025Reveal · crackedWHILE PERFORMING C CHECK IN GMF FOUND CRACK AT MED#5 CUTOUT DOOR REVEAL AT STA 2240 STR 21 NEAR DOOR LOCK RELEASE THIS REPAIR IS ACCOMPLISHED ANS CATOGORIZED AS CAT A REPAIR IN ACCORDANCE WITH SRM 53-60-15 REPAIR 7 (REV 59/20 FEB 2024SDR U2RA2024081500024Pressure Deck · crackedWHILE PERFOMING C CHEHCK IN GMF, FOUNF CRACK ON SKIN AT RH W/G W/W CANTED PRESSURE DECK SURFACE SKIN AT STA 1241 RBL 5.5 CATEGORY B REPAIR WAS ACCOMPLISHED IN ACCORDANCE WITH SRM 53-40-51 REPAIR 6 (REV 59, 20 FEB /2024SDR U2RA2024031500004Battery · no testUPPER DECK RIGHT EMERGENCY DOOR BATTER TEST FAIL - REMOVED AND REPLACED BATTERY PACK IN ACCORDANCE WITH MAINTENANCE MANUAL. OPS CHECK OK.SDR U2RA2024012300001Nose Cowl · dentedAIRCRAFT SUSTAINED DAMAGE TO #4 ENGINE NOSE COWL DURING GROUND HANDLING. ACCOMPLISHED TEMPORARY REPAIR TO NOSE COWL PER FVCI EO 24009-1. THIS IS A TEMPORARY REPAIR AND WILL REQUIRED PERMANENT REPAIR OR COWL REPLACEMENT.SDR U2RA2023091100044Skin Panel · gougedDURING OFF-LOADING OF CARGO, CARGO LOADING VEHICLE STRUCK THE SEAL DEPRESSOR AT THE FORWARD LOWER CORNER OF THE DOOR CUT-OUT. DAMAGE OCCURRED TO AN EXISTING REPAIR DOUBLER; REFER TO AML #63577-2 AND FVCI E.O. 23184-1 REV. IR DATED 09/08/2023. DAMAGED DOUBLERSDR U2RA2023081500040Lamp · inoperativeDURING A-CHECK WO 230107, MRO HANGAR 901 DISCOVERED A MID EMERGENCY LIGHT IN FLIGHT DECK WAS NOT ILLUMINATING. THE LIGHT BULB WAS REPLACED WITH AN ILLUMINATION TEST PRODUCING SATISFACTORY RESULT. SEE HANGAR 901 (CRS: HAIY901D) PROJECT# H1-23-05-00084, WO 18590SDR U2RA2023081100039Cartridge · out of toleranceDURING A-CHECK, ACCOMPLISHMENT OF SCHEDULED BOEING 747 TASK CARD 52-023-05-01, LEFT HAND UPPER DOOR, DISCHARGE CARTRIAGE FOR THE PRESSURE VESSEL M7039 FAILED THE RESISTANCE CHECK. WORK ACCOMPLISHED ON CRS# HAIY901D) HANGAR 901, PROJECT H1-23-05-00084, W/O 1859SDR U2RA2023081100038Cartridge · no testDURING A-CHECK, ACCOMPLISHMENT OF SCHEDULED BOEING 747 TASK CARD 52-023-05-01, RIGHT HAND UPPER DOOR, BATTERY PACK M7038 FAILED TO TEST ON PRESS-TO-TEST SWITCH. WORK ACCOMPLISHED ON (CRS# HAIY901D) HANGAR 901, PROJECT H1-23-05-00084, W/O 18590, NR 0047.SDR U2RA2023081100037Cartridge · no testDURING A-CHECK, ACCOMPLISHMENT OF SCHEDULED BOEING 747 TASK CARD 52-023-05-01, LEFT HAND UPPER DOOR, BATTERY PACK M7037 FAILED TO TEST ON PRESS-TO-TEST SWITCH. WORK ACCOMPLISHED ON (CRS# HAIY901D) HANGAR 901, PROJECT H1-23-05-00084, W/O 18590, NR 0046.SDR 2023F00140Unknown · unknownDURING INSPECTION FOR ROUTINE WO 18360 – 0137 (SB TABLE 2 - INBOARD FLAP INSPECTION/LUBRICATION - AD 2021-02-15 (G)). IT WAS FOUND THAT ON SEQUENCE CARRIAGE NR 5 (R/H WING INBOARD FOREFLAP TRACK# 5), THE NUT ITEM NO. 11, WASHER ITEM NO. 12, OUTER CLAMP-UP WASSDR U2RA2023040300018Unknown · unknownDURING ROUTINE INSPECTION, FOUND RIGHT INBOARD MID FLAP WITH GROUND DAMAGE (DENTED). ACCOMPLISHED A TIME LIMITED MAJOR REPAIR PER FLIGHT VEHICLES CONSULTING ENGINEERING ORDER 23069-1. DATA APPROVED ON FAA FORM 8110-3 DATED 3/31/2023 BY R. MANASHI DERT-876272
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