Service difficulty reports
1,770,704 reports of malfunctions and defects, newest first. Air carriers must report; general aviation reporting is voluntary.
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' 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' 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 QR9R2026081200001Gcu · faulted#2 GEN DISCON CAUTION APPEARED AFTER BOTH ENGINES WERE STARTED, ZERO AMPS ON NR 2. REMOVED AND REPLACED NR 2 GCU IAW 24-30-00, 4-1. MOC SUCCESSFULLY COMPLETED.SDR IPXA2026081238198Pump · low pressureEMERGENCY DECLARED, GREEN ENG HYD PUMP 2 LOW PRESSURE FOLLOWED ECAM ,SELECTED OFF , RESULTED IN LOSS OF GREEN HYD FLUID RESULTED IN GREEN HYD FALURE.SDR DALA2026081204635Wire · damagedSEAT 44AB ESCAPE PATH LIGHT INOPERATIVE. REPAIRED WIRING IAW AMM 33-51. OK FOR SERVICE. (9186616) AIRCRAFT WAS GROUNDED.SDR DALA2026081204633Latch · fodL2 DOOR WILL NOT ARM. REMOVED DEBRIS FROM LATCH ASSY IAW AMM 52-12. OPS CHKD GOOD. (9095152) AIRCRAFT WAS GROUNDED.SDR AALA202608128889Bottle · low pressureAIRCRAFT WAS NOT GROUNDED: R4 DOOR DAMPER AND EMERGENCY OPERATION CYLINDER PRESSURE LOW - SERVICED DOOR DAMPER AND EMERGENCY OPERATION CYLINDER PER JOB CARD 26L80052001SDR AALA202608128534Bottle · low pressureAIRCRAFT WAS NOT GROUNDED: CHECK DOOR PRESSURE INDICATED ON FORWARD ATTENDANT PANEL FOR DOOR L1. ALL INDICATIONS NORMAL IN THE FLIGHT DECK - MAINTENANCE SERVICED THE L1 DOOR DAMPER AND EMERGENCY OPERATION CYLINDER IAW AMM 52-10-00SDR DALA2026081204632Coffeemaker · faultedAFT INBD COFFEEMAKER WILL NOT SECURE. BOTH COFFEEMAKER CIRCUIT BREAKERS PULLED IN AFT GALLEY AS PRECAUTION DUE TO LOG 9170338. R & R AFT INBD COFFEEMAKER DISPENSER IAW AMM 25-35, OPS CHK GOOD. (LP: 9170339, AIRCRAFT WAS GROUNDED)SDR DALA2026081204630Display · shortedSMOKE IN THE COCKPIT DUE TO UPPER ECAM DISPLAY SHORTED, CREW TURNED OFF DISPLAY AND SMOKE DISSIPATED. REPLACED UPPER ECAM DU (4WT1). (LP: 9588150, AIRCRAFT WAS GROUNDED)SDR CALA2026081218528Lamp · inoperativeEMERGENCY EXIT SIGN NEAR DOOR R2 HAS SEVERAL LAMPS INOPERATIVE. R & R THE LAMPS IAW AMM 33-51-01, OPS CHECK SAT.SDR AALA202611042629Fork · burredAIRCRAFT IN BASE MAINTENANCE: DURING INSPECTION OF 80VU RACK ON JOBCARD 26T12053007 FOUND LEFT LOWER LATERAL FITTING TO BE BURRED W=0.320 INCH ON LEFT-HAND STRINGER 32. MAINTENANCE PERFORMED PERMANENT REPAIR ON 80VU RACK LOWER LATERAL FITTINGS LEFT AND RIGHT SSDR AALA202611028578Fork · burredAIRCRAFT IN BASE MAINTENANCE: DURING INSPECTION OF 80VU RACK ON J/C 26T12053007 FOUND L/H LOWER LATERAL FITTING TO BE BURRED (FORK END RH SIDE REPLACED DUE TO KIT). MAINTENANCE REPLACED PART WITH IDENTICAL PART, PERFORMED PERMANENT REPAIR ON 80VU RACK LOWER LASDR IPXA2026100732340Floorbeam · damagedFLOORBEAM AT FR54, BTW Y2462 AND Y1959 HAS A GOUGE AROUND SCREW HOLE ON BOTTOM SIDE. INSTALLED NEW FLOORBEAM AT FR54, BTW Y2462 AND Y1959 MDC, IAW SRM 51-40-21.SDR IPXA2026100632273Adapter · corrodedMAIN DECK FLOOR STRUCTURE, AT FR 62 Y0, CLS ADAPTER HAS CORROSION. INSTALLATION OF NEW CLS ADAPTER AT FR 62 Y0 I.AW. A300-600 SRM 51-40-21-001.SDR IPXA2026100632272Adapter · corrodedMAIN DECK FLOOR STRUCTURE, AT FR 58 Y0, CLS ADAPTER HAS CORROSION. INSTALLATION OF NEW CLS ADAPTER AT MD FLOOR STRUCTURE AT FR58 Y0 IAW SRM 51-40-21-001,SDR IPXA2026100632726Adapter · corrodedMDC FLOOR, FR 60, Y0 R/H CLS ADAPTER WITH CORROSION. VERIFIED INSTALLATION OF NEW CLS ADAPTER AT FR 60, Y0 R/H I.AW. SRM 51-40-21-001. INSTALLATION OF NEW CLS ADAPTER AT FR 60, Y0 R/H I.AW. A300-600 SRM 51-40-21-001. VERIFIED PARTS MARKING IAW UPS GMM 09-08.SDR IPXA2026100632694Adapter · corrodedMDC FLOOR, FR 65, Y0 R/H CLS ADAPTER WITH CORROSION. VERIFIED CLS ADAPTER INSTALLATION PER SRM 51-40-21-001SDR IPXA2026100632584Adapter · corrodedMDC FLOOR, FR 66, Y0 R/H CLS ADAPTER WITH CORROSION. INSTALLED NEW CLS ADAPTER AT Z200 - MDC FLOOR, FR 66, Y0 R/H.P/N UPA53275455201.TRAVELER # T26/1875628.I.A.W A300-600 SRM 51-40-21-001.SDR IPXA2026100632573Adapter · corrodedMDC FLOOR, FR 75, L/H SIDE OF -Y1580.5, CLS ADAPTER WITH CORROSION ON BASE. INSTALLED NEW CLS ADAPTER AT Z200 - MDC FLOOR, FR 75, L/H SIDE OF -Y1580.5. I.A.W A300-600 SRM 51-40-21-001.SDR IPXA2026100632700Seat Track · corrodedMAJOR REPAIR, MDC SEAT TRACK, BTWN FR 65 & 66, Y0, CORRODED. LOCATED AND DRILLED.SDR IPXA2026100132589Seat Track · corrodedMAJOR REPAIR, MDC FLOOR, BTW FR 71 & 72, -Y1456, SEAT TRACK CORRODED AT R/H LATERAL FACE. LOCATED AND DRILLED A SPLICE SEAT TRACK AND SPLICE UNION IAW SRM 53-10-16, FIG 201, AND SRM 51-40-44.SDR SWIA2026081177533Floorbeam · elongatedWHILE LOCATING AND DRILLING NEW SERVICEABLE RH CAP ANGLE PN CC670-34096-1, ELONGATED 1EA NUTPLATE HOLE IN FS 280 BEAM PN CC670-34094JP-2 AT APPROX RBL 38 C-CHECK RO 10062026COMPLIED WITH CUTOUT REPAIR TO ELONGATED NUTPLATE SCREW HOLE IN FS280 CROSSBEAM BETWESDR SIMA20260811006Doubler · corrodedCOCKPIT FLOOR STRUCTURE UNDER CO-PILOTS SIDE FLOORBOARDS HAVE NUMEROUS AREAS OF CORROSION. (MAJOR REPAIR) (LEVEL 2 CORROSION). PERFORMED PERMANENT REINFORCING REPAIR ON CO-PILOTS COCKPIT FLOOR IAW ENVOY ERS-EJ-53MR-5524.SDR SIMA20260811005Seal Depressor · crackedFWD SRVICE DOOR FWD UPPER SEAL DEPRESSOR INTERIOR PLATE HAS POSSIBLE CRACK. (MAJOR REPAIR). RAR FWD SRVICE DOOR FWD UPPER SEAL DEPRESSOR IAW ERJ 170 SRM 51-40-08.SDR SIMA20260811004Doubler · corrodedCOCKPIT FLOOR STRUCTURE UNDER PILOTS SIDE FLOORBOARDS HAVE NUMEROUS AREAS OF CORROSION. (MAJOR REPAIR). REMOVED AND REPLACED COCKPIT FLOOR STRUCTURE UNDER PILOTS SIDE FLOORBOARDS IAW ERS-EJ-53MR-5525.SDR U2RA202609070005Frame · crackedR/H WING TO BODY FAIRING (STA 880 ) STRUCTURE CRACK ON FRAME ASSY AT BSTA 800, RBL 125,WL 180 PERMANENT REPAIR PER B747 SRM 53-00-71 REPAIR A. WITHOUT DEVIATIONS FAA FORM 8100-9 ISSUEDSDR CALA2026092819856Doubler · damagedFUSELAGE SEC 46 SKIN DOUBLER REPAIR BS 1219 - 1241, S28 - 29L, REQUIRES ACCOMPLISHMENT OF PART 1 INTERIM REPAIR. PER ECRA 5360-02189, ACCOMPLISHED PART 1, STEP 1, & 2. STEP 2- REVIEWED GMM 08-05-25 AND OTHER DOCUMENTS AS NECESSARY AND ENSURED COMPLIANCE WITHSDR AALA202609279871Hinge Fitting · excess playAIRCRAFT IN BASE MAINTENANCE: NOSE LANDING GEAR AFT RIGHT DOOR AFT HINGE FITTING HAS EXCESSIVE PLAY - REPLACED HINGE FITTING POER CMM 52-82-32SDR AALA202609279849Hinge Fitting · excess playAIRCRAFT IN BASE MAINTENANCE: NOSE LANDING GEAR AFT RIGHT DOOR FORWARD HINGE FITTING HAS EXCESSIVE PLAY - REPLACED HINGE FITTING POER CMM 52-82-32SDR SWIA2026081177258Vane · chafedLEFT INBD FLAP VANE, INBD LEADING EDGE CAP REQUIRES REPLACEMENT DUE TO CHAFE DAMAGE OUT OF LIMITS. REPLACED THE CHAFED FLAP VANE IAW SRM 51-42-13, & DWG 601R14302, REV E. COMPLIED WITH SKY CARD 51-900-1003 SKY. MAJOR REPAIRSDR SWIA2026081177257Vane · chafedLEFT INBD FLAP VANE, OTBD LEADING EDGE CAP REQUIRES REPLACEMENT DUE TO CHAFE DAMAGE OUT OF LIMITS. REPLACED THE CHAFED FLAP VANE IAW SRM 51-42-13, & DWG 601R14302, REV E. COMPLIED WITH SKY CARD 51-900-1003 SKY. MAJOR REPAIR.SDR IPXA2026090730575Mount · gougedSTR- DURING OK TO INSTALL FOUND #2 ENG PYLON AFT STRUT MOUNT I/B SIDE TO HAVE (3) GOUGES FROM BULGING SCREWS ON PNL 443ML ATA 54 ACCOMPLISHED THE REPAIR PER EO-98451-REQ1 AND STE-SAA EA 757-5724-01-B0812 REV IR. CASS FORM COMPLETED ON T3F18E009C5M2SDR IPXA2026090532016Support · crackedMAIN DECK FLOOR STRUCTURE, AT FR 74 AND 75 LH SIDE, Z-PROFILE HAS CRACKS (2EA SPOTS). INSTALLED NEW T-PROFILE IN MAIN DECK FLOOR STRUCTURE, AT FR 74 AND 75 LH SIDE. IAW SRM 51-40-21-001 AND SRM 53-18-18-001.SDR IPXA2026092127542Support · crackedLEFT FR 47 HORIZONTAL JUNCTION AREA. CRACK INDICATION NOTED AT HOLE "P" IN ALL LAYERS. VERIFIED E.A.#300-5710-27-A4579, PRELIMINARY 4, STEP 56. VERIFIED UPS EO-68606-JIC001 INSTRUCTIONS COMPLETED (T3F18E002MT2B).SDR IPXA2026092127516Support · crackedLEFT FR47 HORIZONTAL JUNCTION AREA. CRACK INDICATION NOTED AT HOLE "D" IN ALL LAYERS. VERIFIED E.A.#300-5710-27-A4579, PRELIMINARY 4, STEP 56. VERIFIED UPS EO-68606-JIC001 INSTRUCTIONS COMPLETED (T3F18E002MT2B).SDR IPXA2026092127471Support · crackedLEFT FR 47, HORIZONTAL JUNCTION AREA. CRACK INDICATION NOTED AT HOLE B IN ALL LAYERS. VERIFIED E.A.#300-5710-27-A4579, PRELIMINARY 4, STEP 56. VERIFIED UPS EO-68606-JIC001 INSTRUCTIONS COMPLETED (T3F18E002MT2B).SDR IPXA2026090432523Seat Track · corrodedMDC FLOOR, FR 80, -Y450, SEAT TRACK WITH CORROSION. VERIFIED APPLICATION OF SURFACE PROTECTION COATS IAW SRM 51-75-10. AND GMM 04.02 VERIFIED REMOVAL OF EWIS PROTECTION IAW ESPM 20-54-50-02.SDR IPXA2026090332495Seat Track · corrodedMDC FLOOR, FR 80, Y0, SEAT TRACK WITH CORROSION. VERIFIED APPLICATION OF SURFACE PROTECTION COATS IAW A300-600 SRM 51-75-10. AND UPS GMM 04.02 VERIFIED REMOVAL OF EWIS PROTECTION IAW A300-600 ESPM 20-54-50-02.SDR IPXA2026090331979Seat Track · corrodedMAIN DECK FLOOR STRUCTURE, AT FR 80 SEAT TRACK Y450 HAD CORROSION (2EA SPOTS). INSTALLATION OF SPLICE SEAT TRACK 2EA P\N: R5327049020000 BTCH: 0004506809 AND SEAT TRACK 1EA P\N: R5307007120200 BTCH: 0004479769, IAW A300-600 SRM 51-40-21 AND SRM 53-10-16. ANDSDR IPXA2026092132499Profile · crackedMDC, FR 80, R/H Z PROFILE WITH CRACK. INSTALLED T-PROFILE R/H SIDE . IAW SRM 53-18-15-001 AND SRM 53-21-10-001.SDR IPXA2026092131455Floor Support · crackedMAIN DECK FLOOR STRUCTURE, AT FR 80/82, LT SIDE BTWN Y1221.2 AND Y1580.5, Z PROFILE HAS A CRACK. INSTALLED T-PROFILE L/H SIDE P/N: A53981401200; BATCH: 0004506526 MAIN DECK FLOOR STRUCTURE, AT FR 80/82, LH SIDE BTWN Y1221.2 AND Y1580.5, I.A.W A300-600 SRM 53-SDR IPXA2026090432479Seat Track · corrodedMDC FLOOR, FR 80, -Y1137.1, SEAT TRACK CORRODED. .INSTALLED NEW SECTION OF SEAT-TRACK P/N: R5307007120200 AND 02EA SPLICE P/N: R5327049020000 IN MDC FLOOR, FR 80, -Y1137.1. IAW A300-600 SRM 53-10-16 AND SRM 51-40-21-001.SDR IPXA2026091527525Spar · crackedLEFT FR 47 HORIZONTAL JUNCTION AREA. CRACK INDICATION NOTED AT HOLE F IN ALL LAYERS. VERIFIED EA 300-5710-27-A4579, PRELIMINARY 4, STEP 56.SDR SWAA2026092149269Scuff Plate · crackedCRACK ON THE FWD CORNER SCUFF PLATE IN THE AFT CARGO BAY. REPAIRED THE FWD CORNER SCUFF PLATE IAW SRM 53-60-15-2R-1, REPAIR 1, & BAC 5975.SDR SWAA2026092104666Strap · corrodedCORROSION ON STRAP, BS 420 - 500, STR 25L IN THE FWD CARGO BAY. EVALUATED CAPSTRIP AND DID NOT FIND ALLOWABLE DAMAGE IAW SRM 53-00-53-1A- 2, REPLACED THE CAPSTRIP (STRAP) IAW SRM 51-10-02-0G, STEP 9, AND DWG 453A1600, SHEET 106, REV-.SDR SWAA2026091028072Fairing · crackedNR 1 ENGINE AFT FAIRING TRAILING EDGE IS CRACKED. REMOVED AND REPLACED #1 ENGINE AFT FAIRING TRAILING EDGE IAW SRM 51-40-02-0G-0 SRM 51-40-05-0G-0 DWG 313A2400 REV E. DWG 313A2700 REV B AIPC 54-52-06-03 ALL STEPS COMPLETED.SDR SWAA2026091039814Intercostal · crackedMAIN CABIN FWD WET AREA, LH SIDE: STRUCTURE INTERCOSTAL HAS A CRACK BETWEEN STA 294.5 AND 303.9, STR 16L. MAIN CABIN FWD WET AREA LH SIDE: STRUCTURE INTERCOSTAL HAS A CRACK BETWEEN STA 294.5 AND 303.9 STR 16L. REMOVED AND REPLACED INTERCOSTAL DUE TO NO LIMITS SDR SWAA2026091002390Baffle · crackedFWD CARGO BAY BAFFLE BS440 TO BS460 WL156 LBL25 IS CRACKED CRACKED ON FWD CARGO BAY L/H BAFFLE FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS ARE GIVEN IN THE SRM. PART REPLACEMENT REQUIRED IAW SRM 51-10-02-0G-0. REMOVED AND REPLACED BAFFLE BS440 TO BS460 WL156 LBSDR REXA2026091001789Stringer · damagedMISDRILL AND ELONGATED HOLES ON STGR 24RH BTW FS 501 AND FS 517 WERE FOUND AT FWD CARGO COMPARTMENT STRUCTURE, STGR 24RH BTW FS 501 AND FS 517 AT FWD CARGO COMPARTMENT STRUCTURE WAS REPAIRED PER CRJ900 SRM53-00-03-201-001-A02SDR CNMA20260910002Stiffener · crackedCRACKED STIFFENER AT STA 246.0 FLOORBEAM FWD SIDE LBL 40SDR AALA202609041633Web · corrodedAIRCRAFT IN BASE MAINTENANCE: FOUND EXFOLIATION CORROSION ON WEB AROUND GALLEY MOUNT AREA AT FS 988 RBL 32. REMOVED AND REPLACED WEB IAW BOEING DRAWING 147A5700 AND EA 378310.