Service difficulty reports
1,771,154 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 R61A2026072600211Skin · crackedFOUND CRACK ON RH WING MAIN BOX, LOWER SKIN, INBOARD OF RIB 17. MAJOR REPAIR, MECHANIC PERFORMED REPAIR TO RT WING MAIN BOX IAW WITH ETD2026-170-012770 AND SRIIM CHAPTER 51INSPECTOR PERFORMED RII INSPECTION OF MAJOR REPAIR IAW ETD2026-170-012770 AND SRIIM TASDR CALA2026072818063Engine · odorSMELLED BURNING/COOKING ODOR WHEN POWER LEVERS ADVANCED FOR TAKEOFF. ODOR DISSIPATED A FEW MINUTES AFTER TAKEOFF. THROUGHOUT FLT ENG 2 SHOWED APPROX 30DEG. HIGHER EGT THAN ENG 1 AND APPROX 400LB/HR HIGHER FUEL BURN. FLIGHT CREW STATED ODOR WENT AWAY AFTER TSDR KCSA2026072643Door · no discrepancyDOOR ENTRY L5. VERIFIED #5 ENTRY DOOR WARN SWITCH IAW B747-400 AMM 52-11-01. OPS CHECK GOOD.SDR CALA2026072718059Skin · crackedHIDDEN DAMAGE INSP, RT WING INBD FLAP UPPER SKIN CRACKED APPROX 2"AT I/B SIDE. REMOVED 70 E/A FASTENERS AND INSTALLED RT WING INBD FLAP UPPER, REMOVED AND INSTALLED 3 E/A BOLTS IAW B757-200 SRM 51-40-02-0G-0, PERFORMED POST REPAIR INSPECTION AT RT WING INBD FSDR CALA2026072718057Pan · corrodedCORROSION AT AFT CARGO WASTE TANK BAY BETWEEN STA 847 AND 867 ON FUSELAGE PAN AREA NEAR RISE HOSE FITTING. REMOVED AND REPLACED PAN ASSEMBLY IN REF TO B-737NG SRM 51-40-02, SRM 51-40-05 & DWG 146A7401.SDR 2026072609019Landing Gear · faultedWE WERE CLIMBING THROUGH APPROXIMATELY FL200 WHEN WE FELT A CLUNK IN THE NOSE AREA WE THINK, AND THE RED, "GEAR UNLOCK" LIGHT ILLUMINATED AND STAYED ON FOR THE DURATION OF THE FLIGHT UNTIL WE SELECTED GEAR DOWN AGAIN FOR LANDING. WE GOT THE LIGHT IN THE CLIMB SDR SWAA2026072796341Slide · low pressureAFT SVC DOOR SLIDE PRESSURE GAUGE IN THE RED. REMOVED AND REPLACED IAW AMM 25-66-01-401.SDR SWAA2026072726286Power Supply · faultedOVERWING EMERGENCY LIGHTS ON LEFT SIDE DOOR STAYS ILLUMINATED IN ARM POSITION. REMOVED AND REPLACED M1694 LT OVERWING EGRESS LIGHT BATTERY AND POWER SUPPLY IAW M/M 33-51-06SDR SWIA2026072676674Warning Message · illuminatedFLAP FAIL CAUTION MESSAGE. QRH ACTION. LANDED FLAPS 1 UNEVENTFUL. BRAKES 6996 (FLIGHT 4288) OPEN.SDR FJTA2026072716502Windshield · crackedWHILE CLIMBING THROUGH FL220 THE OUTER PANE OF THE FIRST OFFICER'S WINDSHIELD SHATTERED. THIS WINDSHIELD WAS RECENTLY REPLACED ON 7/18/2026 WITH AN OVERHAULED UNIT. TAT AT REPLACEMENT WAS 23586.9 AND TAC 25141.SDR VNAA2026072721301Structure · damagedBIRDSTRIKE WITH LARGE BIRD AT 800FT AGL ON TAKE OFF. MAIN IMPACT BELOW FO'S WINDSHIELD. [AROUND 160KTS] / REPAIR COMPLETED IAW WITH REO 690-53-11-2228 AND SRM 51-40-11-001-001-A01SDR ABXA20260726336Circuit Breaker · trippedFIRE DET. CARGO DC CB OPEN. RESET FIRE DET CARGO DC CB, PERFORMED AFLOT DET. TEST NO ISSUES NOTED, SYSTEM OK AT THIS TIME, IAW AMM 26-11-00 AND 20-60-01 AIRCRAFT REMAINS ETOPS 180. A/C RETURNED TO SERVICE.SDR HNAA2026072700637A/C Pack · odorOIL SMELL IN FLIGHTDECK FROM PACK 1. FACT 27JUL26 01:02 CLT INSPECTED PAX 1. FOUND TO BE GOOD. FOUND PAX 2 TO HAVE MELTED DUCT. REMOVED AND REPLACED DUCT AS REQUIRED. PERFORMED OP CHECK IAW 21-51-00. OP CHECK GOOD. NO DEFECTS NOTED A/C OKAY FOR SERVICESDR HNAA2026072700636Unknown · odorWHILE TAXIING BURNING OIL SMELL NOTED IN CABIN AND ON FLIGHT DECK. RAN BOTH PACKS WITH BOTH ENGINES AND APU BLEEDS. NO ODOR NOTED. SUSPECT ODOR TO BE FROM FAILED E2 STARTUP. A/C OK FOR SERVICE AT THIS TIMESDR HNAA2026072700634Control Panel · faultedUNABLE TO CONTROL EMERGENCY LIGHTS FROM FLIGHT ATTENDANT PANEL. R & R F/A'S CONTROL PANEL IAW AMM 25-27-09-000 AND 400-801-A. OPS CHECK GOOD. OK FOR SERVICE.SDR YENA2026072700624Warning Message · illuminatedFLT 346, BCN-BOS. (ETOPS) ACFT GEN CLASS II MESSAGE APPEARED AFTER ENGINE SHUTDOWN ( CLASS II MAINTENANCE MESSAGES DISPLAYED ON ECAM STATUS PAGE OF ECAM SYSTEM DISPLAY FAULT(S) INDICATED BY GPCU OR AC GEN ) OPEN.SDR YENA2026072700623Warning Message · illuminatedFLT 1926, LGW-BOS. (ETOPS) ENGINE 1 HEAT SYSTEM DEGRADED ECAM ON TAXI TO GATE EXTINGUISHED ON ENGINE SHUT DOWN ( HEAT SYS DEGRAD CAUTIONS ON ECAM E/WD) OPEN.SDR DXTA2026072709019Warning Message · illuminatedWE WERE CLIMBING THROUGH APPROXIMATELY FL200 WHEN WE FELT A CLUNK IN THE NOSE AREA WE THINK, AND THE RED, GEAR UNLOCK LIGHT ILLUMINATED AND STAYED ON FOR THE DURATION OF THE FLIGHT UNTIL WE SELECTED GEAR DOWN AGAIN FOR LANDING. WE GOT THE LIGHT IN THE CLIMB ANSDR QMLA2026072720050Unknown · odorDURING THE FLIGHT, AN ONGOING FUEL ODOR WAS PRESENT IN THE CABIN. BOTH CREW MEMBERS DETECTED THE ODOR, AND THE NURSE REPORTED BECOMING NAUSEATED FROM THE ODOR. AFTER SHUTDOWN, ENTERED THE AFT CABIN AND CONFIRMED THE FUEL ODOR WAS STILL PRESENT. THE ODOR WAS SDR CALA2026072718045Sign · detachedEMERGENCY EXIT SIGN AND THE FA CALL PANEL IN THE AFT GALLEY LOOSE AND HANGING CROOKED. REPLACED AFT OVERHEAD EMER LIGHT ASSY. EMER LIGHTS AND PA CALL LIGHTS CK NORMAL.SDR CALA2026072718044Battery · faultedCABIN EMERGENCY LIGHTING OP CHK SHOWS FAULT, EPSU UNIT FWD LT, ON PTP SCREEN. REMOVED AND REPLACED FWD LT EPSU BATTERY IAW AMM 33-51-38. PTP CABIN EMERGENCY LIGHTING OP CHK GOOD. OK TO SERVICE.SDR CALA2026072718039Skin · gougedRAMP REPORTS GOUGE ON LT FUSELAGE UNDER CAPTAIN'S SIDE WINDOW. DENT LOCATED BTWN BS 251.5 - 259.5, & STRINGERS 19-20L. . REMOVED SCRATCH IAW SRM 53-00-01-1A-1, PAR 2.E, & PAR 4.B(2)(D), FIG 103 DETAIL C. PERFORM HFEC AFTER BLENDED AT BS 245.5 8" ABOVE STR 1SDR CALA2026072618024Battery Pack · faultyEMERGENCY BATTERY PACK M1673 INOPERATIVE. R & R THE BATTERY PACK M1673 IAW AMM 33-51-06-960-802. OPS CHKD GOOD.SDR CALA2026072618022Battery · faultedEPSU SYSTEM TEST FAULT 10WL FWD L. EPSU 10WL SELF TEST SHOWS BATTERY FAULT. REMOVED AND REPLACED EPSU BATTERY IAW AMM 33-51-00-710-812-A. NEW BATTERY TESTED OK, OK FOR SERVICE.SDR CALA2026072618020Adiru · faultedRT IRS FAULT ON CLIMBOUT. ATB, REMOVED AND REPLACED AIR DATA INERTIAL REFERENCE UNIT IAW AMM 34-21-01. OPS CHKD GOOD AND NO FAULT LIGHT ON AT THIS TIME.SDR IXXA20260726001Stiffener · crackedNR 1 PYLON AFT V WEB O/B VERTICAL STIFFENER IS CRACKED AT LOWER EDGESDR JR2R20260726383Shear Tie · corrodedAFT OF AFT CARGO COMPARTMENT, SHEAR TIE CORRODED AT FR85 STR29R - STR28R. REMOVED AND REPLACEDSDR JR2R20260726375Shear Tie · corrodedAFT OF AFT CARGO COMPARTMENT, SHEAR TIE CORRODED AT FR75 STR29R - STR28R. REMOVED AND REPLACEDSDR JR2R20260726385Shear Tie · corrodedAFT OF AFT CARGO COMPARTMENT, SHEAR TIE CORRODED AT FR86 STR29R - STR28R. REMOVED AND REPLACEDSDR JR2R20260726411Floor Support · corrodedFR16 OTBD FWD FLOOR SUPPORT HAD LIGHT CORROSION. REMOVED AND REPLACEDSDR SWIA2026072577744Stringer Splice · corrodedCORROSION FOUND ON STRINGER SPLICE 26L, BS 333, REMOVED AND REPLACED STRINGER SPLICE IAW SRM 51-42-06-001-001-A01, AND DWG SH670-32420, REV E. COMPLIED WITH ALL STEPS OF 51-900-1002-SKY.SDR SWIA2026072577266Skin · out of limitsRIGHT AILERON LOWER MOST OTBD LEADING EDGE SKIN FOUND TO BE OUT OF LIMITS. REMOVED AND INSTALLED A NEW SKIN IAW SRM 51-42-06, SRM 51-42-21, AND DWG CC670-13000, REV D. COMPLIED WITH TASK CARD 51-900-1003-SKY.SDR SWIA2026072577265Skin · out of limitsLEFT AILERON LOWER MOST OTBD LEADING EDGE SKIN FOUND TO BE OUT OF LIMITS ON HN00327396, & MX32674480. REMOVED AND REPLACED THE SKIN PANEL IAW SRM 51-42-06, SRM 51-42-21, AND DWG CC670-13000, REV D. COMPLIED WITH TASK CARD 51-900-1003-SKY.SDR SWIA2026072577232Frame Angle · corrodedFOUND CORROSION ON FRAME BS 589 REINFORCEMENT ANGLE. REPLACED CORRODED FRAME BS 589 REINFORCEMENT ANGLE WITH NEW IAW DWG 601R36025, REV-P, & SRM 51-42-06. COMPLIED WITH TASK CARD 51-900-1003-SKY.SDR SIMA20260725004Stringer Splice · crackedCENTER FUSELAGE III STRINGER SPLICE 09L AT FR 74 CRACKED. REMOVED AND REPLACED CENTER FUSELAGE III STRINGER SPLICE 09L BETWEEN FR 56 AND FR 74 IAW ERJ 170 SRM 51-40-08.SDR SIMA20260725003Seat Track · crackedRH LOWER SEAT TRACK FLANGE IS CRACKED AT FR 50 AND FR 54. (MAJOR REPAIR) PERFORMED TEMPORARY REPAIR TO RH LOWER SEAT TRACK INBD FLANGE AT FR 50 AND FR 54 IAW ERS-EJ-53MR-5536 PTA.SDR IPXA2026091153076Longeron · corrodedLONGERON 17L UPPER SURFACE AREA BETWEEN STA 1885 AND 1963 AND ATTACHMENT TO SKIN PANELS TO INCLUDE ALL ADJACENT STRUCURE HAS AREAS OF CORROSION AND MISSING PROTECTIVE FINISH AND TOPCOAT. APPLIED TOPCOAT TO REWORKED AREAS AT LONGERON 17L UPPER SURFACE AREA BETWSDR IPXA2026091153193Angle · corrodedLONGERON 17L LOWER SURFACE BETWEEN STA 1885 AND 1963 AND ATTACHMENT TO SKIN PANELS TO INCLUDE ALL ADJACENT STRUCURE HAS AREAS OF CORROSION AND MISSING PROTECTIVE FINISH AND TOPCOAT. INSTALLED 1EA NEW SEAL SUPPORT AND 1EA NEW GUSSET. RE-INSTALLED 1EA SEAL RETAISDR IPXA2026090462271Skin · corrodedCOMP-RH WING I/B FLAP UPPER SKIN SURFACE HAS CORROSION. FLAP BEING REPLACED ON TASK CARD # T3F18E009B8KN LINE 1088SDR IPXA2026091154285Bracket · corrodedAPU COMPARTMENT FWD BULKHEAD STA 1885 ALL WIRE HARNESSES AND POWER CABLE CLAMP SUPPORT BRACKETS ATTACHED TO BULKHEAD HAVE CORROSION AND OR MISSING PROTECTIVE FINISH AND COAT. RL050 INSTALLED 13EA BRACKETS ON APU COMPARTMENT FWD BULKHEAD STA 1885 REF. B757-200 SDR IPXA2026090153257Skin Panel · debondedAPU COMPARTMENT RT SIDE HONEYCOMB SKIN PANEL LOWER END DISBONDED BETWEEN FRAME STA 1941 AND 1963 JUST ABOVE LONGERON 17R. RL046 PERFORMED REPAIR PER B757-200PF SRM 51-70-10-2R-4 REPAIR 4 (REPAIRS TO LARGE DAMAGE) FIGURE 201 DETAIL A REV 125. MAJOR REPAIR.SDR IPXA2026091153139Skin · debondedAPU COMPARTMENT R/H SIDE HONEYCOMB SKIN PANEL DISBONDED AREA BETWEEN FRAME STA 1918 AND 1941 AND 24" ABOVE LONGERON 17R. RL045 REPAIRED PER SRM 51-70-10-2R-4 REPAIR 4 (REPAIRS TO LARGE DAMAGE) FIGURE 201 DETAIL A REV 125 USING B757-200PF SRM 51-70-10-2R-0 REV SDR ASAA2026072568561Sidewall Support · crackedAFT CARGO LT SIDEWALL SUPPORT CRACKED LBL45 STA 727B AND 727D. GROUNDED - YES. REPAIRED AFT CARGO L/H SIDEWALL SUPPORT STA 727B AND 727D IAW EA 800-53EA-30621.SDR SWAA2026090219549Floor Panel · damagedELONGATED HOLES FLOOR PANEL 140CF AT AFT CARGO BAY. REPLACED THE FLOOR PANEL 140CF IAW DWG 453A2610, SHT 12, REV C.SDR ASAA2026072568411Cargo Track · crackedAFT CARGO R/H CARGO TRACK CRACKED STA 727C. GROUNDED - YES. REPAIRED AFT CARGO R/H CARGO TRACK IAW B737-800 SRM 53-00-53-2R-3.SDR ASAA2026072568410Baffle · corrodedAFT CARGO RT BAFFLE CORRODED BS 767 - 747. GROUNDED - YES. REMOVED AND REPLACED AFT CARGO RT BAFFLE IAW SRM 51-40-05-0G-0, AND 51-40-02-0G-0.SDR ASAA2026072568409Transition Panel · corrodedAFT CARGO LT TRANSITION CORRODED STA 727 TO STA 807. GROUNDED - YES. REMOVED DAMAGE FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-1A-2. REPAIRED AFT CARGO LT TRANSITION IAW SRM 53-00-53-2R-5.W:2" O:0.040" R:0 L:2" D:0.040".SDR ASAA2026072568408Transition Panel · corrodedAFT CARGO RT TRANSITION CORRODED BS 727 - 767. GROUNDED - YES. REPAIRED AFT CARGO RT TRANSITION IAW SRM 53-00-53-2R-5.SDR ASAA2026072568407Shield · corrodedAFT CARGO FWD SHIELD CORRODED STA 787 TO STA 767. GROUNDED - YES. AFT CARGO FWD SHIELD CORRODED STA 787 TO STA 767.SDR ASAA2026072568406Scuff Plate · corrodedAFT CARGO SCUFF PLATE WEB CORRODED STA 847 TO STA 787. GROUNDED - YES. REMOVED DAMAGE FOUND TO BE OUT OF LIMITS IAW B737-800 SRM 53-60-15-1A-1, REMOVED AND REPLACED WEB IAW B737-800 SRM 51-40-02-0G-0.