Service difficulty reports
1,771,708 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 SWAA2026033073630Bracket · crackedCRACKED BRACKET, BS 500H, STRINGER 26L, IN THE FWD CARGO BAY. REPLACED THE BRACKET AND FASTENERS IAW SRM 51-40-02, SRM 51-10-02, ITEM 9, & DWG 143A7505, SHEET 137, REV-.SDR SWAA2026033073631Bracket · crackedCRACKED BRACKET, BS 500H, STRINGER 26L, IN THE FWD CARGO BAY. REPLACED THE BRACKET IAW SRM 51-40-02, SRM 51-10-02, ITEM 9, & DWG 143A7505, SHEET 137, REV-.SDR SWAA2026033073633Bracket · crackedCRACKED BRACKET, BS 500G, STRINGER 26R, IN THE FWD CARGO BAY. REPLACED THE BRACKET IAW SRM 51-10-02, ITEM 9, SRM 51-40-02, & DWG 143A7505, SHEET 137, REV - .SDR SWAA2026033073634Bracket · crackedCRACKED BRACKET, BS 500F, STRINGER 26R, IN THE FWD CARGO BAY. REPLACED THE BRACKET IAW SRM 51-10-02, ITEM 9, SRM 51-40-02, AND DWG 143A7505, SHEET 138, REV -.SDR SWAA2026033073637Bracket · crackedCRACK BRACKET, BS 500E, STRINGER 26R, IN THE FWD CARGO BAY. REPLACED THE BRACKET IAW SRM 51-40-02, AND DWG 143A7505, SHEET 138, REV-.SDR JJBA20260327022Gusset · corrodedLH GUSSET UNDER LAV CORRODED BEYOND LIMITS. REMOVED AND REPLACED GUSSET.SDR JJBA20260327021Gusset · corrodedRH GUSSET UNDER LAV CORRODED BEYOND LIMITS. REMOVED AND REPLACED GUSSET.SDR JJBA20260327020Gusset · corrodedCENTER GUSSET UNDER LAV CORRODED BEYOND LIMITS. REMOVED AND REPLACED GUSSET.SDR JJBA20260327019Bracket · crackedPNEUMATIC BRACKET AT FRAME 47 CRACKED. REMOVED AND REPLACED BRACKET.SDR JJBA20260327018Doubler · corrodedRH OMEGA BEAM DOUBLER AT FRAME 20 CORRODED. CORROSION FOUND TO BE .017" DEEP. REMOVED AND REPLACED DOUBLER.SDR SWAA2026032479030Frame · no discrepancyFRAME STRAP CONFIGURATION LOCATED ON S-20R TO S-22R DOES NOT MATCH 5311-I-17336-NG WITH FIGURE 15 STEP 20 BS 328. IAW EA 26-153-00548 THE CONFIGURATION IS ACCEPTABLE.SDR SWAA2026032473653Cargo Track · crackedCRACKED CARGO TRACK, RBL 13.84, BS 747. FAULT RESOLVED IN OTHER FAULT, SEE TTG8Q01AL90RSDR SWAA2026032473662Cargo Track · crackedCRACKED CARGO TRACK RBL 13.84, BS 767. REPAIRED THE CARGO TRACK, RBL 13.84, BTWN BS 727D - 787 IAW SRM 53-00-53-2R-3, REPAIR 3 ALTERNATIVE 1, DETAIL A, FIGURE 203, SHEET 1.SDR SWAA2026032473655Cargo Track · crackedCRACKED TRACK RBL 13.84, BS 727E, WL 156. FAULT RESOLVED IN OTHER FAULT SEE TTG8Q01AL90RSDR SWAA2026032473665Angle · crackedTWO CRACKED ANGLES, BS 907 - 927, STRINGERS 25 - 27R. REPLACED THE ANGLES IAW SRM 51-40-02, DWG 147A7221, SHEET 24, REV-.SDR SWAA2026032473657Web · corrodedCORRODED WEB BS 807, RBL 63, WL198. REPLACED THE WEB AND FASTENERS IAW SRM 51-10-02, ITEM 9, DWG 143A8312, SHEET 1, REV D, & DWG 146A8310, SHEET 16, REV A.SDR SWAA2026032473512Lens · brokenBROKEN LENS OF THE EMERGENCY LIGHT. REPLACED THE LENS IAW AMM 33-51-01-960-801, STEP 2.C.(1).(A), & (4).SDR SWAA2026032473517Lens · brokenBROKEN LENS OF THE EMERGENCY LIGHT. REPLACED THE LENS IAW AMM 33-51-01-960-801, STEP 2.C.(1).(A), & 2.C.(4).SDR SWAA2026032473650Access Panel · crackedCRACK ON LEADING EDGE RIB ACCESS PANEL 331B, LE HSS 105.26, LT HORIZONTAL STAB. REPLACED LEADING EDGE RIB ACCESS PANEL 331B IAW SRM 51-40-02-0G-0, AND DWG 186A1001, SHEET19, REV:-. AND DWG 186A1304, SHEET 1, REV A.SDR SWAA2026032473656Support · corrodedCORROSION SUPPORT ZEE, BS 727B - 767, RBL 21, WL156. REPLACED SUPPORT ZEE IAW SRM 51-10-02-0G-0, ITEM 9, SRM 51-40-02-0G-0, DWG 146A7500, SHEET 113, REV-, & DWG 146A7502, SHEET 49, REV-.SDR SWIA2026022375555Seat Track · corrodedFORWARD WET AREA SEAT TRACK BETWEEN FRAMES 19 AND 20, Y=-276 HAS UPPER SURFACE CORROSION. REMOVED AND REPLACED FWD WET AREA SEAT TRACK AT FRAME 12-20 Y-276MM REF EMB 175 SRM 51-40-08. THIS REPAIR DOESN'T AFFECT THE WEIGHT AND BALANCE. NO FURTHER ACTION REQUIRESDR SWAA2026031073486Strip · corrodedFWD CARGO COMPARTMENT LEFT FLOOR CAPSTRIPS (3 LONG ONES) HAVE CORROSION ON LOWER SIDE AROUND NUMERUS FASTENER HOLE LOCATIONS. . R & R FWD CARGO COMPARTMENT LT FLOOR CAPSTRIPS PER AMM 25-52-06.SDR SWAA2026031073575Strip · corrodedFWD CARGO COMPARTMENT RT FLOOR CAPSTRIPS (2 LONG ONES) HAVE CORROSION ON LOWER SIDE AROUND NUMERUS FASTENER HOLE LOCATIONS. R & R FWD CARGO RT CAP STRIPS (2EA.) IAW AMM 25-52-06.SDR SWAA2026030973417Stringer · crackedPOSSIBLE CRACK INDICATION ON STRINGER 7L OF AFT PRESSURE BULKHEAD CENTER WEB. REMOVED PRIMER IAW AMM 51-21-11, VERIFIED CRACK IAW NDT MANUAL 51-00-00, PROCEDURE 23, STEP 7.D. (2) DYE PENETRANT. MEASURES .0973,SDR SWAA2026030973485Floorboard · delaminatedCABIN CENTER FLOORBOARD 241RF HAD AN AREA OF DELAMINATION. REMOVED AND REPLACED THE FLOORBOARD 241RF IAW AMM 53-21-00.SDR DALA2026030801598Apu · odorON TAXI IN, FLT ATTENDANTS NOTIFIED PILOTS OF A SMOKEY HAZE IN THE CABIN. IT WAS DESCRIBED AS SMELLING "FRUITY" AND LIKE " ANTI-FREEZE". PILOTS THEN GOT A CONDITION HOT AIR FAULT ECAM MESSAGE. APU WAS ON WITH, APU BLEED OFF. SHUT DOWN APU + ENGINES AND DISAPATSDR FDEA202602230320Safety Wire · brokenREF WRI 25-60/2795 DURING FEA INSPECTION SAFETY WIRE ON THE RIGHT DOOR SLIDE PACK RELEASE MECHANISM BROKE. MEL: 52-11-01-02 AMM: 52-00-00-9 AMM: 25-66-01-4 ACCOMPLISHED DDG RESTORATION PROCEDURE - INSTALLED SERVICEABLE R1 DOOR MOUNTED ESCAPE SLIDE PACKSDR AALA202603030126Feeder Cable · brokenAIRCRAFT WAS NOT GROUNDED: SEAT ROW 9ABC EMERGENCY ESCAPE PATH LIGHT INOPERATIVE. MAINTENANCE FOUND EMERGENCY LIGHT SEAT HARNESS / CABLE HAD A BROKEN WIRE / PIN AT SEAT 9ABC AND REPLACED PER AMM 33-51-00. A SATISFACTORY OPERATIONAL CHECK OF THE EMERGENCY LIGHSDR QXEA2026022700044Girt Bar · fodFLIGHT 2067. L1 ARMING LEVER STICKING. REMOVED FROM SERVICE. PERFORMED GVI OF VENT FLAP, GIRT BAR & FLOOR POCKETS. CLEANED DEBRIS FROM GIRT BAR/ FLOOR POCKETS. PERFORMED FUNCTIONAL CHECK OF FWD PAX DOOR VENT FLAP PER E175 AMM 52-11-25-720-801-A. FUNCTIONAL CHESDR AALA202602275361Light · inoperativeAIRCRAFT WAS NOT GROUNDED: SEAT ROW 9ABC EMERGENCY ESCAPE PATH LIGHT INOPERATIVE. (OPEN)SDR AALA202602279204Trunnion · wornAIRCRAFT IN BASE MAINTENANCE: RIGHT HAND INBOARD FLAP TRUNNION SHOWS SIGNS OF WEAR ON THE LOWER AFT SIDE AND UPPER FRONT SIDE. REPLACED TRUNNION PER CMM 57-52-23.SDR AALA202602276772Wire · brokenAIRCRAFT WAS GROUNDED: SEAT ROW 35 ABC AND 36ABC EMERGENCY PATH LIGHTS ARE INOPERATIVE. MAINTENANCE FOUND A BROKEN WIRE ON THE EMERGENCY LIGHT HARNESS AND REPAIRED IT PER ESPM 20-48-21. A SATISFACTORY OPERATIONAL CHECK OF THE EMERGENCY LIGHTING SYSTEM WAS ACCOSDR AALA202602271400Hinge Fitting · excess playAIRCRAFT IN BASE MAINTENANCE: LEFT HAND HORIZONTAL STABILIZER ELEVATOR #2 HINGE ARM END FITTING HAS EXCESSIVE PLAY. REPLACED HINGE ARM END FITTING PER AMM 55-16-42.SDR DALA2026022701399Blades · damagedSHIP 3942 -ATB/IFSD- LEFT ENGINE FAILED DURING TAKEOFF. CORRECTIVE ACTION: LPT BLADES HEAVILY DAMAGED AND METAL IN THE TAILPIPE. REMOVED AND REPLACED THE LEFT ENGINE ASSEMBLY IAW JIC 7100-4423-LH. ALL OPS AND LEAK CHECK OK.SDR CALA2026022714123Skin · crackedCRACK FOUND AT RIGHT HORIZONTAL STAB LOWER SKIN AT HSS 129.50 , INBD ROW , 9" FROM FRONT SPAR. CRACK LENGTH 1". REPAIRED RT HORIZONTAL STAB LOWER SKIN AT APPROX STA 129.5 IAW SRM 55-10-01-2R-11. ESFR ENTRY REQUIRED, DIP ENTRY REQUIRED. CATEGORY B REPAIR INSSDR DALA2026022701377Dampener · no testAIRCRAFT 3165, DONT PASS OPERATIONAL TEST PASSENGER CREW DOOR 841 DOOR DAMPER (REFER TO AMDS CARD 5210-7089-RF (RII)) AT FWD GALLEY AREA. CORRECTIVE ACTION: REPLACED PASSENGER CREW DOOR 841 EMERGENCY DAMPER PN: FE240-004, SN: 3977 AS PER A320 FAM AMM 52-11-14-SDR SWAA2026022673568Cap · crackedAFT CARGO CAP STRIP THAT FITS ACROSS THE BOTTOM OF THE FWD BULKHEAD PANEL 142NW IS CRACKED. INSTALLED AFT CARGO CAP STRIP IAW AMM 50-12-01.SDR SWAA2026022673306Battery Pack · inoperativeEMERGENCY LIGHTS INOPERATIVE. R & R BATTERY PACKS AT ROW 7 ABC AND FWD CENTER GALLEY IAW AMM 33-51-06; OPS CHECKED GOOD.SDR DXTA2026022607017Valve · faultyAFTER FLIGHT WITH APU ON IT TAKES UP TO 30 SECONDS FOR SEAL TO DEFLATE ENOUGH TO ALLOW OPENING OF THE MAIN CABIN DOOR. SUBSEQUENTLY AFTER FLIGHT WITH APU ON IT TAKES UP TO 10 SECONDS FOR SEAL TO DEFLATE ENOUGH TO OPEN THE MAIN CABIN DOOR. REMOVED FAILED DEFLASDR DXTA2026022607011Battery · faultyEMERGENCY LIGHTS FLICKERING ON AND OFF. REMOVED INTERMITTENT NR 1 BATTERY INSTALLED RECEIVED REPAIRED EMERGENCY BATTERY INTO NR 1 LOCATION. OPS CHECK GOOD. ALL ACCESSED AREAS CLOSED. ALL WORK PERFORMED IAW AMM 33-52-01. REMOVED INTERMITTENT NR 2 BATTERY INSSDR CALA2026022614102Engine · vibrationNR 1 ENG VIBRATION INDICATION. VIBRATION HIT 5.5. VIBRATION NOTED THROUGH AIRFRAME BY AIRCREW, SUGGESTS NOT AN INDICATION ISSUE. PERFORMED TEST NR 12A, LOW PRESSURE SYSTEM TRIM BALANCE OF NR 1 ENGINE REF 71-00-00-700-812-G00 AND CHANGED FAN BALANCE WEIGHTS. SDR CALA2026022614078Hydraulic Line · damagedLOST NR 1 ENG, HYD SYS IN FLT. PILOTS REPORTED NR 1 ENG EDP & ELEC PUMP LIGHTS ILLUMINATED DURING FLT. THE EDP REMAINED ILLUMINATED WHILE ELEC LIGHT SWITCHED OFF. PRESSURIZED HYD SYS -A- IAW FIM 29-30 TASK 812. CONDUCTED NR 1 ENG DRY MOTOR PROCEDURE IAW SDR CALA2026022614076Bulkhead Web · corrodedFOUND CORRODED TAIL COMPARTMENT INTERNAL PRESSURE BULKHEAD, LT AFT FACE OTBD BS 1088, ABOVE S-6L. ACCOMPLISHED A REPAIR OF BULKHEAD WEB IAW SRM 51-40-02-0G-0, ESR-WI 100-14616 AND ECRA 5380-01442.SDR CALA2026022614074Angle · crackedFOUND CRACK IN THE RT WING REAR SPAR FIXED T/E DEFLECTION CONTROL RIB, FIXED PANEL LOWER HORIZONTAL BULB SEAL RETAINER WEB SUPPORT OTBD END RIVET TAIL. REMOVED AND REPLACED THE ANGLE IAW SRM 51-40-02-0G-0.SDR DALA2026022501349Wire · frayedDURING WALK AROUND, FOUND R2 SLIDE LIGHT ON. FOUND THE FWD GIRT BAR PROXIMY SENSOR WIRE FRAYED. R & R SENSOR IAW AMM 25-66. OPS NORMAL. (8558066)SDR IPXA2026022551482Support Angle · crackedLEFT-HAND ELEVATOR, OUTBOARD, TRAILING EDGE WEDGE INTERNAL STRUCTURE CRACKED. REMOVED CRACKED/DAMAGED SUPPORT ANGLE IAW B747 SRM 51-40-02. INSTALLED NEW ANGLE IAW BOEING DWG. PL 65B03710.SDR IPXA2026022552524Power Supply · inoperativeFOUND M5055 POWER SUPPLY MALFUNCTION. (REPLACE) IAW AMM 33-51-04-902-001-001 REV.115 REPLACED POWER SUPPLY (M5055) AT UPPER DECK LEFT SIDE AND PERFORMED POWER SUPPLY TEST, THE RESULT WAS SATISFACTORY.SDR FDEA202602230270Floor Panel · puncturedPUNCTURE ON FLOOR PANEL 241LFF MDC FLOOR PANEL 241LFF MDC WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR 4-B FIG 201 SHEET 2 REV 93 AUG 15/2025SDR FDEA202602230269Floor Panel · puncturedPUNCTURE ON FLOOR PANEL 251DFF MDC FLOOR PANEL 251DFF MDC WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR 4-B FIG 201 SHEET 2 REV 93 AUG 15/2025SDR DALA2026022501336Cusp Web · crackedCRACK ON RH CUSP WEB AT Y=940 AND Y= 665 X=-53 TO X=-56 ALSO Y=716 X= -44. DAMAGED AREA REPAIRED PER B717-200 SRM 53-00-55 (1464546)