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 IPXA2026090530479Stiffener · corrodedAPU COMPARTMENT STA-1885 LIGHT SWITCH/ INTERPHONE SUPPORT BRACKET AND ATTACHED HORZ STIFFINER HAS CORROSION AND FILLET SEALANT MISSING IN AREAS. RL013 INSTALLED LIGHT SWITCHES S428 AND APU INTERPHONE JACK D413 IAW B757 AMM 23-41-00-400-801 AND SWPM 20-83-11 ANSDR IPXA2026090432341Skin Panel · damagedAFT SIDE OF FRAME STA 1963 AND LOWER METAL HONEYCOMB SKIN PANEL LEVELING COMPOUND AROUND DRAIN HOLES SEPERATED FROM CORRODED STRUCTURE. RL038 INSTALLED SKIN AT PANEL AT STA 1963 IAW SRM 51-40-02-OG-0SDR IPXA2026090431507Doubler · corrodedTAIL CONE STA 1992 FRAME FWD AND AFT SIDES HAVE AREAS OF CORROSION AND AREAS OF PROTECTIVE FINISH BLISTERING UP AND PEELING OFF CIRCUMFERENTIALLY AROUND FRAME. RL033 INSTALLED FRAME (RING) AT TAIL CONE STA 1992 IAW SRM 51-40-02-0G-0.SDR IPXA2026083141623Wedge · dentedMAJOR REPAIR, LT WING OTBD FLAP UPPER SURFACE OF T/E WEDGE HAD TWO DENTS INBD & OUTBD. FABRICATED REPAIR PLIES TO INSTALLED AT TWO DAMAGE AREA DAMAGE AREA NR 1 LOCATED 53.5' FORM I/B-OTBD AND 8.5" FROM T/E- FWD, SIZE OF DAMAGE IS 2.75" IN DIAMETER. DAMAGE ASDR IPXA2026082728931Skin · corrodedMAJOR REPAIR, EXTERNAL FUSELAGE SKIN HAS CORROSION BS 1885, LONERON 17R. PERFORMED REPAIR PER SRM 53-80-01-2R-3, REPAIR 3.SDR IPXA2026090342747Skin · dentedMAJOR REPAIR. LT WING OTBD MAIN FLAP UPPER SURFACE INBD T/E AREA DENTED. FABRICATED REPAIR PLIES TO INSTALLED AT DAMAGE AREA LOCATED 57" FORM INBD-OTBD AND 11" FROM T/E- FWD, SIZE OF DAMAGE IS 2.5" IN DIAMETER. IAW SRM 57-53-01-2R-1, FIGURE 201, DETAIL IISDR SIMA20260724008Seat Track · corrodedSSI 53-10-027: FWD GALLEY RH CENTER FLOOR BEAM HAS MULTIPLE AREAS OF CORROSION BTW FR 17-18. (MAJOR REPAIR) (LEVEL 2 CORROSION) REMOVED AND REPLACED FWD GALLEY RH CENTER FLOOR BEAM BTW FR 11-21 IAW ERJ 170 SRM 51-40-08.SDR SWAA2026090260340Support Angle · crackedCRACK SUPPORT ANGLE BTW BS 291.5 - 294.5, RBL 53 IN THE FWD GALLEY. REPLACED SUPPORT ANGLE IAW SRM 51-40-02, SRM 51-10-02, ITEM 9, AND DWG 141A8310, SHEET 1, REV D.SDR SWAA2026090280457Support Angle · crackedCRACKED SUPPORT ANGLES, BS 694, BL0. REPLACED THE SUPPORT ANGLE IAW SRM 51-40-02, DWG 273A9111, SHEET 10, REV-, & DWG 111A6000, SHEET 352, REV.SDR SWAA2026090208490Rib · crackedCRACKED LEADING EDGE RIB ACCESS PANEL 331B, LE STA 151.75 AT LT HORIZONTAL STAB. REPLACED THE RIB IAW SRM 51-40-05, & DWG 186A1001, SHEET 19, REV-.SDR SWAA2026090263939Intercostal · crackedCRACK WEB - INTERCOSTAL FLOOR STRUCTURE BTW STA 277 TO STA 294.5 AND BL 0 AT FWD GALLEY AREA 2026-446715 REPLACED WEB - INTERCOSTAL AND FASTENERS ON FLOOR STRUCTURE BTW STA 277 TO STA 294.5 AND BL 0 AT FWD GALLEY AREA IAW B737-800 SRM 51-40-02 SRM 51-10-02 ISDR SWAA2026090204055Intercostal · crackedCRACK WEB - INTERCOSTAL FLOOR STRUCTURE LOCATED BTW STA 328 TO STA 344 AND LBL 46 AT FWD GALLEY AREA 2026-446716 REPLACED WEB - INTERCOSTAL FLOOR STRUCTURE LOCATED BTW STA 328 TO STA 344 AND LBL 46 AT FWD GALLEY AREA IAW B737-800 SRM 51-40-05-0G-0 SRM 51-10-02SDR SWAA2026090239440Panel · crackedCRACK FLOOR STRUCTURE BREAK PANEL LOCATED BS540 BTW BL0 TO RBL24.5 AT PASSENGER CABIN 2026-446738 REPLACED BRAKE PANEL LOCATED BS540 BTW BL0 TO RBL24.5 AT PASSENGER CABIN IAW B737-800 SRM 51-40-02-0G-0 AND DWG 143A0060 SHEET 64 REV-. SEE INDIVIDUAL SIGN OFF BESDR SWAA2026090230341Angle · crackedCRACK INNER CHORD LOC BS 303.9 LBL55 AT FWD GALLEY AND LAV. REPLACED INNER CHORD LOCATED BETWEEN BS 270 TO BS 360 LBL55 AT FWD GALLEY AND LAV IAW SRM 51-40-02, DWG 141A8110, SHT 1, REV E, DWG 142A0050, SHT 15, REV-, & DWG 141A8110, SHT 11, REV-.SDR SWAA2026083193655Panel · crackedPANEL 561AB NUMEROUS SCREW HOLES CRACKED. REMOVED DAMAGE PER SRM 51-70-05-2R-8 INSPECTED WORK PERFORMED ON C/A #1 APPLIED REPAIR PLIES AND COOKED REPAIR PER SRM 51-70-05-2R-8. INSPECTED WORK PERFORMED ON C/A #3 RESIN SEALED REPAIR PER SRM 51-70-08-0G-0 AND REFSDR SWAA2026083113537Panel · crackedPANEL 561CB HAS NUMEROUS SCREW HOLES CRACKED. REMOVED DAMAGE PER SRM 51-70-05-2R-8. REPAIRED DAMAGED FASTENER HOLES IAW SRM 51-70-05-2R-8. RESIN SEALED REPAIR IAW SRM 51-70-08-0G-0 AND REFINISHED PER AMM 51-21-99. REPAIRED DAMAGED FASTENER HOLES IAW SRM 51-SDR VNAA202608310023Hinge Fitting · corrodedAFTER REMOVAL NLG AFT DOOR, CORROSION ON HING FITTING LT WAS FOUND. DUE TO EXCESSIVE DAMAGE ON HINGE FITTING LT WAS REPLACED IAW SRM 53-00-00-101-001-A01 AND SRM 51-41-02-001-001-A01.SDR VNAA202608310021Floor Support · crackedCRACKED ON FLOOR SUPPORT, RBL 12 BTWN BS 221.73 - 229 AT FWD FUSELAGE INTERNAL STRUCTURE (FLIGHT COMPARTMENT FLOOR STRUCTURE BELOW WL 79.50) WAS FOUND. CRACK ON FLOOR SUPPORT WAS REPAIRED IAW REO 690-53-11-2237. REV -.SDR VNAA202608310020Stringer · corrodedINITIAL INSPECTION: CORROSION ON STRINGER 24R, BS453 - 469 AT FWD CARGO BAY. STRINGER 24R, BS 453 - 469 WAS REPAIRED IAW SRM 53-00-03-201-001-A02.SDR VNAA202608310019Bracket · corrodedCORROSION ON MACHINED BRACKET (8EAS) OF FLOOR STRUCTURE AT FWD CARGO BAY BTWN BS 517 - 661 + 16.00 AND STR 22L TO 26R. ON MACHINED BRACKET (4EAS) OF FLOOR STRUCTURE AT FWD CARGO COMPARTMENT BTW FS517.00 TO FS661.00 + 16.00 AND STGR 22LH TO 26RH PAINT WERE REMSDR SIMA20260724007Floor Support · corrodedSSI 53-10-027 FWD GALLEY RH FLOOR SILL CORRODED AT FR 17. (LVL 2 CORR). REMOVED AND REPLACED FWD GALLEY RH FLOOR SILL BETWEEN FR 17 AND FR 20 IAW ERJ 170 SRM 51-40-08.SDR SIMA20260724006Floorbeam · corrodedFWD GALLEY LH CENTER FLOORBEAM CORRODED AT FR 17. (LVL 2 CORR) (MAJOR REPAIR). PERFORMED PERMANENT REPAIR TO FWD GALLEY LH CENTER FLOORBEAM AT FR 17 IAW SRM 53-10-10/REPAIR 01P.SDR AALA202608263201Light · no testAIRCRAFT IN BASE MAINTENANCE: LEFT FORWARD EXTERIOR OVERWING EMERGENCY LIGHTING ASSEMBLY IS INOPERATIVE - REPLACED LIGHT ASSEMBLY AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK PER AMM 33-51-15 WITH NO ISSUES NOTEDSDR AALA202608267390Light · no testAIRCRAFT IN BASE MAINTENANCE: LEFT AFT EXTERIOR OVERWING EMERGENCY LIGHTING ASSEMBLY IS INOPERATIVE - REPLACED LIGHT ASSEMBLY AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK PER AMM 33-51-15 WITH NO ISSUES NOTEDSDR AALA202608260076Light · no testAIRCRAFT IN BASE MAINTENANCE: RIGHT AFT EXTERIOR OVERWING EMERGENCY LIGHTING ASSEMBLY IS INOPERATIVE - REPLACED LIGHT ASSEMBLY AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK PER AMM 33-51-15 WITH NO ISSUES NOTEDSDR AALA202608267225Light · no testAIRCRAFT IN BASE MAINTENANCE: RIGHT FORWARD EXTERIOR OVERWING EMERGENCY LIGHTING ASSEMBLY IS INOPERATIVE - REPLACED LIGHT ASSEMBLY AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK PER AMM 33-51-15 WITH NO ISSUES NOTEDSDR SWAA2026082574208Scuff Plate · crackedFWD SERVICE DOOR SCUFF PLATE WAS CRACKED.SDR SWAA2026082493739Panel · crackedPANEL 511AT CRACKED. REPAIRED PANEL 511AT IAW SRM 51-70-05-2R-6.SDR HNAA2026082400775Yoke · crackedLEFT ENGINE PYLON LOWER FWD YOKE CRACKED. R & R YOKE IAW SRM 51-40-02.SDR SIMA20260724005Floor Support · corrodedFWD GALLEY LT FLOOR SUPPORT BRACKET CORRODED AT FR 17. (LVL 2 CORROSION) REMOVED AND REPLACED FWD GALLEY LT FLOOR SUPPORT BRACKET AT FR 17 IAW SRM 51-40-08.SDR SWAA2026082141542Control Module · faultedNR 2 ENGINE OVERHEAT LIGHT ILLUMINATED AFTER START. PERFOMED BITE TEST OF ENGINE FIRE DETECTION CONTROL MODULE REF FIM 26-10 TASK 801. NO FAULTS PRESENT. PER FIM 26-10 TASK 811 NEXT STEP REQUIRES HIGHT POWER ENGINE RUN. PER FIM 26-10 NO OBVIOUS DEFECTS RESISSDR SWAA2026082119418Access Panel · damagedELONGATED HOLE ON ACCESS PANEL 661CB AT RT WING. REPAIRED ACCESS PANEL 661CB AT RT WING IAW SRM 51-70-04-2R-9, REPAIR 9.SDR SWAA2026082141596Attach Angle · crackedBS 663 VAPOR BARRIER, ATTACH ANGLE CRACKED, RBL 9. REPAIRED THE ATTACH ANGLE IAW EA M-26-157-01481, C/W M-26-157-01481.SDR SWAA2026082176203Access Panel · damagedELONGATED HOLE ON RT WING ACCESS PANEL 661BB. REPAIRED THE ACCESS PANEL IAW SRM 51-70-04-2R-10, REPAIR 10.SDR SWAA2026082181268Attach Angle · crackedBS 663 VAPOR BARRIER ATTACH ANGLE CRACKED, LBL 9. REPAIRED THE ATTACH ANGLE IAW EA M-26-157-01480, C/W EA -26-157-01480.SDR SWAA2026082136646Access Panel · damagedELONGATED HOLE ON LT WING ACCESS PANEL 561CB. REPAIRED THE ACCESS PANEL IAW SRM 51-70-04-2R-10, REPAIR 10.SDR SWAA2026082199941Attach Angle · crackedBS 663 VAPOR BARRIER, ATTACH ANGLE CRACKED, LBL 34. REMOVED THE ATTACH ANGLE IAW SRM 51-40-02. REPAIRED THE ATTACH ANGLE EA M-26-157-01480, C/W EA M-26-157-01480.SDR SWAA2026082179612Access Panel · damagedELONGATED COUNTERSINK HOLE, RT WING ACCESS PANEL 661AB. REPAIRED THE ACCESS PANEL IAW SRM 51-70-04-2R-9, REPAIR 9.SDR SWAA2026082197029Access Panel · damagedELONGATED HOLE ON LT WING ACCESS PANEL 561AB. REPAIRED ACCESS PANEL 561AB IAW SRM 51-70-04-2R-9, REPAIR 9.SDR SWAA2026082166051Attach Angle · crackedBS 663 VAPOR BARRIER, ATTACH ANGLE CRACKED, RBL 34. REPAIRED THE ATTACH ANGLE PER EA M-26-157-01481 CHANGED PARAMETERS C/W EA M- 26-157-01481.SDR SWAA2026082000234Access Panel · damagedELONGATED HOLE ACCESS PANEL 561BB AT LT WING. REPAIRED ACCESS PANEL 561BB AT LT WING IAW B737-700 SRM 51-70-04-2R-10 REPAIR 10.SDR SWAA2026081703268Skin · corrodedCORROSION ON FUSELAGE EXTERIOR SKIN AT BS 917 AROUND THE VACUUM WASTE VENT CUTOUT. REPAIRED THE SKIN IAW SRM 53-70-01-2R-3.SDR SWAA2026081772706Rib · crackedCRACKED LEADING EDGE RIB ACCESS PANEL 331B, HSS 95.96, LT HORIZONTAL STAB. REPLACED RIB IAW SRM 51-10-02, ITEM 9, DWG 186A1303, SHEET 1, REV A, AND DWG 186A1001, SHEET 19, REV -.SDR IPXA2026080537727Web · corrodedMCD FR 74 - FR 75 LH FLOOR WEB IS CORRODED. LOCATED AND DRILLED L/H PLATE SUPPORT BTWN FR74 AND FR75 IAW A300-600 SRM 51-40-44. INSTALLATION OF FRAME WEB BETWEEN FR 74 AND FR 75 IAW SRM 51-40-21.SDR SWAA2026081277498Floor Panel · delaminatedCABIN FLOOR PANEL 231KF HAD A LARGE DELAMINATION ON THE AFT END. R & R IAW AMM 53-21-00-401.SDR SWAA2026081196185Angle · crackedCRACKED ANGLE ASSY, AFT FACE, BS 400 BTWN S25L - 26L IN THE FWD CARGO BAY. REPLACED THE ANGLE & FASTENERS IAW SRM 51-40-02-0G-0, SRM 51-10-02-0G-0, & DWG 143A7505, SHEET 81, REV-.SDR SWAA2026081158732Angle · crackedCRACKED ANGLE ASSY, FWD FACE, BS 420 BTWN S25L - 26L IN FWD CARGO BAY. REPLACED FASTENERS AND ANGLE ASSY, IAW SRM 51-10-02, STEP 9, SRM 51-40-02, AND DWG 143A1212, SHEET 68, REV-.SDR SWAA2026080672921Handle · unsecureL2 DOOR ASSIST HANDLE NEEDS TO BE SECURED. L2 DOOR ASSIST HANDLE TIGHTENED IAW AMM 52-13-31-400-802.SDR AALA202608040993Light · inoperativeAIRCRAFT WAS NOT GROUNDED: ROW 12-16 LEFT SIDE SIDEWALL LIGHTS INOP. MAINTENANCE REPLACED OVERWING EXIT LIGHT ASSY IAW AMM 33-21-00. ALL LIGHTS FROM ROW 12-16 LIGHT UP. ALL LIGHTS OPS CHECK GOOD.SDR DALA2026073104430Combustion Case · damagedATB, IFSD - FLIGHT CREW PERFORMING AIR TURN BACK DUE TO LEFT ENGINE FIRE INDICATION. MAINTENANCE INSPECTED AND FOUND DAMAGE TO COMBUSTOR CASE (APPROXIMATELY 12 O'CLOCK POSITION), ENGINE CHANGE REQUIRED.(A011187)(AIRCRAFT GROUNDED)