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 UIEA2026040800168Skin · corrodedM/D STA 1480 FWD, STR 9L TO STR 10L SKIN INT FOUND CORROSION(<P>CORROSION REMOVED AS PER SRM 51-10-02 AND REPROTECTED AS PER SRM 51-20-01, REWORK AREA MEASURED ORG 0.120" L:6" X W: 2" X D: 0.009", WITHIN SRM 53-00-01-1A-1 ALLOWABLE DAMAGE 1 FIG 101 LIMITS. NO SDR UIEA2026040800169Skin · corrodedM/D STA 1480 FWD STR 10L TO STR 11L SKIN INT FOUND CORROSION(<P>CORROSION REMOVED AS PER SRM 51-10-02 AND REPROTECTED AS PER SRM 51-20-01, REWORK AREA MEASURED ORG 0.120" L:5" X W: 1.7" X D: 0.009", WITHIN SRM 53-00-01-1A-1 ALLOWABLE DAMAGE 1 FIG 101 LIMITS. NSDR UIEA2026040800170Skin · corrodedM/D STA1480 FWD STR 14L TO STR 15L SKIN INT FOUND CORROSION(<P>CORROSION REMOVED AS PER SRM 51-10-02 AND REPROTECTED AS PER SRM 51-20-01, REWORK AREA MEASURED ORG 0.090" L: 3.5" X W: 2" X D: 0.011", WITHIN SRM 53-00-01-1A-1 ALLOWABLE DAMAGE 1 FIG 101 LIMITS. NSDR UIEA2026041500182Step · damagedM/D - STA 500 LADDER #7 (COUNT FROM BOTTOM) FOOTSTEP I/B WEB FWD AND AFT CORNER FOUND NON-STANDARD REPAIR.(<P>FWD AND AFT CORNER REPAIRED AS PER RI-25-13-18107 REV A. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2026041500183Skin · crackedM/D - ENTRY DOOR L1 INNER SKIN CRACK AT WINDOW CUTOUT AFT UPPER CORNER AREA(<P>INNER SKIN CRACK AREA REPAIRED AS PER RI-52-10-18136 REV A. NO FURTHER DEFECTS NOTED.</P>)SDR UIEA2026041500184Beam · cracked1EA CRACK WAS FOUND ON BEAM RUNNING AFT AT BS260-280 WL 170 LH NOSE WHEEL WELL SIDE PANEL(<P>CRACK BEAM REPLACED AS PER SRM 51-10-02 AND NEW BEAM INSTALLED AS PER SRM 51-40-02. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2026041500185Skin · corrodedM/D - RHS BS 980 TO 1000 STR 13R TO 14R FX SKIN INTERNAL FOUND CORROSION(<P>CORROSION REMOVED AS PER SRM 51-10-02 AND REPROTECTED AS PER SRM 51-20-01, REWORK AREA MEASURED ORG:0.124" L:6" X W:2" X D:0.011", WITHIN SRM 53-00-01-1A-1 ALLOWABLE DAMAGE 1 FIG 101 LSDR UIEA2026041500186Skin · corrodedM/D RHS BS 1000 TO 1020 STR 15R TO 16R FX SKIN INTERNAL FOUND CORROSION(<P>CORROSION REMOVED AS PER SRM 51-10-02 AND REPROTECTED AS PER SRM 51-20-01, REWORK AREA MEASURED ORG: 0.150" L:6" X W:1.5" X D: 0.017", WITHIN SRM 53-00-01-1A-1 ALLOWABLE DAMAGE 1 FIG 10SDR UIEA2026041500187Skin · corrodedM/D RHS BS 1000 TO 1020 STR 16R TO 17R FX SKIN INTERNAL FOUND CORROSION(<P>CORROSION REMOVED AS PER SRM 51-10-02 AND REPORTECTED AS PER SRM 51-20-01, REWORK AREA MEASURED ORG: 0154" L: 3" X W: 1" X D: 0.019", WITHIN SRM 53-00-01-1A-1 ALLOWABLE DAMAGE 1 FIG 101SDR UIEA2026041500188Skin · corrodedM/D - STA 1000 AFT, S-10L TO S-11L INTERNAL SKIN FOUND CORROSION(<P>CORROSION REMOVED AS PER SRM 51-10-02 AND REPROTECTED AS PER SRM 51-20-01, REWORK AREA MEASURED ORG: 0.128", L: 3" X W: 1.5" X D: 0.012", WITHIN SRM 53-00-01-1A-1 ALLOWABLE DAMAGE 1 FIG 101 LISDR UIEA2026041500189Skin · corrodedM/D -STA 1241 FWD STR 13L- STR 14L INT SKIN FOUND CORROSION(<P>CORROSION AREA REMOVED AS PER SRM 51-10-02 AND REPROTECTED AS PER SRM 51-20-01, REWORK AREA MEASURED ORG 0.220" L: 4" X W: 2.5" X D: 0.018", WITHIN SRM 53-00-01-1A-1 ALLOWABLE DAMAGE 1 FIG 101 LIMISDR UIEA2026041500190Skin · corrodedM/D - STA 1241 FWD STR 14L - STR 15L INT SKIN FOUND CORRODED.(<P>CORROSION REMOVED AS PER SRM 51-10-02 AND REPROTECTED AS PER SRM 51-20-01, REWORK AREA MEASURED ORG 0.220" L : 7" X W: 2" X D: 0.017", WITHIN SRM 53-00-01-1A-1 ALLOWABLE DAMAGE 1 FIG 101 LIMITS. SDR UIEA2026041500191Skin · corrodedM/D STA 1241 FWD STR 15L - STR 16L INT SKIN FOUND CORRODED.(<P>CORROSION AREA REMOVED AS PER SRM 51-10-02 AND REPROTECTED AS PER SRM 51-20-01, REWORK AREA MEASURE ORG 0.288", L: 4" X W: 3" X D: 0.019", WITHIN SRM 53-00-01-1A-1 ALLOWABLE DAMAGE 1 FIG 101 LIMITSSDR UIEA2026041500192Skin · corrodedM/D STA 1241 FWD STR 16L - STR 17L INT SKIN FOUND CORRODED.(<P>CORROSION REMOVED AS PER SRM 51-10-02 AND REPROTECTED AS PER SRM 51-20-01, REWORK AREA MEASURED ORG: 0.230", L: 6" X W: 2.5" X D: 0.019", WITHIN SRM 53-00-01-1A-1 ALLOWABLE DAMAGE 1 FIG 101 LIMITS.SDR UIEA2026041500193Skin · corrodedM/D STA 1241 FWD STR 17L - STR 18L INT SKIN FOUND CORRODED.(<P>CORROSION AREA REMOVED AS PER SRM 51-10-02 AND REPROTECTED AS PER SRM 51-20-01, REWORK AREA MEASURED, ORG: 0.220" L: 9" X W: 2" X D: 0.027", WITHIN SRM 53-00-01-1A-1 ALLOWABLE DAMAGE 1 FTG 101 LIMISDR UIEA2026041500194Bracket · corrodedU/D - LBL 23 BS 480 FLR SUPPORT BRACKET FOUND CORROSION(<P>CORROSION BRACKET REPLACED AS PER SRM 51-10-02 AND NEW BRACKET HOLES TRANSFERRED AS PER SRM 51-40-05 AND NEW BRACKET INSTALLED AS PER SRM 51-40-02. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2026041500195Seat Track · crackedM/D - STA 980 TO 1000, RBL 11.33 SEAT TRACK FOUND CRACKED.(<P>SEAT TRACK REPAIRED AS PER SRM 53-00-52-2R-12 REPAIR 12 FIG 201 ( PERMANENT REPAIR ). NO FURTHER DEFECTS NOTED.</P>)SDR UIEA2026041500196Seat Track · crackedM/D - STA 980 TO 1000, LBL 11.33 SEAT TRACK FOUND CRACKED.(<P>SEAT TRACK REPAIRED AS PER SRM 53-00-52-2R-12 REPAIR 12 FIG 201. NO FURTHER DEFECTS NOTED.</P>)SDR UIEA2026041500197Skin · corrodedCORROSION FOUND AT STA 1720 S44L SKIN INNER SURFACE ( APPROX 2.5" X 2.25" )(<P>CORROSION REMOVED AS PER SRM 51-10-02 AND REPROTECTED AS PER SRM 51-20-01, REWORK AREA MEASURED ORG: 0.071", L: 6" X W: 2.5" X D: 0.006", WITHIN SRM 53-00-01-1A-1 ALLOWABLE DAMAGE 1SDR UIEA2026041500198Skin · corrodedM/D RHS BS 980 TO 1000 STR 15R TO STR 16R FX SKIN INT FOUND CORROSION(<P>CORROSION REMOVED AS PER SRM 51-10-02 AND REPROTECTED AS PER SRM 51-20-01, REWORK AREA MEASURED ORG: 0.150" L: 6" X W: 1.5" X D: 0.014", WITHIN SRM 53-00-01-1A-1 ALLOWABLE DAMAGE 1 FIG 10SDR UIEA2026041500199Skin · corrodedRHW I/B T/E FORE FLAP O/B UPPR ACC PNL INTERNAL SURFACE EDGE SEVERAL AREA FOUND CORROSION(<P>CORROSION REMOVED AS PER SRM 51-10-02 AND REPROTECTED AS PER SRM 51-20-01, REWORK AREA MEASURED ORG: 0.105", L: 13" X W: 1" X D: 0.002", WITHIN SRM 57-53-01-1A-0 ALLOWSDR UIEA2026041500200Support · cracked1EA CRACK FOUND ON RHS BS 2598 UPPER CORNER HORI STAB HINGE SUPPORT FRAME(<P>FRAME CRACK AREA REPAIRED AS PER ATLAS AIR EO 4453A749 REV 7 PART 2 STEP 4 (B) AND STEP 5. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2026041600201Support Fitting · crackedRHW T/E I/B CAVITY #7 SPOILER ACTUATOR SUPPORT FITTING O/B LOWER EDGE FOUND CRACKED.(<P>SUPPORT FITTING O/B LOWER EDGE CRACK AREA REPAIRED AS PER RI-57-51-18166 REV A. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2026041700202Fairing · cracked#2 PYLON AFT FAIRING FWD UPPR RH SKIRT ANGLE FOUND CRACK(<P>SKATE ANGLE CRACK AREA REPAIRED AS PER RI-54-56-18197 REV A. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2026041700208Frame · chafed#1L CORE COWL REAR FRAME MIDDLE AREA FOUND CHAFING.(<P>FRAME CHAFING AREA REPAIRED AS PER ATLAS AIR EA-1971A269 REV 0. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2026041700209Web · corrodedU/D LBL 10 TO 20 BS 480 TO 500 FLOOR SUPPORT WEB FOUND CORROSION(<P>WEB FABRICATED AS PER DWG 141U5421 AND PL, WEB REPLACED AS PER SRM 51-10-02, AND NEW WEB HOLES TRANSFERRED AS EPR SRM 51-40-05, AND NEW WEB INSTALLED AS PER SRM 51-40-02. NO FURTHER DEFECTS NOSDR UIEA2026041700210Doubler · corrodedU/D LBL 10" - LBL 14" BS 480-500 FLOOR SUPPORT WEB ATT. DOUBLER CORROSION(<P>DOUBLER FABRICATED AS PER DWG 141U5422, AND PL DOUBLER REPLACED AS PER SRM 51-10-02, AND NEW DOUBLER HOLES TRANSFERRED AS PER SRM 51-40-05, AND NEW DOUBLER INSTALLED AS PER SRM 51-40-SDR UIEA2026041800211Panel · corrodedRHW I/B T/E AFT FLAP MID UPPR PNL FWD LWR SURFACE SEVERAL AREA CORROSION(<P>CORROSION AREA REPAIRED AS PER RI-57-53-18206 REV A. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2026041800212Web · crackedLH BS 1480 WEB CRACKED 1/4" ADJACENT LONGERON FITTING LOWER AREA(<P>WEB REAIRED AS PER SRM 53-40-08-2R-1 REPAIR 1 FIG 201 AND RI-53-40-18137 REV A. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2026041800214Fairing · cracked#1R T/R COWL 6 O/C T/E FAIRING FOUND CRACKED(<P>FAIRING CRACK AREA REPAIRED AS PER ATLAS AIR EA-1978A270 REV 0. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2026041800216Channel · crackedRH H.STAB O/B T/E WEDGE FWD CHANNEL FOUND CRACKED(<P>CHANNEL REPLACED AS PER RI-55-10-18182 REV A. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2026041800217Structure · corrodedRH WLG W/W STA 1241 AREA CENTER TANK RIGHT O/J PUMP ( M225 ) CUTOUT FOUND CORROSION(<P>CORROSION AREA REPAIRED AS PER RI-57-10-18226 REV A. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2026041900219Frame · chafed2L CORE COWL INNER FRAME AT 8 O'CLOCK FOUND CHAFING(<P>FRAME CHAFING AREA REPAIRED AS PER SRM 54-45-02-2R-1 REPAIR 1 REV 106 DATE: 20 FEB 2026 AND ATLAS AIR EA-1971A-270 REV 0. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2026041900220Beam · crackedLHW L/E NEAR #2 PYLON O/B D-BEAM WEB FOUND CRACK ( ILES 693 )(<P>WEB CRACK AREA REPAIRED AS PER RI-57-41-18207 REV B. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2026041900221Frame · noneAFT CARGO STA 1800 FRAME WEB NEAR STR 38R - STR 40R FOUND UNIDENTIFIED EXISTING REPAIR(<P>EXISTING REPAIR PART REINSTALLED AS PER BOEING NCR 408271F. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2026042000222Rib · crackedLHW FRONT SPAR TO L/E CAVITY ILES 756 SUPPORT RIB FOUND CRACK(<P>RIB CRACK AREA REPAIRED AS PER RI-57-41-18176 REV A. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2026042000223Rib · crackedRHW L/E TO FRONT SPAR CAVITY ILES 756 SUPPORT RIB FOUND CRACK(<P>RIB CRACK AREA REPAIRED AS PER RI-57-41-18175 REV A. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2026042200232Beam · crackedRHW L/E NEAR #4 PYLON I/B D-BEAM WEB CRACK ( ILES 1116 )(<P>CRACK WEB REPLACED AS PER SRM 51-10-02, AND NEW WEB HOLES TRANSFERRED AS PER SRM 51-40-05, AND NEW WEB INSTALLED AS PER SRM 51-40-02 AND RI-57-41-18200 REV A. NO FURTHER DEFECTS NOTED.</P>)SDR UIEA2026042200233Beam · crackedRHW L/E NEAR #4 PYLON I/B D-BEAM UPPR CHORD FOUND CRACK ( ILES 1116 )(<P>UPPER CHORD CRACK AREA REPAIRED AS PER RI-57-41-18200 REV A. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2026042200234Beam · crackedRHW L/E NEAR #4 PYLON I/B D-BEAM LOWER CHORD CRACK(<P>LWR CHORD CRACK AREA REPAIRED PER RI-57-41-18200 REV A. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2026042200235Floor Panel · puncturedBULK CARGO CTR FLOOR PANEL AT STA 2040 TO 2060 RH SIDE AREA WITH A PUNCTURE.(<P>FLOOR PNL PUNCTURE AREA REPAIRED AS PER RI-25-54-18173 REV A. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2026042200236Skin · cracked2L CORE COWL EXTERIOR SURFACE T/E AT 12 O'CLOCK POSITION FOUND CRACKED(<P>SKIN CRACK AREA REPAIRED AS PER ATLAS AIR EA-1971A268 REV 1. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2026042400245Floorbeam · corrodedU/D LBL 10 TO 30 BS 500 FLOOR SUPPORT SPLICE PLATE FOUND CORROSION(<P>SPLICE PLATE FABRICATED AS PER BOEING DWG 141U5422 AND PL, AND NEW SPLICE PLATE HOLES TRANSFERRED AS PER SRM 51-40-05, AND NEW SPLICE PLATE INSTALLED AS PER SRM 51-40-02. NO FURTHER DEFECTS SDR UIEA2026042400246Web · crackedU/D LBL 10 TO LBL 35 BS 500 - BS 540 FLOOR SUPPORT SHEAR WEB CORROSION(<P>SHEAR WEB FABRICATED AS PER BOEING DWG 141U5421 AND PL, AND NEW SHEAR WEB HOLES TRANSFERRED AS PER SRM 51-40-05, AND NEW SHEAR WEB INSTALLED AS PER SRM 51-40-02. NO FURTHER DEFECTS NOTEDSDR UIEA2026042600248Floor Support · crackedM/D BS 1860 - 1880 RHS O/B RBL 116" FLOOR SUPPORT L ANGLE FOUND CRACK.(<P>FLOOR SUPPORT CRACK AREA REPAIRED AS PER RI-25-21-18246 REV A. NO FURTHER DEFECTS NOTED.SDR UIEA2026042700250Seat Track · crackedM/D - BS 1050-1070 RBL 77 SEAT TRACK RHS FLANGE FOUND CRACK(<P>SEAT TRACK CRACK AREA REPAIRED AS PER SRM 53-40-52-2R-3 REPAIR 3 FIG 201. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2026042700252Skin · misrepairedFUSELAGE SKIN AT STA 2564-2575 STR 38R - STR 42R FOUND UNIDENTIFIED EXISTING REPAIR(<P>SKIN REPAIRED AS PER RI-53-80-18257 REV B. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2026042700253Stringer · noneFWD CARGO STA 790 - 810 STR 43L FOUND UNIDENTIFIED EXISTING REPAIR(<P>EXISTING REPAIR REINSTALLED AS PER BOEING NON-CONFORMANCE NUMBER 430034F. NO FURTHER DEFECTS NOTED.</P>)SDR UIEA2026042800254Duct · crackedNHR 3 ENG RH CORE COWL PRECOOLER OUTLET DUCT INNER GILL FOUND CRACKED.(<P>NEW PRECOOLER DUCT REPAIRED AND INSTALLED AS PER ATLAS AIR EA-1971A274 REV 0. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2026042800256Skin · corroded1EA CORROSION FOUND ON FUSELAGE LOWER SKIN INNER SURFACE AT STA 2185 STR 47R(<P>SKIN CORROSION AREA REPAIRED AS PER RI-53-60-18178 REV A. NO FURTHER DEFECTS NOTED.</P>)