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 AALA202605015754Battery Pack · no testAIRCRAFT WAS GROUNDED: SEAT MOUNTED EMERGENCY ESCAPE PATH LIGHTS FROM ROW 26 TO 33 FAILED TO ILLUMINATE WHEN EMERGENCY LIGHTS WERE ACTIVATED DURING ACCOMPLISHMENT OF JC 08T20033001. FOUND EMERGENCY BATTERY PACK NOT CHARGING AND BATTERY DEPLETED, REMOVED AND SDR DXTR2026050100314Skin · corrodedPOSSIBLE CORROSION ON LOWER LT WING SKIN AT TIP CAP. REMOVED CORROSION FROM SKIN REF SRM 51-10-01. NDT SERVICES PROVIDED BY TOLEDO JET CENTER, CRS 2TJR420B ON WORK ORDER 85280. NO CRACKS NOTED IN THE AREA OF INSPECTION AT THIS TIME. COMPLIED WITH STEPS 1 TSDR 2026FA0000311Tube · meltedOWNER ADVISED TECHNICIAN THAT NEITHER OF THE TWO AIRSPEED INDICATORS WERE READING. WHEN TECHNICIAN OPENED INSPECTION PANELS NEAR THE PITOT PROBE, THE PLASTIC TUBING WAS FOUND TO BE MELTED THROUGH BY WHAT APPEARED TO BE A WIRE. TECHNICIAN FOUND THAT THE WIRES CSDR IPXA2026050962784Access Panel · damagedMAJOR REPAIR, LT VERTICAL STABILIZER ACCESS PANEL 322DL, AT FSS 295.915 TO 371.308, HAD HAIL DAMAGE.SDR SWIA2026043077330Skin · erodedEROSION NOTED AT LT INBD, FLAP LOWER SKIN BETWEEN FLS 50-59 AND FLS 78-85. REPAIRED THE INBD FLAP LOWER SKIN BETWEEN FLS 50498 - FLS 74-718, LT IAW REO 601R-57-52-2563 -.SDR SWIA2026043077326Skin · dentedDENT NOTED ON LT INBD FLAP LOWER SKIN AT APPROX FLS 71-72 AND 15 INCHES FROM TE. INSTALLED REPAIR DOUBLER AND APPLIED AERODYNAMIC SEALANT AT LT INBD FLAP LOWER SKIN IAW REO 601R-57-52-678, REV-C.SDR SWIA2026043077289Vane · erodedEROSION NOTED ON THE LT INBD FLAP VANE LOWER SKIN AT FLS 50 - 59 AND FLS 78 - 85. THE LT INBD FLAP WAS REPLACED ON HN 310594, MX TRANS 32170861. NO FURTHER ACTION REQUIRED AT THIS TIMESDR SWIA2026043077194Intercostal · corrodedPAX DOOR, CENTER INTERCOSTAL DD2 IS CORRODED. REMOVED AND REPLACED PAX DOOR CENTER INTERCOSTAL DD2 IAW SRM 51-42-06-00, AND 51-42-21-00. COMPLETED TASK CARD 51-900-1003-SKY, NO WEIGHT CHANGE. REF CONTINUATION CARD FOR WORK PERFORMED.SDR SWIA2026043077188Intercostal · corrodedPAX DOOR, CENTER INTERCOSTAL DD4 WAS CORRODED. PAX DOOR, CENTER INTERCOSTAL DD4 WAS REMOVED & REPLACED WITH A NEW ONE IAW SRM 51-42-06-00, & SRM 51-42-21-00. COMPLETED TASK CARD 51-900-1003-SKY. NO WEIGHT CHANGE. REF CONTINUATION CARD FOR WORK PERFORMED.SDR SWIA2026043077181Intercostal · corrodedPAX DOOR, CENTER INTERCOSTAL DD3 IS CORRODED. PAX DOOR, CENTER INTERCOSTAL DD3 WAS REMOVED AND REPLACED WITH A NEW ONE IAW SRM 51-42-06-00 AND SRM 51-42-21-00. COMPLETED TASK CARD 51-900-1003-SKY. NO WEIGHT CHANGE, REF CONTINUATION CARD FOR WORK PERFORMED.SDR 2026FA0000726Stiffener · crackedL/H WING FWD LWR I/B SKIN, TOP AFT STIFFENER CRACKED. REPLACED WITH NEWSDR CALA2026082718970Pressure Blkhd · crackedSUPPORT TASK: 2EA CRACKS FOUND ON RH CENTER WING BOX REAR SPAR VERTICAL PRESSURE WEB AT THE RBL 31.83 TO 40.00 BAY AND RBL 40.00 TO 45.64 BAY.TRANSCRIBED FROM AAR GSO NRC 9288075 COMPLETED ESFR THIS IS A CATEGORY B REPAIR AND REQUIRES A HIGH FREQUENCY EDDY CUSDR REXA2026070301039Intercostal · corrodedCORROSION ON INTERCOSTALS (3 EAS) BTW FS 349 TO FS 364 NEAR STGR 27 ALSO STGR 26R AT MAIN AVIONICS COMPARTMENT INTERCOSTALS BTW 7LH AND 27RH, BTW FS 349 TO FS 364 NEAR STGR 27R WERE REPAIRED PER EA CRJ953-22320 REV IR AND EA NO: CRJ953-22321 REV IR AND INTERCSDR REXA2026070301037Intercostal · corrodedCORROSION ON INTERCOSTALS (3 EAS) BTW FS 394 TO FS 409 NEAR STGR 27 ALSO STGR 26L AT MAIN AVIONICS COMPARTMENT INTERCOSTALS (3 EAS) BTW FS 394 TO FS 409 NEAR STGR 27 ALSO STGR 26L AT MAIN AVIONICS COMPARTMENT WERE REPAIRED PER EA NO: CRJ953-20508 REV ASDR REXA2026070301036Frame Splice · crackedCRACK ON FRAME SPLICE AT 31.87% AND STGR 2L TO VERTICAL STABILIZER REAR SPAR DATUM, ON AFT ACCESSORIES COMPARTMENT. FRAME SPLICE AT 31.87% AND STGR 2L TO VERTICAL STABILIZER REAR SPAR DATUM, ON AFT ACCESSORIES COMPARTMENT WAS REPAIRED PER REO 690-53-71-107 REVSDR SWIA2026043076374Repair · corrodedEXTERNAL FUSELAGE STATION 985 STG27, REPAIR PATCH HAS CORROSION IN VARIOUS AREAS, BLENDED AND TREATED CORROSION ON REPAIR PATCH ON EXTERNAL SKIN AT FS985.00 AND STGR27 PER MHIRJ REO 670-53-51-395 REV-- DATED 2026-05-06, REO 670-53-00-290 REV. -F DATED 2019-0SDR BAGA2026062300006Battery · failedHEAVY CHECK, UPPER FUSELAGE PAX CABIN EXIT MARKER LT & RT EMERGENCY LIGHT INOP. REPLACE ELPU NR 3.SDR SCNA20260616250Angle · wornWEAR ON ANGLE AT LOWER SURFACE OF INB MAIN FLAP APROX ITEF 75.97 AT LT & RT WINGS. ANGLES WERE REPLACED AT LOWER SURFACE OF INB MAIN FLAP APROX ITEF 75.97 AT LT & RT IAW SRM 51-40-02-0G-0.SDR VNAA202606120004Bracket · corrodedCORROSION ON BRACKET (FWD SURFACE) OF CONNECTOR HARNESSES AT LT (PX19P1 AND PX34P1) RT (PX17P1 AND PX33P1) MLG WHEEL WELL. CORROSION ON BRACKET (FWD SURFACE) OF CONNECTOR HARNESSES AT LH(PX19P1 AND PX34P1) / RH(PX17P1 AND PX33P1) MLG WHEEL WELL WAS REMOVED PSDR SIMA20260430003Shear Tie · corrodedSSI: 53-10-016) SHEAR CLIP AT FR17 BETWEEN STGR 24R AND STGR 25R IS CORRODED (MAJOR REPAIR) (LEVEL 2 CORROSION) RAR SHEAR CLIP AT FR17 BETWEEN STGR 24R AND STGR 25R IAW ERJ 170 SRM 51-40-08.SDR SWAA2026060394137Scuff Plate · crackedCRACK ON FWD CORNER SCUFF PLATE LOC ON AFT CARGO COMPARTMENT. REPAIRED FWD CORNER SCUFF PLATE LOC ON AFT CARGO COMPARTMENT IAW SRM 53-60-15-2R-1 REPAIR 1; AND BAC 5975.SDR HNAA2026060200471Partition · gougedLH COCKPIT PARTITION LOWER PIN HOLE LOCATION ON INTERNAL FUSELAGE STRUCTURE IS GOUGED. ACCOMPLISHED PERMANENT REPAIR TO LH COCKPIT PARTITION LOWER PIN HOLE LOCATION ON NTERNAL FUSELAGE GOUGE IAW EMB 145 SRM 53-21-02RE, ITEM 4, FIG 204 AND EO1-53-26-0245.SDR AALA202606026018Stringer Splice · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CARGO COMPARTMENT STRINGER SPLICE AT STA 847 AND S26R. REPLACED STRINGER SPLICE PER AARD 51-00-05-1.SDR HNAA2026060200473Floorbeam · damagedCENTER FLOOR BEAM GUSSET HAS TWO ELONGATED HOLES AT NUTPLATE ATTACHMENT BETWEEN FRAMES 70-71. REMOVED AND REPLACED CARGO. CENTER FLOOR BEAM GUSEET AND PERFORMED REPAIR ON CENTER FLOOR BEAM BETWEEN FRAMES 70-71 IAW EMB 145 SRM 51-20-03, 51-40-02, EMB 145 ETD2SDR SWAA2026060194290Angle · crackedCRACK ON ANGLE LOCATED BS 500H AFT SIDE AND S-26R AT FWD CARGO COMPARTMENT. REPLACED ANGLE LOCATED BS 500H AFT SIDE AND S-26R AT FWD CARGO COMPARTMENT IAW SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DWG 143A7505; SHEET 138; REV -.SDR SWAA2026060194294Angle · crackedCRACKED ANGLE LOCATED BS500G FWD SIDE AND S-26L AT FWD CARGO COMPARTMENT. REPLACED ANGLE LOCATED BS500G FWD SIDE AND S-26L AT FWD CARGO COMPARTMENT IAW SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DWG 143A7505; SHEET 137; REV -.SDR SWAA2026060194297Angle · crackedCRACKED ANGLE LOCATED BS 500G FWD SIDE AND S-26R AT FWD CARGO COMPARTMENT. REPLACED REPAIR ANGLE AND FASTENERS LOCATED BS 500G FWD SIDE AND S-26R AT FWD CARGO COMPARTMENT IAW B737-800 SRM 51-40-02 ; SRM 51-10-02 ITEM 9 AND DWG 143A7505; SHEET 139; REV-.SDR SWAA2026060194298Angle · crackedCRACK GUSSET ANGLE LOCATED BS 500I AT LEVEL STR 19R AT FWD CARGO COMPARTMENT. REPLACED GUSSET ANGLE AND FASTENERS LOCATED ON BS 500I AT LEVEL STR 19R AT FWD CARGO BAY IAW SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DWG: 143A7902; SHEET: 256 AND 257; REV: B.SDR SWAA2026060194289Angle · crackedCRACKED ANGLE LOCATED BS 500H FWD SIDE AND S-26R AT FWD CARGO COMPARTMENT. REPLACED ANGLE AND FASTENERS LOCATED BS 500H FWD SIDE AND S-26R AT FWD CARGO COMPARTMENT IAW SRM 51-10-02 ITEM 9, SRM 51-40-02 AND DWG 143A7505, SHEET 137; REV-.SDR SWAA2026060194296Angle · crackedCRACKED ANGLE LOCATED BS 500G AFT SIDE AND S-26R AT FWD CARGO COMPARTMENT. REPLACED ANGLE AND FASTENERS LOCATED BS 500G AFT SIDE AND S-26R AT FWD CARGO COMPARTMENT IAW SRM 51-10-02 ITEM 9 ; SRM 51-40-02 AND DWG 143A7505; SHEET 139; REV-.SDR SWAA2026052894463Skin · corrodedCORROSION ON FWD EXTERNAL SKIN AT BS1016, STR 25R. REMOVED CORROSION AND EVALUATED REWORK AREA IAW SRM 53-00-01-1A-1, ALLOWABLE DAMAGE 1.SDR SWAA2026052894466Floor Panel · delaminatedDELAMINATED FLOOR PANEL 232SF IN THE PAX CABIN. REPAIRED THE FLOOR PANEL 232SF AT PASSENGER CABIN IAW SRM 53-00-50-2R-7, REPAIR 7.SDR SWAA2026052894465Skin · corrodedCORROSION ON AFT EXTERNAL SKIN AT BS1016 AT LEVEL STR 27L LOWER FUSELAGE. REMOVED CORROSION LOC. ON EXTERNAL SKIN AT BS1016 AT STR 27L LOWER FUSELAGE IAW SRM 51-10-02 AND EVALUATED REWORKS AREAS LOC. ON FWD AND AFT EXTERNAL SKIN AT BS1016 AT STR 27L LOWER FUSSDR SWAA2026052894464Skin · corrodedCORROSION ON FWD EXTERNAL SKIN AT BS 1016 AT STR 27R LOWER FUSELAGE. REMOVED CORROSION LOC. ON EXTERNAL SKIN AT BS 1016 AT STR 27R LOWER FUSELAGE IAW SRM 51-10-02 AND EVALUATED REWORKS AREA LOC. ON FWD AND AFT EXTERNAL SKIN AT BS 1016 AT LEVEL STR 27R LOWER SDR SWAA2026052794428Support Angle · crackedCRACK ON SUPPORT ANGLE LOCATED ACCESS PANEL 834DZ AT AFT ENTRY DOOR . REPLACED SUPPORT ANGLE LOCATED ACCESS PANEL 834DZ AT AFT ENTRY DOOR MEASURE CRACK IS:0.279? IAW SRM 51-40-02; SRM 51-10-02 ITEM 9 AND DWG 411A2119 SHEET 72 REV: - .SDR SWAA2026052794302Support Angle · crackedCRACK ON SUPPORT ANGLE LOCATED BTW BS 500I TO BS 520 LBL 1 WL 208.1 AT PASSENGER CABIN . REPLACED SUPPORT ANGLE LOCATED BTW BS 500I TO BS 520 LBL 1 WL 208.1 AT PASSENGER CABIN IAW BOEING 737-800 SRM-51-10-02 ITEM 9 AND DGW 143A5400 SHEET: 189 AND 190 REV-.SDR SWAA2026052703510Reveal · crackedCRACK ON REVEAL ASSY LOCATED ACCESS PANEL 844AW AT AFT GALLEY DOOR. REPLACED REVEAL ASSY LOCATED ACCESS PANEL 844AW AT AFT GALLEY DOOR IAW SOPM 20-50-01 REV 40 AND DWG 411A2104 REV - SHEET 30, CRACK MEASURES: 1.5070 IN.SDR SWAA2026052794427Support Web · crackedCRACK SUPPORT WEB LOCATED OUTBOARD FAN COWL ON ENGINE 2. REPLACED SUPPORT WEB LOCATED OUTBOARD FAN COWL ON ENGINE 2 IAW SRM 51-10-02-0G-0 PARAGRAPH 9; SRM 51-40-02-0G-0 AND CMM 71-13-30 REV 34. PAGE 10090 DETAIL P; FIGURE 3; SHEET 5.SDR SWAA2026052794301Support Web · crackedCRACK SUPPORT WEB LOCATED INBOARD FAN COWL ON ENGINE 1. REPLACED SUPPORT WEB AND FASTENERS LOCATED ON INBOARD FAN COWL AT ENGINE 1 IAW SRM 51-10-02-0G-0 PARAGRAPH 9; SRM 51-40-02-0G-0 AND CMM 71-13-30 PAGE 10090. MEASUREMENT OF CRACK: 1.317 INCH.SDR SWAA2026052694300Support Beam · crackedCRACKED SUPPORT BEAM NR 4 LOCATED FWD GALLEY DOOR. REPLACED SUPPORT BEAM #4 LOCATED FWD GALLEY DOOR IAW B737-800 SRM 51-40-02; SRM 51-10-02 ITEM 9 AND DRAWING 141A6516 SHEET 142 REV-.SDR SWAA2026052694432Plate · crackedCRACKED CORRUGATED PLATE TRAILING EDGE AT ORSS294 AT LT WING. REPLACED CORRUGATED PLATE TRAILING EDGE AT ORSS294 AT LT WING IAW SRM 51-40-02 SRM 51-10-02 ITEM 9. MEASURE OF CRACK IS L=0.890 INCH.SDR SWAA2026052694434Angle · crackedCRACK ANGLE TRAILING EDGE AT ORSS277 AT LT WING . REPLACED ANGLE ON TRAILING EDGE AT ORSS277 AT LT WING IAW B737-800 SRM 51-40-02 SRM 51-10-02 Ï¿½TEM 9 AND DWG 115A6200 SHEET:17 REV:ASDR AALA202605250280Attach Angle · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK IN WING CENTER SECTION REAR SPAR VAPOR BARRIER ATTACH ANGLE AT STA 663 BETWEEN LBL 18 AND LBL 72. REPAIRED ANGLE PER SRM 57-10-10-2R-5 AND EA 374988.SDR AALA202605220244Stringer Splice · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON STRINGER SPLICE AT STA 794 AND S26R. REPLACED STRINGER SPLICE PER AARD 51-00-05-1.SDR AALA202605220638Tie Down · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON L1 ENTRY DOOR FORWARD GIRT BAR TIEDOWN AT STA 312 AND LBL 55. REPLACED TIEDOWN PER AARD 51-00-05-1.SDR AALA202605227718Tie Down · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON L1 ENTRY DOOR AFT GIRT BAR TIEDOWN AT STA 344 AND LBL 60. REPLACED TIEDOWN PER AARD 51-00-05-1.SDR SWAA2026052294431Plate · crackedCRACK CORRUGATED PLATE TRAILING EDGE AT IRSS217 AT RT WING. REPLACED CORRUGATED PLATE TRAILING EDGE AT IRSS217 AT RT WING IAW SRM 51-40-02 AND DWG 115A2713 SHEET 6 REV A.SDR SWAA2026052294433Plate · crackedCRACK CORRUGATED PLATE TRAILING EDGE AT ORSS304 AT LT WING. REPLACED CORRUGATED PLATE TRAILING EDGE AT ORSS304 AT LT WING IAW B737-800 SRM 51-40-02 SRM 51-10-02 ITEM 9. MEASURE OF CRACK IS L=0.565 INCH.SDR SWAA2026052294430Support Beam · crackedCRACK SUPPORT BEAM TRAILING EDGE LOCATED ORSS288 AT RT WING. REPLACED SUPPORT BEAM TRAILING EDGE LOCATED ORSS288 AT RT WING IAW SRM 51-40-02-0G AND DWG 115A3712 SHEET 7 REV A.SDR AALA202605223005Floor Support · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT PASSENGER CABIN FLOOR STRUCTURE INTERCOSTAL AT STA 950 AND RBL 48. REPLACED INTERCOSTAL PER AARD 51-00-05-1.