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.

SDR VNAA202606120045Seat Track · corrodedCORROSION ON SIDE SEAT RAILS BTW FS 669 TO FS 847 RH SIDE (3 E/AS) ALSO BTW FS 847.20 TO FS 997 RH SIDE (2 E/AS) AT C PAX. SIDE SEAT RAILS BTW FS 669 TO FS 847 RH SIDE (3 E/AS) ALSO BTW FS 847.20 TO FS 997 RH SIDE (2 E/AS) AT C PAX WAS EVALUATED PER SRM 53-4Apr 2, 2026 · N649NN · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA202606120044Access Panel · corrodedCORROSION ON SEVERAL LOCATIONS OF THE ACCESS PANEL SEATING SURFACE (621AT, 621AB & 621BR) (521AT, 521AB & 521BR) BOTH WINGS. CORROSION ON SEVERAL LOCATIONS OF THE ACCESS PANEL SEATING SURFACE (621AT, 621AB & 621BR) (521AT, 521AB & 521BR) BOTH WINGS. WERE REPAApr 2, 2026 · N649NN · Cndair CL6002D24 · Wing, Plate/SkinSDR VNAA202606120043Rib · crackedCRACK ON RIB LEADING EDGE SS 57.16 AT RT WING. CRACK ON RIB LEADING EDGE SS 57.16 AT RT WING WAS REPAIRED PER REO 690-57-41-240 REV-.Apr 2, 2026 · N649NN · Cndair CL6002D24 · Fuselage Main, BulkheadSDR AALA202606019595Stringer · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON STRINGER 21R AT STA 887 PLUS 10 INCHES. REPAIRED STRINGER PER EA 374883.Apr 2, 2026 · N992AN · Boeing 737823 · Fuselage Main, Longeron/StringerSDR 2026FA0000458Stiffener · crackedL/H WING FWD LWR I/B SKIN, TOP AFT STIFFENER CRACKED. REPLACED WITH NEW.Apr 2, 2026 · N875G · Piper PA28181 · Wing Miscellaneous StructureSDR AALA202605221009Stringer · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CARGO COMPARTMENT STRINGER 21R AT STA 907. REPLACED STRINGER PER AARD 51-00-05-1.Apr 2, 2026 · N992AN · Boeing 737823 · Fuselage Main, Longeron/StringerSDR AALA202605226874Intercostal · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON INTERCOSTAL AT STA 927 PLUS 3 INCHES, AND AT S21R. REPLACED INTERCOSTAL PER AARD 51-00-05-1.Apr 2, 2026 · N992AN · Boeing 737823 · Fuselage Miscellaneous StructureSDR AALA202605220507Skin · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CARGO COMPARTMENT INTERNAL FUSELAGE SKIN BETWEEN STA 867 AND 887 OUTBOARD OF S26R. ACCOMPLISHED DOUBLER REPAIR PER SRM 51-10-02 AND EA 374893.Apr 2, 2026 · N992AN · Boeing 737823 · Fuselage Main, Plate/SkinSDR AALA202605223942Skin · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CARGO COMPARTMENT INTERNAL FUSELAGE SKIN BETWEEN STA 867 AND 887 OUTBOARD OF S27R. ACCOMPLISHED DOUBLER REPAIR PER SRM 51-10-02 AND EA 374893.Apr 2, 2026 · N992AN · Boeing 737823 · Fuselage Main, Plate/SkinSDR AALA202605223139Skin · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON FUSELAGE SKIN INTERNAL SIDE, BETWEEN STA 747 AND 767, BETWEEN S26R AND S27R. ACCOMPLISHED DOUBLER REPAIR PER SRM 51-10-02 AND EA 374893.Apr 2, 2026 · N992AN · Boeing 737823 · Fuselage Main, Plate/SkinSDR AALA202605226240Stringer · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CARGO COMPARTMENT STRINGER 22R BETWEEN STA 856 AND STA 868. SPLICE REPAIRED STRINGER PER SRM 51-00-05-1.Apr 2, 2026 · N992AN · Boeing 737823 · Fuselage Main, Longeron/StringerSDR AALA202605226481Stringer · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CARGO COMPARTMENT STRINGER 22R BETWEEN STA 868 AND STA 887. REPLACED STRINGER PER SRM 53-00-03-2R.Apr 2, 2026 · N992AN · Boeing 737823 · Fuselage Main, Longeron/StringerSDR AALA202605225314Stringer · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CARGO COMPARTMENT STRINGER 22R AT STA 872. REPLACED STRINGER PER AARD 51-00-05-1.Apr 2, 2026 · N992AN · Boeing 737823 · Fuselage Main, Longeron/StringerSDR AALA202605222783Shield · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CARGO COMPARTMENT SHEILD AT STA 868 AND S25R. REPLACED SHIELD PER AARD 51-00-05-1.Apr 2, 2026 · N992AN · Boeing 737823 · Fuselage Miscellaneous StructureSDR SIMA20260402003Seat Track · gougedSSI # 53-22-012 RH CTL 2 UPPER SEAT TRACK HAS SEVERAL GOUGES (MAJOR REPAIR) MECHANICALLY MEASURED BLENDED AREA ON RH CTR 2 UPPER SEAT TRACK, ALL AREAS FOUND TO BE WITHIN ALLOWABLE LIMITS, EXCEPT FOR FR 47 & FR 57 IAW ERJ 170 SRM 53-10-10 AND ENVOY ETN-EJ-53-01Apr 2, 2026 · N779RN · Emb ERJ170100SE · Fuselage, Seat/Cargo Attach FittingsSDR SIMA20260402001Seat Track · gougedSSI 53-22-012 LH CENTER SEAT TRACK HAS CORROSION BETWEEN FR 58/59 (MAJOR REPAIR) (LEVEL 2 CORROSION) REMOVED CORROSION ON LH CENTER SEAT TRACK BETWEEN FR 59 AND REMECHANICALLY MEASURED THE FWD OF FRM 59 AND FOUND TO BE BEYOND ALLOWABLE LIMITS IAW ERJ 170 SRM 5Apr 2, 2026 · N779RN · Emb ERJ170100SE · Fuselage, Seat/Cargo Attach FittingsSDR SIMA20260402002Seat Track · gougedLEFT CENTER 2 SEAT TRACK IS GOUGED IN SEVERAL SPOTS (MAJOR REPAIR). REMOVED GOUGES ON LH CENTER 2 SEAT TRACK IN SEVERAL SPOTS BY BLENDING IAW ERJ 170 SRM 51-10-03 AND UPON FURTHER INVESTIGATION TWO AREAS IS BEYOND ALLOWABLE LIMITS BETWEEN FR 46/47/AND 48/49 ANApr 2, 2026 · N779RN · Emb ERJ170100SE · Fuselage, Seat/Cargo Attach FittingsSDR SWAA2026051185960Scuff Plate · crackedCRACK ON AFT CORNER SCUFF PLATE AT AFT CARGO COMPARTMENT. REPAIRED AFT CORNER SCUFF PLATE AT AFT CARGO COMPARTMENT IAW BOEING 737-800 SRM 53-60-15-2R-1 REPAIR 1 AND BAC 5975.Apr 2, 2026 · N8637A · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2026051185759Skin · debondedLEFT WING OUTBD AFT FLAP INBD LOWER SKIN HAS A DISBONDED AREA. REMOVED AND REPLACED LEFT OUTBOARD AFT FLAP PER AMM 27-51-22.Apr 2, 2026 · N8534Z · Boeing 7378H4 · Trailing Edge FlapsSDR SWAA2026051185788Angle · crackedCRACKED SLAT 7 O/B ANGLE OF I/B AUXILIARY TRACK AT RT WING. REPLACED ANGLE LOCATED ON SLAT 7 O/B ANGLE OF I/B AUXILIARY TRACK AT RT WING IAW SRM 51-10-02 AND SRM 51-40-02Apr 2, 2026 · N8637A · Boeing 7378H4 · Leading Edge DevicesSDR SWAA2026051185793Crossbeam · crackedCRACK ON BRAKE PANEL LOCATED BS 540 BTW BL 0 TO LBL 24.75 WL 208.1 AT PASSENGER CABIN. REPLACED BREAK PANEL LOCATED BS 540 BTW LBL 0 TO LBL 24.75 WL 208.1 AT PASSENGER CABIN IAW SRM 51-10-02-0G ITEM 9; SRM 51-40-02-0G AND DWG: 143A0060; SHEET: 64; REV: - .Apr 2, 2026 · N8637A · Boeing 7378H4 · Fuselage Main, StructureSDR SWAA2026051185789Support Angle · crackedCRACK ON SUPPORT ANGLE LOCATED BS 270 LBL 1 WL 208.1 AT FLIGHT COMPARTMENT. REPLACED SUPPORT ANGLE LOCATED BS 270 LBL 1 WL 208.1 AT FLIGHT COMPARTMENT IAW SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DWG: 141A5210; SHEET:33.Apr 2, 2026 · N8637A · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR VNAA20260511019Slat Track · wornLEFT SLAT NO. 3-1 HAS MULTIPLE CHAFED SPOTS FROM CONTACT WITH ROLLERS. REPAIRED LH SLAT 3-1 IAW REO 670-57-42-2332REV: -- DATED:2026-01-16.Apr 2, 2026 · N512AE · Cndair CL6002C10 · Leading Edge DevicesSDR VNAA20260511018Slat Track · wornLEFT SLAT NO. 2-3 HAS MULTIPLE CHAFED SPOTS FROM CONTACT WITH ROLLERS. REPAIRED LH SLAT 2-3 IAW REO 670-57-42-2333 REV:--DATED 2026-01-16.Apr 2, 2026 · N512AE · Cndair CL6002C10 · Leading Edge DevicesSDR VNAA20260511017Slat Track · wornLEFT SLAT NO. 2-1 HAS MULTIPLE CHAFED SPOTS FROM CONTACT WITH ROLLERS. REPAIRED LH SLAT 2-1 IAW MHIRJ REO 670-57-42-2329 REV-- DATED 1-16-26.Apr 2, 2026 · N512AE · Cndair CL6002C10 · Leading Edge DevicesSDR VNAA20260511016Slat Track · wornLEFT SLAT NO. 1-3 HAS MULTIPLE CHAFED SPOTS FROM CONTACT WITH ROLLERS. REPAIRED LH SLAT 1-3 IAW REO 670-57-42-2331 REV-- DATED 2026-03-11.Apr 2, 2026 · N512AE · Cndair CL6002C10 · Leading Edge DevicesSDR VNAA20260511015Slat Track · wornLEFT SLAT NR 1-2 HAS MULTIPLE CHAFED SPOTS FROM CONTACT WITH ROLLERS. REPAIRED LH SLAT 1-2 IAW REO 670-57-42-2323 REV-- DATED 2026-01-15.Apr 2, 2026 · N512AE · Cndair CL6002C10 · Leading Edge DevicesSDR VNAA20260511014Slat Track · wornLEFT SLAT NR 1-1 HAS MULTIPLE CHAFED SPOTS FROM CONTACT WITH ROLLERS. REPAIRED LH SLAT 1-1 IAW MHIRJ REO 670-57-42-2326 REV-- DATED 1-15-26.Apr 2, 2026 · N512AE · Cndair CL6002C10 · Leading Edge DevicesSDR 2026FA0000348Pressure Sensor · malfunctionedPILOT REPORTED HIGH OIL PRESSURE, SECURED THE ENGINE IN FLIGHT AND PREFORMED A PRECAUTIONARY LANDING.Apr 2, 2026 · N281HC · Agusta AW109SP · Engine Oil PressureSDR SWAA2026050885787Support Beam · no discrepancyCRACKED SUPPORT BEAM NR 4 LOCATED FWD GALLEY DOOR. PERFORMED EDDY CURRENT HFEC INSPECTION ON SUPPORT BEAM #4 LOCATED FWD GALLEY DOOR. IAW NDT MANUAL PART 6 51-00-00 PROCEDURE 23. NO CRACK INDICATION FOUND.Apr 2, 2026 · N8637A · Boeing 7378H4 · Fuselage Main, StructureSDR SWAA2026050885954Floor Panel · delaminatedDELAMINATED FLOOR PANEL 221BF AT FWD GALLEY AREA. REPAIRED FLOOR PANEL 221BF AT FWD GALLEY AREA IAW B737-800 SRM 53-00-50-2R-1 REPAIR 1.Apr 2, 2026 · N8637A · Boeing 7378H4 · Fuselage Floor PanelSDR VNAA20260508011Slat Track · wornRIGHT SLAT TRACK 3-3 HAS CHAFING/WEAR MARKS FROM CONTACT WITH ROLLERS IN MULTIPLE PLACES. REPAIRED RH SLAT TRACK 1-2 IAW MHIRJ REO 670-57-42-2334 REV-.Apr 2, 2026 · N512AE · Cndair CL6002C10 · Leading Edge DevicesSDR VNAA20260508010Slat Track · wornRIGHT SLAT TRACK 2-3 HAS CHAFING/WEAR MARKS FROM CONTACT WITH ROLLERS IN MULTIPLE PLACES. REPAIRED RH SLAT TRACK 2-3 IAW MHIRJ REO 670-57-42-2338 REV-.Apr 2, 2026 · N512AE · Cndair CL6002C10 · Leading Edge DevicesSDR VNAA20260508009Slat Track · wornRIGHT SLAT TRACK 2-2 HAS CHAFING/WEAR MARKS FROM CONTACT WITH ROLLERS IN MULTIPLE PLACES. REPAIRED RH SLAT TRACK 2-2 IAW MHIRJ REO 670-57-42-2336 REV.-.Apr 2, 2026 · N512AE · Cndair CL6002C10 · Leading Edge DevicesSDR VNAA20260508008Slat Track · wornRIGHT SLAT TRACK 1-3 HAS CHAFING/WEAR MARKS FROM CONTACT WITH ROLLERS IN MULTIPLE PLACES. REPAIRED RH SLAT TRACK 1-3 IAW MHIRJ REO 670-57-42-2335 REV-.Apr 2, 2026 · N512AE · Cndair CL6002C10 · Leading Edge DevicesSDR VNAA20260508007Slat Track · wornRIGHT SLAT TRACK 1-2 HAS CHAFING/WEAR MARKS FROM CONTACT WITH ROLLERS IN MULTIPLE PLACES. REPAIRED RH SLAT TRACK 1-2 IAW REO 670-57-42-2325 REV-.Apr 2, 2026 · N512AE · Cndair CL6002C10 · Leading Edge DevicesSDR VNAA20260508006Slat Track · wornRIGHT SLAT TRACK 1-1 HAS CHAFING/WEAR MARKS FROM CONTACT WITH ROLLERS IN MULTIPLE PLACES. REPAIRED RT SLAT TRACK 1-1 IAW REO 670-57-42-2327 REV: -- DATED 2026-01-16.Apr 2, 2026 · N512AE · Cndair CL6002C10 · Leading Edge DevicesSDR VNAA20260508005Slat Track · wornLEFT SLAT NO. 3-3 HAS MULTIPLE CHAFED SPOTS FROM CONTACT WITH ROLLERS. REPAIRED LH SLAT 3-3 IAW MHIRJ REO 670-57-42-2342 REV:-- DATED: 2026-01-20.Apr 2, 2026 · N512AE · Cndair CL6002C10 · Leading Edge DevicesSDR VNAA20260508004Slat Track · wornLEFT SLAT NO. 3-2 HAS MULTIPLE CHAFED SPOTS FROM CONTACT WITH ROLLERS. REPAIRED LT SLAT 3-2 IAW MHIRJ REO 670-57-42-2340 REV--.Apr 2, 2026 · N512AE · Cndair CL6002C10 · Leading Edge DevicesSDR SWAA2026050485800Nut Plate · crackedCRACK RAIL NUT PLATES INTERNAL CAVITY LEADING EDGE LOCATED OFSS491 AT RT WING. REPLACED RAIL NUT PLATES AND FASTENERS INTERNAL CAVITY LEADING EDGE LOCATED OFSS491 AT RT WING IAW SRM 51-10-02; SRM 51-40-02 AND DWG 112A4402 SHEET 13 REV -.Apr 2, 2026 · N255WN · Boeing 7377H4 · Wing, Attach FittingsSDR SWAA2026050495357Nut Plate · crackedCRACK RAIL NUT PLATES INTERNAL CAVITY LEADING EDGE LOCATED OFSS491 AT RT WING. REPLACED RAIL NUT PLATES AND FASTENERS INTERNAL CAVITY LEADING EDGE LOCATED OFSS491 AT RT WING IAW B737-700 SRM 51-10-02; SRM 51-40-02 AND DWG 112A4402 SHEET 13 REV -.Apr 2, 2026 · N255WN · Boeing 7377H4 · Wing, Attach FittingsSDR SWAA2026050485798Nut Plate · crackedCRACK RAIL NUT PLATES INTERNAL CAVITY LEADING EDGE LOCATED OFSS574 AT RT WING. REPLACED RAIL NUT PLATES LOC. INTERNAL CAVITY LEADING EDGE OFSS574 AT RT WING IAW SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DWG 112A4402 SHEET 13 REV .Apr 2, 2026 · N255WN · Boeing 7377H4 · Wing, Attach FittingsSDR SWAA2026043085948Support Bracket · crackedCRACKED SUPPORT BRACKET ON THE PNEUMATIC DUCT, BS 540, RBL 6 IN THE AIR CONDITIONING BAY. REPLACED THE SUPPORT BRACKET IAW SRM 51-10-02, ITEM 9, AND SRM 51-40-02.Apr 2, 2026 · N244WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2026043085949Support Bracket · crackedCRACKED SUPPORT BRACKET, ON PNEUMATIC DUCT, BS 540, LBL 6 IN THE AIR CONDITIONING BAY. REPLACED THE SUPPORT BRACKET IAW SRM 51-10-02, ITEM 9, AND SRM 51-40-02.Apr 2, 2026 · N244WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR CALA2026042915827Floor Support · corrodedAFT WET AREA; FLOOR SUPPORT BETWEEN FLOOR BEAM STA. 947.5 AND FLOOR BEAM STA. 967 RBL 50 MULTIPLE POINTS CORROSION. REQUIRE REPLACE. REMOVED AND REPLACED INTERCOSTAL BS 927- STA 947 RBL 50 IAW SRM 51-40-02-0G-0 STEP 7, SRM 51-40-05 TABLE A, SRM 51-20-01 STEP Apr 2, 2026 · N37290 · Boeing 737824 · Fuselage Miscellaneous StructureSDR IPXA2026042894871Plate · missingFOUND MAIN ENTRY DOOR CUTOUT STOP PLATE MISSING AT AFT MID SIDE. I.A.W AMM 52-11-01-700-801 REV.50 INSTALL MAIN ENTRY DOOR CUTOUT STOP PLATE AT AFT MID SIDE.Apr 2, 2026 · N610UP · Boeing 7478F · Fuselage Main, StructureSDR ASAA2026040265679Tee Angle · corrodedAFT WET AREA LT SIDE BS 986.5 UPPER TEE CHORD HAS MULTIPLE SPOTS OF COROSION. GROUNDED - YES. EVALUATED CORROSION, ORIG THICK IS .150", REMOVED .065",REMAINING IS .085" FOUND OUT OF LIMITS IAW SRM 53-70-51-1A-1. REMOVED AND REPLACED TEE CHORD SECTION IAW SRM 5Apr 2, 2026 · N528AS · Boeing 737890 · Fuselage Main, Floor BeamSDR SWAA2026042785989Window Frame · crackedF/O NR 1 WINDOW FRAME OTBD UPPER CORNER CRACKED ACCOMPLISHED REPAIR NR 1 WINDOW OTBD POST IAW EA 26-153-00937 WIP1 AND WIP2.Apr 2, 2026 · N7736A · Boeing 7377BD · Fuselage Main, StructureSDR CALA2026042415670Stabilizer · corrodedAFT WET AREA; POSSIBLE CORROSION ON FLOOR SUPPORT STABILIZER BTW STA 947 AND 964, RBL 11. (REF AAR NR 1000073111). REMOVED AND REPLACED FLOOR SUPPORT STABILIZER BTW STA 947 AND 964, RBL 11 IAW B737-800 SRM 51-40-02-0G-0 AND DWG 147A5760. (WORK ACCOMPLISHED BY Apr 2, 2026 · N37290 · Boeing 737824 · Fuselage Miscellaneous StructureSDR AALA202604223806Attach Bracket · crackedAIRCRAFT IN BASE MAINTENANCE: AFT CARGO WALL ATTACH BRACKET AT FLOOR CRACKED BS 867 AND LBL 12. REMOVED WALL ATTACH BRACKET, INSTALLED NEW WALL ATTACH BRACKET. PER SRM 51-40-02Apr 2, 2026 · N992AN · Boeing 737823 · Fuselage Main, Attach Fittings