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 VNAA202607010003Seat Track · corrodedCORROSION AND GOUGES ON LH SIDE SEAT RAIL AT STGR 15L 03 SEGMENTS: (01) BTW STA FS379 TO FS483, INITIAL INSPECTION: CORROSION AND GOUGES ON RH SIDE SEAT RAIL AT STGR 15R 03 SEGMENTS: BTW STA FS379 TO FS483, FS483 TO FS573, FS573 TO FS669 AT PASSENGER COMPARTMay 15, 2026 · N530EA · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA202607010002Seat Track · corrodedCORROSION AND GOUGES ON LH SIDE SEAT RAIL AT STGR 15L 03 SEGMENTS: (01) BTW STA FS379 TO FS483, (02) FS483 TO FS573, (03) FS573 TO FS669 AT PASSENGER COMPARTMENT. WERE EVALUATED, LH SIDE SEAT RAIL AT STGR 15L 03 SEGMENTS: (01) BTW STA FS379 TO FS483, (02) FS4May 15, 2026 · N530EA · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA202607010001Seat Track · corrodedCORROSION ON RT SEAT RAIL RBL9 03 SEGMENTS: (01) BTW FS350.00 TO FS485.00. (02) BTW FS485 TO FS581, (03) BTW FS581 TO FS677 AT PAX CABIN. WERE EVALUATED, RH SEAT RAIL RBL9 03 SEGMENTS: (01) BTW FS350.00 TO FS485.00. (02) BTW FS485 TO FS581, (03) BTW FS581 TO May 15, 2026 · N530EA · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR SWAA2026063003549Floor Panel · pulledAFT FLOOR PANEL 242TF UPPER SURFACE HAS PULLED STRANDS<[01] 242TF AFT FLOOR PANEL FOUND UPPER AND LOWER SURFACE DAMAGE HAS BEEN REPAIRED IAW SRM 53-00-50-2R-1.;[02] VERIFIED CORRECTIVE ACTION ITEM 1.May 15, 2026 · N929WN · Boeing 7377H4 · Fuselage Floor PanelSDR VNAA202606300015Seat Track · corrodedCORROSION ON LH SEAT RAIL LBL 9, 03 SEGMENTS: (01) BTW FS375 TO FS485. (02) BTW FS485 TO FS581. (03) BTW FS581 TO FS677. AT PAX CABIN. EVALUATED, LH SEAT RAIL LBL 9, 03 SEGMENTS: (01) BTW FS375 TO FS485. (02) BTW FS485 TO FS581. (03) BTW FS581 TO FS677. AT PAMay 15, 2026 · N530EA · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR 2026FA0000548Backboard · damagedBACKBOARD CABLE ASSEMBLY CLASHES WITH THE BACKBOARD AND BACK STRUCTURE CAUSING DAMAGE TO BOTH PARTS. DUE TO THE DAMAGE TO THE PRIMARY STRUCTURE (BACK STRUCTURE) WOULD RECOMMEND ISSUING AN OR AS A VOLUNTARY AND CONDUCT A RCA. REVIEW WITH REPAIRS IF THEY HAVE SMay 15, 2026 · Fuselage Miscellaneous StructureSDR SWAA2026062903537Floor Panel · pulledAFT FLOOR PANEL 241YF UPPER SURFACE HAS PULLED STRANDS. REPAIRED PER SRM 53-00-50-2R-1-A00939.May 15, 2026 · N929WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2026062903543Floor Panel · pulledAFT FLOOR PANEL 242UF UPPER SURFACE HAS PULLED STRANDS. 242UF AFT FLOOR PANEL FOUND UPPER AND LOWER SURFACE DAMAGE HAS BEEN REPAIRED IAW SRM 53-00-50-2R-1.May 15, 2026 · N929WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2026062903535Floor Panel · pulledAFT FLOOR PANEL 241AAF UPPER SURFACE HAS PULLED STRANDS. FABRICATION OF NEW 241AAF FLOOR PANEL REPLACEMENT HAS BEEN ACCOMPLISHED IAW SRM 53-00-50-2R-0.May 15, 2026 · N929WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2026062903540Floor Panel · pulledAFT FLOOR PANEL 241ABF UPPER SURFACE HAS PULLED STRANDS. AFT FLOOR PANEL 241ABF UPPER SURFACE WITH PULLED STRANDS WAS REPAIRED PER SRM 53-00-50-2R-1.May 15, 2026 · N929WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2026062903536Floor Panel · pulledAFT FLOOR PANEL 241XF UPPER SURFACE HAS PULLED STRANDS. AFT FLOOR PANEL 241XF UPPER SURFACE WITH PULLED STRANDS WAS REPAIRED PER SRM 53-00-50-2R-1.May 15, 2026 · N929WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2026062903547Floor Panel · pulledFWD FLOOR PANEL 222BF UPPER SURFACE HAS PULLED STRANDS. FWD FLOOR PANEL 222BF UPPER SURFACE WITH PULLED STRANDS WAS REPAIRED PER SRM 53-00-50-2R-1.May 15, 2026 · N929WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2026062903548Floor Panel · pulledFWD FLOOR PANEL 222DF UPPER SURFACE HAS PULLED STRANDS. PULLED STRANDS ON UPPER SURFACE OF FWD FLOOR PANEL 222DF WERE REPAIRED IAW SRM 53-00-50-2R-1.May 15, 2026 · N929WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2026062903407Stub Frame · crackedCRACK ON FSD STUB FRAME .6' ABOVE SEAL DEPRESSOR AT BS291.5 + 9, REMOVED DAMAGE FSD STUB FRAME, LOCATED, DRILLED, AND INSTALLED NEW FSD STUB FRAME AT BS 291+9 IAW SRM 51-40-02-0G-0, AND DWG 141A8370, REV D.May 15, 2026 · N929WN · Boeing 7377H4 · Fuselage Main, FrameSDR FDEA202605150792Bearing Fitting · damagedCARGO DOOR/HYD SYS - DETAILED VISUAL INSPECTION OF THE MAIN DECK CARGO DOOR (MDCD) ACTUATOR BEARING FITTING AT FRAME 23 AND 24 - AOT A52W016-24 COMPLIED WITH EO 6-5230-E0378588 C P5. TITLE: DOORS - CARGO DOOR/HYD SYS - DETAILED VISUAL INSPECTION OF THE MAIMay 15, 2026 · N660FE · Airbus A300F4605R · Cargo/Baggage DoorsSDR SWAA2026062203199Floor Panel · pulledFLOOR PANEL 231XF UPPER SKIN HAS AREAS OF PULLED STRANDS. THE FLOOR PANEL WAS REPLACED WITH A NEWLY FABRICATED FLOOR PANEL IAW SRM 53-00-50-2R-0 & DWG 144A5810.May 15, 2026 · N8646B · Boeing 7378H4 · Fuselage Floor PanelSDR SWAA2026062203201Floor Panel · pulledFLOOR PANEL 231ZF UPPER SKIN HAS AREAS OF PULLED STRANDS. THE FLOOR PANEL WAS REPLACED WITH A SERVICEABLE FLOOR PANEL IAW SRM 51-10-02-0G-0, PARA 9.A.1.May 15, 2026 · N8646B · Boeing 7378H4 · Fuselage Floor PanelSDR SWAA2026062203200Floor Panel · pulledFLOOR PANEL 241BF UPPER SKIN HAS AREAS OF PULLED STRANDS. THE FLOOR PANEL WAS REPLACED WITH A NEWLY FABRICATED FLOOR PANEL DUE TO AMOUNT OF ALL DAMAGE IAW SRM 53-00-50-2R-0, AND DWG 144A5810.May 15, 2026 · N8646B · Boeing 7378H4 · Fuselage Floor PanelSDR SWAA2026062203204Floor Panel · pulledFLOOR PANEL 242AF UPPER SKIN HAS AREAS OF PULLED STRANDS. THE FLOOR PANEL WAS REPLACED WITH A NEWLY FABRICATED FLOOR PANEL IAW SRM 53-00-50-2R-0, DWG 144A5810.May 15, 2026 · N8646B · Boeing 7378H4 · Fuselage Floor PanelSDR SWAA2026062203202Floor Panel · pulledFLOOR PANEL 232SF UPPER SKIN HAS MULTIPLE AREAS OF PULLED STRANDS. THE FLOOR PANEL 232SF WAS REPLACED WITH A SERVICEABLE FLOOR PANEL IAW SRM 51-10-02-0G-0, PARA 9.A.1.May 15, 2026 · N8646B · Boeing 7378H4 · Fuselage Floor PanelSDR SWAA2026062203203Floor Panel · pulledFLOOR PANEL 241AF UPPER SKIN HAS AREAS OF PULLED STRANDS. REPAIRED IAW SRM 53-00-50-2R-0-B00275,May 15, 2026 · N8646B · Boeing 7378H4 · Fuselage Floor PanelSDR SWAA2026062203776Scuff Plate · crackedACD FWD CORNER SCUFF PLATE IS CRACKED. REMOVED AND REPLACED ACD FWD CORNER SCUFF PLATE IAW SRM 51-40-02, AND DWG 146A8341, REV A.May 15, 2026 · N8646B · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2026061803496Angle · crackedCRACKED ANGLE AT BS 663.75 RBL34 UPPER POSITION. REPLACED ANGLE BS 663.75 BTW RBL 5 TO RBL 65 UPPER POSITION IAW SRM 51-10-02, ITEM 9, SRM 51-40-02, AND DWG 111A1000, SHEET 349, REV-.May 15, 2026 · N500WR · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2026061803493Support Angle · crackedCRACK ON SUPPORT ANGLE LOCATED BTW BS 291.5 TO BS 294.5 AT LEVEL STR 17R AT FWD GALLEY AREA. REPLACED SUPPORT ANGLE LOCATED BTW BS 291.5 TO BS 294.5 AT LEVEL STR 17R AT FWD GALLEY AREA IAW SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DWG 141A8310; SHEET 33; REV-.May 15, 2026 · N500WR · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2026061803395Angle · crackedCRACKED ANGLE TRAILING EDGE LOCATED ORSS 280 RT WING. REPLACED ANGLE TRAILING EDGE LOCATED ORSS 280 RT WING IAW ALLOWABLE DAMAGE 57-51-02-1A-1 ALLOWABLE DAMAGE 1, NOT FOUND ALLOWABLE DAMAGE, SRM 51-10-02-0G-0, ITEM 9, SRM 51-40-02-0G-0, AND DWG 115A6200, SHEEMay 15, 2026 · N500WR · Boeing 7378H4 · Wing Miscellaneous StructureSDR SWAA2026061803396Frame · crackedCRACKED FRAME, BS 312 BTW STR 5L - 6L. PERFORMED PERMANENT REPAIR ON FRAME IAW EA M-22-153-01244.May 15, 2026 · N500WR · Boeing 7378H4 · Fuselage Main, FrameSDR SWAA2026061803494Support Bracket · crackedCRACKED SUPPORT BRACKET, BS 867 BTW STR 2R - 3R IN THE PAX CABIN. REPLACED SUPPORT BRACKET IAW SRM 51-40-02 SRM 51-10-02 ITEM 9 AND DWG 146A7901, SHEET 66, REV A.May 15, 2026 · N500WR · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR AALA202606183294Shear Plate · crackedAIRCRAFT IN BASE MAINTENANCE: CRACKED AFT CABIN FLOOR SHEAR PLATE BETWEEN FR 69 AND FR 70 AT S23R. REPLACED SHEAR PLATE PER SRM 51-42-11.May 15, 2026 · N155UW · Airbus A321211 · Fuselage Miscellaneous StructureSDR AALA202606182573Shear Plate · crackedAIRCRAFT IN BASE MAINTENANCE: CRACKED AFT CABIN FLOOR SHEAR PLATE BETWEEN FR 69 AND FR 70 AT S23L. REPLACED SHEAR PLATE PER SRM 51-42-11.May 15, 2026 · N155UW · Airbus A321211 · Fuselage Miscellaneous StructureSDR SWIA2026051576230Beam · corrodedAFT WET AREA LT BEAM AT FR 85-87, Y-10". CORROSION AT MULTIPLE LOCATIONS. REMOVED AND REPLACED AFT WET AREA LT BEAM AT FR 85-87, Y-10" PER SRM 51-40-08.May 15, 2026 · N141SY · Emb ERJ170200LR · Fuselage Miscellaneous StructureSDR SWIA2026051576228Beam · corrodedAFT WET AREA RT BEAM AT FR 86-89, Y+10", CORROSION AT MULTIPLE LOCATIONS. REMOVED AND REPLACED AFT WET AREA RT BEAM AT FR 86-89, Y+10" PER SRM 51-40-08May 15, 2026 · N141SY · Emb ERJ170200LR · Fuselage Miscellaneous StructureSDR SWIA2026051576226Seat Track · corrodedAFT WET AREA LH SEAT TRACK CORROSION AT MULTIPLE LOCATIONS AT FR 78-85, Y-10". REMOVED AND REPLACED AFT WET AREA LT SEAT TRACK AT FR 78-85, Y-10" PER E175 SRM 51-40-08.May 15, 2026 · N141SY · Emb ERJ170200LR · Fuselage, Seat/Cargo Attach FittingsSDR IPXA2026060906876Tee Angle · corrodedRH WING TO BODY T-CHORD AT STA 1060 IS CORRODED. INSTALLED NEW T-CHORD IAW SRM B757-200 TASK: 51-40-02May 15, 2026 · N423UP · Boeing 75724APF · Aerodynamic FairingsSDR IXXA20260612CC01Skin · corrodedRIGHT WING UPPER SKIN HAS CORROSION AT WBL 109.9 AND 70 INCHES FWD OF REAR SPAR.May 15, 2026 · N503AZ · Boeing 767338 · Wing, Plate/SkinSDR SWAA2026061103387Intercostal · crackedBRACKET INBOARD OF THE INBD RT WING DEFLECTION CONTROL RIB INBD INTERCOSTAL IS CRACKED. REMOVED AND REPLACED THE BRACKET ANGLE IAW SRM 5-40-02.May 15, 2026 · N8540V · Boeing 7378H4 · Wing Miscellaneous StructureSDR 1Q2R202606100004Panel · dentedLEFT INBOARD LEADING EDGE FLAP SKIN DENTED BETWEEN ST 29.00 AND 60.50. PERFORMED PERMANENT REPAIR IAW REO 670-57-52-658, REV--.May 15, 2026 · N522AE · Cndair CL6002C10 · Trailing Edge FlapsSDR SWAA2026061003430Support Beam · corrodedCORROSION SUPPORT BEAM LOCATED TRAILING EDGE BTW ORSS 334 TO ORSS 442 WL 190 AT RT WING. REPLACED SUPPORT BEAM LOCATED TRAILING EDGE BTW ORSS 334 TO ORSS 442 WL 190 AT RT WING IAW SRM 51-10-02 ITEM 9 AND DWG 115A3700 SHEET, 51 REV-.May 15, 2026 · N7749B · Boeing 7377BD · Wing Miscellaneous StructureSDR CALA2026060816861Tee Angle · gougedMAIN CABIN FLOOR SUPPORT SUBSTRUCTURAL T ANGLE AT APPROX STA 951 IS GOUGED ON THE UPPER SURFACE AT APPROX LBL 20. REMOVED DAMAGE ORIG THICKNESS 0.075, REMOVED 0.012 REMAINING 0.063 AND REPAIRED IAW ECRA 5375-01024.May 15, 2026 · N14240 · Boeing 737824 · Fuselage Miscellaneous StructureSDR ASAA2026051566477Baffle · crackedLEFT BAFFLE AT BS 500J - 500K IS CRACKED. GROUNDED - YES. REMOVED AND REPLACED BAFFLE IAW SRM 51-40-02-0G-0.May 15, 2026 · N464AS · Boeing 737990ER · Fuselage Main, StructureSDR HNAA2026060200476Floor Support · crackedRH SILL CRACKED BTW FR64-68. R & R SILL IAW SRM 51-40-02May 15, 2026 · N908AE · Emb EMB145LR · Fuselage Miscellaneous StructureSDR J7SA2026060200481Fce · unserviceableCREW RECEIVED SPOILER FAIL CAS ON LANDING. REPLACED FCE #2. RIGGED FCE #2 AND PERFORMED OPERATIONAL CHECKS. NO FAULTS FOUND. WORK PERFORMED IAW EMB-505 AMM 27-03-01.May 15, 2026 · N366FX · Emb EMB505 · Drag Control SystemSDR 2026FA0000470Shutoff Valve · leakingFUEL SHUT OFF VALVE NOT STOPPING FUEL COMPLETELY. FUEL DRIPPING FROM FUEL STRAINER DURING INSPECTION.May 15, 2026 · N25158 · Cessna 172S · Aircraft Fuel Distribution SystemSDR IPXA2026052901241Actuator · corrodedFOUND RT WING NR 14 OTBD, INBD SIDE KRUEGER FLAP ROTARY ACTUATOR CORROSION. I.A.W AMM 27-81-06-404-011 REV. 50 STEP 3.A TO 3.E.(2).(C), INSTALLED THE NO. 14 OUTBD'S INBD SIDE ROTARY ACTUATOR.May 15, 2026 · N611UP · Boeing 7478F · Leading Edge Slat ActuatorSDR IPXA2026052901221Actuator · corrodedFOUND LT WING NR 11 OUTBD SIDE AND NO.13 OUTBD'S INBD SIDE KRUEGER FLAP ROTARY ACTUATOR CORROSION. I.A.W AMM 27-81-06-404-011 REV. 50 STEP 3.A TO 3.E.(2).(C), INSTALLED THE NO. 11 OUTBD SIDE AND NO. 13 OUTBD'S INBD SIDE ROTARY ACTUATOR.May 15, 2026 · N611UP · Boeing 7478F · Leading Edge Slat ActuatorSDR CALA2026052916636Frame · dentedAFT CARGO COMPARTMENT FRAME AT BS 1580, STRINGER 25L DENTED. ACCOMPLISHED REPAIR IAW EC/RA:5360-02157, REV A, AND VT MAE EA 7 57-5360-13-A4460, REV.May 15, 2026 · N13113 · Boeing 757224 · Fuselage Main, FrameSDR CALA2026052916634Frame · dentedAFT CARGO COMPARTMENT FRAME AT BS 1420, S26L DENTED. REPAIR ACCOMPLISHED IAW EC/RA: 5360-02149 AND VT MAE EA: 757-5 360-13-A4463 REV-.May 15, 2026 · N13113 · Boeing 757224 · Fuselage Main, FrameSDR SWAA2026052803528Blade · crackedCRACK ON BLADE ASSEMBLY AT ACCESS PANEL 343AT ON RH HORIZONTAL STABILIZER. REPLACED BLADE ASSEMBLY ON ACCESS PANEL 343AT ON RH HORIZONTAL STABILIZER IAW SRM 51-40-02.May 15, 2026 · N949WN · Boeing 7377H4 · Horizontal Stabilizer, Plate/SkinSDR SWAA2026052803529Blade · crackedCRACKED BLADE ASSEMBLY AT ACCESS PANEL 343AB ON RH HORIZONTAL STABILIZER. REPLACED BLADE ASSEMBLY ON ACCESS PANEL 343AB ON RH HORIZONTAL STABILIZER IAW SRM 51-40-02.May 15, 2026 · N949WN · Boeing 7377H4 · Horizontal Stabilizer Miscellaneous StructureSDR CALA2026052816579Frame · dentedAFT CARGO COMPARTMENT L/H SIDE, FRAME AT BS 1480 AND S26L HAS A DENT. ACCOMPLISHED WORK PER UAL EC/RA NO: 5360-02150 AND VTMAE E.A. 757-5360-13-A4451 REV-.May 15, 2026 · N13113 · Boeing 757224 · Fuselage Main, FrameSDR CALA2026052716550Support Angle · crackedMAIN DECK FLOOR STRUCTURE ANGLE SUPPORT IS CRACKED AT AFT CARGO COMPARTMENT AT BSTA 1320 AND RBL 45.50. NR# 144684 PART FABRICATED AND REPLACED. REMOVED AND REPLACED ANGLE SUPPORT AT MAIN DECK FLOOR STRUCTURE AT AFT CARGO COMPARTMENT AT BSTA 1320 AND RBL 45.50May 15, 2026 · N13113 · Boeing 757224 · Fuselage Miscellaneous Structure