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.

SDR SWIA2026071677785Seat Track · damagedLBL9 SEAT RAIL SCRATCHED AND CORRODED BETWEEN APPROXIMATELY FS559005TO FS5590092 C-CHECK RO 10172026REMOVED ANDINSTALLED NEW LBL9 SEAT RAIL, BETWEEN APPROXIMATELY FS559005 TO FS5590092, REFCRJ 200 AMM 53-01-11-400-802 FOUND THE SEAT TRACK CORROSION IS EXFOLJul 16, 2026 · N917SW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR SWIA2026071677784Seat Track · damagedLBL9 SEAT RAIL SCRATCHED AND CORRODED BETWEEN APPROXIMATELY FS5590094 TO FS56400 C-CHECK RO 10172026 REPLACE AND INSTALLED NEW LBL9 SEAT RAIL, BETWEEN APPROXIMATELY FS5590094 TO FS56400, REFCRJ 200 AMM 53-01-11-400-802 FOUND THE SEAT TRACK WITH DEEP PITTING AJul 16, 2026 · N917SW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR SWIA2026071677783Seat Track · damagedLBL9 SEAT RAIL SCRATCHED AND CORRODED BETWEEN APPROXIMATELY FS56400 TO FS61900 C-CHECK RO 10172026REMOVED AND INSTALLED NEW LBL9 SEAT RAIL, BETWEEN APPROXIMATELY FS56400 TO FS61900, REFCRJ 200 AMM 53-01-11-400-802 FOUND SEAT TRACK HAS DEEP PITTING AND EXFOLJul 16, 2026 · N917SW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR SWIA2026071677782Seat Track · damagedRBL 27 SEAT TRACK SCRATCHED AND CORRODED, BS 559. 48 - 559. 58. REPLACED THE SEAT TRACK IAW AMM 53-01-11-400-802.Jul 16, 2026 · N917SW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR SWIA2026071677781Seat Track · damagedRBL 27 SEAT TRACK SCRATCHED AND CORRODED BS 559. 94 TO BS 564. REPLACED THE SEAT TRACK, IAW AMM 53-01-11-400-802.Jul 16, 2026 · N917SW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR SWIA2026071677780Seat Track · corrodedRBL 27 SEAT TRACK SCRATCHED AND CORRODED, BS 564 TO 619. REPLACED THE SEAT TRACK, IAW AMM 53-01-11-400-802.Jul 16, 2026 · N917SW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR SWIA2026071677779Seat Track · scratchedLBL 27 SEAT TRACK SCRATCHED AND CORRODED BTWN APPROX BS 559 TO BS 559.94. REPLACED SEAT TRACK, IAW AMM 53-01-11-400-802.Jul 16, 2026 · N917SW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR SWIA2026071677778Skin · chafedRIGHT APRON SKIN CHAFED FROM UPPER WING SKIN AND STUB FAIRING CONTACT. REPAIRED RT APRON SKIN IAW SRM 51-42-06, REV 39, AND REO 601R-53-41-115, REV A.Jul 16, 2026 · N917SW · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR SWIA2026071677767Skin · chafedLEFT APRON SKIN CHAFED FROM UPPER WING SKIN & STUB FAIRING CONTACT. REPAIRED LEFT APRON SKIN UPPER WING SKIN IAW REO 601R-53-41-115, REV A. COMPLIED WITH ALL STEPS OF REO 601R-53-41-115, REV A. COMPLIED WITH 51-900-1003-SKY.Jul 16, 2026 · N917SW · Cndair CL6002B19 · Wing, Plate/SkinSDR SWIA2026071677765Floor Support · corrodedLEFT FLOOR SUPPORT CORRODED BTWN APPROX BS 559 TO 559.085. REMOVED CORROSION AT LEFT FLOOR SUPPORT IAW SRM 51-21-06. FOUND TO BE OUT LIMITS IAW REO 601R-53-00-526, REV-. REPAIRED LEFT FLOOR SUPPORT IAW REO 601R-53-51-758 REV--, COMPLIED WITH ALL STEPS OF REOJul 16, 2026 · N917SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR IPXA2026091685762Panel · corrodedMAIN DECK CARGO COMP. CENTER BOX TOP SKIN LH BTW Y1959 TO Y2462 FR46-47 WITH CORROSION. COMPLIED WITH UPS EO-98290-REQ1 AND VT-MAE EA 300-5710-27-A4575, REV. -.Jul 16, 2026 · N136UP · Airbus A300F4622R · Fuselage Main, StructureSDR IPXA2026091101707Skin · corrodedAPU COMPARTMENT TAILCONE LOWER BILGE ALUMINUM HONEYCOMB SKIN PANELS BETWEEN BS 1963 AND 1992 HAS AREAS OF CORROSION TO INCLUDE ATTACHMENT TO FRAMES WITH AREAS OF MISSING FINISH. RL051 RE-INSTALLED LWR BILGE ALUM HONEYCOMB SKIN PNL BTWN STA 1963 & 1992 AT APU CJul 16, 2026 · N455UP · Boeing 75724APF · Aerodynamic FairingsSDR IPXA2026091100666Angle · corrodedRIGHT HORIZONTAL STAB TO ELEVATOR BONDING STRAP ATTACH BRACKET HAS CORROSION AT HORZ STAB REAR SPAR OTBD SIDE OF MOST OTBD HINGE. RT HORIZ STAB TO ELEVATOR BONDING STRAP ATTACH BRACKET WAS REMOVED IAW SRM 51-40-02-0G-0 DUE TO MORE THAN 50% EXFOLIATION CORROSIJul 16, 2026 · N455UP · Boeing 75724APF · Horizontal Stabilizer Miscellaneous StructureSDR IPXA2026091199459Floor Panel · damagedMAJOR REPAIR, FWD CARGO COMP FLOOR PANEL 132MG HAS CORNER BROKEN. PANEL 132MG IS FABRICATED IAW SREO-16407-REQ001 ((APPX B) A300 MAIN DECK CARGO COMPARTMENT FLOOR PANEL FABRICATIONJul 16, 2026 · N143UP · Airbus A300F4622R · Fuselage Floor PanelSDR IPXA2026090292229Web · crackedE&E BS BETWEEN FR 7 TO 10 LT Y953 WEB CRACKED AT COCKPIT FLOOR LEVEL. INSTALLED NEW WEB AT E&E COMPARTMENT BETWEEN FR 7 TO 10 LH Y953 IAW SRM 51-40-21.Jul 16, 2026 · N136UP · Airbus A300F4622R · Fuselage Miscellaneous StructureSDR IPXA2026082697869Support Angle · brokenPANEL 475AL, RH FWD INTEROR AREA IS CRACKED. INSTALLED NEW SUPPORT ANGLE AT PANEL 475AL RT FWD IAW SRM 51-40-21.Jul 16, 2026 · N136UP · Airbus A300F4622R · Nacelle/Pylon Miscellaneous StructureSDR AALA202609057826Window Frame · crackedAIRCRAFT IN BASE MAINTENANCE: CRACKED FLIGHT DECK WINDSHIELD FRAMING LEFT-HAND CENTER POST OF WINDSHIELD UPPER BOLT VERTICAL WALL AREA AT FR 2 AND Y0 - REPAIRED WINDSHIELD FRAME PER EA 377417Jul 16, 2026 · N195UW · Airbus A321211 · Fuselage Main, StructureSDR AALA202609053371Fitting · crackedAIRCRAFT IN BASE MAINTENANCE: CRACKED FLIGHT DECK WINDSHIELD FRAMING LEFT-HAND CONTINUITY FITTING BETWEEN FR 1 AND FR 2 AY Y0 - REPLACED CONTINUITY FITTING PER EA 377417Jul 16, 2026 · N195UW · Airbus A321211 · Fuselage Main, StructureSDR AALA202609056961Fitting · crackedAIRCRAFT IN BASE MAINTENANCE: CRACKED FLIGHT DECK WINDSHIELD FRAMING RIGHT-HAND CONTINUITY FITTING BETWEEN FR 1 AND FR 2 AY Y0 - REPLACED CONTINUITY FITTING PER EA 377417Jul 16, 2026 · N195UW · Airbus A321211 · Fuselage Main, StructureSDR AALA202609039005Window Frame · crackedAIRCRAFT IN BASE MAINTENANCE: CRACKED FLIGHT DECK WINDSHIELD FRAMING CENTER WINDSHIELD POST UPPER BOLT MOUNTING VERTICAL WALL RIGHT SIDE AT FR 2 AND Y0 - REPAIRED WINDSHIELD FRAMING PER EA 377417Jul 16, 2026 · N195UW · Airbus A321211 · Fuselage Main, StructureSDR HNAA2026082700806Shear Tie · crackedSHEAR TIE CRACKED AT FR 67 BTWN STRINGERS 6 - 7L. R & R SHEAR TIE IAW SRM 51-40-02.Jul 16, 2026 · N925AE · Emb EMB145LR · Fuselage Internal Mounting StructureSDR HNAA2026082700805Shear Tie · crackedSHEAR TIE CRACKED AT FR 66 BTWN STR 6 - 7L. R & R THE SHEAR TIE IAW SRM 51-40-02.Jul 16, 2026 · N925AE · Emb EMB145LR · Fuselage Internal Mounting StructureSDR HNAA2026082700801Intercostal · crackedAFT CARGO DOOR MECHANISM X3, INTERCOSTAL CRACKED, TOP, VERTICAL, AND BELOW. R & R INTERCOASTAL IAW SRM 51-40-02Jul 16, 2026 · N925AE · Emb EMB145LR · Cargo/Baggage DoorsSDR IPXA2026082692177Frame Angle · crackedE&E COMPARTMENT AT FR 10 LH Y953 HAS A CRACKED BRACKET AT COCKPIT FLOOR LEVEL . INSTALLED NEW BRACKET " ON E&E COMP. AT FR.10 LH Y953 IAW SRM 51-40-21.Jul 16, 2026 · N136UP · Airbus A300F4622R · Fuselage Main, FrameSDR REXA2026082601718Hinge · crackedSECONDARY NRC FROM NRC. 00318: AFTER REMOVAL PAINT CRACK ON FWD HINGE OF THE FLAP STEP PLATE AT AFT BAGGAGE BAY DOOR CUTOUT WAS FOUND. FWD HINGE OF THE FLAP STEP PLATE AT AFT BAGGAGE BAY DOOR CUTOUT (MM670-35624-003) WAS REPLACED PER CRJ-900 SRM 51-42-06-001-Jul 16, 2026 · N926XJ · Cndair CL6002D24 · Fuselage, Door HingeSDR AALA202608259747Support Frame · corrodedAIRCRAFT IN BASE MAINTENANCE: FORWARD SIDE OF NOSE LANDING GEAR, FORWARD BULKHEAD LOWER FRAME SUPPORTS AND SUPPORT ANGLES HAS INTERGRANULAR CORROSION AT STATION 224.8, LBL 4 TO RBL 5. MAINTENANCE CUT OUT CORRODED FRAME AND SPLICED IN A NEW, SERVICABLE FRAME OFJul 16, 2026 · N903AN · Boeing 737823 · Fuselage Main, StructureSDR DALA2026082504825Skin · corrodedERA 627451-14 REV B: MID FUSELAGE SKIN - FRAME 34-35, S36L-S36R - CORROSION. SUBJECT REPAIR REQUIRES FOLLOW-ON ACTION. ACCOMPLISH SECTION II WITHIN 52,500 FLIGHT HOURS OR 30,000 FLIGHT CYCLES FROM TIME OF SECT. I REPAIR AT 15,269 FH AND 6,972 FC (WITHIN AIRCRAJul 16, 2026 · N117DU · Airbus BD5001A10 · Fuselage Main, Plate/SkinSDR HNAA2026082500787Shear Tie · crackedSHEAR TIE CRACKED AT FR73 BTW STR 8-10R. R & R SHEAR TIE IAW SRM 51-40-02Jul 16, 2026 · N925AE · Emb EMB145LR · Fuselage Internal Mounting StructureSDR HNAA2026082500785Shear Tie · crackedSHEAR TIE CRACKED AT FR 72 BTW STR 17-18L. R & R SHEAR TIE IAW SRM 51-40-02Jul 16, 2026 · N925AE · Emb EMB145LR · Fuselage Internal Mounting StructureSDR HNAA2026082500783Shear Tie · crackedSHEAR TIE CRACKED AT FR73 BTW STR 8-10L. RAR SHEAR TIE IAW SRM 51-40-02Jul 16, 2026 · N925AE · Emb EMB145LR · Fuselage Internal Mounting StructureSDR HNAA2026082500781Shear Tie · crackedSHEAR TIE CRACKED AT FR62 BTW STR8-9R. R & R SHEAR TIE IAW STR51-40-02Jul 16, 2026 · N925AE · Emb EMB145LR · Fuselage Internal Mounting StructureSDR HNAA2026082400764Floor Support · crackedRIGHT OMEGA BEAM INBD AND OTBD ANGLES CRACKED AT BTW FR 47-48. R & R ANGLES IAW SRM 51-40-02.Jul 16, 2026 · N925AE · Emb EMB145LR · Fuselage Miscellaneous StructureSDR HNAA2026082400756Skin · crackedFUSELAGE EXTERNAL SKIN HAS A POSSIBLE CRACK AT AFT SIDE OF OXYGEN SERVICING DOOR, IN THE RH RVSM AREA. REMOVED CRACKED AREA OF FUSELAGE SKIN AT AFT EDGE OF OXYGEN SERVICING DOOR CUTOUT IAW ETD2026-145-012451 REV: A. FABRICATED, INSTALLED REPAIR DOUBLER AND FIJul 16, 2026 · N935AE · Emb EMB145LR · Fuselage Main, Plate/SkinSDR HNAA2026082400755Floor Support · corrodedRT CABIN FLOOR SILL NR 6 IS CORRODED IN MULTIPLE AREAS. REMOVED AND INSTALLED NEW RH FLOOR SILL #6 IAW EMB 145 SRM 51-40-02.Jul 16, 2026 · N935AE · Emb EMB145LR · Fuselage Miscellaneous StructureSDR HNAA2026082400754Floor Support · crackedCARGO LT FLOOR SUPPORT BETWEEN FR 68 - 71 CORRODED AROUND NUT PLATE HOLES. R & R CARGO LT FLOOR SUPPORT BETWEEN FR 68 - 71 IAW SRM 51-40-02.Jul 16, 2026 · N935AE · Emb EMB145LR · Fuselage Miscellaneous StructureSDR HNAA2026082400753Floor Support · crackedCARGO LT FLOOR SUPPORT BETWEEN FR 61 - 65 CORRODED AROUND NUT PLATE HOLES. RAR CARGO LT FLOOR SUPPORT BETWEEN FR 61/65 IAW SRM 51-40-02.Jul 16, 2026 · N935AE · Emb EMB145LR · Fuselage Miscellaneous StructureSDR HNAA2026082400752Frame · crackedCARGO FR 73 HAS POSSIBLE CRACK BETWEEN STGR 16R /17R. R & R FR 73 BTW STGR 14R-17L IAW EMB 145 SRM 51-40-02.Jul 16, 2026 · N935AE · Emb EMB145LR · Fuselage Main, FrameSDR HNAA2026082000744Floor Support · crackedLT OMEGAQ BEAM INBD VERTICAL FLANGE CRACKED AT FR36. REPAIRED IAW ETD2026-145-012746 AND EO 1-53-26-0386Jul 16, 2026 · N925AE · Emb EMB145LR · Fuselage Miscellaneous StructureSDR IPXA2026081286146Retainer · wornAPU COMPARTMENT FWD BULKHEAD SAFETY CATCH ANGLE FOR RT APU DOOR 316AR WORN THIN. RL017. INSTALLED 1 NEW RETAINER AT STA 1885.20 BELOW WL 210 (APU COMP. FWD BULKHEAD), IAW B757-200PF SRM 51-40-02-0G-0 REV 125 20MAY2026 AND BOEING DWG 148N8402.Jul 16, 2026 · N455UP · Boeing 75724APF · APU Cowling/ContainmentSDR HNAA2026082000743Rib · crackedVERTICAL STAB TRAILING EDGE UPPER RIB CRACKED. REPAIRED IAW ETD2026-145-012759 AND EO1-55-26-0354Jul 16, 2026 · N939AE · Emb EMB145LR · Vertical Stabilizer, Spar/RibSDR SWAA2026081972545Seat Track · wornCAPT. AFT INBD SEAT TRACK UPPER SURFACE WORN. R & R THE SEAT TRACK IAW AMM 25-11-11.Jul 16, 2026 · N8706W · Boeing 7378 · Fuselage, Seat/Cargo Attach FittingsSDR SWAA2026081929718Seat Track · wornFIRST OFFICER AFT INBD SEAT TRACK UPPER SURFACE WORN. R & R THE SEAT TRACK IAW AMM 25-11-11.Jul 16, 2026 · N8706W · Boeing 7378 · Fuselage, Seat/Cargo Attach FittingsSDR IPXA2026081486342Channel · chafedAPU ACCESS DOOR 316AR FIRE LOOP SUPPORT RAIL HAS CHAFING DAMAGE AT AFT END AND DONT FORGET TO PROVIDE CLEARANCE AFTER REPAIR. RL022. LOCATED AND DRILLED NEW CHANNEL AT APU ACCESS DOOR 316AR, IAW SRM 51-40-05-0G-0. OK TO INSTALL NEW CHANNEL. INSTALLED NEW APU Jul 16, 2026 · N455UP · Boeing 75724APF · Auxiliary Power Unit (APU) DoorsSDR IPXA2026081501707Skin · corrodedAPU COMPARTMENT TAIL CONE LOWER BILGE ALUMINUM HONEYCOMB SKIN PANELS BETWEEN BS 1963 & 1992 HAD AREAS OF CORROSION TO INCLUDE ATTACHMENT TO FRAMES WITH AREAS OF MISSING FINISH. VERIFIED THE ABOVE STEP 17. INSTALLATION OF LWR-BILGE-ALUMN-HONEYCOMB-SKIN-PANEJul 16, 2026 · N455UP · Boeing 75724APF · APU Cowling/ContainmentSDR SWAA2026081704519Rib · crackedCRACKED LEADING EDGE RIB, LE HSS 105.26, RT HORIZONTAL STAB. REPLACED RIB & FASTENERS LOCATED LEADING EDGE HSS 105.26 AT RT HORIZONTAL STAB IAW SRM 51-40-02-0G-0, & DWG 186A1001, SHEET 10, REV:A.Jul 16, 2026 · N499WN · Boeing 7377H4 · Horizontal Stabilizer, Spar/RibSDR IPXA2026080800710Attach Bracket · corrodedLEFT HORIZONTAL STAB TO ELEVATOR BONDING STRAP ATTACH BRACKET HAS CORROSION AT HORIZONTAL STAB REAR SPAR OTBD SIDE OF MOST OTBD HINGE. RL048 INSTALLED BRACKET AT LT HORIZONTAL STAB REAR SPAR OTBD SIDE OF MOST OTBD HNGE IAW SRM 51-40-02-0G-0.Jul 16, 2026 · N455UP · Boeing 75724APF · Horizontal Stabilizer Miscellaneous StructureSDR IPXA2026081586787Splice Strap · corrodedAFT FUSELAGE SKIN PANEL SUPPORT FRAME BS 1992 FWD SIDE SPLICE PLATE AT 6:00 POSITION HAS CORROSION WITH POSSABLE CORROSION ON AFT SIDE. INSTALLED NEW FABRICATED DOUBLER AT AFT FUSELAGE SKIN PANEL SUPPORT FRAME STA 1992 FWD SIDE, IAW SRM 51-40-02-0G-0.Jul 16, 2026 · N455UP · Boeing 75724APF · Fuselage Miscellaneous StructureSDR SCNA20260814362Skin · damagedINITIAL INSPECTION: ELONGATED FASTENER HOLE ON EXTERNAL FUSELAGE SKIN BTW STA 500G/500H AND STGR S-25L/ S-24L - - ELONGATED FASTENER HOLE ON EXTERNAL FUSELAGE SKIN BTW STA 500G/-500H AND STGR S-25L/ S-24L WAS REPAIRED PER ETI-737-26-071 REV. 2, MM4-SCA-26-0024Jul 16, 2026 · N820SY · Boeing 7378FH · Fuselage Main, Plate/SkinSDR HNAA2026081400683Floor Support · corrodedCARGO FLOOR RAMP FLOOR SUPPORT AT FR-65 LOWER END AROUND NUT-PLATE HOLE HAS CORROSION. R & R THE CARGO RAMP FLOOR SUPPORT AT FR65 IAW EMB 145 SRM 51-40-02Jul 16, 2026 · N942LL · Emb EMB145LR · Fuselage Miscellaneous StructureSDR SWAA2026081212781Access Panel · crackedCRACKED ACCESS PANEL 542CR, LT WING. REPLACED AND INSTALLED THE ACCESS PANEL 542CR, DOCUMENT ON TTG8Q01CPSAM.Jul 16, 2026 · N7732A · Boeing 7377BD · Wing, Plate/Skin