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 AALA202607144969Shear Plate · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CABIN FLOOR SHEAR PLATE BETWEEN FR 69 AND FR 70 AT S23R. REPLACED SHEAR PLATE PER SRM 51-42-11.May 28, 2026 · N9012 · Airbus A319115 · Fuselage Miscellaneous StructureSDR HNAA2026070900589Shear Tie · crackedSHEAR TIE CRACKED AT FR 67 BTW STR 6-7L. R & R SHEAR TIE IAW SRM 51-40-02May 28, 2026 · N652RS · Emb EMB145LR · Fuselage Internal Mounting StructureSDR HNAA2026070300566Spar · crackedTHE LEFT WING SPAR 1 AT RIB 9 SHOWS A RELEVANT INDICATION OF A CRACK AT THE FWD LOWER FLANGE. PERFORMED PERMANENT REPAIR OF THE LT SPAR I AT RIB 9 IAW SRM 57-20-05, ITEM 3, ETD ETD2026-145-009722 AND EO1-57-26-0281.May 28, 2026 · N923AE · Emb EMB145LR · Wing SparSDR HNAA2026070300570Door Sill · corrodedCARGO DOOR CUTOUT LOWER SILL CORRODED ON FORWARD END. R & R CARGO DOOR CUTOUT LOWER SILL IAW SRM 51-40-02.May 28, 2026 · N923AE · Emb EMB145LR · Fuselage Main, StructureSDR SWIA2026052876420Intercostal · corrodedPASSENGER DOOR INTERCOSTAL DD4 FWD IS CORRODED. REMOVED OLD PASSENGER DOOR INTERCOSTAL DD4 FWD REF. SRM 51-42-06-001-001-A01. & INSTALLED NEW PASSENGER DOOR INTERCOSTAL DD4 FWD IAW SRM 51-42-06-001-001-A01 REV 38 AND DWG 601R31702 REV -N. LEAK CHECK FAILED .May 28, 2026 · N770SK · Cndair CL6002C10 · Passenger/Crew DoorsSDR HNAA2026063000559Support Angle · crackedLUGGAGE DOOR LIFTING MECHANISM SUPPORT ANGLE CRACKED AT FR 68 STR 4R. R & R ANGLE IAW SRM 51-40-02May 28, 2026 · N652RS · Emb EMB145LR · Fuselage Miscellaneous StructureSDR SWAA2026062907209Support Bracket · crackedCRACKED SUPPORT BRACKET, BS 540 AIR CONDITIONING BAY LT SIDE. INSPECTED AND REPLACED SUPPORT BRACKET ON PNEUMATIC DUCT BS 540 AND LBL 6 AT AIR CONDITIONING BAY IAW DWG 212A1101, SHEET 3, REV - AND SOPM 20-50-00.May 28, 2026 · N260WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR HNAA2026062900557Doubler · damagedBULKHEAD PIN DOUBLER HOLE ELONGATED AT BTW FR14-15 BTW STR4-5L. REPAIRED IAW SRM 53-21-02May 28, 2026 · N652RS · Emb EMB145LR · Fuselage Main, BulkheadSDR AALA202606283815Door Sill · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT RIGHT PASSENGER / CREW DOOR CUT OUT LOWER SILL AT FR 66 AND S23R. REPLACED LOWER SILL PER SRM 51-42-11.May 28, 2026 · N9012 · Airbus A319115 · Fuselage Main, StructureSDR HNAA2026062500554Shear Tie · crackedSHEAR TIE CRACKED AT FR 67 BTW 5 - 6R. R & R SHEAR TIE IAW SRM 51-40-02.May 28, 2026 · N652RS · Emb EMB145LR · Fuselage Internal Mounting StructureSDR AALA202606249458Fitting · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT RIGHT PASSENGER, CREW DOOR CUT OUT LOWER SILL CENTER SHAPE FITTING BETWEEN FR 66 AND FR 68 AT S23R. REPLACED CENTER SHAPE FITTING PER SRM 51-42-11.May 28, 2026 · N9012 · Airbus A319115 · Fuselage Miscellaneous StructureSDR HNAA2026062400552Shear Tie · crackedSHEAR TIE CRACKED AT FR56 BTW S5-6R. R & R SHEAR TIE IAW SRM 51-40-02.May 28, 2026 · N652RS · Emb EMB145LR · Fuselage Internal Mounting StructureSDR SWAA2026062307138Vapor Barrier · crackedCRACKED VAPOR BARRIER WEB RT SIDE AT BS 663.75 MAIN WHEEL WELL. REPAIRED VAPOR BARRIER WEB RT SIDE AT BS 663.75 MAIN WHEEL WELL COMPARTMENT IAW SRM 57-10-10-2R-2, REPAIR 2.May 28, 2026 · N476WN · Boeing 7377H4 · Fuselage Main, BulkheadSDR AALA202606235480Fitting · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT RIGHT PASSENGER / CREW DOOR CUT OUT LOWER SILL FORWARD CORNER SHAPE FITTING AT FR 66 AND S23R. REPLACED CORNER SHAPE FITTING PER SRM 51-72-11.May 28, 2026 · N9012 · Airbus A319115 · Fuselage Miscellaneous StructureSDR SWAA2026062207450Scuff Plate · crackedFWD CARGO DOOR CENTER SCUFF PLATE CRACKED. REPAIRED FWD CARGO DOOR CENTER SCUFF PLATE IS CRACKED IAW SRM 53-30-15-2R-1.May 28, 2026 · N478WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2026062207451Scuff Plate · crackedFWD CARGO DOOR AFT SCUFF PLATE CRACKED. REPAIRED FWD CARGO DOOR AFT SCUFF PLATE IAW SRM 53-30-15-2R-1.May 28, 2026 · N478WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2026062207452Scuff Plate · crackedAFT CARGO DOOR FWD SCUFF PLATE CRACKED. REPAIRED AFT CARGO DOOR FWD SCUFF PLATE IAW SRM 53-30-15-2R-1.May 28, 2026 · N478WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2026062207295Vapor Barrier · crackedCRACK ON VAPOR BARRIER RT SIDE BS 663.75 AT MAIN WHELL WELL. EVALUATED CRACK LOC. ON VAPOR BARRIER RT SIDE BS663.75 AT MAIN WHEEL WELL AND FOUND OUT LIMIT DUE TO THE DAMAGE EXCEED ALLOWABLE DAMAGE LIMITS IAW AMM 57-10-10-1A-2 ALLOWABLE DAMAGE 2, VAPOR BARRIEMay 28, 2026 · N951WN · Boeing 7377H4 · Fuselage Main, BulkheadSDR SWAA2026062207301Web · crackedCRACKED WEB INBD FAN COWL INTERNAL AREA ON ENGINE 1. REPLACED WEB INBOARD FAN COWL INTERNAL AREA ON ENGINE 1 IAW 71-13-30, PAGE 10092 AND SRM 51-10-02, ITEM 9.May 28, 2026 · N951WN · Boeing 7377H4 · Nacelle/Pylon Miscellaneous StructureSDR IPXA2026061688559Skin · erodedERODED SKIN, LT WING L/E LOWER PANEL 521EB FWD EDGE. IAW SRM 51-70-07-0G-0 REV. 106 REMOVED THE EROSION MATERIALS AND CLEAN. BOND THE REPAIR PLIES WITH FILM ADHESIVE CURED AT 260 F FOR 130 MINUTES WITH A MINIMUM VACUUM OF 22 IN/HG. IAW AMM 20-51-01-912-008, May 28, 2026 · N577UP · Boeing 74744AF · Wing, Plate/SkinSDR IPXA2026061688661Skin · erodedERODED SKIN, RT WING L/E NR.3 PYLON PNL NO.471DL. IAW AMM 20-51-01-912-008, REV 116. REMOVED THE PANEL 471DL. REMOVED THE EROSION MATERIALS AND CLEAN. BOND THE REPAIR PLIES AND THE FOIL WITH RESIN CURED AT 200 F FOR 220 MINUTES WITH MINIMUM VACUUM OF 22 IN/HGMay 28, 2026 · N577UP · Boeing 74744AF · Wing, Plate/SkinSDR AALA202606191141Fitting · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT FORWARD PASSENGER / CREW DOOR CUTOUT LOWER SILL CENTER SHAPE FITTING BETWEEN FR 16 AND FR 20 AT S23L. REPLACED CENTER SHAPE FITTING PER SRM 51-72-11.May 28, 2026 · N9012 · Airbus A319115 · Emergency ExitsSDR SWAA2026061807351Fitting · crackedREMOVE AND REPLACE SLAT 1 LT WING DUE TO SECONDARY FINDING: CRACK ON FITTING SLAT 1. REPLACED LEADING EDGE SLAT 1 IAW AMM 27-81-21-401. TESTED OK .May 28, 2026 · N482WN · Boeing 7377H4 · Leading Edge DevicesSDR IPXA2026061201031Strap · corrodedAPU INLET DOOR AFT STRAP HAS CORROSION STA1825.00,S-3R TO S6R. INSTALLED PARTS OF REPAIR (STRAP 1, STRAP 2, FILLER 3, FILLER 4 AND OUTER STRAP) I.A.W. B757-200 PF SRM 51-40-02-0G-0 DETAIL I.May 28, 2026 · N413UP · Boeing 75724APF · APU Cowling/ContainmentSDR IPXA2026061202381Angle · corrodedAPU INLET DOOR UPPER ANGLE FROM STA 1787.45 TO STA 1825.00 S-3R HAS CORROSION. INSTALLED NEW UPPER ANGLE I.A.W. B757-200PF SRM 51-40-02-0G-0May 28, 2026 · N413UP · Boeing 75724APF · Fuselage Miscellaneous StructureSDR IXXA20260615CC01Skin · delaminatedDURING OK TO INSTALL LT INBD ELEVATOR FOUND INBD CORNER EDGE TO BE DAMAGED.May 28, 2026 · N503AZ · Boeing 767338 · Elevator, Plate/SkinSDR IPXA2026061388574Skin · crackedCRACKED SKIN, RT WING T/E PANEL 673CB. IAW AMM 06-09-08-912-001, REV 116, REMOVED PANEL 673CB. IAW AMM 20-51-01-912-008, REV 116 TO INSTALL PANEL 673CB.May 28, 2026 · N577UP · Boeing 74744AF · Wing, Plate/SkinSDR IPXA2026061388605Skin · erodedERODED RT WING LEADING EDGE LOWER FIXED PANEL 611BB. IAW SRM 57-41-01-2R-2, REFER TO SRM 51-70-07-0G-0 REV. 106. REMOVED THE DAMAGE MATERIALS AND CLEAN. BOND THE REPAIR PLIES WITH FILM ADHESIVE CURED AT 260 F FOR 130 MINUTES WITH A MINIMUM VACUUM OF 22 IN/HG. May 28, 2026 · N577UP · Boeing 74744AF · Wing, Plate/SkinSDR IPXA2026061388652Skin · erodedERODED SKIN, LT WING L/E LOWER PANEL 531AB FWD EDGE. IAW SRM 57-41-01-2R-2 REFER TO SRM 51-70-07-0G-0 REV. 106. REMOVED THE ERODED MATERIALS AND CLEAN. BOND THE REPAIR PLIES WITH FILM ADHESIVE CURED AT 260 F FOR 130 MINUTES WITH A MINIMUM VACUUM OF 22 IN/HGMay 28, 2026 · N577UP · Boeing 74744AF · Wing, Plate/SkinSDR IPXA2026061303166Tee Angle · corrodedBS 1060 LWR SURFACE, JUST BEHIND OF BEACON LIGHT, FRAME WITH EVIDENCE OF CORROSION. INSTALLED NEW TEE ANGLE AT BS 1060 LWR SURFACE, JUST BEHIND OF BEACON LIGHT IAW SRM 51-40-02-0G-0.May 28, 2026 · N413UP · Boeing 75724APF · Fuselage Main, Attach FittingsSDR IPXA2026060903107Intercostal · corrodedBS 1040 LWR SURFACE, AROUND OF RH A/C PACK HOT AIR EXHAUST, FRAME WITH EVIDENCE OF CORROSION. INSTALLED NEW INTERCOSTAL IAW B757-200PF SRM 51-40-02-0G-0May 28, 2026 · N413UP · Boeing 75724APF · Fuselage Miscellaneous StructureSDR HNAA2026061000493Shear Tie · cracked53-2068 SHEAR TIE CRACKED AT FR68 BTW STR6-9L. R & R SHEAR TIE IAW SRM 51-40-02May 28, 2026 · N652RS · Emb EMB145LR · Fuselage Internal Mounting StructureSDR IPXA2026060288459Seal · peelingPEEL OFF - MOLDING SEAL, L/H WING L/E NO.4 V.C FLAP EXTERNAL OUTBD SIDE AND UPPER CORNER AREA.  I.A.W. 747-400F SRM 57-43-02-2R-5 REV. 106 REFER TO SOPM 20-50-12 REV. 159.May 28, 2026 · N577UP · Boeing 74744AF · Leading Edge DevicesSDR IPXA2026060288498Seal · peelingFAULT - PEEL OFF - MOLDING SEAL, L/H WING L/E NO.3 V.C FLAP EXTERNAL OUTBD SIDE AND UPPER CORNER AREA. (REPAIR) REVIEWED TASK PER GMM-MTX 09.05.01.09. I.A.W. 747-400F SRM 57-43-02-2R-5 REV. 106 REFER TO SOPM 20-50-12 REV. 159 PERFORM REPAIRÂMay 28, 2026 · N577UP · Boeing 74744AF · Leading Edge DevicesSDR IPXA2026060288508Seal · peelingPEEL OFF - MOLDING SEAL, L/H WING L/E NO.2 V.C FLAP EXTERNAL INBD SIDE AND UPPER CORNER AREA. I.A.W. SRM 57-43-02-2R-5 REV. 106 REFER TO SOPM 20-50-12 REV. 159.May 28, 2026 · N577UP · Boeing 74744AF · Leading Edge DevicesSDR FDEA202605280682Fan · failedPRIOR TO PUSH, HEARD A LOUD POP ON THE FLIGHT DECK. STATUS MESSAGE: EQUIP VENT FAN. REPLACED EQUIPMENT COOLING VENT FAN PER MM 21-27-20-4, FOUND REMOVED FAN WITH ALL BLADES DESTROYED. PERFORMED OPS TEST PER SAME MM. TEST FAILED WITH MAINTENANCE MESSAGE 2May 28, 2026 · N844FD · Boeing 777FHT · Air Distribution FanSDR AALA202606095393Cover · crackedAIRCRAFT IN BASE MAINTENANCE: PASSENGER CABIN, L2 DOOR CUT-OUT, DOOR WARNING SENSOR COVER IS CRACKED. REPLACED COVER PER AMM 52-71-11.May 28, 2026 · N324RA · Boeing 7378 · Door Warning SystemSDR MASA20260608157Beam · corrodedDURING HEAVY CHECK INSPECTIONS OF R1 DOOR CUT-OUT LOWER BEAM ON SLIDE FITTING FWD HOUSING EDGE CORROSION REMOVED BY BLENDING !AW SRM 51-10-03, BLENDED AREA FOUND WITH IN LIMITS IAW SRM 53-10-11 AD 02, DUI WITH 10X MAG GLASS C/OUT, "NO FAULT FOUND" BLENDED AREAMay 28, 2026 · N88335 · Emb ERJ170200LR · Fuselage Main, StructureSDR MASA20260608156Beam · corrodedDURING HEAVY CHECK INSPECTIONS OF L1 DOOR CUT-OUT LOWER BEAM ON SLIDE FITTING FWD HOUSING EDGE CORROSION REMOVED BY BLENDING IAW SRM 51-10-03, BLENDED AREA FOUND WITH IN LIMITS IAW SRM 53-10-11 AD 02, DUI WITH 10X MAG GLASS C/OUT, NO FAULT FOUND, BLENDED AREMay 28, 2026 · N88335 · Emb ERJ170200LR · Fuselage Main, StructureSDR MASA20260608151Crossbeam · corrodedDURING HEAVY CHECK INSPECTIONS OF CFI WET AREA, FWD FUS CROSS BEAM, FR 14, RBL 18, SPOT OF CORROSION ON UPPER FLANGE EDGE REMOVED BY BLENDING IAW SRM 51 10 03, FOUND TO BE WITH IN LIMITS IAW SRM IAW 53 SRM 10 10, 51 23 AD02. 04, DVI WITH 10X 23 05, MAG C/OUMay 28, 2026 · N88335 · Emb ERJ170200LR · Fuselage Main, StructureSDR MASA20260608144Hinge · corrodedWASTE SERVICE DOOR CORRODED HINGE REPLACED IAW SRM 51 41 02. REV 45. CORROSION LEVEL 2.May 28, 2026 · N88335 · Emb ERJ170200LR · Fuselage, Door HingeSDR MASA20260608143Shear Tie · corrodedDURING HEAVY CHECK INSPECTIONS OF LOWER SKIN, CORRODED SHEAR TIE AT FR 86, BETWEEN STR 28R AND 27R. REMOVED AND REPLACED IAW SRM 51-41-01 AND SRM 51-41-02. REV 45. CORROSION LEVEL2May 28, 2026 · N88335 · Emb ERJ170200LR · Fuselage Internal Mounting StructureSDR IPXA2026060288536Seal · peelingFAULT - PEEL OFF - MOLDING SEAL, L/H WING L/E NO.2 V.C FLAP EXTERNAL OUTBD SIDE AND UPPER CORNER AREA. I.A.W. SRM 57-43-02-2R-5 REV. 106 REFER TO SOPM 20-50-12 REV. 159 PERFORM REPAIR AS BELOW STEP :May 28, 2026 · N577UP · Boeing 74744AF · Leading Edge DevicesSDR IPXA2026060103232Tee Angle · corrodedSTA 900 APPROX, LWR SURFACE, JUST IN FRONT OF LH A/C PACK PANEL, FRAME WITH EVIDENCE OF CORROSION. VERIFIED RESTORATION OF SURFACE PROTECTION IAW B757-200PF SRM51-20-01 AND AMM51-21-15.May 28, 2026 · N413UP · Boeing 75724APF · Fuselage Main, Attach FittingsSDR AALA202606053393Bearing · defectiveAIRCRAFT IN BASE MAINTENANCE: FORWARD RIGHT PASSENGER / CREW DOOR HIGH LOCKING MECHANISM WILL NOT SPRING BACK. MAINTENANCE REPLACED BEARING ASSEMBLY PER CMM 52-11-15 AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK.May 28, 2026 · N102UW · Airbus A320214 · Passenger/Crew DoorsSDR IPXA2026060488562Skin · crackedCRACKED SKIN, RT WING T/E UPPER FIXED PNL WBL 232. IAW SRM 51-40-02-0G REV.106 AND BOEING DWG 113U1011, SHEET 22, REV A. INSTALL FASTENERS AT RT WING T/E UPPER FIXED PANEL WBL 232.May 28, 2026 · N577UP · Boeing 74744AF · Wing, Plate/SkinSDR HNAA2026060400487Shear Tie · crackedSHEAR CLIP CRACKED AT FR67 BTW STR6-7L. RAR SHEAR CLIP IAW SRM 51-40-02May 28, 2026 · N908AE · Emb EMB145LR · Fuselage Internal Mounting StructureSDR REXA2026060400900Heater · inoperativeFWD FLIGHT ATTENDANT CALLED REPORTING A STRONG SMELL (A STRONG FUME ODOR) DURING CLIMB OUT. NO EICAS INDICATIONS NO SMOKE OBSERVED IN THE FLIGHT DECK. THE SMELL SEEMED TO BE STRONGEST IN THE GALLEY AREA. R & R GALLEY EXHAUST FAN IAW AMM 21-23-93. OPC NOMay 28, 2026 · N912XJ · Cndair CL6002D24 · Heating SystemSDR IPXA2026060288681Skin · debondedDISBOND SKIN, R/H WING T/E OTBD MID FLAP WEDGE UPPER SKIN. PERFORMED NDT/UT FOR REWORKED AREA AND PLUS 6" AROUND HEATED AREA, IAW NDT MANUAL PART 1 51-01-01 REV.182. NO DEFECT FOUND.May 28, 2026 · N577UP · Boeing 74744AF · Trailing Edge FlapsSDR IPXA2026060288239Erosion Shield · damagedEROSION - MOLDING SEAL, R/H WING NO.17 V.C FLAP. (REPAIR) 1. I.A.W. 747-400F SRM 57-43-02-2R-5 REV. 106 REFER TO SOPM 20-50-12 REV. 159 PERFORM REPAIR AS REMOVE THE RAIN EROSION SHIELDS AND CLEAN. 1.2 APPLY THE SEALANT TO REPAIR AREA CURED AT 70°F FOR 48 HOUMay 28, 2026 · N577UP · Boeing 74744AF · Trailing Edge Flaps