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 SWAA2026051992504Shield · corrodedCORROSION ON FWD CARGO COMPARTMENT DOOR CUT-OUT AFT SHIELD AT STA 500+10; RBL 24; WL 156. REMOVED AND REPLACED FWD CARGO COMPARTMENT DOOR CUT-OUT AFT SHIELD IAW SRM 51-40-02-0G-0 AND DWG 143A0080 0027, REV -.Apr 24, 2026 · N258WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2026051992754Threshold Web · corrodedACB SUB THRESHOLD WEB HAS AREAS OF CORROSION. REMOVED AND REPLACED ON ACB SUB THRESHOLD WEB FROM BS 794 TO 847, RBL 22 IAW SRM 51-40-02 AND DWG 146A8340, 0028, REV -.Apr 24, 2026 · N258WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2026051992756Shield · corrodedR/H FLOOR TO SIDEWALL SUPPORT BS 767-787 HAS AREAS OF CORROSION. REMOVED AND REPLACED SHIELD BS 767 TO 787, RBL 22, WL 158 IAW SRM 51-40-02-0G-0, AND DWG 146A0081, REV-.Apr 24, 2026 · N258WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR R61A2026051800138Skin · damagedDURING HEAVY CHECK LEFT HAND H-STAB TRAILER EDGE INBOARD RIB 11 FOUND TO HAVE TOOLING DAMAGE. REPAIRED RIB 11 IAW ETD 2026-170-007862.Apr 24, 2026 · N733YX · Emb ERJ170100LR · Horizontal Stabilizer, Plate/SkinSDR R61A2026051800137Skin · dentedDURING HEAVY CHECK FOUND DENT ON THE RIGHT SIDE OF THE NOSE UNDER THE RIGHT DV WINDOW AFT. REPAIRED DENT IAW EMB ETD 2026-170-007353Apr 24, 2026 · N733YX · Emb ERJ170100LR · Fuselage Main, Plate/SkinSDR R61A2026051800136Seat Track · corrodedDURING HEAVY CHECK FWD FUSELAGE FLOOR SUPPORT STRUCTURE LT INBD SEAT TRACK AT FR 12-20 FOUND CORRODED BEYOND LIMITS. REMOVED AND REPLACED SEAT TRACK IAW EMB 170/175 SRM 51-41-01 51-41-02 AND 51-43-01Apr 24, 2026 · N733YX · Emb ERJ170100LR · Fuselage, Seat/Cargo Attach FittingsSDR R61A2026051800135Seat Track · corrodedDURING HEAVY CHECK FWD FUSELAGE FLOOR STRUCTURE R/H I/B SEAT AT FR 12-20 CORRODED BEYOND LIMITS. REMOVED AND REPLACED SEAT TRACK IAW EMB 170/175 SRM 51-41-01 51-41-02 AND 51-43-01Apr 24, 2026 · N733YX · Emb ERJ170100LR · Fuselage, Seat/Cargo Attach FittingsSDR R61A2026051800127Floor Support · corrodedDURING HEAVY CHECK FWD FUSELAGE FLOOR SUPPORT STRUCTURE FLOORBEAM AT FR 19-20 LBL 42 FOUND CORRODED. REMOVED AND REPLACED FLOOR SUPPORT STRUCTURE FLOOR BEAM IAW EMB 170/175 SRM 51-43-03, 51-43-04 AND 51-41-02Apr 24, 2026 · N733YX · Emb ERJ170100LR · Fuselage Miscellaneous StructureSDR REXA2026051500593Angle · brokenRTN FINDING: BROKEN ANGLE CLIP, LOCATED ON FS364.00 AND LBL27.00 OF CPAX FLOOR STRUCTURE. CLIP LOCATED ON FS364.00 AND LBL27.00 OF CPAX FLOOR STRUCTURE WAS REPLACED PER CRJ-900 SRM 51-42-10-001-001-A01Apr 24, 2026 · N137EV · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR AALA202605157539Hinge Pin · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION OUTBOARD PIN SPOILER 5 ON LH WING. THE MEASURES OF CORROSION ARE: L = 0.750 INCH, W = 0.326 INCH, D = 0.006 INCH. MAINTENANCE REPLACED PIN-HINGE SPOILER IAW SRM A319 51-72-11-911-001.Apr 24, 2026 · N9010R · Airbus A319115 · SpoilersSDR AALA202605137385Hinge Pin · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION OUTBOARD PIN SPOILER 2 ON LH WING. MEASURES OF CORROSION ARE: L = 0.217 INCH, W = 0.101 INCH, D = 0.006 INCH. MAINTENANCE REPLACED PIN-HINGE SPOILER IAW SRM A319 51-72-11-911-001.Apr 24, 2026 · N9010R · Airbus A319115 · SpoilersSDR SWAA2026051292705Elec Connector · brokenFWD R/H OVERWING EXIT DOOR PANEL ABOVE HAS BROKEN CONNECTOR. REMOVED AND REPLACED R/H FWD OVERWING LIGHT ASSEMBLY M2837 PER AMM 33-21-00-960-805 STEPS 10A THROUGH 10C(6).Apr 24, 2026 · N8639B · Boeing 7378H4 · Light System WiringSDR AALA202605124149Hinge Pin · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION INBOARD PIN SPOILER 1 ON LT WING. THE MEASURES OF CORROSION ARE: L = 0.752 INCH, W = 0.215 INCH, D = 0.098 INCH. MAINTENANCE REPLACED PIN-HINGE SPOILER IAW SRM A319 51-72-11-911-001.Apr 24, 2026 · N9010R · Airbus A319115 · SpoilersSDR AALA202605129361Hinge Pin · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION OUTBOARD PIN SPOILER 1 ON LH WING. MEASURES OF CORROSION ARE: L = 0.512 INCH, W = 0.120 INCH, D = 0.016 INCH. MAINTENANCE REPLACED PIN-HINGE SPOILER IAW SRM A319 51-72-11-911-001.Apr 24, 2026 · N9010R · Airbus A319115 · SpoilersSDR REXA2026051200580Lug · damaged"R/H WING SIDE AILERON HINGE #3 (I/B) HAS A PREVIOUSLY O/S LUG LABELED ""E"". CURRENT LUG INTERNAL DIAMETER MEASURES (0.8910""). NOMINAL LUG INTERNAL DIAMETER IS (0.8750""). ENGINEERING IS REQUIRED. REPAIRED RH WING SIDE AILERON FITTING #3 IB LUG IAW MHIRJ REOApr 24, 2026 · N691CA · Cndair CL6002D24 · Wing, Control Surface Attach FittingsSDR REXA2026051200579Lug · damaged"R/H WING SIDE AILERON HINGE #2 (I/B) HAS A PREVIOUSLY O/S LUG LABELED ""C"". CURRENT LUG INTERNAL DIAMETER MEASURES (0.8910""). NOMINAL LUG INTERNAL DIAMETER IS (0.8750""). ENGINEERING IS REQUIRED. REPAIRED RH WING SIDE AILERON FITTING #2 IB LUG IAW MHIRJ REOApr 24, 2026 · N691CA · Cndair CL6002D24 · Wing, Control Surface Attach FittingsSDR REXA2026051200578Lug · damaged"R/H WING SIDE AILERON HINGE #3 (O/B) HAS A PREVIOUSLY O/S LUG LABELED ""F"". CURRENT LUG INTERNAL DIAMETER MEASURES (0.8910""). NOMINAL LUG INTERNAL DIAMETER IS (0.8750""). ENGINEERING IS REQUIRED. REPAIRED RH WING SIDE AILERON FITTING #3 OB LUG IAW MHIRJ REOApr 24, 2026 · N691CA · Cndair CL6002D24 · Wing, Control Surface Attach FittingsSDR REXA2026051200577Lug · damaged"R/H WING SIDE AILERON HINGE #2 (O/B) HAS A PREVIOUSLY O/S LUG LABELED ""D"". CURRENT LUG INTERNAL DIAMETER MEASURES (0.8910""). NOMINAL LUG INTERNAL DIAMETER IS (0.8750""). ENGINEERING IS REQUIRED. REPAIRED RH WING SIDE AILERON FITTING #2 OB LUG IAW MHIRJ REOApr 24, 2026 · N691CA · Cndair CL6002D24 · Wing, Control Surface Attach FittingsSDR REXA2026051200576Lug · damaged"L/H WING SIDE AILERON HINGE #3 (O/B) HAS A PREVIOUSLY O/S LUG LABELED ""F"". CURRENT LUG INTERNAL DIAMETER MEASURES (0.9065""). NOMINAL LUG INTERNAL DIAMETER IS (0.8750""). ENGINEERING IS REQUIRED. REPAIRED LH WING SIDE AILERON #3 FITTING OB LUG IAW MHIRJ REOApr 24, 2026 · N691CA · Cndair CL6002D24 · Wing, Control Surface Attach FittingsSDR REXA2026051200575Lug · damaged"L/H WING SIDE AILERON HINGE #3 (I/B) HAS A PREVIOUSLY O/S LUG LABELED "E". CURRENT LUG INTERNAL DIAMETER MEASURES (0.9065""). NOMINAL LUG INTERNAL DIAMETER IS (0.8750""). ENGINEERING IS REQUIRED. REPAIRED LH WING SIDE AILERON FITTING #3 IB LUG IAW MHIRJ REO 6Apr 24, 2026 · N691CA · Cndair CL6002D24 · Wing, Control Surface Attach FittingsSDR SWAA2026050692308Battery Pack · inoperativeEMERGENCY LIGHTS BY LEFT OVERWING EXITS ARE INOPERATIVE. REMOVED AND REPLACED BATTERY PACK AT LEFT OVERWING EXIT IAW AMM 33-51-06. NO FAULTS NOTED.Apr 24, 2026 · N8531Q · Boeing 7378H4 · Emergency LightingSDR SWAA2026050692307Battery Pack · inoperativeEMERGENCY LIGHTS BY RIGHT OVERWING EXITS ARE INOP. REMOVED AND REPLACED BATTERY PACK AT RIGHT OVERWING EXIT PER AMM 33-51-06. NO FAULTS NOTED.Apr 24, 2026 · N8531Q · Boeing 7378H4 · Emergency LightingSDR AALA202605054670Stop Fitting · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK INDICATION FOUND IN HOLE H3 AT FRAME 16 RH SIDE DOOR STOP FITTING NR 7 (ONLY INTERCOSTAL LAYER) AREA AT PASSENGER CABIN CRACK DIRECTION 9 0 CLOCK VIEW LOOKING FWD. CRACK DEPTH 0.100 IN. APPROX.Apr 24, 2026 · N809AW · Airbus A319132 · Fuselage Main, StructureSDR HNAA2026050500378Floor Panel · damagedLEFT DOUBLER FOR COCKPIT FLOOR BOARD 221GF, MIDDLE FLANGE FOR FLOOR PANEL FASTENER IS BENT DOWN AND CRACKED ALONG PILOTS SEAT TRACK. (APPROX. 1.5- 2 IN LONG BEND). REMOVED DAMAGED AREA ON L/H DOUBLER FOR COCKPIT FLOOR 221GL,AT MIDDLE FLANGE INSTALLED NEW BACKApr 24, 2026 · N654AE · Emb EMB145LR · Fuselage Floor PanelSDR VNAA2026050417002Pin · looseRIGHT ENG VIBE BETWEEN 1.5-1.9 CONTINUOUSLY. RAN QRH PROCEEDURE 3 TIMES. WHEN WE DECREASED POWER VIBES INCREASED TO 1.9; IN CLIMB DETENT VIBES DECREASED. REMOVED AND REPLACED RH ENGINE FAN BLADE PINS IAW CRJ 900 AMM 12-20-72-640-803-A01. PERFORMED VIBRATION RApr 24, 2026 · N587NN · Cndair CL6002D24 · Engine Mount SectionSDR CALA2026050415934Apu · faultedON TAXI OUT SMOKE STARTED TO COME INTO THE COCKPIT. AFTER THAT THE LT PACK FAILED AND RAN THE CHECKLISTS. SMOKE CLEARED ONCE LT PACK WAS SECURED. FLIGHT CREW DEBRIEFED. FLIGHT CREW FOLLOWED SMOKE CHECKLIST. FLIGHT CREW FOUND LT PACK OFF LIGHT ILLUMINATED WHENApr 24, 2026 · N794UA · Boeing 777222 · Airborne Auxiliary Power Unit (APU) SystemSDR FDEA202604240530Frame · crackedINSPECTION OF FR40 LOWER JUNCTION FASTENER HOLE NR 3 RT SIDE FOUND CRACK SIGNAL. COMPLIED WITH EA:6-5710-T0387217 P1 TO REPAIR FR40 RH SIDE LOWER JUNCTION CRACKED FASTENER HOLE #3, MAJOR REPAIR IAW FEDEX GMM6-2-100. SEE WRI 57107960 FOR WORK DETAILS.Apr 24, 2026 · N662FE · Airbus A300F4605R · Fuselage Main, FrameSDR IPXA2026042665993Panel · crackedDURING OK TO INSTALL PANEL 623BB, FOUND CRACK AT THE FWD UPPER RADIUS OF PANEL CUTOUT, DOT 55-006. INSTALLED REFORCING PLATE IAW SRM 57-41-12-227.Apr 24, 2026 · N122UP · Airbus A300F4622R · Wing Main, Frame StructureSDR IPXA2026042856061Depressor · deformedDEFORMED DEPRESSOR , MAIN DECK CGO DOOR AFT CUTOUT DEPRESSURE SEAL AREA (REPLACE) INSTALLED DEPRESSOR. I.A.W AMM 20-11-00-910-802 REV.147.TORQUED THE SCREW TO 35 IN-LB.Apr 24, 2026 · N384UP · Boeing 767300 · Fuselage Main, StructureSDR VNAA20260501023Rib · crackedCRACK ON RIB OF FIXED LEADING EDGE STA FS=58.41 (UPPER SIDE) AT RH WING. RIB OF FIXED LEADING EDGE STA FS=58.41 (UPPER SIDE) AT RH WING WAS REPLACED PER CRJ900 SRM 51-42-06-001-001-A01, SRM 51-42-10-001-001-A01 AND SRM 51-42-21-001-001-A01.Apr 24, 2026 · N617NN · Bombdr CL6002D15 · Wing, Rib/BulkheadSDR VNAA20260501022Slider · corrodedCORROSION ON INB SLIDER AT UPPER TRANSCOWL ENG RH. UPPER TRANSCOWL RH WAS REPLACED PER CRJ900 AMM 78-33-01Apr 24, 2026 · N617NN · Bombdr CL6002D15 · Engine Thrust ReverserSDR HYIA20260430002Cooling Fan · failedFLIGHT CREW REPORTED SMOKE IN THE CABIN. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND THE COPILOT AVIONICS COOLING FAN HAVE FAILED. THE FAN WAS REPLACED WITH NO FURTHER DEFECTS NOTED.Apr 24, 2026 · N133CA · Tecnam P2012 · Air Distribution FanSDR HYI2026F00000Cooling Fan · failedFLIGHT CREW REPORTED SMOKE IN THE CABIN. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND THE COPILOT AVIONICS COOLING FAN HAVE FAILED. THE FAN WAS REPLACED WITH NO FURTHER DEFECTS NOTED.Apr 24, 2026 · N133CA · Tecnam P2012 · Air Distribution FanSDR AALA202604304797Vapor Barrier · degradedAIRCRAFT IN BASE MAINTENANCE: EXISTING REPAIR ON LEFT HAND WHEEL WELL VAPOR BARRIER IS DEGRADED LOCATED 28 INCHES OYTBOARD OF KEEL BEAM AT BS 663 LBL 31.83 TO LBL 45.64. APPLIED PERMANENT REPAIR ON LEFT HAND VAPOR BARRIER. PER B737-NG AARD 57-10-10-9 AND B737-Apr 24, 2026 · N874NN · Boeing 737823 · Fuselage Main, BulkheadSDR IPXA2026042955931Scuff Plate · dentedDENTED PLATE, BULK CARGO DOOR CUTOUT MID SCUFF PLATE AREA. I.A.W AMM 53-13-02-404-007, REV 147 INSTALL BULK CARGO DOOR SCUFF PLATE.Apr 24, 2026 · N384UP · Boeing 767300 · Fuselage Miscellaneous StructureSDR AALA202604309442Angle · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK IN FORWARD CARGO COMPARTMENT BILGE BAFFLE CLIP AT STA 500H AND LBL 26. REPLACED BAFFLE CLIP PER AARD 53-00-01-06.Apr 24, 2026 · N956NN · Boeing 737823 · Fuselage Miscellaneous StructureSDR AALA202604301680Angle · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK IN FORWARD CARGO COMPARTMENT BILGE BAFFLE CLIP AT STA 500G AND LBL 23. REPLACED BAFFLE CLIP PER AARD 51-00-05-1.Apr 24, 2026 · N956NN · Boeing 737823 · Fuselage Miscellaneous StructureSDR AALA202604304614Angle · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK IN FORWARD CARGO COMPARTMENT BILGE BAFFLE CLIP AT STA 500G AND LBL 23. REPLACED BAFFLE CLIP PER AARD 53-00-01-06.Apr 24, 2026 · N956NN · Boeing 737823 · Fuselage Miscellaneous StructureSDR DALA2026043002743Power Supply · inoperativeL1 SLIDE ARMED INDICATOR LIGHT INOPERATIVE ON FWD ATTENDANT LIGHTING CONTROL PANEL. REPLACED PSEU PER B767 400 AMM 32-09. (7985697) (AIRCRAFT GROUNDED)Apr 24, 2026 · N830MH · Boeing 767432ER · Door Warning SystemSDR CALA2026042915823Stub Beam · gougedR2 DOOR LOWER STUB BEAM GOUGED. ALL WORK PERFORMED ON AAR GSO NON-ROUTINE 9288443. REMOVED DAMAGE, ORIGINAL THICKNESS .060, REMOVED .025, REMAINING .035. OUT OF LIMITS IAW SRM 52-10-02-1A-4 DETAIL E. REMOVED AND REPLACED STUB BEAM 147A6149-6 IAW DWG 147A6149.Apr 24, 2026 · N37255 · Boeing 737824 · Passenger/Crew DoorsSDR CALA2026042915821Skin · gougedR2 DOOR INNER SKIN LOWER HINGE CUTOUT HAS A DEEP SCRATCH AND BARE METAL. TALL WORKED PERFORMED ON AAR GSO NON-ROUTINE 9288623. FABRICATION OF NEW INNER SKIN IAW DWG 147A6152. REMOVED AND REPLACED LWR INNER SKIN PN# 147A6152-6 IAW DWG 147A6502 REV F.Apr 24, 2026 · N37255 · Boeing 737824 · Passenger/Crew DoorsSDR CALA2026042915811Unknown · odorFAINT BURNING ODOR FROM MIDDLE LAV AREA. PERFORMED SMOKE/FUME CONDITIONAL INSPECTION IAW AMM 05-51-56. NO VISIBLE SMOKE NOTED AND NO ODOR DETECTED. FA REPORTS ODOR DISSIPATED AND CAN NO LONGER BE SMELLED. NO DEFECTS NOTED.Apr 24, 2026 · N37577 · Boeing 7379 · Air Distribution SystemSDR CALA2026042915810Duct · splitSMOKE ODOR CONDITIONAL INSP REQUIRED PER AMM 05-51-XX DUE TO AN INCIDENT REPORTED BY THE CREW.SMOKE ODOR CONDITIONAL INSP REQUIRED PER AMM 05-51-XX DUE TO AN INCIDENT REPORTED BY THE CREW. REF AMM 05-51-58-800-801-C3, CREW DEBRIEF PER CONDITIONAL INSPECTION RApr 24, 2026 · N794UA · Boeing 777222 · Pneumatic Distribution SystemSDR DALA2026042902730Hinge Fitting · damagedSHIP 9565 LH WING T.E. FLAP ON FWD IDLER HINGE FITTING OUTBD LUG BORE DAMAGED. CORRECTIVE ACTION: REPAIRED PER ER/A 633228-14. (1559850) (AIRCRAFT GROUNDED)Apr 24, 2026 · N934AT · Boeing 717200 · Trailing Edge FlapsSDR DALA2026042902723Angle · crackedCRACK ON ANGLE ADJACENT TO FUSELAGE SKIN ON STA Y=1178 CANT AND LONG 17 LH SIDE. REPAIRED PER PRI 633860-14 (1561136) (AIRCRAFT GROUNDED)Apr 24, 2026 · N963AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR REXA2026042900414Fitting · crackedRIGHT FWD OVERWING EMERGENCY EXIT DOOR, THE UPPER AFT ALIGNMENT SPIGOT FITTING STRUCTURE NEAR THE BASE, HAS EVIDENCE OF A CRACK. REPAIRED IAW REO 670-52-21-103 REV -- DATE 2024-11-06 AND CRJ 900 SRMS 51-26-01-001-001-A01 AND 51-42-21-001-001-A01. SEE MAINTEApr 24, 2026 · N691CA · Cndair CL6002D24 · Emergency ExitsSDR SWAA2026042892383Seal · crackedLEFT HORIZONTAL STAB UPPER STABILIZER TO BODY FRONT SPAR SLIDING SEAL IS CRACKED. R & R LT HORZONTAL STAB FRONT UPPER SLIDER IAW AMM 53-31-31Apr 24, 2026 · N8582Z · Boeing 7378H4 · Horizontal Stabilizer Miscellaneous StructureSDR SWAA2026042892384Seal · crackedRIGHT HORIZONTAL STAB UPPER STABILIZER TO BODY FRONT SPAR SLIDING SEAL IS CRACKED. R & R RT HORZONTAL STAB FRONT UPPER SLIDER IAW AMM 53-31-31Apr 24, 2026 · N8582Z · Boeing 7378H4 · Horizontal Stabilizer Miscellaneous StructureSDR SWAA2026042892415Seal · crackedRT HORIZONTAL STABILIZER FORWARD UPPER SLIDING SEAL HAS A 3 VERTICAL CRACK ALONG THE FORWARD EDGE. REMOVED AND REPLACED RT HORIZONTAL STABILIZER FORWARD UPPER SLIDING SEAL. REF AMM 53-31-31.Apr 24, 2026 · N8925Q · Boeing 7378 · Horizontal Stabilizer Miscellaneous StructureSDR SWAA2026042892416Seal · crackedLEFT HORIZONTAL STABILIZER FORWARD UPPER SLIDING SEAL HAS A 3 VERTICAL CRACK ALONG THE FORWARD EDGE. REMOVED AND REPLACED LT HORIZONTAL STABILIZER FORWARD UPPER SLIDING SEAL IAW AMM 53-31-31.Apr 24, 2026 · N8925Q · Boeing 7378 · Horizontal Stabilizer Miscellaneous Structure