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 VNAA20260418006Diaphragm · crackedCRACK ON SUPPORT STRUCTURE ON FS 849 AND STGR 24L BELLOW FUSELAGE FAIRING 195DL. CRACK ON SUPPORT STRUCTURE ON FS 849 AND STGR 24L BELLOW FUSELAGE FAIRING 195DL WAS REPAIRED REO 690-53-82-277 REV. -.Apr 18, 2026 · N605NN · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR VNAA20260418005Drag Angle · crackedCRACK ON RH VERTICAL STABILIZER TO FUSELAGE AFT DRAG ANGLE BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATUM (TRACE AT BL0.00). CRACK ON RH VERTICAL STABILIZER TO FUSELAGE AFT DRAG ANGLE BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATUM (TRACE AT BL0.00) WAS REPAApr 18, 2026 · N605NN · Cndair CL6002D24 · Vertical StabilizerSDR VNAA20260418004Drag Angle · crackedCRACK ON LH VERTICAL STABILIZER TO FUSELAGE AFT DRAG ANGLE BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATUM (TRACE AT BL0.00) LH VERTICAL STABILIZER TO FUSELAGE AFT DRAG ANGLE BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATUM (TRACE AT BL0.00) WAS REPAIRED PER Apr 18, 2026 · N605NN · Cndair CL6002D24 · Fuselage, Stabilizer Attach FittingsSDR VNAA20260418003Hinge Fitting · wornCORROSION ON HINGE FITTINGS (2 EAS) AND HINGE ARMS (2 EAS) ON AFT TOILET SERVICE DOOR 196ER. CORROSION ON HINGE FITTINGS (2 EAS) AND HINGE ARMS (2 EAS) ON AFT TOILET SERVICE DOOR 196ER. WERE EVALUATED DUE TO EXCESSIVE CORROSION MUST BE REPLACED PER CRJ-900 SRApr 18, 2026 · N605NN · Cndair CL6002D24 · Fuselage, Door HingeSDR VNAA20260418002Skin · damagedLIGHTNING-STRIKE ON UPPER SKIN BTW RIB Nº5 AND Nº7 AT LH ELEVATOR STAB, LIGHTNING-STRIKE ON UPPER SKIN BTW RIB Nº5 AND Nº7 AT LH ELEVATOR STAB WAS REPAIRED PER REO 690-55-21-137 REV --Apr 18, 2026 · N605NN · Cndair CL6002D24 · Elevator, Plate/SkinSDR VNAA20260418001Hinge Arm · wornWEAR ON FWD INNER HINGE ARM (UPPER AND LWR AREA) AT CENTER BAGGAGE BAY DOOR MECHANISM. WEAR ON FWD INNER HINGE ARM (UPPER AND LWR AREA) AT CENTER BAGGAGE BAY DOOR MECHANISM. WAS REPAIRED PER REO 690-52-35-628REV -.Apr 18, 2026 · N605NN · Cndair CL6002D24 · Cargo/Baggage DoorsSDR R61A2026041800107Skin · crackedCRACK WING SKIN AT FWD SIDE OF RH WW AT RIB 3 AS MARKED.Apr 18, 2026 · N240JQ · Emb ERJ170200LR · Wing, Plate/SkinSDR R61A2026041800010Skin · crackedCRACK ON RH WING LOWER SURFACE AT SPAR 2 BETWEEN RIBS 4/5.Apr 18, 2026 · N240JQ · Emb ERJ170200LR · Wing, Plate/SkinSDR SWIA2026041776852Frame · corrodedBS 333 FRAME CORRODED BTWN STR 20L TO STR 21L. R & R BS 333 FRAME, STR 20L - 23L IAW SRM 51-42-06, AND SRM 51-42-21, COMPLETED TASK CARD 51-900-1003-SKY.Apr 17, 2026 · N926SW · Cndair CL6002B19 · Fuselage Main, FrameSDR SWIA2026041776850Floor Support · corrodedRBL 9 FLOOR SUPPORT HAS MULTIPLE AREA OF CORROSION FROM BS 409+128 TO 559. PERFORMED A MAJOR REPAIR BY REPLACING THE RT RBL 9 FLOOR SUPPORT FROM BS 409+128 - 559 IAW REO 601R-53-00-005 IAW 601R-53-51-3428. COMPLETED STRUCTURAL MAJOR REPAIR TASK CARD 51-900-10Apr 17, 2026 · N926SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA2026041776847Floor Support · corrodedLBL 9 FLOOR SUPORT HAD MULTIPLE AREAS OF CORROSION ON INBD AND OTBD FLOOR SUPPORT BS 409+128 - 559. PERFORMED A MAJOR REPAIR BY REPLACING THE UPPER CAP OF THE LBL 9 FLOOR SUPPORT BTWN BS 409+128 & 559 IAW REO 601R-53-41-3427, REV-. COMPLETED TASK CARD 51-900-Apr 17, 2026 · N926SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA2026041776845Frame · corrodedBS 319 FRAME CORRODED BTWN STR 20L TO STR 21L. R & R THE FRAME SECTOR AT BS 319 BTWN STR 18L & 21L IAW SRM 51-42-06, & 51-42-21. COMPLETED TASK CARD 51-900-1003-SKY.Apr 17, 2026 · N926SW · Cndair CL6002B19 · Fuselage Main, FrameSDR SWIA2026041776314Frame · chafedDURING AUDIT OF TASK CARD 53-350-500 IT WAS FOUND THAT THERE IS A CHAFED FRAME AREA AFT OF APU EXHAUST BS 654.50. REPAIRED FRAME AFT OF APU EXHAUST BS 654.5 IAW SRM 51-42-06, 51-42-21, DWG 601R35004, REV BJ, AND REO 601R-53-61-8529, REV.--. COMPLIED WITH TASApr 17, 2026 · N951SW · Cndair CL6002B19 · Fuselage Main, FrameSDR IPXA2026061056763Splice Angle · gougedMAIN CARGO DECK RT FRAME 47 SPLICE FITTING BETWEEN STRG 24 AND STRG 26 HAS (2 EA) SPOTS OF TOOLING DAMAGE ON AFT FACE ON SPLICE FITTING. ACCOMPLISHED PERMANENT REPAIR PER EO-97689-REQ1 AND EA 300-5236-27-A4484 REV.Apr 17, 2026 · N163UP · Airbus A300F4622R · Fuselage Main, StructureSDR IPXA2026061056670Fitting · gougedMAIN CARGO DECK RH FRAME 47 SPLICE FITTING BETWEEN STRG 24 AND STRG 26 HAS GOUGES ON FWD FACE OF SPLICE FITTING. ACCOMPLISHED PERMANENT REPAIR PER EO-97689-REQ1 AND EA 300-5236-27-A4484 REV. -.Apr 17, 2026 · N163UP · Airbus A300F4622R · Fuselage Miscellaneous StructureSDR 1Q2R2026061200001Skin · gougedEA 57-2025-0380 FOR SLAT PANEL 622EZ REQUIRED PERMANENT REPAIR. PERFORMED PERMANENT REPAIR IN ACCORDANCE WITH MHI RJ REO 670-57-42-2470 REV. --, DATED APRIL 13, 2026.Apr 17, 2026 · N522AE · Cndair CL6002C10 · Leading Edge DevicesSDR IPXA2026060556348Frame · crackedCWB CENTER SPAR WEB REINFORCEMENT LH SIDE. 1(EA) INBOARD UPPER FASTENER HOLE CRACKED. VERIFIED E.A.#300-5710-27-A4452, PRELIMINARY 3, STEP 14. C/W VERIFIED BLAIN BUSHES (3EA) INSTALLED WITH NITROGEN LIQUID IN AFFECTED HOLE AS PER FIGURE 2, REPAIR DWGS R007-12Apr 17, 2026 · N141UP · Airbus A300F4622R · Fuselage Main, FrameSDR IPXA2026060556413Frame · crackedCWB CENTER SPAR WEB REINFORCEMENT RH SIDE. 1(EA) INBOARD UPPER FASTENER HOLE CRACKED. ZONE 142 OUT OF SEQ. INSTALLED WITH NITROGEN LIQUID IN AFFECTED HOLE AS PER FIGURE2, REPAIR DWGS R007-12001 ISSUE C. ACCOMPLISH THE PERMANENT REPAIR PER EO-97608-REQ1 AND Apr 17, 2026 · N141UP · Airbus A300F4622R · Fuselage Main, FrameSDR IPXA2026060456403Mount · damagedNR 1 ENGINE, AFT MOTOR ATTACH FITTING HAS CORROSION AND PITTING ON MATTING SURFACE ALL RII STEPS C/W REF GMM CH4. WITNESSED INSTALL AND VERIFIED CRITICAL TORQUE STEPS OK FOR INSTALL.Apr 17, 2026 · N144UP · Airbus A300F4622R · Engine Mount SectionSDR SWAA2026060190522Skin · debondedDEBONDED LOWER SKIN LOCATED IB SIDE OF OB AFT FLAP AT RT WING. PERFORMED PERMANENT REPAIR ON RH WING T/E OUTBD AFT FLAP WEDGE PANEL ON UPPER AND LOWER SKIN IAW SWA EA 26-157-01292-WIP2.Apr 17, 2026 · N8635F · Boeing 7378H4 · Trailing Edge FlapsSDR SWAA2026060190521Skin · delaminatedDELAMINATED AFT FLAP LOCATED INBOARD EDGE OF OUTBOARD FLAP AT LT WING. PERFORMED PERMANENT REPAIR ON LT WING T/E OUTBD AFT FLAP WEDGE PANEL ON UPPER AND LOWER SKIN IAW SWA EA# 26-157-01295-WIP1.Apr 17, 2026 · N8635F · Boeing 7378H4 · Trailing Edge FlapsSDR CALA2026052116424Support Angle · corrodedCORROSION-FWD WET AREA L-1 CUTOUT THRESHOLD I/B SUPPORT ANGLE. REMOVED AND REPLACED SUPPORT ANGLE AT L1 DOOR THRESHOLD I/B POSITION IAW SRM 51-40-02-0G-0, AND DWG 141A8110,Apr 17, 2026 · N73270 · Boeing 737824 · Fuselage Miscellaneous StructureSDR SWAA2026052090277Stub Frame · crackedCRACK INDICATION FOUND ON STUB FRAME, BS 294.5, 4.2 INCHES BELOW STRINGER 8R. REPLACED STUB FRAME IAW SRM 51-40-02, SRM 51-10-02, ITEM 9, AND DWG 141A8370, SHEET 9, & 10, REV D.Apr 17, 2026 · N250WN · Boeing 7377H4 · Fuselage Main, FrameSDR HNAA2026052000416Doubler · not reportedFUSELAGE EXTERNAL SKIN REPAIR DOUBLER BETWEEN FR 35/36 AT STR 1L HAS NO REPAIR INFORMATION. RE-ACCOMPLISHED DOUBLER REPAIR ON FUSELAGE EXTERNAL SKIN BETWEEN FR 35/36 AT STR 1L IAW ETD2026-145-007253-A AND EO1-53-26-0222.Apr 17, 2026 · N655AE · Emb EMB145LR · Fuselage Main, Plate/SkinSDR HNAA2026052000415Repair · chafedSTRINGER 19R PREVIOUS REPAIR BETWEEN FR 52/53 CHAFED. PERFORMED NEW REPAIR OF STRINGER 19R (2 ANGLE REPAIR) BETWEEN FR 52/53 IAW SRM 53-24-02RE, ITEM 2, FIG 202 AND EO1-53-26-0231.Apr 17, 2026 · N655AE · Emb EMB145LR · Fuselage Main, Longeron/StringerSDR REXA2026051500600Fitting · corrodedCORROSION FLOOR FITING IN FWD ACCESS 107 AND AFT ACCESS 108 (2EAS) ON GALLEY 1 SUMMARY OF NRC 00151: FLOOR FITINGS IN FWD ACCESS 107 AND AFT ACCESS 108 (2EAS) ON GALLEY 1 WERE REPLACED PER SAFRAN CMM 25-33-67 REV.NO 10Apr 17, 2026 · N137EV · Cndair CL6002D24 · Fuselage, Equipment Attach FittingsSDR REXA2026051500599Fitting · corrodedCORROSION FLOOR FITING IN FWD ACCESS 107 AND AFT ACCESS 108 (2EAS) ON GALLEY 1 SUMMARY OF NRC 00151: FLOOR FITINGS IN FWD ACCESS 107 AND AFT ACCESS 108 (2EAS) ON GALLEY 1 WERE REPLACED PER SAFRAN CMM 25-33-67 REV.NO 10Apr 17, 2026 · N137EV · Cndair CL6002D24 · Fuselage, Equipment Attach FittingsSDR REXA2026051500598Fitting · corrodedCORROSION FLOOR FITING IN FWD ACCESS 306 AND ACCESS 305 (2EAS) ON GALLEY 3 SUMMARY OF NRC 00150: FLOOR FITINGS IN FWD ACCESS 306 AND 305 (2EAS) ON GALLEY 3 WERE REPLACED PER ZODIAC AEROSPACE CMM 25-33-18 REV.NO 5Apr 17, 2026 · N137EV · Cndair CL6002D24 · Fuselage, Equipment Attach FittingsSDR REXA2026051500597Fitting · corrodedCORROSION FLOOR FITING IN FWD ACCESS 306 AND ACCESS 305 (2EAS) ON GALLEY 3 SUMMARY OF NRC 00150: FLOOR FITINGS IN FWD ACCESS 306 AND 305 (2EAS) ON GALLEY 3 WERE REPLACED PER ZODIAC AEROSPACE CMM 25-33-18 REV.NO 5Apr 17, 2026 · N137EV · Cndair CL6002D24 · Fuselage, Equipment Attach FittingsSDR REXA2026051500588Fitting · corrodedCORROSION WAS FOUND ON LUGS BORES L2, L5 AND L6 AT LH AILERON CENTER FITTING AND SCRATCH ON HINGE 4 LOWER BORE CORROSION ON LUGS BORES L2, L5 AND L6 AND SCRATCH ON HINGE 4 LOWER BORE WERE REPAIRED PER REO 670-57-61-237 REV:--, REO 690-57-61-513 REV:-- & CLEANEApr 17, 2026 · N137EV · Cndair CL6002D24 · Wing, Control Surface Attach FittingsSDR SWAA2026051190480Skin · delaminatedLH OB AFT FLAP; HAS AN AREA OF DELAM IN LOWER TRAILING EDGE WEDGE SKIN AT THE IB END. AREA MEASURES APPROXIMATELY 8.5 X 14 IN SIZE. NEW LEFT WING OUTBOARD AFT FLAP INSTALLED.Apr 17, 2026 · N8534Z · Boeing 7378H4 · Trailing Edge FlapsSDR IPXA2026050856714Skin · ground damageK-LOADER HAND RAIL STRUCK AIRCRAFT FWD OF CARGO DOOR 1. I.A.W AMM 25-53-03-404-030 REV.148 INSTALLED FORWARD CARGO BALL PANEL NEAR STA 511 RBL 33.Apr 17, 2026 · N385UP · Boeing 767300 · Fuselage Main, Plate/SkinSDR R61A2026050800119Skin · cracked"CRACK LOWER LH WING FWD OF WW CUTOUT AT RIB 3A. REPAIRED CRACK LOWER LH WING FWD OF WW CUTOUT AT RIB 3A INSTALLED PERMANENT REINFORCING REPAIR. REF. ETD2026-170-007024"Apr 17, 2026 · N138HQ · Emb ERJ170200LR · Wing, Plate/SkinSDR SWAA2026050690234Scuff Plate · crackedCRACK FWD CORNER SCUFF PLATE AT AFT CARGO DOOR CUT-OUT. REPAIRED FWD CORNER SCUFF PLATE AT AFT CARGO DOOR CUT OUT IAW SRM 53-60-15-2R-1, REPAIR 1, & BAC 5975.Apr 17, 2026 · N467WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2026050690438Rib · crackedCRACKED INSPAR RIB 111.10 LOCATED AT 20 INCHES OF FRONT SPAR AT RT HORIZONTAL STAB. PERFORMED PERMANENT REPAIR ON RIB 111.10 LOCATED AT 20 INCHES OF FRONT SPAR AT RT HORIZONTAL STAB IAW SRM 55-10-09-2R-4, REPAIR 4.Apr 17, 2026 · N467WN · Boeing 7377H4 · Horizontal Stabilizer, Spar/RibSDR SWAA2026050690439Rib · crackedCRACKED INSPAR RIB 111.10 LOCATED AT 28 INCHES OF FRONT SPAR AT RT HORIZONTAL STAB. PERFORMED PERMANENT REPAIR INSPAR RIB 111.10 LOCATED AT 28 INCHES OF FRONT SPAR AT RT HORIZONTAL STAB IAW SRM 55-10-09-2R-4, REPAIR 4.Apr 17, 2026 · N467WN · Boeing 7377H4 · Horizontal Stabilizer, Spar/RibSDR SWAA2026050690440Rib · crackedCRACKED INSPAR RIB 111.10 LOCATED AT 37 INCHES OF FRONT SPAR AT RT HORIZONTAL STAB. PERFORMED PERMANENT REPAIR ON RIB 111.10<BR>AT 37 INCHES OF FRONT SPAR AT RT HORIZONTAL STAB IAW SRM 55-10-09-2R-4, REPAIR 4.Apr 17, 2026 · N467WN · Boeing 7377H4 · Horizontal Stabilizer, Spar/RibSDR SWAA2026050690441Rib · crackedCRACKED INSPAR RIB 129.50 LOCATED 18 INCHES OF FRONT SPAR AT LT HORIZONTAL STAB. PERFORMED PERMANENT REPAIR LOC. INSPAR RIB 129.50 LOCATED 18 INCHES OF FRONT SPAR AT LT HORIZONTAL STAB IAW SRM 55-10-09-2R-4, REPAIR 4.Apr 17, 2026 · N467WN · Boeing 7377H4 · Horizontal Stabilizer, Spar/RibSDR SWAA2026050690233Scuff Plate · crackedCRACK AFT CORNER SCUFF PLATE AT AFT CARGO DOOR CUT-OUT. REPAIRED AFT CORNER SCUFF PLATE AT AFT CARGO DOOR CUT OUT IAW B737-700 SRM 53-60-15-2R-1 REPAIR 1. AND BAC 5975.Apr 17, 2026 · N467WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR AALA202605053536Skin · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON FUSELAGE SKIN AROUND LAVATORY VENT OPENING AT BS 917. REPAIRED SKIN. PER SRM 51-10-02-0G.Apr 17, 2026 · N956NN · Boeing 737823 · Fuselage Main, Plate/SkinSDR AALA202605057990Skin · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON FUSELAGE SKIN AROUND DRAIN AT STATION AT BS 727A BETWEEN STR 26R AND 27R. REPAIRED SKIN. PER SRM 51-10-02-0G.Apr 17, 2026 · N956NN · Boeing 737823 · Fuselage Main, Plate/SkinSDR IPXA2026050149922Tee Angle · corrodedFWD CARGO DOOR OUTER TEE IS CORRODED. INSTALLED NEW OUTER TEE IAW SRM 51-40-02-0G-0.Apr 17, 2026 · N421UP · Boeing 75724APF · Cargo/Baggage DoorsSDR CALA2026050115920Skin · damagedRAMP REPORTS LD CONTAINER EMBEDDED INTO AIRCRAFTDAMAGE TO LEFT SIDE OF FUSELAGE BS 500 D-E, S18 -20R, IAW SRM 53-00-01-1A-5 FIGURE 101 . REMOVED FWD CARGO SIDEWALL LINER IAW AMM 25-52-06-000-801 PER AVO17236 ITEM 1 THRU 7 PERFORMED HFEC PER 737 NDT MANUAL PARTApr 17, 2026 · N68811 · Boeing 737924ER · Fuselage Main, Plate/SkinSDR AALA202604292313Air Filter · contaminatedAIRCRAFT WAS GROUNDED: STRONG MUSTY ODOR IN FLIGHT DECK AND AFT CABIN DURING DESCENT. REMOVED AND REPLACED RECIRCULATION FAN HEPA LEFT FILTER (AALA202604219046) AND RIGHT FILTER (AALA202604292313). PER JC08C12221001.Apr 17, 2026 · N969AN · Boeing 737823 · Air Distribution SystemSDR IPXA2026042657472Retainer · brokenFAULT-STR-ZONE 500. AFTER REMOVAL OF LH WING PANEL 572PB, (2EA) CRACKS FOUND AT INNER PANEL SEAL RETAINER. INSTALLED NEW PANEL IAW SRM 51-40-21-001.Apr 17, 2026 · N141UP · Airbus A300F4622R · Wing Main, Frame StructureSDR SWAA2026042490498Scuff Plate · crackedCRACK ON AFT SCUFF PLATE AT AFT CARGO COMPARTMENT DOOR CUTOUT. REPAIRED AFT CORNER SCUFF PLATE AT AFT CARGO COMPARTMENT IN ACCORDING WITH SRM 53-60-15-2R-1; REPAIR 1.Apr 17, 2026 · N8640D · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR AALA202604249791Fitting · crackedAIRCRAFT IN BASE MAINTENANCE: WINDSHIELD FRAMING CENTER POST LH HALF FOUND CRACKED IN AREA A. MAINTENANCE REPLACE CONTINUITY FITTING RH SIDE IAW EA 372184.Apr 17, 2026 · N653AW · Airbus A320232 · Fuselage Main, StructureSDR SWAA2026042390445Girt Bar · out of adjustDAMAGED FASTENER THAT ATTACHES THE FWD. GIRT BAR RETAINER CLIP ON FED ESCAPE SLIDE PACK COVER. CORRECTLY INSTALLED FED SLIDE GIRT BAR RETAINER IAW SRM 51-40-02 AND AIPC 25-66-00-13.Apr 17, 2026 · N8880G · Boeing 7378 · Emergency EquipmentSDR SWAA2026042390446Girt Bar · corrodedCORROSION ON THE FED ESCAPE SLIDE GIRT BAR.<[01] VERIFIED AND CLEANED FED ESCAPE SLIDE GIRT BAR. IAW SRM 51-10-02 PAR 4. D. (2) AND SOPM 20-30-80. NO DAMAGE NOTED. REMOVED AND REINSTALLED FED ESCAPE SLIDE GIRT BAR IAW AMM 25-66-01-000-803 AND AMM 25-66-01-400-Apr 17, 2026 · N8880G · Boeing 7378 · Emergency EquipmentSDR JJBA20260423025Skin · canningAPU SKIN OIL CANNING UPPER BETWEEN PROFILES, SIDE LH. REPAIRED APU COWLING SKIN.Apr 17, 2026 · N14177 · Emb EMB145XR · APU Cowling/Containment