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 SWAA2026033075900Intercostal · crackedCRACKED INTERCOSTAL, BS 312 - 328, LBL 45, WL 208. REMOVED & REPLACED THE INTERCOSTAL IAW SRM 51-40-02-0G-0, & DWG 141A5400, SHEET 26, REV-.Mar 2, 2026 · N923WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2026033075901Intercostal · crackedCRACKED INTERCOSTAL, BS 328 - 344, LBL 45, WL 208. REMOVED & REPLACED THE INTERCOSTAL IAW SRM 51-40-02-0G-0, & DWG 141A5400, SHEET 44, REV -.Mar 2, 2026 · N923WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2026033075682Scuff Plate · crackedAFT CARGO BAY AFT CORNER SCUFF PLATE CRACKED. REPAIRED THE SCUFF PLATE IAW SRM 53-60-15-2R-1.Mar 2, 2026 · N249WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2026033075681Scuff Plate · crackedAFT CARGO BAY FWD CORNER SCUFF PLATE CRACKED. AFT CARGO BAY FWD CORNER SCUFF PLATE WAS REPLACED IAW SRM 51-10-02-0G-0, PARAGRAPH 9.Mar 2, 2026 · N249WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2026033075775Shield · corrodedCORROSION ON ACD FWD SHIELD WEB BETWEEN BS 767 - 794, RBL 23, WL 156, REMOVED & REPLACED THE SHIELD IAW SRM 51-40-02, AND DWG 146A0081, 0034, REV-.Mar 2, 2026 · N249WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2026033075776Shield · corrodedCORROSION ON ACD AFT SHIELD WEB BETWEEN BS 847 - 867, RBL 23, WL 156. REMOVED & REPLACED THE SHIELD IAW SRM 51-40-02, AND DWG 146A0081, 0034, REV-.Mar 2, 2026 · N249WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2026033075777Threshold Web · corrodedCORROSION ON ACD SUB THRESHOLD WEB BETWEEN BS 794 - 847, RBL 26, WL 156. REMOVED AND REPLACED THE SUB THRESHOLD WEB IAW SRM 51-10-02-0G-0, PARAGRAPH 9,Mar 2, 2026 · N249WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2026033075993Threshold Web · corrodedCORROSION ON FCD SUB THRESHOLD WEB BETWEEN BS 440 - 492, RBL 26, WL 156. REMOVED AND REPLACED THE SUB THRESHOLD WEB, IAW SRM 51-40-02-0G-0, & DWG 143A8330, REV A.Mar 2, 2026 · N249WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2026032775911Support · corrodedCORROSION FWD CARGO BAY AFT LOWER BULKHEAD SUPPORT HAS MULTIPLE AREAS AROUND FASTENER HOLES BS500D LBL21 TO RBL21. REMOVED AND INSTALLED NEW FWD CARGO BAY AFT LOWER BULKHEAD SUPPORT IAW SRM 51-40-02-0G-0 AND DWG 143A7902 REV:-.Mar 2, 2026 · N923WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2026032775912Support Plate · corrodedCORROSION AFT CARGO BAY L/H FLOOR TO SIDEWALL SUPPORT PLATE MULTIPLE AREAS AROUND NUT PLATE HOLES BS727B TO BS767 LBL22 WL156<[01] REMOVED AND INSTALLED NEW L/H FLOOR TO SIDEWALL SUPPORT BS 727 TO 847 LBL 22 IAW SRM 51-40-02-0G-0 AND DWG 146A7500 REV:-.Mar 2, 2026 · N923WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2026032775913Support Plate · corrodedCORROSION AFT CARGO BAY RT FLOOR TO SIDEWALL SUPPORT PLATE HAS MULTIPLE AREAS AROUND NUT PLATE HOLES BS 727B TO 767 RBL22 WL156. REMOVED AND INSTALLED NEW R/H FLOOR TO SIDEWALL SUPPORT BS 727 TO 847 LBL 22 IAW SRM 51-40-02-0G-0 AND DWG 146A7500 REV-.Mar 2, 2026 · N923WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2026032775908Seat Track · corrodedCORROSION ON TOP & IN WELL OF PAX CABIN SEAT TRACK LBL 45 BS 500+8 TOP, BS 500A+7 WELL, BS 500B+18 WELL., WL 208. REMOVED CORROSION ON PAX CABIN SEAT TRACK LBL 45 WL 208 AT BS 500+8 ON TOP PER SRM 51-10-02-0G-0. AREA BLENDED IS L4' X W1' X D0.026' FOUND TO BMar 2, 2026 · N923WN · Boeing 7377H4 · Fuselage, Seat/Cargo Attach FittingsSDR SWAA2026032675894Floorbeam · corrodedCORROSION ON FLOOR BEAM BS 986 LBL 45 WL 208<[01] REMOVED AND REPLACED DAMAGE UPPER T-CHORD BS 986 RBL1-LBL50 WL 208 I.A.W SRM 51-40-02-0G-0 AS SHOWN IN CC# U152596 DATED 04/27/2020 PER SRM 53-70-51-2R-4 REPAIR 4 WITHOUT ANY DEVIATION.;[02] VERIFIED; CORRECTIVMar 2, 2026 · N923WN · Boeing 7377H4 · Fuselage Main, Floor BeamSDR IPXA2026030974670Floorboard · brokenMAJOR REPAIR, MCD FLOORBOARD 241XCF AFT CORNER IS BROKEN. THE FLOORBOARD FABRICATED IAW  SREO-9692-REQ001, VERIFIED RII REQUIREMENT COMPLETED, IAW UPS GMM 04.02.01.15.Mar 2, 2026 · N416UP · Boeing 75724APF · Fuselage Floor PanelSDR QXEA2026032600070Seat Track · damagedLEFT HAND LATERAL SEAT TRACK AT FRAME 21-23 IS SCRATCHED AND GOUGED. NO LIMITS FOR DAMAGE. FABRICATED AND TREATED NEW SEAT TRACK. REPLACED THE TRACK IAW E175 SRM 51-40-08.Mar 2, 2026 · N633QX · Emb ERJ170200LR · Fuselage, Seat/Cargo Attach FittingsSDR ASAA2026030265109Door · lack of lubeMAINTENANCE CONTROL/TECH SERVICES REQUEST: FOLLOW UP TO L2 DOOR HARD TO CLOSE. GROUNDED - YES. (RESOLVED ON W/O: 2086506 TASKCARD: N/R-00005 ) NO FAULTS FOUND; LUBRICATED L2 DOOR IAW B737-900ER AMM 12-25-12-640-801 STEP 2.F.Mar 2, 2026 · N247AK · Boeing 737990ER · Passenger/Crew DoorsSDR IPXA2026031781646Bracket · crackedLH WING, KRUEGER AREA, I/B INNER BRACKET HAS A CRACK. DOT 90-04 VERIFIED  NEW BRACKET AT LH WING KRUEGER AREA INSTLLED IAW A300-600 SRM 51-40-21, JOB COMPLETED.Mar 2, 2026 · N162UP · Airbus A300F4622R · Wing, Attach FittingsSDR IPXA2026031781689Bracket · crackedLH WING, KRUEGER AREA, I/B BRACKET HAS A CRACK. DOT 90-05 VERIFIED NEW BRAKET INSTALLATION IAW SRM 51-40-21 ON LH WING, KRUEGER I/B AREA.Mar 2, 2026 · N162UP · Airbus A300F4622R · Wing, Attach FittingsSDR CALA2026032314728Compressor · damagedPER CREW DEBRIEF, NR 1 ENG COMPRESSOR STALL, ENG SHUTDOWN IN FLIGHT. REMOVED AND REPLACED ENGINE 1.Mar 2, 2026 · N24972 · Boeing 7879 · Turbine Engine Compressor SectionSDR IPXA2026031672729Frame · crackedLEFT WING SHOCK STRUT DOOR FAIRING RUB CRACK FRAME. (REPLACE) INSTALLED NEW FRAME I.A.W SRM 51-40-02-0G REV.106 AND BOEING DWG NO: 65B11675 SH 1 REV.K AND 65B11675 SH2 REV.G AND 65B11675 SH3 REV.KMar 2, 2026 · N574UP · Boeing 74744AF · Landing Gear DoorsSDR DALA2026031901901Strut · corrodedCORROSION ON INTERCONNECTING STRUTS LH. REMOVED INTERCONNECTING STRUTS L/H P/N:D5757032201100, S/N: 02370 ON UNSERVICEABLE CONDITION AS PER FAM AMM 27-51-44- 000-001-A EXCEPT STEP 3.D.(2). JOB IN PROGRESS. REPLACED INTERCONNECTING STRUT ON LH WING AS PER A320Mar 2, 2026 · N365NB · Airbus A319114 · Trailing Edge FlapsSDR DALA2026031901896Strut · corrodedCORROSION ON INTERCONNECTING STRUTS RT. REMOVED INTERCONNECTING STRUTS IAW AMM 27-51-44- 000-001-A EXCEPT STEP 3.D.(2). REPLACED INTERCONNECTING STRUT IAW AMM 27 -51-44-000-001-A AND AMM 27-51-44-400-001-A,Mar 2, 2026 · N365NB · Airbus A319114 · Wing Main, Frame StructureSDR IPXA2026031579385Transition Panel · corrodedTRANSITION PANEL FROM AFT CARGO COMPARTMENT STA1310 TO STA 1360 R/H CORROSION AND HOLES DAMAGED. INSTALLED NEW TRANSITION PANEL AFT CARGO COMPARTMENT STA 1310 TO STA 1360 R/H IAW SRM 51-40-02-0GMar 2, 2026 · N416UP · Boeing 75724APF · Fuselage Miscellaneous StructureSDR SWAA2026031775859Seal · crackedLEFT HORIZONTAL STAB FORWARD UPPER SLIDER SEAL IS CRACKED. REMOVED AND REPLACED THE SLIDER SEAL IAW AMM 53-31-31.Mar 2, 2026 · N8857Q · Boeing 7378 · Horizontal Stabilizer Miscellaneous StructureSDR QXEA2026031700055Seat Track · corrodedAT PASSENGER CABIN RT SEAT TRACK BETWEEN FR.31 AND FR.32 HAS CORROSION. REMOVED AND REPLACED CORRODDED SEAT TRACK SECTION IAW SRM 53-00-10-02-01, REPAIRS O/P ETD2026-170-003479 & ETD2022-170-022163. APPLIED TOPCOAT IAW SRM 51-23-06, APPLIED CIC IAW CPM 51Mar 2, 2026 · N633QX · Emb ERJ170200LR · Fuselage, Seat/Cargo Attach FittingsSDR SWIA2026030275518Floorbeam · corrodedFRAME 84 FLOORBEAM CORRODED AT END OF SEAT TRACK. REPAIRED THE FLOORBEAM IAW SRM 53-00-10, REPAIR 01, & ETD2022-170-022163, REV:C.Mar 2, 2026 · N211SY · Emb ERJ170200LR · Fuselage Main, Floor BeamSDR SWIA2026030275517Floorbeam · corrodedFRAME 87 FLOORBEAM CORRODED. R & R THE FLOORBEAM IAW SRM 51-40-08.Mar 2, 2026 · N211SY · Emb ERJ170200LR · Fuselage Main, Floor BeamSDR SWIA2026030275516Floorbeam · corrodedFRAME 87 FLOORBEAM CORRODED. R & R THE FLOORBEAM IAW SRM 51-40-08.Mar 2, 2026 · N211SY · Emb ERJ170200LR · Fuselage Main, Floor BeamSDR SWIA2026031705515Floorbeam · corrodedPAX FLOOR STRUCTURE FR84 RT FLOORBEAM CORRODED AT END OF SEAT TRACK. REPAIRED FLOORBEAM IAW SRM 53-00-10/REPAIR 01, & ETD2022-170-022163 REV:C.Mar 2, 2026 · N211SY · Emb ERJ170200LR · Fuselage Main, Floor BeamSDR IPXA2026031702729Frame · crackedCRACKED LT WING SHOCK STRUT DOOR FAIRING RUB, CRACKED FRAME.Mar 2, 2026 · N574UP · Boeing 74744AF · Fuselage Main, FrameSDR IPXA2026031784226Angle · crackedNR 1 ENG AFT PYLON FARING SUPPORT ANGLE L BRACKET ON INBD SIDE IS CRACKED. REMOVED BRACKET ON NR 1 ENGINE AFT PYLON FARING IAW SRM 51-40-02. INSTALLED A NEW L ANGLE IAW SRM 51-40-02.Mar 2, 2026 · N416UP · Boeing 75724APF · Nacelle/Pylon, Main FrameSDR IPXA2026030973683Battery · inoperative**SUPPLEMENTAL SDR** FAULT - FOUND EMERGENCY LIGHT DID NOT STAY ON FOR 15 MINUTES (REPLACE). I.A.W AMM 33-51-07-022-001, 33-51-07-422-012 REV. 147 REPLACED THE BATTERY PACK, AND CONDITION CHECK NORMAL. REVIEW COMPLETEMar 2, 2026 · N348UP · Boeing 76734AF · Emergency LightingSDR IPXA2026031475852Web · crackedNR 1 ENG, AFT PYLON, INNER BOX, BTWN RIB 19 TO RIB 20, PLATE STRUCTURE AT HYD PRESSURIZATION LINE FITTING CUTOUT HAS A CRACKS (2EA). REMOVED WEB FROM #1 PYLON LOWER SPAR EXTENTION MEMBER UNDER AFT FAIRING IAW SRM 51-40-21-001. INSTALLED SPAR EXTENTION MEMBER AMar 2, 2026 · N162UP · Airbus A300F4622R · Nacelle/Pylon Miscellaneous StructureSDR IPXA2026030874565Seat Track · wornFOUND SEAT TRACK ASSY INBOARD AFT OF FIRST OFFICER SEAT WORN, POSITION (REPLACE) 1. I.A.W AMM 25-11-01-822-095-001 REV.147, REPLACED TRACK ASSY. JOB COMPLETED AND CONDITION CHECK NORMAL.Mar 2, 2026 · N348UP · Boeing 76734AF · Fuselage, Seat/Cargo Attach FittingsSDR IPXA2026031281768Bracket · crackedLEFT WING, ACCESS PANEL 575AB AREA, INNER TOP BRACKET HAS A CRACK. REMOVED BRACKET AT LT WING, ACCESS PANEL 575AB AREA, INNER TOP. IAW SRM-51-40-21. INSTALLED PLATE MOUNTING USING EXISTING FASTENERS, IAW SRM 51-40-21.Mar 2, 2026 · N162UP · Airbus A300F4622R · Wing Miscellaneous StructureSDR IPXA2026031383459Bracket · crackedRIGHT WING LEADING EDGE INSIDE THE ACCES PANEL 675AB HYD LNES SUPPORT BRACKET BROKEN. INSTALLED NEW BRACKET-MOUNTING AT RT WING LEADING EDGE INSIDE THE ACCES PANEL 675AB, IAW SRM 51-40-21.Mar 2, 2026 · N162UP · Airbus A300F4622R · Wing Miscellaneous StructureSDR DALA2026031301751Spar Cap · damagedSHIP 9562 ERA 614420-14AD REV A ISSUED FOR REPAIRS TO RH WING REAR LOWER SPAR CAP AND WING SKIN, ACCOMPLISH ERA 614420-14AD (1476521).Mar 2, 2026 · N939AT · Boeing 717200 · Wing SparSDR IPXA2026031284337Transmitter · inoperativeAIR TURN BACK, UNABLE TO RECEIVE HF RADIO TRANSMISSIONS ON EVERY HF FREQ WE COULD FIND. CONTACTED DISPATCH, ATB REQUIRED. PRIOR TO DEPT HF CHECK WITH OTHER AIRPLANE SUCCESSFUL ON BOTH HF RADIOS. HF RIGHT. T/S RIGHT HF SYSTEM FOUND SQUELCH ON PREVENTING RECEIVEMar 2, 2026 · N384UP · Boeing 767300 · HF Communications SystemSDR IPXA2026031284304Transmitter · inoperativeATB, UNABLE TO RECEIVE HF RADIO TRANSMISSIONS ON EVERY HF FREQ WE COULD FIND. CONTACTED DISPATCH, ATB REQUIRED. PRIOR TO DEPT HF CHECK WITH OTHER ARCFT SUCCESSFUL ON BOTH HF RADIOS. HF LT. T/S LT HF SYS, FOUND HF TRANSCEIVER STUCK ON 10MHZ AND FREQUENCY WOULMar 2, 2026 · N384UP · Boeing 767300 · HF Communications SystemSDR SWAA2026031175787Stringer · crackedSTRINGER 22R CRACKED AT BS 344. REPAIRED IAW EA 26-153-00584.Mar 2, 2026 · N8745K · Boeing 7378 · Fuselage Main, Longeron/StringerSDR SWAA2026031176090Stringer Splice · crackedSTRINGER SPLICE 27R AT BS 440 IS CRACKED. STRINGER SPLICE IS SHEARED THROUGH. R & R THE STRINGER SPLICE IAW SRM 51-40-02.Mar 2, 2026 · N8745K · Boeing 7378 · Fuselage Main, Longeron/StringerSDR SWAA2026031176091Skin · crackedDURING OPEN HOLE NDT INSPECTION OF STR 22R, A CRACK INDICATION NOTED AT BS 344+4 AND 344+6 OF STRINGER. REPAIRED IAW EA 26-153-00584.Mar 2, 2026 · N8745K · Boeing 7378 · Fuselage Main, Plate/SkinSDR SWAA2026031175789Bear Strap · deformedFWD CARGO DOOR SURROUND DOUBLER (BEAR STRAP) IS DEFORMED AT STA 440; S-27R. SEE EA.126-153-00594 FOR WORK PERFORMED.Mar 2, 2026 · N8745K · Boeing 7378 · Fuselage Main, Plate/SkinSDR AALA202603118235Latch · brokenAIRCRAFT IN BASE MAINTENANCE: FOUND BROKEN LATCH ON AFT ESCAPE HATCH PANEL. MAINTENANCE REPLACED LATCH IAW AMM-20-11-00.Mar 2, 2026 · N871AY · Boeing 7878 · Emergency ExitsSDR AALA202603103671Stop Pad · out of positionAIRCRAFT IN BASE MAINTENANCE: LEFT HAND FORWARD OVER WING EMERGENCY EXIT DOOR FORWARD LOWER STOP PAD IS ROTATED AND NEEDS REPOSITIONED. REMOVED AND REPLACED STOP PAD PLATE AT LEFT HAND FORWARD OVERWING EMERGENCY EXIT DOOR, PER B737 MAX8 AMM 52-22-01 PERFORMED Mar 2, 2026 · N307TA · Boeing 7378 · Emergency ExitsSDR DALA2026031001639Doubler · crackedSHIP 9529 COMPLY WITH ERA 630489-14 LH WING MLG SUPPORT UPPER DOUBLER CRACKS. CORRECTIVE ACTION: COMPLIED WITH ERA 630489-14. (7952424)Mar 2, 2026 · N991AT · Boeing 717200 · Wing Main, Frame StructureSDR DALA2026031001629None · noneDTE ERA 520355-14 REV B. REPAIR PER ERA 520355-14 REV B SECTION V IS LIMITED TO 12 MONTHS FROM REPAIR EMBODIMENT @ 02MAR2026. C/A: REVISE AND UPDATE ERA 520355-14 WITH DTE RESULTS PRIOR TO 02MAR2027. ASSOCIATED ER/A 14-520355 ADDED FOR AC 3277. (LP: 1476200)Mar 2, 2026 · N377NW · Airbus A320211 · Standard Practices/StructuresSDR IPXA2026030774969Floor Panel · crackedAFT CARGO FLOOR PANEL CRACK AT STA 1327 BL 0. INSTALL NEW PANEL I.A.W SRM 51-40-02-0G REV.94.Mar 2, 2026 · N351UP · Boeing 76734AF · Fuselage Floor PanelSDR HNAA2026030200165Gasket · leakingAMMAENDED: STRONG FUEL SMELL/ODOR ENTERED COCKPIT AND CABIN ON APU START HAS EXTENSIVE HISTORY - APU FAIL ON EICAS MESSAGE ALSO DISPLAYED MEL 02MAR26 11:53 GRR C06116 49-1 APU AUXILIARY POWER UNIT DFRL 04MAR26 08:46 SBY ENGINE PROGRAMS DEPARTMMar 2, 2026 · N690AE · Emb EMB145LR · APU Engine Fuel and ControlSDR GTIA2026030539287Unknown · odorPINE HEEDS SMELL FILLOWED BY ELECTRICAL BURNING SMELL ISOLATED TO COCKPIT . DESCRIPTION OF ODOR/FUMES: PERSISTENT, SMOKE/ BURNING SMELL / ELECTRICAL SMELL. APPARENT CABIN SOURCE: UNKNOWN FLIGHT DECK. NO VISIBLE SMOKE/HAZE. NO MEDICAL ATTENTION REQUIRED.-PERFOMMar 2, 2026 · N618NK · Airbus A320232 · Air Distribution System