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 2026FA0000716Stiffener · crackedR/H WING FWD LWR I/B SKIN, FWD STIFFENER CRACKED. REPLACED WITH NEWJul 9, 2026 · N779G · Piper PA28181 · Wing Miscellaneous StructureSDR 2026FA0000704Skin · crackedR/H WING FWD WING WALK SKIN CRACKED ON CORRUGATED SKIN. REPLACED WING WALK CORRUGATED SKIN ASSY WITH NEWJul 9, 2026 · N779G · Piper PA28181 · Wing, Plate/SkinSDR IPXA2026082686422Adapter · corrodedMDC CLS FR26 BETWEEN Y1959 AND Y2462 SHOWS EVIDENCE OF CORROSION. ACCOMPLISHED EO-98365-REQ1 SEE T3F18E009DMX5.Jul 9, 2026 · N144UP · Airbus A300F4622R · Fuselage Main, StructureSDR AALA202609029004Floor Support · corrodedAIRCRAFT IN BASE MAINTENANCE: FOUND CORROSION ON INTERCOSTAL BETWEEN FS 787 AND FS 807 AT STR 21L. REMOVED AND REPLACED INTERCOSTAL PN 146A9403-21 IAW AARD 51-00-05 AND BOEING DWGS 146A9401, AND 146A7550.Jul 9, 2026 · N904AN · Boeing 737823 · Fuselage Miscellaneous StructureSDR SWIA2026070976982Angle · crackedANGLE @ WS 48.30 R/H HAS 2 CRACKS (C-CHECK RO 08/29/2026)REMOVED AND REPLACED NEW CAP (ANGLE) ON THE R/H WS 48.30 IAW CRJ 200 SRM 57-21-12,51-42-20,51-40-11,51-23-00.Jul 9, 2026 · N982SW · Cndair CL6002B19 · Wing Miscellaneous StructureSDR SWIA2026070976978Angle · crackedANGLE @ WS 48.30 L/H HAS A CRACK (C-CHECK RO 08/29/2026)REMOVED AND REPLACED NEW CAP (ANGLE) ON L/H FROM WS 48.30 IAW CRJ200 SRM 51-42-20,51-40-11,57-21-12.Jul 9, 2026 · N982SW · Cndair CL6002B19 · Wing Miscellaneous StructureSDR IPXA2026082681011Fitting · crackedCENTER FUSELAGE BASE FRAME FITTING C45 LT SIDE HAS A CRACK. ACCOMPLISHED A REPLACEMENT OF THE BASE FRAME FITTING FR 45 LT IAW EO-46789-JIC003, REV 1, REPLACEMENT-BASE FRAME FITTINGS, FR41 AND FR46, LT. REPAIR PERFORMED IAW EO-46789-JIC003.Jul 9, 2026 · N144UP · Airbus A300F4622R · Fuselage Main, StructureSDR IPXA2026082680739Fitting · crackedCENTER FUSELAGE BASE FRAME FITTING FR 44 RH SIDE HAS A CRACK. ACCOMPLISHED EO-46789-JIC008 REV2 REPAIR-BASE FRAME FITTING, FR 41 TO FR 46, RH SIDE (SB A300-57-6177) .Jul 9, 2026 · N144UP · Airbus A300F4622R · Fuselage Miscellaneous StructureSDR IPXA2026082680711Fitting · crackedCENTER FUSELAGE BASE FRAME FITTING FR 46 RH SIDE HAS A CRACK. ACCOMPLISHED EO-46789-JIC008 REV2 REPAIR-BASE FRAME FITTING, FR 41 TO FR 46 (FR46), RH SIDE (SB A300-57-6177).Jul 9, 2026 · N144UP · Airbus A300F4622R · Fuselage Miscellaneous StructureSDR 2026F00186Egt Indication · illuminatedNR 1 ENGINE EGT OVER LIMIT, FLIGHT CREW OBSERVED TEMPERATURE 985 DEG C WITH MASTER CAUTION WARNING.Jul 9, 2026 · N966AD · Airbus A321211 · Engine EGT/TIT Indicating SystemSDR IPXA2026080380704Fitting · crackedMAJOR REPAIR, CENTER FUSELAGE BASE FRAME FITTING FR 45 RT SIDE HAS A CRACK. ACCOMPLISHED REPAIR IN ACCORDANCE WITH EO-98327-REQ1 AND VT-MAE EA 300-5710-27-A4570, REV. -.Jul 9, 2026 · N144UP · Airbus A300F4622R · Fuselage Main, StructureSDR REXA2026082401627Floor Support · crackedAFTER ANGLE FLOOR SUPPORT REMOVAL AT LBL 12 IN REF NRC 00250,CRACK WAS FOUND. ANGLE FLOOR SUPPORT AT LBL 12 BTW 265 TO 280 WAS DRILLED AND TREATED PER CRJ 900 SRM 51-40-11-001-001-A01, CRJ 900 SRM 51-21-11-001-001-A01 AND SRM 51-25-06-001-001-A01 WILL BE INSTAJul 9, 2026 · N928XJ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2026082401606Fitting · corrodedCORROSION WAS FOUND ON FITTING HANDRAIL (2EAS). FITTING HANDRAIL (2EAS) WERE REPLACED PER CRJ-900 SRM 51-42-20-001-001-A01Jul 9, 2026 · N928XJ · Cndair CL6002D24 · Passenger/Crew DoorsSDR REXA2026082401605Fitting · corrodedCORROSION WAS FOUND ON FITTING HANDRAIL (2EAS). FITTING HANDRAIL (2EAS) WERE REPLACED PER CRJ-900 SRM 51-42-20-001-001-A01Jul 9, 2026 · N928XJ · Cndair CL6002D24 · Passenger/Crew DoorsSDR IPXA2026073085880Seat Track · corrodedMDC CLS AT FR27/Y0 SHOWS EVIDENCE OF CORROSION. INSTALLED CLS TRACK ADAPTER AT Z200 FR27/YO IAW A300-600 SRM 51-40-21-001.Jul 9, 2026 · N144UP · Airbus A300F4622R · Fuselage, Seat/Cargo Attach FittingsSDR SWAA2026081744212Crossbeam · crackedCRACKED BRAKE PANEL ON FLOOR STRUCTURE LOCATED STA 540 AND BTW BL 0 TO LBL 24.75. REPLACED BRAKE PANEL ON FLOOR STRUCTURE IAW SRM 51-10-02, ITEM 9, AND DWG 143A0060, SHEET 64, REV-.Jul 9, 2026 · N8651A · Boeing 7378H4 · Fuselage Main, StructureSDR SWAA2026081733855Crossbeam · crackedCRACK BRAKE PANEL ON FLOOR STRUCTURE, BS 540 BTW BL 0 - RBL 24.75 IN PASSENGER CABIN. REPLACED BRAKE PANEL AND FASTENERS ON FLOOR STRUCTURE IAW SRM 51-10-02, ITEM 9, & DWG 143A0060, SHEET 64, REV-.Jul 9, 2026 · N8651A · Boeing 7378H4 · Fuselage Main, StructureSDR HNAA2026081400718Yoke · crackedR/H ENGINE LOWER FWD ENGINE YOKE FITTING HAS A CRACK. REMOVED AND REPLACED CRACKED RH ENGINE LOWER FWD ENGINE YOKE FITTING IAW PDT FCD1-54-21-0017D AND REMOVED AND REPLACED RH ENGINE LOWER AFT YOKE FITTING, AND RH ENGINE UPPER FWD AND AFT YOKE FITTING IAW PDTJul 9, 2026 · N942LL · Emb EMB145LR · Engine Mount SectionSDR HNAA2026081400717Fitting · damagedRUDDER I LOWER ACTUATOR FITTING UPPER DOUBLE HAT BUSHING UPPER HAT BUSHING FITS LOOSE IN FITTING. REMOVED AND REPLACED 2 HAT BUSHINGS WITH 2 OVERSIZE HAT BUSHINGS, REAMED RUDDER I LOWER ACTUATOR FITTING UPPER DOUBLE HAT BUSHING HOLE TO (.7543") TO ACCOMODATE Jul 9, 2026 · N942LL · Emb EMB145LR · Rudder Miscellaneous StructureSDR HNAA2026081400698Bracket · crackedLEFT LOWER OVERWING BRACKET #5 IS CRACKED AT THE AFT END. ACCOMPLISHED SPLICE REPAIR FOR LH LOWER OVERWING BRACKET #5 AT THE AFT END IAW EMB 145 SRM 57-20-01-RE ITEM 3, FIG 203, 204, AND EO1-57-26-0360.Jul 9, 2026 · N942LL · Emb EMB145LR · Fuselage Main, Attach FittingsSDR HNAA2026081400697Bushing · wornLH AILERON PCA FITTING HAS MISSING HAT BUSHINGS WITH WORN HOLES. REMOVED AND REPLACED WORN LH AILERON PCA FITTING IAW EMB145 SRM 51-40-02 AND AMM 20-10-01.Jul 9, 2026 · N942LL · Emb EMB145LR · Wing Main, Frame StructureSDR HNAA2026081400696Support · crackedF137636 272DR HAS POSSIBLE CRACK AT RIVETS FOR SAFTEY PIN SUPPORT. PERFORMED CUTOUT, FABRICATED, PREPPED AND INSTALLED REPAIR FILLER AND DOUBLER TO CRACKED AREA OF 272DR AT SAFETY PIN SUPPORT AREA IAW PIEDMONT EO1-52-26-0359, ETD2026-145-013427 AND EMB 145 SRJul 9, 2026 · N942LL · Emb EMB145LR · Service DoorsSDR HNAA2026081400695Profile · dentedCARGO DOOR LOWER OUTER PROFILE IS DENTED WITH GOUGE IN IT. REMOVED AND REPLACED CARGO DOOR LOWER OUTER PROFILE IAW SRM 51-40-02, 51-20-01Jul 9, 2026 · N942LL · Emb EMB145LR · Cargo/Baggage DoorsSDR HNAA2026081400694Door Frame · crackedCARGO DOOR AFT FRAME IS CRACKED AND BENT AT LOWER SCREW HOLE. PERFORMED PERMANENT REPAIR OF CARGO DOOR AFT FRAME AT LOWER SCREW HOLE IAW ETD2026-145-012259 REV. A AND EO1-52-26-0335.Jul 9, 2026 · N942LL · Emb EMB145LR · Fuselage Main, StructureSDR HNAA2026081400693Web · crackedCARGO DOOR LOWER INNER SKIN IS CRACKED AND BENT LOWER AFT CORNER. REMOVED AND REPLACED UNSERVICEABLE CARGO DOOR LOWER INNER SKIN ( WEB ) IAW EMB 145 SRM 51-40-02, 51-20-01Jul 9, 2026 · N942LL · Emb EMB145LR · Fuselage Miscellaneous StructureSDR HNAA2026081400692Profile · bentCARGO LOWER L PROFILE IS BENT WHERE STAY HANDLE ATTACHES LOWER AFT CORNER. REMOVED AND REPLACED CARGO DOOR LOWER L PROFILE IAW EMB 145 SRM 51-40-02, 51-20-01Jul 9, 2026 · N942LL · Emb EMB145LR · Cargo/Baggage DoorsSDR IPXA2026080786372Seat Track · corrodedMDC SEAT TRACK BETWEEN FR27 AND FR28/ Y1959 SHOWS EVIDENCE OF CORROSION. INSTALLED NEW SEAT TRACK AND 2 EA SPLICE ON MDC AT FR27 TO FR32 Y1959 L/H SIDE IAW A300-600 SRM 53-10-16-201.Jul 9, 2026 · N144UP · Airbus A300F4622R · Fuselage, Seat/Cargo Attach FittingsSDR IPXA2026080981011Shear Tie · crackedCENTER FUSELAGE BASE FRAME FITTING C45 LH SIDE HAS A CRACK. VERIFIED, BASE FRAME FITTING FR45 LT REPLACED IAW EO-46789-JIC003 REV1, STEP 69 TO STEP 84.Jul 9, 2026 · N144UP · Airbus A300F4622R · Fuselage Internal Mounting StructureSDR IPXA2026080786502Adapter · corrodedFR 32, BTW Y1959 AND Y2462, CLS ADAPTER WITH CORROSION. REPLACED CLS ADAPTER, MDC, FR 32, BTW Y1959 AND Y2462, CLS ADAPTER IAW SRM 51-40-21-001Jul 9, 2026 · N144UP · Airbus A300F4622R · Fuselage, Seat/Cargo Attach FittingsSDR SWAA2026081266013Access Panel · delaminatedDELAMINATED ACCESS PANEL 194FL, LOWER BELLY FAIRING. REPAIRED THE ACCESS PANEL IAW SRM 51-70-05-2R-2, REPAIR 2.Jul 9, 2026 · N7732A · Boeing 7377BD · Aerodynamic FairingsSDR SWAA2026081272883Ring · corrodedCORROSION ON RING, FUEL TANK ACCESS PANEL 632HB, RT WING. REPLACED THE RING ON THE FUEL TANK ACCESS PANEL IAW SRM 51-10-02, ITEM 9.Jul 9, 2026 · N7732A · Boeing 7377BD · Wing Main, Frame StructureSDR SWAA2026081282730Support Angle · crackedCRACKED SUPPORT ANGLE, BS 500D, STR 28L IN THE FWD CARGO BAY. REPLACED THE SUPPORT ANGLE IAW SRM 51-10-02, ITEM 9, & DWG 143A7902, SHT 126, REV A.Jul 9, 2026 · N7732A · Boeing 7377BD · Fuselage Miscellaneous StructureSDR SWIA2026070976831Antenna · out of limitsCOMPLY WITH AFT ATG ANTENNA PERMANENT REPAIR REF. DRAWING 170-2365-02-RS AND M-93 ERJ175-53-26-03 (EA ERJ4111A-44). COMPLIED WITH AFT ATG ANTENNA PERMANENT REPAIR BY INSTALLING A DOUBLER AND FILLER REPAIR AT FR 82-83, STR 27-28L IAW DWG 170-2365-02-RS, AND M-9Jul 9, 2026 · N184SY · Emb ERJ170200LR · Standard Practices/StructuresSDR SWIA2026070976829Antenna · out of limitsCOMPLY WITH FWD ATG ANTENNA PERMANENT REPAIR IAW DRAWING 170-2365-02-RS AND M-93 ERJ175-53-26-03 (EA ERJ4111A-44). COMPLIED WITH FWD ATG ANTENNA PERMANENT REPAIR.IAW DRAWING 170-2365-02-315 APPENDIX B.Jul 9, 2026 · N184SY · Emb ERJ170200LR · Standard Practices/StructuresSDR SWIA2026070976826Antenna · out of limitsCOMPLY WITH RH SIDE ATG ANTENNA PERMANENT REPAIR REF. DRAWING 170-2365-02-RS AND M-93 ERJ175-53-26-03 (EA ERJ4111A-44) (C-CHECK RO 08/10/2026)COMPLIED WITH RH SIDE ATG ANTENNA PERMANENT REPAIR. REF DRAWING 170-2365-02-314 APPENDIX A.Jul 9, 2026 · N184SY · Emb ERJ170200LR · Standard Practices/StructuresSDR SWIA2026070976824Antenna · out of limitsCOMPLY WITH LT SIDE ATG ANTENNA PERMANENT REPAIR IAW DWG 170-2365-02-RS AND M-93 ERJ175-53-26-03 (EA ERJ4111A-44). COMPLIED WITH LT SIDE ATG ANTENNA PERMANENT REPAIR IAW DRAWING 170-2365-02-RS, AND M-93 ERJ175-53-26-03 (EA ERJ4111A-44).Jul 9, 2026 · N184SY · Emb ERJ170200LR · Standard Practices/StructuresSDR SIMA20260709002Glowstrip · fadedFRONT RIGHT CABIN EMERGENCY PHOTOLUMINESCENT STRIP FADED DOES NOT ILLUMINATE. RAR FRONT RIGHT CABIN PHOTOLUMINESCENT STRIP IAW AMM 33-50-51 MEL RESTORED.Jul 9, 2026 · N284JN · Emb ERJ170200LR · Emergency LightingSDR SWIA2026070976749Shear Tie · corrodedSHEAR TIE CORRODED IN AFT CARGO BAY, FR 76 BTWN S28R-29R. REMOVED AND REPLACED THE SHEAR TIE IAW SRM 51-40-08.Jul 9, 2026 · N604CZ · Emb ERJ170200LR · Fuselage Internal Mounting StructureSDR SWIA2026070976748Shear Tie · corrodedSHEAR TIE CORRODED IN AFT CARGO BAY, FR 75, BTWN S28L-29L. REMOVED & REPLACED THE SHEAR TIE IAW SRM 51-40-08.Jul 9, 2026 · N604CZ · Emb ERJ170200LR · Fuselage Internal Mounting StructureSDR SWIA2026070976745Shear Tie · corrodedSHEAR TIE CORRODED AT AFT CARGO FR 74, STR 29L-29R. REMOVED AND REPLACED SHEAR TIE IAW SRM 51-40-08.Jul 9, 2026 · N604CZ · Emb ERJ170200LR · Fuselage Internal Mounting StructureSDR SWIA2026070976744Shear Tie · corrodedSHEAR TIE CORRODED AT AFT CARGO FR 75, STR 29R-28R. REMOVED AND REPLACED THE SHEAR TIE IAW SRM 51-40-08.Jul 9, 2026 · N604CZ · Emb ERJ170200LR · Fuselage Internal Mounting StructureSDR SWIA2026070976743Shear Tie · corrodedSHEAR TIE CORRODED AT AFT CARGO FR 75, STR 29L-29R. REMOVED AND REPLACED THE SHEAR TIE, FR 75, STR 29L-29R IAW SRM 51-40-08.Jul 9, 2026 · N604CZ · Emb ERJ170200LR · Fuselage Internal Mounting StructureSDR SWIA2026070976741Shear Tie · corrodedSHEAR TIE CORRODED AT AFT CARGO FR 74, STR 28R-29R. REMOVED AND REPLACED SHEAR TIE IN AFT CARGO FR 74 STR 28R-29R. IAW SRM 51-40-08. SEE CONTINUE CARD FOR WORK PERFORMED.Jul 9, 2026 · N604CZ · Emb ERJ170200LR · Fuselage Internal Mounting StructureSDR SWAA2026080540700Skin · crackedCRACK LOWER SURFACE OF RT WING LEADING EDGE SLAT 7 NOSE SKIN AT ACTUATOR LOCATION AROUND THE FASTENER. PERFORMED A REPAIR ON LOWER SURFACE OF LEADING EDGE SLAT 7 NOSE SKIN IAW SRM 57-42-01-2R, REPAIR 8, & DWG 114A5020, REV A, SHEET 38.Jul 9, 2026 · N953WN · Boeing 7377H4 · Leading Edge DevicesSDR SWAA2026080580743Skin · crackedCRACKED LOWER SURFACE OF LEADING EDGE SLAT 6 NOSE SKIN AT THE ACTUATOR LOCATION. AROUND FASTENER. PERFORMED A REPAIR ON THE LOWER SURFACE OF LEADING EDGE SLAT 6 NOSE SKIN IAW SRM 51-40-02, AND SRM 57-42-01-2R-8, REPAIR 8, AND DWG 114A5030, REV A, SHEET 2.Jul 9, 2026 · N953WN · Boeing 7377H4 · Leading Edge DevicesSDR IPXA2026072481022Shear Tie · crackedCENTER FUSELAGE BASE FRAME FITTING C46 LH SIDE HAS A CRACK. ACCOMPLISHED IAW EO-46789-JIC007 REV2 REPAIR-BASE FRAME FITTING, FR46 TO FR 46 (FR46),LH SIDE (SB A300-57-6177) T3F18E0095MF8 STEP 54 - 64.Jul 9, 2026 · N144UP · Airbus A300F4622R · Fuselage Internal Mounting StructureSDR IPXA2026071185916Adapter · corrodedMDC CLS AT FR28/Y0 SHOWS EVIDENCE OF CORROSION. INSTALLED NEW CLS ADAPTER AT MDC FR28/Y0 IAW SRM 51-40-21.Jul 9, 2026 · N144UP · Airbus A300F4622R · Fuselage Main, StructureSDR AALA202608044980Floor Support · corrodedAIRCRAFT IN BASE MAINTENANCE: RIGHT AFT WET AREA, FLOOR SUPPORT AT STATION 947+1", RBL 26 HAS INTERGRANULAR CORROSION (AFT SIDE OF INBOARD AFT LAV MOUNT). MAINTENANCE REPLACED INTERCOSTAL AT STATION 947+1", RBL 26 PER AARD 51-00-05-1.Jul 9, 2026 · N957NN · Boeing 737823 · Fuselage Miscellaneous StructureSDR 2026FA0000615Hydraulic Line · leakingON DESCENT LT AND RT "HYD LOW FLOW" ANNUNCIATORS START FLICKERING THEN WENT FULLY ON. EXTENDED LANDING GEAR BUT ONLY LT MAIN WENT DOWN AND LOCKED. BLEW THE LANDING GEAR BLOWDOWN BOTTLE, HEARD THE BOTTLE BLOW BUT HAD NO FURTHER DOWN AND LOCKED INDICATION. AFTERJul 9, 2026 · N441SK · Cessna 441 · Hydraulic System, MainSDR R61A2026080200216Skin · damagedLIGHTNING STRIKE FWD FUSELAGE BETWEEN FRAMES 11-12 STRINGERS 24R-23R.MECHANIC REMOVED DAMAGE AND PERFORMED PERMANENT REINFORCING REPAIR AT FWD FUSELAGE BETWEEN FRAMES 11-12 STRINGERS 24R-23R IAW ETD2026-170-012519 REV. AJul 9, 2026 · N865RW · Emb ERJ170100SE · Fuselage Main, Plate/Skin