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 2026FA0000717Stiffener · crackedRIGHT WING FWD LWR I/B SKIN, FWD STIFFENER CRACKED. REPLACED WITH NEWJul 14, 2026 · N755G · Piper PA28181 · Wing Miscellaneous StructureSDR 2026FA0000705Skin · crackedRIGHT WING FWD WING WALK SKIN CRACKED ON CORRUGATED SKIN. REPLACED WING WALK CORRUGATED SKIN ASSY WITH NEWJul 14, 2026 · N755G · Piper PA28181 · Wing, Plate/SkinSDR IPXA2026082657227Bracket · corrodedHORIZONTAL STAB, RT LOWER APRON ATTACH AREA, NR 10 BRACKET, CORROSION AROUND ALL SCREW HOLES. INSTALLED NEW BRACKET HORIZONTAL STAB, RT LOWER NR 10 BRACKET IAW SRM 51-40-21-001.Jul 14, 2026 · N144UP · Airbus A300F4622R · Horizontal Stabilizer Miscellaneous StructureSDR IPXA2026082657391Bracket · corrodedHORIZONTAL STAB, LT UPPER APRON ATTACH AREA, NR 7 BRACKET WITH CORROSION. INSTALLED A NEW BRACKET NR 7, IAW SRM 51-40-21-001.Jul 14, 2026 · N144UP · Airbus A300F4622R · Horizontal Stabilizer Miscellaneous StructureSDR IPXA2026082657322Bracket · damagedHORIZONTAL STAB, LEFT LOWER APRON ATTACH AREA, NR 5 BRACKET, 1 SCREW HOLE WITH DRILL HOLE DAMAGE. INSTALLED BRACKET NR 5 IN HORIZONTAL STAB, LT LOWER APRON. IAW SRM 51-40-21-001 AND SRM 55-11-28, PAGE 2, PAGE 3.Jul 14, 2026 · N144UP · Airbus A300F4622R · Horizontal Stabilizer Miscellaneous StructureSDR IPXA2026091160874Skin · crackedNR 1 PYLON, PRECOOLER AREA, INTERNAL LT SKIN, AT RIB 4, WITH CRACK. INSTALLED RIVETS (7EA) STEP 10 AND (1EA) STEP 1 AT NR 1 PYLON, PRECOOLER AREA, INTERNAL LT SKIN, AT RIB 4 IAW SRM 51-40-21-001.Jul 14, 2026 · N136UP · Airbus A300F4622R · Nacelle/Pylon, Plate/SkinSDR IPXA2026091160860Skin · crackedNR 1 PYLON, PRECOOLER AREA, INTERNAL RT SKIN, AT RIB 4, WITH CRACK. INSTALLED RIVETS (8EA) AT NR 1 PYLON, PRECOOLER AREA, INTERNAL LT SKIN, AT RIB 4 IAW SRM 51-40-21-001.Jul 14, 2026 · N136UP · Airbus A300F4622R · Nacelle/Pylon, Plate/SkinSDR IPXA2026090362282Attach Fitting · corrodedCEILING PANEL ATTACHMENT FITTING AT FR 54, BTW Y953 AND Y1456 IS CORRODED.Jul 14, 2026 · N136UP · Airbus A300F4622R · Fuselage Miscellaneous StructureSDR IPXA2026082749871Drain Pan · corrodedAFT CARGO COMP. FLOOR LEVEL RH BETWEEN FR.59. & FR.60 UNDER FLOOR PANEL 151MG DRAINAGE PLATE COVER STRAP CORRODED (2SPOTS). PART ATTACHED TO DRAIN PAN ASSEMBLY IAW A300-600 SRM 51-40-21 AND 51-24-00.Jul 14, 2026 · N136UP · Airbus A300F4622R · Fuselage Miscellaneous StructureSDR IPXA2026082749194Drain Pan · corrodedAFT CARGO COMP. FLOOR LEVEL BETWEEN FR.59. & FR.60. UNDER FLOOR PANEL 152MG DRAINAGE PLATE COVER STRAP CORRODED (2SPOTS). PART ATTACHED TO DRAIN PAN ASSEMBLY IAW SRM 51-40-21 AND 51-24-00.Jul 14, 2026 · N136UP · Airbus A300F4622R · Fuselage Miscellaneous StructureSDR IPXA2026082748728Drain Pan · corrodedAFT CARGO BAY FLOOR LEVEL BETWEEN FR.59 & FR.60 DRAINAGE PLATE COVER STRAP CORRODED UNDER RT FLOOR PANEL 152NG. PART ATTACHED TO DRAIN PAN ASEMBLY IAW SRM 51-40-21, AND 51-24-00.Jul 14, 2026 · N136UP · Airbus A300F4622R · Fuselage Miscellaneous StructureSDR IPXA2026082148918Floor Support · corrodedAFT CARGO BAY, FLOOR LEVEL AFT FLOOR PANEL 152NG STRUCUTURE CORRODED. INSTALLATION OF SPLICE AT AFT CARGO COMP IAW SRM 51-40-21.Jul 14, 2026 · N136UP · Airbus A300F4622R · Fuselage Miscellaneous StructureSDR SWAA2026090262944Floorbeam · corrodedSTA 947 FLOOR BEAM HAS PITTING AND CORROSION AT LBL 51 REMOVED CORROSION ON STA.947 FLOOR BEAM UPPER CHORD AT LBL 51 MEASURED CORROSION REMOVAL TO BE 0.055" DEEP REMAINING THICKNESS IS 0.125" (ORIGINAL THICKNESS IS 0.180") FLOOR BEAM UPPER CHORD IS OUT OF LIMIJul 14, 2026 · N8706W · Boeing 7378 · Fuselage Main, Floor BeamSDR REXA2026082401556Stiffener · corrodedAFTER TOP PANEL REMOVAL, CORROSION ON STIFFERNERS OF THE TOP PANEL WAS FOUND ON FWD PASSENGER DOOR. STIFFENERS (3 EAS) WERE REPLACED AND STIFFERNERS (2 EAS) WERE REMOVED AND CLEANED AND AFTER STIFFENER WERE CLEANED AND DVI WAS PERFORMED AND NOT CORROSION WAS FJul 14, 2026 · N928XJ · Cndair CL6002D24 · Passenger/Crew DoorsSDR HNAA2026082400750Skin · gougedCARGO DOOR INNER SKIN IS GOUGED AT VB4 AND HB4. REMOVED AND REPLACED CARGO DOOR INNER SKIN IAW SRM 51-40-02.Jul 14, 2026 · N935AE · Emb EMB145LR · Cargo/Baggage DoorsSDR SWAA2026081950712Floor Support · corrodedSTA 948 INTERCOSTAL THAT ATTACHES AFT OF FLOORBEAM OF 947 AT LBL 51 HAS PITTING AND CORROSION. LOCATED AND DRILLED NEW INTERCOSTAL PER SRM 51-40-05 AND DRAWING 147A5650. INSTALL WILL BE COMPLETED ON TASK CARD TTG8Q01D6ER9 STEP 7. CORROSION OUT OF LIMITS PEJul 14, 2026 · N8706W · Boeing 7378 · Fuselage Miscellaneous StructureSDR SWAA2026081956254Floorbeam · corrodedBS 947 FLOORBEAM HAS PITTING AND CORROSION AT RBL 51. REMOVED CORROSION ON THE FLOORBEAM UPPER TEE, MEASURED CORROSION REMOVAL TO BE 0.070" DEEP REMAINING THICKNESS IS 0.110" (ORIGINAL THICKNESS IS 0.180") THE FLOORBEAM UPPER TEE OUT OF LIMITS IAW SRM 53-70-5Jul 14, 2026 · N8706W · Boeing 7378 · Fuselage Main, Floor BeamSDR HNAA2026081900736Door Frame · corrodedSERVICE DOOR AFT FRAME #22 CORRODED. REPAIRED IAW SRM 53-00-04Jul 14, 2026 · N939AE · Emb EMB145LR · Fuselage Main, StructureSDR SWAA2026081789106Plate · crackedCRACKED CORRUGATED PLATE T-E, IRSS 213, LT WING. REPLACED THE CORRUGATED PLATE IAW SRM 51-10-02, ITEM 9, SRM 51-40-02, DWG 115A2713, SHT 6, REV A, & DWG: 115A2001, SHT 78, REV. A THE LENGTH OF CRACK IS: 1.409 TOOL USED: DIGITAL CALIPER P/N: 500-197-30 S/N: Jul 14, 2026 · N8651A · Boeing 7378H4 · Wing Main, Frame StructureSDR SWAA2026081744521Web · crackedCRACKED WEB, ORSS 275, LT WING T/E. REPLACED THE WEB, IAW SRM 51-10-02, ITEM 9, SRM 51-40-02, & DWG 115A2512, SHEET 16, REV-.Jul 14, 2026 · N8651A · Boeing 7378H4 · Wing Miscellaneous StructureSDR SWAA2026081795946Light · deterioratedDETERIORATED PHOTOLUMINESCENT STRIP IN PAX CABIN. REPLACED THE PHOTOLUMINESCENT STRIP IAW AMM 33-51-15-400-802, STEP 1.E.(1), & DWG 33500007, REV 2, SHEET 2.Jul 14, 2026 · N499WN · Boeing 7377H4 · Emergency LightingSDR HNAA2026081700726Gusset · crackedSERVICE DOOR AFT GUSSET CORRODED BTW FR 22-23. R & R THE GUSSET IAW SRM 51-40-02.Jul 14, 2026 · N939AE · Emb EMB145LR · Fuselage Miscellaneous StructureSDR HNAA2026081400722Floor Support · corrodedRT OMEGA BEAM CORRODED AT BTW FR60-61. REPAIRED IAW SRM 53-24-10Jul 14, 2026 · N939AE · Emb EMB145LR · Fuselage Miscellaneous StructureSDR HNAA2026081400723Floor Support · corrodedCTR OMEGA BEAM CORRODED BTW FR60-61. REPAIRED IAW SRM 53-24-10Jul 14, 2026 · N939AE · Emb EMB145LR · Fuselage Miscellaneous StructureSDR HNAA2026081400720Floor Support · corrodedLEFT OMEGA BEAM IB FLANGE CRACKED AT FR21. REPAIRED IAW ETD2026-145-012350 AND EO 1-53-26-0343Jul 14, 2026 · N939AE · Emb EMB145LR · Fuselage Miscellaneous StructureSDR HNAA2026081400708Shear Tie · crackedSHEAR CLIP AT FR 24 BETWEEN STRINGER 15R AND 16R IS CRACKED. REMOVED AND REPLACED SHEAR CLIP AT FR 24 BETWEEN STRINGERS 15R AND 16R IAW EMB 145 SRM 51-40-02.Jul 14, 2026 · N942LL · Emb EMB145LR · Fuselage Internal Mounting StructureSDR HNAA2026081400707Shear Tie · crackedSHEAR TIE AT FR 24 BETWEEN STRINGER 14R AND 15R IS CRACKED. FURTHER INVESTIGATION SHOWS ACTUAL STR LOCATION OF CRACKED SHEAR CLIP TO BE BETWEEN STR 16-17R, NOT BETWEEN 14-15R. REMOVED AND REPLACED SHEAR CLIP AT FR 24 BETWEEN STRINGERS 16R AND 17R IAW EMB 145 Jul 14, 2026 · N942LL · Emb EMB145LR · Fuselage Internal Mounting StructureSDR HNAA2026081400668Crossbeam · corrodedCTR CROSSBEAM AT FR 20 IS CORRODED. R & R CROSSBEAM IAW SRM 51-40-02Jul 14, 2026 · N939AE · Emb EMB145LR · Fuselage Main, StructureSDR HNAA2026081300665Floor Support · crackedCTR OMEGA BEAM IB ANGLE CRACKED AT BTWFR20-21. RAR ANGLE IAW SRM 51-40-02Jul 14, 2026 · N939AE · Emb EMB145LR · Fuselage Miscellaneous StructureSDR CALA2026081318569Spar Web · corrodedCORROSION AT THE RT OUTER WING SPAR WEB AT FUEL BOOST PUMP IAW ECRA 5720-03656. PERFORMED AN INSPECTION OF REPAIR TO RT WING FRONT SPAR WEB AT FUEL BOOST PUMP CUTOUT ON ACFT IAW PART 2 OF LATEST REVISION OF ECRA 5720-03656. ACCOMPLISHED INTERIM REPAIR PERFORMJul 14, 2026 · N14249 · Boeing 737824 · Wing SparSDR CALA2026081118476Bulkhead Web · crackedCRACK FOUND IN LT WHEEL WELL AT UPPER SECTION OF FWD WALL (BS 663) IAW AAR N/R 100048007, ACCOMPLISHED REPAIR (CATEGORY B) AT LT VERTICAL PRESSURE DECK WEB IAW SRM 57-10-10-2R-3 REPAIR 3 ALTERNATIVE 2 PARAGRAPH 5 FIG 204. ACCOMPLISHED REPAIR (CATEGORY B) AT Jul 14, 2026 · N39297 · Boeing 737824 · Fuselage Main, BulkheadSDR SWAA2026081107566Battery Pack · dischargedFOUND SEVERAL EMERGENCY LIGHTS INOPERATIVE AT FWD SIDE OF CABIN. RESEATED FWD BATTERY PACK CHARGED BATTERY & PERFORMED SATISFACTORY OPS CHECK IAW AMM 33-51-06. RESEATED FWD EMERGENCY BATTERY PACK, CHARGED BATTERY & PERFORMED SATISFACTORY OPS CHECK IAW AMM 3Jul 14, 2026 · N489WN · Boeing 7377H4 · Emergency LightingSDR IPXA2026081160860Skin · crackedNR 1 PYLON, PRECOOLER AREA, INTERNAL RT SKIN, AT RIB 4, WITH CRACK. EWIS, NR 1 PYLON PRECOOLER CAVITY IAW ESPM 20-54-50-02.Jul 14, 2026 · N136UP · Airbus A300F4622R · Nacelle/Pylon, Plate/SkinSDR IPXA2026081160882Rib · crackedNR 1 PYLON, RIB 3A WITH CRACK.Jul 14, 2026 · N136UP · Airbus A300F4622R · Nacelle/Pylon, Frame/Spar/RibSDR DALA2026081004594Skin · corrodedFWD LAV TANK EXHAUST PORT HAS CORROSION. REPAIRED FWD LAV EXHAUST PORT IAW SRM 53-60-01-2R-3 (8393110) (AIRCRAFT GROUNDED)Jul 14, 2026 · N193DN · Boeing 767332 · Fuselage Main, Plate/SkinSDR SWAA2026080553996Frame · crackedCRACKED FRAME, BS 312, S5L & 6L IN THE FWD GALLEY AREA. REPAIRED FRAME IAW M-22-153-01244, SEE TTG8Q01D738K. COMPLETED TASK.Jul 14, 2026 · N953WN · Boeing 7377H4 · Fuselage Main, FrameSDR SWAA2026080502010Web · crackedCRACKED SUPPORT WEB, OTBD FAN COWL UPPER POSITION ON NR 2 ENGINE. REPLACED THE SUPPORT WEB AND FASTENERS IAW SRM 51-40-02-0G-0, SRM 51-10-02-0G-0, ITEM 9, & 71-13-30.Jul 14, 2026 · N953WN · Boeing 7377H4 · Nacelle/Pylon Miscellaneous StructureSDR SCNA20260716307SSmoke Goggles · missingFWD FACING SUPERNUMERARY SEATS MISSING SMOKE GOGGLES ( SUPERNUMERARY SEATS ) PLACED SMOKE GOOGLE ON EACH FWD FACING SEATS IAW AMM 25-64-00 THIS CLEARS MEL 25-31.Jul 14, 2026 · N5153A · Boeing 73783N · Emergency EquipmentSDR SWAA2026080414529Strap · out of toleranceE/E COMPARTMENT, BS 328 BETWEEN S20R TO S22R, FRAME STRAP CONFIGURATION DOES NOT MATCH FIG. 15 PER EO 5311-I-17336-NG REF FAULT TTG8Q0157B6V AS PER EA 26-153-01902 THE CONFIGURATION IS ACCEPTABLE. VERIFIED CORRECTIVE ACTION 1Jul 14, 2026 · N495WN · Boeing 7377H4 · Fuselage Main, StructureSDR IPXA2026073161872Adapter · corrodedMDC AT FR57.1, Y100 BY FLOOR PANEL 251LG, CLS HAS CORROSION, DOT 78-18. REMOVED CLS ADAPTER AT MDC AT FR58, Y100 BY FLOOR PANEL 251LG I.A.W. A300-600 SRM 51-40-20. INSTALLED NEW CLS ADAPTER P/N: A53275402202 IAW TRAVELER #: T26/1871958 ON MDC AT FR57.1, Y100 BJul 14, 2026 · N136UP · Airbus A300F4622R · Fuselage Miscellaneous StructureSDR CALA2026080318232Skin · nickedNICK WAS FOUND OUT OF LIMITS ON FUSELAGE SKIN BETWEEN BS 500AD - 500E, STR 27R - 26R. PERFORMED REPAIR AT EXTERNAL FUSELAGE SKIN BETWEEN STA 500D 500E AND STR 27R / STR26R - ALL WORKS WERE ACCOMPLISHED IAW SRM 53-00-01-2R-1, SRM-51-20-01-0G-0,AMM 20-60-07-913Jul 14, 2026 · N26232 · Boeing 737824 · Fuselage Main, Plate/SkinSDR R61A2026080200215Shear Tie · gougedSHEAR CLIP GOUGED IN RADIUS AT FR 12 STRS 6R - 7R. FABRICATED AND INSTALLED NEW SHEAR CLIP IAW SRM 51-40-08.Jul 14, 2026 · N865RW · Emb ERJ170100SE · Fuselage Internal Mounting StructureSDR SWAA2026073106687Attach Angle · crackedLEFT BS 663 UPPER ATTACH ANGLE IS CRACKED ON VAPOR BARRIER, LBL 13, WL 167.68, A CRACK FOUND TO BE OUT OF LIMITS IAW SRM 57-10-10-1A-2. REPAIRED THE LT BS 663 UPPER ATTACH ANGLE ON VAPOR BARRIER, WL167.68 IAW EA-M-157-01480.Jul 14, 2026 · N8545V · Boeing 7378H4 · Fuselage Main, Attach FittingsSDR SWAA2026073149054Attach Angle · crackedRIGHT BS 663 UPPER ATTACH ANGLE IS CRACKED ON VAPOR BARRIER RBL 8, WL 167.68 CRACK FOUND TO BE OUT OF LIMITS IAW SRM 57-10-10-1A-2. REPAIRED RT BS 663 UPPER ATTACH ANGLE ON VAPOR BARRIER WL167.68, IAW EA-M-157-01481.Jul 14, 2026 · N8545V · Boeing 7378H4 · Fuselage Main, Attach FittingsSDR IPXA2026073057244Support · corrodedHORIZONTAL STAB, R/H LOWER APRON ATTACH AREA, NR 4 BRACKET, CORROSION AROUND 4 SCREW HOLES. LOCATED AND DRILL NEW SUPPORT RT HORIZONTAL STAB LOWER APRON ATTACH AREA, NR 4 BRACKET IAW SRM 51-40-44-001. INSTALLED HORIZONTAL STAB, RT APRON PANEL 343AR IAW AMM 55Jul 14, 2026 · N144UP · Airbus A300F4622R · Horizontal Stabilizer Miscellaneous StructureSDR IPXA2026073057393Support · corrodedHORIZONTAL STAB, L/H UPPER APRON ATTACH AREA, NR 8 BRACKET WITH CORROSION. RESTORED SURFACE PROTECTION.APPLIED TREATMENT AND PRIMER IAW SRM 51-21-10-001.APPLIED TOPCOAT IAW SRM 51-75-10-201Jul 14, 2026 · N144UP · Airbus A300F4622R · Horizontal Stabilizer Miscellaneous StructureSDR IPXA2026073057350Support · corrodedHORIZONTAL STAB, L/H UPPER APRON ATTACH AREA, #10 BRACKET WITH CORROSION. RESTORED SURFACE PROTECTION.APPLIED TREATMENT AND PRIMER IAW SRM 51-21-10-001.APPLIED TOPCOAT IAW SRM 51-75-10-201.Jul 14, 2026 · N144UP · Airbus A300F4622R · Horizontal Stabilizer Miscellaneous StructureSDR IPXA2026073057348Support · corrodedHORIZONTAL STAB, L/H UPPER APRON ATTACH AREA, NR 9 BRACKET WITH CORROSION. RESTORED SURFACE PROTECTION.APPLIED TREATMENT AND PRIMER IAW SRM 51-21-10-001.APPLIED TOPCOAT IAW SRM 51-75-10-201Jul 14, 2026 · N144UP · Airbus A300F4622R · Horizontal Stabilizer Miscellaneous StructureSDR IPXA2026072957272Support · corrodedHORIZONTAL STAB, R/H UPPER APRON ATTACH AREA, ONE BRACKET WITH CORROSION. OUT OF SEQUENCE: STEP 2. INSTALLED SUPPORT, USING 04 BOLTS P/N EN611V3-7, BCH 4491492 AND 04 COLLARS. IAW SRM 51-40-21-001Jul 14, 2026 · N144UP · Airbus A300F4622R · Rudder StructureSDR 1Q2R2026072920097Stringer · corrodedAT BS 295, STGR 19 LT FOUND TO BE POSSIBLE CORROSION ON BRACKET. PERFORMED PERMANENT REPAIR IAW RFTS-129854 REV. 0, AND REO 670-53-21-2936, REV--.Jul 14, 2026 · N523AE · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer