Service difficulty reports

1,770,511 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 DALA2026100505479Pump · failedDE - DUE TO GREEN SYSTEM HYDRAULIC QTY LOSS. REPLACED #1 AND #2 ENG EDP. PERFORMED ALTERNATE FLUSHING PROCEDURES AND REPLACED ALL ASSOCIATED FILTERS. (LP# 9333162, 9333163, 9333164, 9333170; AIRCRAFT WAS GROUNDED)Oct 3, 2026 · N511DN · Airbus A350941 · Hydraulic Pump (Electric/Engine), MainSDR CALA2026100520103Lens · missingLH RETRACTABLE LANDING LIGHT LENS FOUND MISSING. LEFT RETRACTABLE LDG LIGHT LENS SEEMS LOOSE REF AMM 33-42-02. REPLACED LH RETRACTABLE LDG LIGHT RETAINER ASSEMBLY DUE TO MISSING LENS, VERIFIED OPS OF LIGHT.Oct 3, 2026 · N25705 · Boeing 737724 · Exterior LightingSDR CALA2026100520102Fuel Cap · missingMISSING FUEL CAP UPON ARRIVAL. INSTALLED A FUEL CAP.Oct 3, 2026 · N823UA · Airbus A319131 · Fuel StorageSDR CALA2026100520099Adiru · faultyIRS RT FAULT FOLLOWING FIM 34-21 TASK 803, PERFORMED BITE TEST AND FAULT MESSAGES ATTATCHED IN IMAGES. REMOVED AND REPLACED R ADIRU REF. AMM TASK 34-21-01-000-801 AND TASK 34-21-01-400-801. INSTALLATION TEST PASSED.PARTS USED: 60-3421-9-0001,QTY :1 POS - 2 MFGOct 3, 2026 · N27421 · Boeing 737924ER · Attitude and Direction Data SystemSDR VNAA2026100526201Target · missingGEAR DISAGREE ON CLIMB OUT C/A FOUND NLG PROX SENSOR TARGET MISSING. INSTALLED RH NLG CTR PROX SENSOR TARGET.Oct 3, 2026 · N635NN · Cndair CL6002D24 · Landing Gear Position and WarningSDR JR2R20261003051Heat Shield · chafedLEFT AFT PYLON FAIRING HEAT SHIELD HAS EVIDENCE OF CHAFING. REPAIRED PER ETD.Oct 3, 2026 · N85320 · Emb ERJ170200LL · Nacelle/Pylon, Main FrameSDR JR2R20261003861Beam · corrodedAFT WET AREA, WARDROBE BEAM AT FR82-FR84 IS CORRODED. REPAIRED PER ETD.Oct 3, 2026 · N85320 · Emb ERJ170200LL · Fuselage Main, StructureSDR JR2R20261003862Floorbeam · corrodedAFT WET AREA, FR84 CROSSBEAM AT RBL25-RBL31 IS CORRODED. REPAIRED PER ETD.Oct 3, 2026 · N85320 · Emb ERJ170200LL · Fuselage Main, Floor BeamSDR JR2R20261003863Seat Track · corrodedAFT WET AREA, SEAT TRACK END LUG AT FR84 RBL10 IS CORRODED. REPAIRED PER ETD.Oct 3, 2026 · N85320 · Emb ERJ170200LL · Fuselage, Seat/Cargo Attach FittingsSDR JR2R20261003829Floor Support · corrodedFORWARD WET AREA, RBL 10 FLOOR SUPPORT FR 12-FR 14 IS CORRODED. REPAIRED PER ETD.Oct 3, 2026 · N85320 · Emb ERJ170200LL · Fuselage Miscellaneous StructureSDR JR2R20261003715Door Frame · gougedFORWARD E-BAY, RT FUSELAGE FRAME FOR DOOR CUTOUT IS GOUGED. REPAIRED PER ETD.Oct 3, 2026 · N85320 · Emb ERJ170200LL · Fuselage Main, StructureSDR JR2R20261003833Crossbeam · corrodedFORWARD WET AREA, CROSSBEAM AT FR17 RBL13-RBL40 IS CORRODED. REPAIRED PER SRM.Oct 3, 2026 · N85320 · Emb ERJ170200LL · Fuselage Main, StructureSDR JR2R20261003830Floorbeam · corrodedFORWARD WET AREA, RBL10 FR17 EXISTING REPAIR DOUBLER ON BEAM IS CORRODED. REPAIRED PER SRM.Oct 3, 2026 · N88327 · Emb ERJ170200LL · Fuselage Main, Floor BeamSDR JR2R20261003831Floorbeam · corrodedFORWARD WET AREA, FR14 CROSSBEAM AT RBL10-RBL30 IS CORRODED. REPAIRED PER SRM.Oct 3, 2026 · N85320 · Emb ERJ170200LL · Fuselage Main, Floor BeamSDR IXXA2026100302Keelbeam · crackedLH KEEL BEAM WEB CRACKEDOct 3, 2026 · N313AZ · Boeing 767338 · Fuselage Main, KeelSDR IXXA2026100301Keelbeam · crackedKEEL BEAM WEB CRACKEDOct 3, 2026 · N313AZ · Boeing 767338 · Fuselage Main, KeelSDR SWIA2026100277850Seat Track · corrodedRH LONGITUDINAL SEAT TRACK AT FR74 AND Y 1075 HAS CORROSION C-CHECK RO 11022026REMOVED AND REPLACED AFT RH SEAT TRACK PN 170-86082-005, PO 339538 IAW EMB-175, SRM 51-40-08 THIS DOES NOT AFFECT WEIGHT AND BALANCEOct 2, 2026 · N150SY · Emb ERJ170200LR · Fuselage, Seat/Cargo Attach FittingsSDR SWIA2026100277847Floorbeam · corrodedFLOOR BEAM AT FR84 AND Y 2275 HAS CORROSION C-CHECK RO 11022026REMOVED AND REPLACED FLOOR BEAM AT FR84 AND Y 2275 PER E175 SRM 51-40-08 NO FURTHER ACTION REQUIRED NO CHANGE IN WEIGHT AND BALANCEOct 2, 2026 · N150SY · Emb ERJ170200LR · Fuselage Main, Floor BeamSDR SWIA2026100277845Seat Track · corrodedLH LONGITUDINAL SEAT TRACK AT FR81-FR83 AND Y -1075 HAS CORROSION AT 3 LOCATIONS C-CHECK RO 11022026REMOVED AND REPLACED LH LONGITUDINAL SEAT TRACK PN 170-86081-PO 321090 AT FR81-FR83 AND Y -1075 PER EMBRAER 175 SRM 51-40-08 THIS DOES NOT AFFECT WEIGHT AND BOct 2, 2026 · N150SY · Emb ERJ170200LR · Fuselage, Seat/Cargo Attach FittingsSDR SWIA2026100277842Floor Support · corrodedAFT WET AREA FLOOR BEAM AT FR87-FR88 AND Y 1075 HAS CORROSION C-CHECK RO 11022026REMOVED AND REPLACED AFT WET AREA FLOOR BEAM AT FR87-FR88 AND Y 1075 IAW E-175 SRM 51-40-08 NO CHANGE IN WEIGHT AND BALANCEOct 2, 2026 · N150SY · Emb ERJ170200LR · Fuselage Miscellaneous StructureSDR SWAA2026110217205Angle · missingMISSING ANGLE, EXTERNAL SKIN FRONT SPAR BTWN WS 458.5 & WS 512, RT WING. INSTALLED NEW ANGLE LOCATED EXTERNAL SKIN FRONT SPAR LOCATED BTW WS458.50 AND WS512 AT RT WING IAW B737-8 MAX SOPM 20-50-12 DRAWING 12A3500 REVISION A AND BAC 5010.Oct 2, 2026 · N8704Q · Boeing 7378 · Wing Main, Frame StructureSDR SWAA2026110281218Attach Angle · crackedCRACK INDICATION FOUND ON RT BS 663 VAPOR BARRIER ATTACH ANGLE AT RBL 33. REPAIRED IAW EA M-26-157-01481.Oct 2, 2026 · N8555Z · Boeing 7378H4 · Fuselage Main, Attach FittingsSDR SWAA2026103051101Scuff Plate · crackedAFT CARGO DOOR ENTRY, AFT CORNER SCUFF PLATE WAS CRACKED. WELDED THE SCUFF PLATE IAW SRM 53-60-15-2R-1, STEP 4.B.(5).Oct 2, 2026 · N8736J · Boeing 7378 · Fuselage Miscellaneous StructureSDR SWAA2026102930536Baffle · crackedFWD CARGO BAY BAFFLE, BS 500B - 500C, RBL 25, WL 156 CRACKED. REMOVED AND REPLACED THE BAFFLE IAW SRM 51-40-02, & DWG 143A7505, REV -.Oct 2, 2026 · N8655D · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR IPXA2026102968888Strap · corrodedLEFT HORIZONTAL STAB TIP HAS FITTING TO ATTACH BONDING STRAP WITH CORROSION.Oct 2, 2026 · N404UP · Boeing 75724APF · Horizontal Stabilizer Miscellaneous StructureSDR 1Q2R2026102820248Spar · damagedLEFT SIDE OF THE VERTICAL STABILIZER UPPER BOLT HOLE FOR L/E IS ELONGATED. PERFORMED PERMANENT REPAIR IAW RFTS-131148, REV. 0, AND REO 670-55-31-218, REV-.Oct 2, 2026 · N706PS · Cndair CL6002C10 · Vertical Stabilizer, Spar/RibSDR SWAA2026102782520Support Fitting · crackedCRACKED SUPPORT FITTING, BS 947.5, WL 152.7, STRINGER 26L IN THE AFT CARGO BAY. FAULT RESOLVED ON OTHER FAULT. SEE FAULT TTG8Q01ETDVW.Oct 2, 2026 · N273WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR U5QA202610020182Engine · flamed outDURING TAXI, L ENG FLAMEOUT EICAS. ENG AUTO SHUTDOWN. MX C/A: MULTIPLE DAYS OF TROUBLESHOOTING, BORESCOPE INSPECTIONS, ETC. ALONGSIDE ROLLS ROYCE. COULD NOT IDENTIFY ISSUE(S). DECIDED TO LH R&R ENGINE. AWAITED RENTAL AVAILABILITY, R&R LH ENGINE WITH RENTALOct 2, 2026 · N500VJ · Bombdr BD7001A11 · Engine (Turbine/Turboprop)SDR IPXA2026102161735Fitting · out of limitsHOLE N HOLE SIZES MEASURES DIFFERENT FROM THE EO-90930-REQ2 REV 4; FWD FITTING .3780", SPLICE .2840, AFT FITTING .3780". ACCOMPLISHED THE REPAIR PER EO-98948-REQ1 AND EA 300-5710-27-A4658, REV. _.Oct 2, 2026 · N127UP · Airbus A300F4622R · Wing Main, Frame StructureSDR IPXA2026102161645Fitting · out of limitsHOLE M HOLE SIZES MEASURES DIFFERENT FROM THE EO-90930-REQ2 REV 4; FWD FITTING .4530", SPLICE .3070, AFT FITTING .4580". ACCOMPLISHED THE REPAIR PER EO-98948-REQ1 AND EA 300-5710-27-A4658, REV. _.Oct 2, 2026 · N127UP · Airbus A300F4622R · Fuselage Main, StructureSDR IPXA2026102161581Fitting · out of limitsHOLE L HOLE SIZES MEASURES DIFFERENT FROM THE EO-90930-REQ2 REV 4; FWD FITTING .3830", SPLICE .2810, AFT FITTING .3840". ACCOMPLISHED THE REPAIR PER EO-98948-REQ1 AND EA 300-5710-27-A4658, REV. _.Oct 2, 2026 · N127UP · Airbus A300F4622R · Fuselage Main, StructureSDR IPXA2026102161504Fitting · out of limitsHOLE H HOLE SIZES MEASURES DIFFERENT FROM THE EO-90930-REQ2 REV 4; SPLICE .3480, AFT FITTING .4050".ACCOMPLISHED THE REPAIR PER EO-98948-REQ1 AND EA 300-5710-27-A4658, REV. _.Oct 2, 2026 · N127UP · Airbus A300F4622R · Fuselage Main, StructureSDR AALA202610207938Attach Fitting · excess playAIRCRAFT IN BASE MAINTENANCE: RIGHT MAIN LANDING GEAR DOOR FORWARD ATTACH FITTING BEARING HAS EXCESSIVE PLAY - REPLACED ATTACH FITTING PER CMM 52-81-18Oct 2, 2026 · N109NN · Airbus A321231 · Landing Gear DoorsSDR AALA202610204001Attach Fitting · excess playAIRCRAFT IN BASE MAINTENANCE: LEFT MAIN LANDING GEAR DOOR FORWARD ATTACH FITTING BEARING HAS EXCESSIVE PLAY - REPLACED ATTACH FITTING PER CMM 52-81-18Oct 2, 2026 · N109NN · Airbus A321231 · Landing Gear DoorsSDR K11A2026102000401Rib · corrodedL/H HORIZONTAL STAB TRAILING EDGE RIB AT ELEV STA 121 HAS EVIDENCE OF CORROSION ON LOWER SURFACEOct 2, 2026 · N325FL · Boeing 737883 · Horizontal Stabilizer, Spar/RibSDR K11A2026102000400Rib · corrodedL/H HORIZONTAL STAB TRAILING EDGE RIB AT ELEV STA 94 HAS EVIDENCE OF CORROSION ON LOWER SURFACEOct 2, 2026 · N325FL · Boeing 737883 · Horizontal Stabilizer, Spar/RibSDR SWAA2026101908490Skin · crackedEXISTING FASTENER HOLE HAD A CRACK INDICATION AT BS 727G+6.5, IAW EA 26-153-02701 THE CONFIGURATION IS ACCEPTABLE.Oct 2, 2026 · N8626B · Boeing 7378H4 · Fuselage Main, Plate/SkinSDR 2026FA0000842Brake Disc · detachedWHILE APPLYING THE BRAKES ON TAXI OUT A LOUD BANG WAS HEARD FOLLOWED BY AN ABRUPT LEFT TURN WITH NO ABILITY TO STEER OR BRAKE RIGHT. AIRCRAFT HAS CASTERING NOSE WHEEL. UPON BRAKE REMOVAL THE MOUNTING FLANGE WAS FOUND COMPLETELY SEPARATED FROM THE REST OF THE BOct 2, 2026 · N876RM · Cirrus SR22 · Landing Gear Brake SystemSDR K11A2026101500398Rib · corrodedL/H HORIZONTAL STAB TRAILING EDGE RIB ELEV STA 66 HAS EVIDENCE OF CORROSION ON LOWER SURFACEOct 2, 2026 · N325FL · Boeing 737883 · Horizontal Stabilizer, Spar/RibSDR SWAA2026101500242Doubler · crackedEGPR SURROUND DOUBLER CRACKED AT LOWER FLANGE. ACCOMPLISHED REPAIR ON EGPR SURROUND DOUBLER LOWER FLANGE IAW SRM 53-10-15-2R-4.Oct 2, 2026 · N8697C · Boeing 7378H4 · Fuselage Main, Plate/SkinSDR DALA2026101305616Battery Pack · inoperativeEMERGENCY LIGHTS ROWS 12-15 INOPERATIVE. REMOVED AND REPLACED BATTERY PACK AND CHARGER ASSY (6457391)(AIRCRAFT GROUNDED)Oct 2, 2026 · N666DN · Boeing 757232 · Emergency LightingSDR DALA2026101305617Proximity Sensor · faultedL2 DOOR SLIDE LIGHT STAYS ILLUMINATED WITH DOOR DISARMED. R & R L2 AFT GIRT BAR PROX SENSOR IAW AMM 25-66. OPS CHECKED GOOD. (9112858)(AIRCRAFT GROUNDED)Oct 2, 2026 · N591NW · Boeing 757351 · Emergency EquipmentSDR IPXA2026100957455Radome · brokenBROKEN COMPOSITE , RADOME EXTERNAL 2 AREA. IAW EO-35385-JIC001, REV 4, INSTALL RADOME BOOT. I.A.W AMM 53-12-01-402-059 REV.149 INSTALL THE NOSE RADOME. CONDITION CHECK NORMAL.Oct 2, 2026 · N364UP · Boeing 767346 · Aerodynamic FairingsSDR IPXA2026100856727Skin · debondedFAULT - DISBOND - END CAP, R/H WING T/E OUTBD FLAP INBD. MEASURE THE DAMAGE AREA (L:1.5", W:0.1", D:2PLIES, 7" FROM AFT EDGE, AT INBD EDGE). BOND THE REPAIR PLIES WITH RESIN CURED AT 200°F FOR 220 MINUTES WITH MINIMUM VACUUM OF 22 IN/HG I.A.W UPS SREO-70175-ROct 2, 2026 · N354UP · Boeing 76734AF · Trailing Edge FlapsSDR IPXA2026100857298Skin · crackedFAULT - CRACK - SKIN, R/H WING T/E INBD MAIN FLAP INBD UPPER. (REPAIR). MEASURE THE DAMAGE AREA (DIA:1", 16.5" FROM INBD EDGE, 3.5" FROM AFT EDGE). BOND THE REPAIR PLIES WITH RESIN CURED AT 200°F FOR 220 MINUTES WITH MINIMUM VACUUM OF 22 IN/HG I.A.W. 767-300FOct 2, 2026 · N354UP · Boeing 76734AF · Trailing Edge FlapsSDR UIEA2026100400944Pcb · damagedEQUIPMENT COOLING EICAS CAUTION F270 ON CLIMB. CAPT ND BLANK FOR 30", FO PFD FLICKERED ON CLIMB. MESSAGE BLANKED THEN LOST CAPT ND AND FO ND WAS INTERMITTENT. R & R PRINTED CIRCUIT ASSY IAW AMM 21-58-05/401 & IPC 21-58-55-01B. OPS CHK OK; SCREENS ARE NO LONGOct 2, 2026 · N408MC · Boeing 74747UF · Air Conditioning System WiringSDR DALA2026100705557Holder · out of adjustR1 GIRT BAR AFT BRACKET MOUNT DOES NOT HOLD GIRT BAR SECURELY. ADJUSTED HOLDER, OPS OK. (9514300) AIRCRAFT WAS GROUNDEDOct 2, 2026 · N836DN · Boeing 737932ER · Emergency EquipmentSDR IPXA2026100553573Former · brokenBROKEN FORMER, LT WING OUTBD L/E FOLDING NOSE INNER SIDE AT OSS 441.60, ADJACENT NR 5 SLAT INBD AUX TRACK. REMOVED DAMAGE FORMER IAW SRM 51-40-02-0G, REV 96. INSTALL NEW FORMER IAW SRM 51-40-02-0G, REV 96, DWG 114T2241, SH 4, REV -, AND SREO-54290-REQ1, ROct 2, 2026 · N354UP · Boeing 76734AF · Wing Main, Frame StructureSDR CALA2026100720200Static Wick · missingPDA 2 REF LP 3565494 LH HORIZ STAB TRAILING EDGE MOST OUTBOARD STATIC WICK MISSING. LP 3565494 HAS BEEN GENERATED TO REPLACE MISSING STAIC WICK. RPLD MISSING STATIC WICK IAW MM23-61-00 PARTS USED: 18-2361-3-0006Oct 2, 2026 · N27246 · Boeing 737824 · Static Discharge SystemSDR CALA2026100720169Fitting · crackedNR 2 ENG PYLON NACELLE MID STRUCTURE BULKHEAD PP STA 174.30 RBL 9 WITH CRACK. ACCOMPISHED REPAIR ON #2 ENG PYLON MID-BULKHEAD FWD RH LOWE R-FLANGE IAW EC/RA#:5450-03163,VT EA#:757-5450-13-A4626.REF:NR#1 9168Oct 2, 2026 · N17126 · Boeing 757224 · Nacelle/Pylon, Main Frame