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.
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
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR VNA2026F00009Bracket · corrodedCORROSION ON BRACKET'S MACHINED (2EAS) FS 515, (1EA) FS533, (2EAS) FS 565, (2EAS) FS629, (1EA) FS645, AND (2EAS) FS661+8.40 AT CENTER AND FWD BAGGAGE COMPARTMENT. BRACKET'S MACHINED (2EAS) FS 515, (1EA) FS533, (2EAS) FS 565, (2EAS) FS629, (1EA) FS645, AND (2ESDR VNAA202608010007Bracket · corrodedCORROSION ON BRACKET'S MACHINED (2EAS) FS 515, (1EA) FS533, (2EAS) FS 565, (2EAS) FS629, (1EA) FS645, AND (2EAS) FS661+8.40 AT CENTER AND FWD BAGGAGE COMPARTMENT. BRACKET'S MACHINED (2EAS) FS 515, (1EA) FS533, (2EAS) FS 565, (2EAS) FS629, (1EA) FS645, AND (2ESDR VNAA202608010006Bracket · corrodedCORROSION ON BRACKET'S MACHINED (2EAS) FS 515, (1EA) FS533, (2EAS) FS 565, (2EAS) FS629, (1EA) FS645, AND (2EAS) FS661+8.40 AT CENTER AND FWD BAGGAGE COMPARTMENT. BRACKET'S MACHINED (2EAS) FS 515, (1EA) FS533, (2EAS) FS 565, (2EAS) FS629, (1EA) FS645, AND (2ESDR VNAA202608010005Rib · crackedCRACK ON MACHINED WING RIB OF LEADING EDGE SS57.16 AT LH WING. MACHINED WING RIB OF LEADING EDGE SS57.16 AT LH WING WAS REPAIRED PER REO 690-57-41-240 REV - -SDR VNAA202608010004Seal · corrodedSEVERAL CORRSION ON SETTLEMENT AREA OF FAIRING ACCESS PANEL 194AB (AFT SIDE), ON SETTLEMENT AREA OF ACCESS PANELS 174BZ, 174DZ 173BZ AND 173DZ ALSO IN ANGLE OF KEEL BEAM NEAR FS 669.40 AT MLG WHEEL AREA. CORROSION WERE REMOVED ON SETTLEMENT AREA OF FAIRING ACSDR VNAA202608010003Diaphragm · corrodedSEVERAL AREAS OF CORROSION ON SETTLEMENT AREA OF FAIRING ACCESS PANEL 194AB (AFT SIDE), ON SETTLEMENT AREA OF ACCESS PANELS 174BZ, 174DZ 173BZ AND 173DZ ALSO IN ANGLE OF KEEL BEAM NEAR FS 669.40 AT MLG WHEEL AREA. CORROSION WERE REMOVED ON SETTLEMENT AREA OF SDR VNAA202608010002Angle · corrodedSEVERAL CORRSION ON SETTLEMENT AREA OF FAIRING ACCESS PANEL 194AB (AFT SIDE), ON SETTLEMENT AREA OF ACCESS PANELS 174BZ, 174DZ 173BZ AND 173DZ ALSO IN ANGLE OF KEEL BEAM NEAR FS 669.40 AT MLG WHEEL AREA. CORROSION WERE REMOVED ON SETTLEMENT AREA OF FAIRING ACSDR VNAA202608010001Web · corrodedSEVERAL CORRSION ON SETTLEMENT AREA OF FAIRING ACCESS PANEL 194AB (AFT SIDE), ON SETTLEMENT AREA OF ACCESS PANELS 174BZ, 174DZ 173BZ AND 173DZ ALSO IN ANGLE OF KEEL BEAM NEAR FS 669.40 AT MLG WHEEL AREA. CORROSION WERE REMOVED ON SETTLEMENT AREA OF FAIRING ACSDR VNAA202607310003Rib · crackedCRACK ON MACHINED WING RIB OF LEADING EDGE SS57.16 AT RT WING. MACHINED WING RIB OF LEADING EDGE SS57.16 AT RT WING WAS REPLACED IAW SRM 51-42-06-001-001-A01, SRM 51-42-10-001-001-A01, SRM 51-42-21-001-001-A01 AND SRM 51-41-02-001-001-A01.SDR VNAA202607310002Angle · corrodedCORROSION ON KICKPLATE ANGLE AND MID CAP ANGLE OF PASSANGER DOOR LOWER SURROUND STRUCTURE. KICKPLATE ANGLE AND MID CAP ANGLE OF PASSANGER DOOR LOWER SURROUND STRUCTURE WAS EVALUTAED AND FOUND TO EXCESSIVE CORROSION IAW SRM 51-10-06-001-001-A01 AND WERE REPLACSDR VNAA202607310001Door Sill · corrodedCORROSION ON LOWER SILL BTW FS1000 TO FS1047 AT SURROUND STRUCTURE OF THE AFT BAGGAGE-BAY DOOR CUT OUT. CORROSION ON LOWER SILL BTW BS 1000 TO BS 1047 AT SURROUND STRUCTURE OF THE AFT BAGGAGE-BAY DOOR CUT OUT WAS REMOVED PER CRJ-900 SRM 51-21-06-001-001-A01 SDR VNAA202607300020Seat Track · corrodedCORROSION ON SIDE SEAT RAIL (LH 6E/AS & RH 4E/AS) OF STGR15LH/STGR15RH BTW STA FS669.4 TO FS977.0 AT PASSENGER CABIN. DUE TO EXCESSIVE DAMAGE SEAT RAIL (LH 6E/AS & RH 4E/AS) OF STGR15LH/STGR15RH BTW STA FS669.4 TO FS977.0 AT PASSENGER CABIN. WERE REPLACED PESDR VNAA202607300019Seat Track · corrodedCORROSION ON RH SEAT RAIL RBL9 BTW FS349 TO FS485 AND BTW FS485 TO FS581 AT PAX CABIN. SEAT RAIL RBL9 BTW FS349 TO FS485 AND BTW FS485 TO FS581 AT PAX CABIN WERE FOUND OUT OF LIMITS PER CRJ-900 SRM 53-21-49-101-001-A01 AND SRM 53-31-49-101-001-A02 THEREFORESDR VNAA202607300018Seat Track · corrodedCORROSION ON LH SEAT RAIL LBL 9 BTW BS 379 TO BS 485 AT PAX CABIN. LT SEAT TRACK LBL 9 BTW BS 379 - 485 AT PAX CABIN WAS FOUND OUT OF LIMITS IAW SRM 53-21-49-101-001-A01 THEREFORE WAS REPLACED IAW AMM 53-00-49 (CONFIG A12).SDR VNAA202607300017Seat Track · corrodedCORROSION AND GOUGES ON RH SIDE SEAT RAIL AT STGR 15R 03 SEGMENTS: (01) BTW STA FS379 TO FS483, (02) FS483 TO FS573, (03) FS573 TO FS669 AT PASSENGER COMPARTMENT. DUE TO EXCESIVE DAMAGE ON RH SIDE SEAT RAIL AT STGR 15R 03 SEGMENTS: (01) BTW BS 379 TO 483, (0SDR VNAA202607300016Seat Track · corrodedCORROSION AND GOUGES ON LH SIDE SEAT RAIL AT STGR 15L 03 SEGMENTS: BTW STA FS379 TO FS483, FS483 TO FS573, FS573 TO FS669 AT PASSENGER COMPARTMENT. LT SIDE SEAT RAILS AT STGR 15L 03 SEGMENTS: BTW STA FS379.00 TO FS483.00, FS483.00 TO FS573.00, FS573.00 SDR VNAA202607300012Bracket · corrodedCORROSION ON SUPPORTS (2EAS) OF ELECTRICAL HARNESS BTW WS=0.00 AND WS=29.00 THROUGH ACCEES PANL 542AZ, 642AZ AT LH/RH WING AUXILIARY INTERNAL REAR SPAR. SUPPORTS (2EAS) OF ELECTRICAL HARNESS BTW WS=0.00 AND WS=29.00 THROUGH ACCEES PANL 542AZ, 642AZ AT LT/RT WSDR VNAA202607300006Skin · damagedTEMPORARY DISPOSITION FOR BLENDED NICK/GOUGES DAMAGE TO RH INBD FLAP LOWER SKIN BTW FLS25.5-FLS36 & FRONT SPAR & T/E THE SUBJECT CONDITIONS IS STRUCTURALLY ACCEPTABLE FOR 4600 FLIGHT HOURS FROM THE TIME OF INCORPORATION OF THIS REO AT REV. PREVIOUS BLEND OUTSDR VNAA202607300002Door Frame · wornWEARS ON SURROUND STRUCTURE (04 CORNERS) ON FWD & CTR BAGGAGE BAY DOOR. WEAR ON SURROUND STRUCTURE (04 CORNERS) ON FWD & CTR BAGGAGE BAY DOOR WERE REPAIRED PER REO 690-52-35-643 REV. - - AND REO 690-52-35-644 REV - -SDR SCNA20260522210SAttach Fitting · corrodedMAIN CABIN L1 DOOR FWD GIRT BAR ATTACHMENT FITTINGS HOLES HAVE CORROSION. CLEANED AREA ON MAIN CABIN L1 DOOR FWD GIRT BAR ATTACHMENT FITTINGS HOLES. IAW BOEING SOPM 20-30-03. UPON FURTHER EVALUATION. NO CORROSION NOTED ON FITTINGS HOLE. FOUND TO BE ONLY BARESDR SWAA2026061505138Panel · crackedPANEL 194AR INNER SKIN IS CRACKED. REPAIRED IAW SRM 51-70-05-2R-2-A00733, REPAIR 2.SDR ASAA2026052167094Plate · corrodedAFT CARGO L/H SIDEPLATE IS CORRODED FROM STA 727-787. GROUNDED - YES. REMOVED AND REPLACED AFT CARGO L/H SIDEPLATE FROM STA 727-787 I.A.W. B737-800 SRM 51-40-02-0G-0W= 1 1/2" O= .040 R= .030 L= 1" D= .010.SDR SWAA2026063005364Rib · crackedRIGHT HORIZONTAL STAB REMOVABLE LEADING-EDGE 2ND FROM INBD RIB CRACKED. REMOVED, LOCATED, AND DRILLED. REPLACED NEW RT HORIZONTAL STAB REMOVABLE LEADING-EDGE 2ND FROM INBD RIB IAW SRM 51-40-02-0G-0, 51-40-05-0G-0, AND DWG 186A1001, REV B.SDR ASAA2026052166973Web · corrodedAFT CARGO STRAP INBD OF SILL WEB IS CORRODED. GROUNDED - YES. REMOVED AND REPLACED AFT CARGO STRAP INBD OF SILL WEB IAW SRM 51-40-02-0G-0 STEP 7.C., 4.B.SDR ASAA2026052166972Strap · corrodedAFT CARGO STRAP INBD OF SILL WEB IS CORRODED. GROUNDED - YES. REMOVED AND REPLACED AFT CARGO STRAP INBD OF SILL WEB IAW SRM 51-40-02-0G-0 STEP 7.C., 4.B.SDR ASAA2026052166971Door Sill · corrodedFWD CARGO DOOR SILL WEB HAS CORROSION. GROUNDED - YES. REMOVED AND REPLACED FWD CARGO DOOR SILL WEB IAW SRM 51-40-02-0G-0.SDR ASAA2026052166970Web · corrodedAFT CARGO DOOR SILL WEB IS CORRODED. GROUNDED - YES. REMOVED CORROSION SILL WEB FOUND OUT LIMITS IAW SRM 53-60-15-1A-1. REMOVED AND REPLACED AFT CARGO SILL WEB IAW SRM 51-40-02-0G-0.SDR SWAA2026062505441Handle · deterioratedDETERIORATED WASHER ASSISST HANDLE FWD ENTRY DOOR LINING. REPLACED WASHER ASSIST HANDLE FWD ENTRY DOOR LINING IAW AMM 52-11-31-400-802 STEP 3.G. ITEM (2)(B).SDR SWAA2026062505438Stub Frame · crackedCRACK INDICATION ON STUB FRAME LOCATED BETWEEN BS 294.5 TO BS 296.5 AND BETWEEN S-8R TO S-9R AT FWD GALLEY DOOR AREA CRACK LENGTH 0.250 IN. APPROX.AT PASSENGER CABIN. REPLACED STUB FRAME LOCATED ON BS 296.5 BETWEEN STR 7R AND STR 9R UPPER POSITION AT FWD GALLSDR CALA2026062217202Stub Beam · gougedL-1 DOOR HANDLE BOX CUTOUT, UPPER STUB BEAM HAS GOUGES. REMOVED AND REPLACED L-1 DOOR HANDLE BOX CUTOUT UPPER STUB BEAM IAW SRM 51-40-02 AND DWG 141A6163 REV-.SDR HNAA2026061700545Floor Support · corrodedDURING A DOUBLER INSTALL FOUND ADDITIONAL CORROSION ON LH FLOOR SILL AT FR 40. FABRICATED AND INSTALLED DOUBLER ON MID CABIN LH FLOOR SILL AT FR40 IAW ETD 2026-145-008549 REV: B. SEE MAJOR EO# EO1-53-26-0243SDR ASAA2026052166732Shield · corrodedAFT CARGO SHIELD FWD OF CARGO DOOR IS CORRODED. GROUNDED - YES. REMOVED AND REPLACED AFT CARGO SHIELD FWD OF CARGO DOOR IAW B737-800 SRM 51-40-02-0G-0.SDR ASAA2026052166730Shield · corrodedFWD CARGO SHIELD AFT OF DOOR HAS CORROSION. GROUNDED - YES. REMOVED AND REMPLACED FWD CARGO SHIELD AFT OF DOOR IAW SRM 51-40-02-0G-0 STEP 7.SDR SWIA2026052176224Slide · looseDURING REMOVAL OF THE FWD SERVICE DOOR EVACUATION SLIDE, FOUND BOTTOM LACINGS LOOSE FROM GIRT-BAR. REPLACED FWD SERVICE DOOR EVACUATION SLIDE WITH A NEW SLIDE IAW AMM 25-65-01-400-801-A.SDR MASA20260608146Floor Support · corrodedDURING HEAVY CHECK INSPECTIONS OF THE INTERNAL FWD FUSE FLOOR SUPPORT CORRODED FLOOR SUPPORT ANGLE AT FR 16 RT, RBL 28 REMOVED AND REPLACED IAW SRM 51-41-01, REV 45, CORROSION LEVEL2SDR AALA202606088606Hinge Arm · excess playAIRCRAFT IN BASE MAINTENANCE: RIGHT HAND HORIZONTAL STABILIZER ELEVATOR #6 HINGE ARM HAS EXCESSIVE PLAY. REPLACED HINGE ARM PER AMM 55-16-42.SDR AALA202606085368Hinge Arm · excess playAIRCRAFT IN BASE MAINTENANCE: RIGHT HAND HORIZONTAL STABILIZER ELEVATOR #5 HINGE ARM HAS EXCESSIVE PLAY. REPLACED HINGE ARM PER AMM 55-16-42.SDR AALA202606083979Hinge Fitting · excess playAIRCRAFT IN BASE MAINTENANCE: RIGHT HAND HORIZONTAL STABILIZER ELEVATOR #4 HINGE ARM END FITTING HAS EXCESSIVE PLAY. REPLACED HINGE ARM END FITTING PER AMM 55-16-42.SDR AALA202606056692Hinge Fitting · excess playAIRCRAFT IN BASE MAINTENANCE: RIGHT HAND HORIZONTAL STABILIZER ELEVATOR #3 HINGE ARM END FITTING HAS EXCESSIVE PLAY. REPLACED HINGE ARM END FITTING PER AMM 55-16-42.SDR AALA202606057267Hinge Fitting · excess playAIRCRAFT IN BASE MAINTENANCE: RIGHT HAND HORIZONTAL STABILIZER ELEVATOR #2 HINGE ARM END FITTING HAS EXCESSIVE PLAY. REPLACED HINGE ARM END FITTING PER AMM 55-16-42.SDR AALA202606055039Hinge Fitting · excess playAIRCRAFT IN BASE MAINTENANCE: RIGHT HAND HORIZONTAL STABILIZER ELEVATOR #1 HINGE ARM END FITTING HAS EXCESSIVE PLAY. REPLACED HINGE ARM END FITTING PER AMM 55-16-42.SDR HNAA2026060500491Shear Tie · crackedSHEAR TIE CRACKED AT FR80 BTW STR5-7L. R & R SHEAR TIE IAW SRM 51-40-02SDR HNAA2026060500490Support Bracket · crackedLEFT PACK FUSELAGE SUPPORT (ANTI-ROTATION SUPPORT) BRACKET CRACKED. R & R SUPPORT BRACKET IAW SRM 51-40-02.SDR DALA2026060403393Thrust Reverser · corrodedDURING H CHK IN MSP, CORROSION AND/OR MISSING COATING WAS FOUND ON THE #2 ENG, INBD THRUST REVERSER (P/N 999-3001577 WITH FTN 5T0778) TORQUE BOX V-BLADE AT THE UPPER TO LOWER V-BLADE SEGMENTS. DAMAGE EXCEEDS CMM GRAPW1500BA-A-54-30-22-00001-661A-D ALLOWABLE DASDR SWAA2026060205499Skin · delaminatedLH OB AFT FLAP IS DELAMINATED NEAR IB TE. PROCURED NEW LT WING OTBD AFT FLAP. REMOVAL AND INSTALLATION TO BE ACCOMPLISHED ON FAULT TTG8Q01BR3LB. PER AMM 27-51-22-401.SDR HNAA2026060200477Seal · crackedRT UPPER T/R DOOR; 2 METAL PROFILE SEALS CRACKED AT OB SIDE. R & R METAL SEALS IAW SRM 51-40-02SDR AALA202606027444Elec Connector · inoperativeAIRCRAFT WAS NOT GROUNDED: EMERGENCY LIGHT ABOVE OVERHEAD BIN AT SEAT 24F IS OUT. MAINTENANCE REPLACED CONNECTOR IAW AWM 33-15-13 AND SWPM 20-62-00.SDR IPXA2026060192736Window · failedLEFT WINDOW (L1) STARTED ARCING AT PC360 THEN SHATTERED. QRH COMPLETED. REMOVED AND REPLACE L1 WINDOW PER AMM56-11-01. OPS CK GOOD. TORQUED WINDSHIELD POWER TERMINALS AND SENSOR TERMINALS AS REQUIRED BY AMM 56-11-01-424-015.. APPLIED AERODYNAMIC SEALANT TO COSDR REXA2026060100895Tire · blownRIGHT MAIN GEAR BLOWN TIRE. R/R RHOB TIRE IAW J/C 900-32-730-708, PERFORMED TIRE BURST INSPECTION IAW J/C 900-05-900-903, R/R RHOB BRAKE ASSY. IAW J/C 900-32-730-901, R/R RHIB TIRE IAW J/C 900-32-730-708, R/R WHEEL SPEED TRANSDUCER ON RHOB IAW AMM 32-47-01, OPSDR DALA2026053103289None · noneDAMAGE TOLERANCE EVALUATION ( DTE ) REQUIRED FOR REPAIR INSTALLE D AT FR68RH AND S-22 PER ER/A 634286-14AD. C/A: SECTION I IS LIMITED TO 102900FC FROM SECTION I. ER/A TO BE REVI SED PRIOR TO THIS LIMIT ELSE REMOVE A/C FROM SERVICE. ASSOCIATED ER/A 14-634286 AD