Service difficulty reports
1,770,704 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 FDEA202609241423Floor Panel · crushedCRACKS AND CRUSHED CORE ON THE CUTOUTS AREA OF THE FLOOR PANEL 241WFF IN THE MAIN DECK CARGO COMPARTMENT QTY 10. FLOOR PANEL 241WFF IN THE MAIN DECK CARGO COMPARTMENT WAS REPAIRED IAW SRM 53-00- 50-2R PAR 4-B FIG. 201 SHEET 2 REV 96 AUG. 15/2026.SDR FDEA202609241422Floor Panel · debondedDISBONED EDGE PLIES OF FLOOR PANEL 241ZFF IN THE MAIN DECK CARGO COMPARTMENT. FLOOR PANEL 241ZFF IN THE MAIN DECK CARGO COMPARTMENT WAS REPAIRED IAW SRM 53-00-50-2R, PAR 4-G, FIG 201, DETAIL VI, REV. 96. AUG. 15/2026.SDR DALA2026092405332Cone · missingDURING WALKAROUND, FOUND LT FLAP TRACK NR 2 TAILCONE MISSING. PLACED ON A330 CDL 57-00-04B. (8804946) AIRCRAFT WAS GROUNDED.SDR DALA2026092405329Bracket · looseR1 GIRT BAR DISARM BRACKET LOOSE, REMOVED & REINSTALLED SLIDE IAW W/C 2561-9005 AND R & R EVACUATION SLIDE COMPARTMENT DOOR IAW AMM 52-42. (9504750) (AIRCRAFT GROUNDED).SDR DALA2026092405328Skin · damagedFOUND DAMAGE TO AFT CARGO DOOR CUTOUT AFT SKIN EDGE, COMPLIED WITH ER/A 637149-14. (9115046) (AIRCRAFT GROUNDED).SDR 2A6R2026092475408Xmsn Deck · dentedA SURFACE DAMAGE (DENT) IS FOUND ON THE TRANSMISSION DECK UPPER SURFACE, UNDER AFT OTBD SECTION OF THE RH XY FITTING, APPROXIMATELY 2.5” LONG, 0.05” WIDE AND 0.032” DEPTH. FOR DETAILS SEE AIRBUS RDAS-EC135-53-2026-3264ASDR K11A2026092400392Control Panel · failedPRESSURIZATION FAIL DURING DESCENT, MANUAL MODE DID NOT WORK. REMOVED AND REPLACED PRESSURE CONTROL MODULE IAW AMM 21-31-25, OPS CHECK PERFORMED IAW AMM 21-31-00/205 OPS CHECK GOOD NO DEFECTS NOTED, REF LP 737-004-8615 ITEM #2. PERFORMED CABIN PRESSURIZATION SDR REXA2026110402033Angle · crackedCRACK ON CLIP (2EAS) OF THE SUPPORT FRAME BTWN FS 1051.30 - STGR 7RH FWD/AFT FACE AND STGR 7LH FWD FACE. CLIP (2EAS) OF THE SUPPORT FRAME BTWN FS 1051.30 - STGR 7RH FWD/AFT FACE AND STGR 7LH FWD FACE WERE REPLACED PER CRJ900 SRM 51-42-21-001-001-A01SDR REXA2026110402032Angle · crackedCRACK ON CLIP (2EAS) OF THE SUPPORT FRAME BTWN FS 1051.30 - STGR 7RH FWD/AFT FACE AND STGR 7LH FWD FACE. CLIP (2EAS) OF THE SUPPORT FRAME BTWN FS 1051.30 - STGR 7RH FWD/AFT FACE AND STGR 7LH FWD FACE WERE REPLACED PER CRJ900 SRM 51-42-21-001-001-A01SDR REXA2026110402031Support Frame · crackedCRACK ON CLIP (2EAS) OF THE SUPPORT FRAME BTWN FS 1051.30 - STR 7RH FWD/AFT FACE AND STGR 7LH FWD FACE. CLIP (2EAS) OF THE SUPPORT FRAME BTWN FS 1051.30 - STGR 7RH FWD/AFT FACE AND STGR 7LH FWD FACE WERE REPLACED PER CRJ900 SRM 51-42-21-001-001-A01SDR REXA2026110402030Floor Support · crackedCRACK ON FLOOR SUPPORT RBL 12.0 BTW FS 221.73 TO FS 229.00 AT FWD FUSELAGE INTERNAL STRUCTURE (FLIGHT COMPARTMENT FLOOR STRUCTURE BELOW WL79.50) FLOOR SUPPORT RBL 12.0 BTW FS 221.73 TO FS 229.00 AT FWD FUSELAGE INTERNAL STRUCTURE (FLIGHT COMPARTMENT FLOOR STRUSDR AALA202611039803Frame · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK INDICATION FOUND ON LOWER INBOARD HOLE DOOR STOP 1 FRAME 68 LH SIDE CRACK DEPTH 0.100 INCH CRACK DIRECTION 3 O'CLOCK. MAINTENANCE ACCOMPLISHED PERMANENT REPAIR LOCATED LOWER I/B HOLE DOOR STOP 1 FRAME 68 AT LEVEL STRG 22 LH SDR SWAA2026102999032Seat Track · corrodedCORROSION ON THE SEAT TRACK AT LBL 45, BS480+4; BS500+12; BS500B+5; BS500C+15; BS500D+15. REMOVED AND INSTALLED A NEW SEAT TRACK IAW SRM 51-40-02, DWG 143A5300, REV -, & AMM 20-50-11, TABLE 230 & 237.SDR HNAA2026102901047Floor Support · corrodedLEFT OMEGA BEAM REPAIR AT FR58-59 CORRODED. REPAIRED IAW ETD 2026-145-016105 AND EO 1-53-26-0538.SDR HNAA2026102801044Bracket · crackedBRACKET CRACKED ON STR13 TO APU FIREWALL.RAR BRACKET IAW SRM 51-40-02SDR SWAA2026102733895Drag Link · crackedCRACK INDICATION IN THE AFT FASTENER HOLE OF THE DRAG LINK, BS 540, BTWN STRINGERS 21R & 22R. REPAIRED THE DRAG LINK ASSY IAW EA 26-153-02614-WIP1, 26-153-02614-WIP2, 26-153-02614-WIP3, 26-153-02614-WIP4, 26-153-02614-WIP5, 26-153-02614-WIP6, 26-153-02614-WIPSDR SWAA2026102736561Scuff Plate · crackedCRACKED AFT CORNER SCUFF PLATE, REPAIRED THE SCUFF PLATE IAW SRM 53-60-15-2R-1, REPAIR 1, & BAC 5975.SDR SWAA2026102745912Access Panel · damagedELONGATED HOLES ON LT WING ACCESS PANEL 561BB. REPAIRED THE ACCESS PANEL IAW SRM 51-70-04-2R-9, REPAIR 9.SDR HNAA2026102701041Gusset · corrodedCTR FUSE I, CTR GUSSET CORRODED. RAR CTR GUSSET IAW SRM 51-40-02SDR HNAA2026102701039Profile · bentCARGO ENTRY, LWR T-PROFILE BENT AT FR67. RAR IAW SRM 51-40-02, FABRICATED NEW T-PROFILE IAW ETD 2026-145-017139SDR HNAA2026102701038Doubler · corrodedRT OMEGA BEAM DOUBLER CRRODED AT FR22. R & R DOUBLER IAW SRM 51-40-02.SDR HNAA2026102701036Gusset · corrodedRH GUSSET CORRODED BTW FR59-61. RAR GUSSET IAW SRM 51-40-02SDR HNAA2026102701035Floor Support · crackedLEFT FLOOR OMEGA BEAM IB FLANGE CRACKED AT FR23. REPAIRED IAW ETD 2026-145-016868 AND EO 1-53-26-0510SDR SWAA2026102607700Lens · brokenBROKEN LENS EMERGENCY LIGHTS ON MID CABIN (3EA) AND FWD CABIN (2EA) AT PASSENGER CABIN. REPLACED THE LENSES IAW AMM 33-51-03-960-803, STEP 4.D.(2).SDR SWAA2026102665019Cover · missingMISSING COVER ON MID CABIN OVERHEAD EMERGENCY EXIT LIGHT IN THE PAX CABIN. INSTALLED THE COVER IAW AMM 33-51-01-960-802.SDR HNAA2026102601034Floor Support · crackedLH FLOOR OMEGA BEAM IB FLANGE CRACKED AT FR22. REPAIRED IAW ETD 2026-145-016868 AND EO 1-53-26-0510SDR HNAA2026102301028Beam · corrodedSERVICE DOOR ENTRY LWR BEAM HAS CORROSION. RAR BEAM IAW SRM 51-40-02SDR SWAA2026102120461Rib · crackedCRACKED LT HORIZONTAL STAB LEADING EDGE RIB AT ACCESS PANEL 331B, REPLACED THE RIB & FASTENERS IAW SRM 51-40-02, & DWG 186A1001, SHEET 19, REV -.SDR SWAA2026102102572Rib · crackedCRACKED LEADING EDGE RIB, L/E STA 272.62 ON THE RT HORIZONTAL STAB. REPLACED THE RIB IAW SRM 51-40-02-0G-0, SRM 51-10-02-0G-0, STEP 9, AND DWG 186A1001, SHT 19, REV -.SDR AALA202610216494Support Angle · crackedAIRCRAFT IN BASE MAINTENANCE: CENTER AND OUTBOARD WING LOWER SURFACE AT STATION 663 28+7 35 LEFT BUTT LINE HAS CRACK. MAINTENANCE ACCOMPLISHED FINAL INSTALLATION OF THE LEFT-HAND 663 VAPOR BARRIER UPPER ATTACH ANGLE FUEL TANK FASTENERS PER AARD CHAPTER 51-00-0SDR AALA202610218704Lug · corrodedAIRCRAFT IN BASE MAINTENANCE: RIGHT HORIZONTAL STABILIZER REAR SPAR TERMINAL FITTING LOWER LUG HAS EXFOLIATION CORROSION AT STAB STATION 0 AND BUTT LINE 83.05 ON THE AFT FACE. MAINTENANCE REMOVED/BLENDED OUT CORROSION AT STATION 0 AND BUTT LINE 83.05 AND DETERSDR AALA202610219984Vapor Barrier · crackedAIRCRAFT IN BASE MAINTENANCE: CENTER AND OUTBOARD WING LOWER SURFACE AT STATION 663 25+7 32RBL HAS CRACK. INSTALLED NEW RIGHT-HAND 663 VAPOR BARRIER ATTACH ANGLE AT STATION 663 25+7 32RBL PER AARD 51-00-05-1 AND BOEING DRAWING 111A1000.SDR SWAA2026101981865Crossbeam · crackedFLOOR CROSSBEAM CRACKED, BS 540, BL 0 - RBL 25, WL 208. REMOVED AND INSTALLED A NEW FLOOR CROSSBEAM IAW SRM 51-40-02-0G-0, SRM 51-40-05-0G-0, & DWG 143A0060, REV B.SDR SWAA2026101932965Crossbeam · crackedFLOOR CROSSBEAM CRACKED, BS 540, BL 0 - LBL 25, WL 208. REMOVED AND INSTALLED A NEW FLOOR CROSSBEAM IAW SRM 51-40-02-0G-0, SRM 51-40-05-0G-0, AND DWG 143A0060, REV B.SDR AALA202610191512Floor Support · crackedAIRCRAFT IN BASE MAINTENANCE: FORWARD WET AREA INTERCOSTAL CRACKED STATION 322 RBL 31. REMOVED AND REPLACED INTERCOSTAL IAW BOEING DWG 141A5400 AND AARD 51-00-05.SDR HNAA2026101901008Attach Bracket · crackedPASSENGER DOOR INTERNAL HANDLE ATTACH BRACKET WAS CRACKED. REMOVED AND REPLACED THE HANDLE ATTACH BRACKET IAW SRM 51-40-02.SDR HNAA2026101901007Hinge Fitting · excess playRUDDER LOWER HINGE FITTING HAD PLAY. R & R RUDDER HINGE FITTING IAW SRM 51-40-02, & SRM 51-20-01.SDR SWAA2026101676770Web · crackedCRACKED WEB BTWN BS 500G - 500H, STRINGER 26R IN THE FWD CARGO BAY. REPLACED THE WEB & FASTENERS IAW SRM 51-40-02-0G, DWG 143A7505, SHEET 151, & 153, REV -.SDR REXA2026101601939Rib · crackedCRACKED RIB SS 58.41, RT WING LE, THE RIB WAS REPLACED IAW SRM 51-42-06-001-001-A01, SRM 51-42-10-001-001-A01, AND SRM 51-42-21-001-001-A01.SDR REXA2026101601933Stringer Splice · corrodedAFTER REMOVAL OF STRINGER 21R, CORROSION WAS FOUND ON THE STRINGER SPLICE, BETWEEN BS 469 - 485. THE STRINGER SPLICE WAS REPLACED IAW SRM 51-42-06-001-001-A01, & SRM 51-42-21-001-001-A01.SDR AALA202610167328Frame · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK INDICATION FOUND ON LOWER INBOARD HOLE DOOR STOP 1 FR 68 RH SIDE CRACK DEPTH 0.125 CRACK DIRECTION 9 OCLOCK. MAINTENANCE ACCOMPLISHMENT PERMANENT REPAIR LOCATED LOWER IB HOLE DOOR STOP 1 FRAME 68 AT LEVEL STRG 22 RH IAW A319SDR SWIA2026092377746Shear Tie · damagedTWO EXFOLIATED CLEATS FOUND ON FRAME BS 333, STR 23R & STR 24R. REMOVED AND REPLACED THE TWO CLEATS IAW SRM 51-42-06-001-001-A01, AND DWG SH670-32420, REV E. COMPLIED WITH ALL STEPS OF 51-900-1002 SKY.SDR ASAA2026092369240Transition Panel · corrodedFWD CARGO RT TRANSITION PANEL BS 500A TO 500L CORRODED. GROUNDED - YES. REMOVED CORROSION FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-1A-1, REMOVED AND REPLACED TRANSITION PANEL IAW SRM 53-00-53-2R-5.SDR SWAA2026101413584Crossbeam · out of adjustFLOOR CROSSBEAM, BS 540, LBL 24 - RBL 24, MISLOCATED COMMON TO FLOOR PANEL REMOVED, LOCATED, AND DRILLED THE CROSSBEAM IAW SRM 51-40-05.SDR HNAA2026100900963Support · corrodedLEFT SUPPORT CORRODED BTWN FR 53-59. R & R THE SUPPORT IAW SRM 51-40-02SDR HNAA2026100800961Tee Angle · crackedCARGO ENTRY, T-PROFILE CRACKED AT FR66. R & R PROFILE IAW SRM 51-40-02SDR CALA2026100820210Pan · corrodedUPON REMOVAL OF LAV SERVICE PAN FOUND CORROSION ON SKIN AROUND CUTOUT. PER B737 SRM 53-60-01-0I-1 FIGURE 9 SHEET 4 ORIGIONAL SKIN THICKNESS IS .080". REMOVED CORROSION AND FOUND OUT OF LIMITS. REF SRM 53-00-01-1A-5, APPLIED GRID TO DAMAGED AREA. DRILLED HOLESDR AALA202610057148Door Frame · crackedAIRCRAFT IN BASE MAINTENANCE: EXTERNAL POWER RECEPTACLE ACCESS DOOR CUT OUT LOWER EDGE DAMAGED. MAINTENANCE FABRICATED LOCATED DRILLED AND INSTALLED REPAIR FILLER IAW B737-NG SRM 53-10-15-2R-4- REPAIR 4.SDR SWAA2026100510182Scuff Plate · crackedCRACKED FWD CORNER SCUFF PLATE IN THE FWD CARGO BAY. REPAIRED THE FWD CORNER SCUFF PLATE IAW SRM 53-30-15-2R-1, REPAIR 1.SDR AALA202610054248Transition Panel · corrodedAIRCRAFT IN BASE MAINTENANCE: AFT CARGO LH TRANSITION PANEL HAS CORROSION AT SEVERAL LOCATIONS FROM STA 727I+4 TO STA 846. ACCOMPLISHED INSTALLATION OF TRANSITION PANEL AND SPLICE REPAIR IAW SRM 53-00-53-2R REPAIR 5.