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 DALA2026073104447Seat Track · corrodedCABIN SEAT TRACK FOUND CORROSION AT FR 31-FR 34, -Y1552.5. REPLACED SEAT TRACK PER A330 SRM 53-00-15-283-002. (1730676) AIRCRAFT WAS GROUNDED.Jul 31, 2026 · N803NW · Airbus A330323 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2026073104446Seat Track · corrodedCABIN SEAT TRACK CORROSION AT FR 31 - FR 34, Y1552.5. REPLACED SEAT TRACK PER A330 SRM 51-72-11. (1730666) AIRCRAFT WAS GROUNDED.Jul 31, 2026 · N803NW · Airbus A330323 · Fuselage, Seat/Cargo Attach FittingsSDR WX0A2026073132907Unknown · odor(AIRCRAFT NOT GROUNDED) DIRTY SOCK SMELL WAS OBSERVED ON DESCENT FROM AROUND 5000 FEET UNTIL TOUCHDOWN AND TAXI / PERFORMED TC 001 AND LEVEL A DECON IAW AMM 21-00-00-815-802-A. NO ODOR REPRODUCED. COMPLETED STEPS 4.D.(2)- TO END OF PHASE 2 TASK CARD NO SMELLJul 31, 2026 · N327NV · Airbus A319111 · Air Distribution SystemSDR WX0A2026073132906Unknown · odor(AIRCRAFT NOT GROUNDED) DURING TAKE OFF, AFT FA'S 2 & 4 HAD A DIRTY SOCK ODOR. LASTED ABOUT 3 MIN DURING + AFTER TAKE OFF. INTENSITY OF ODOR WAS MODERATE & LIGHT PER FA'S. NO VISIBLE SMOKE EITHER, AIR SOURCE USED AT GATE WAS GROUND AIR & THEN APU AIR, ENG STARJul 31, 2026 · N312NV · Airbus A319111 · Air Distribution SystemSDR DALA2026073104441Bottle · low pressureL2 DOOR ASSIST CYLINDER PRESSURE LOW. SERVICED DOOR ASSIST BOTTLE PER A321 AMM 52-15. (9125737) AIRCRAFT WAS GROUNDED.Jul 31, 2026 · N363DN · Airbus A321213 · Passenger/Crew DoorsSDR UIEA2026073100675Clamp · missingMISSING CLAMP ON #1 TORQUE ROD. REINSTALLED BAND CLAMP PER AMM 20-51-01 & IPC 654/6625-2441. OK FOR SERVICE.Jul 31, 2026 · N868GT · Boeing 7478F · Main Landing Gear Attach SectionSDR ABXA20260731341Dampener · faultedDURING ENGINE START AND PUSHBACK, R YAW DAMPER. NON CREW DEFERRABLE. A/C RETURNED TO BLOCKS (BTB). MTC DEFERRED RH YAW DAMPER IAW ABX-MEL-22-21-1 A/C REMAINS CAT III B. COMPLIED MX PROCEDURES & PLACARD INSTALLED. A/C RETURNED TO SERVICE.Jul 31, 2026 · N651GT · Boeing 767231 · Auto Flight SystemSDR 2026FA0000614Housing · damagedTHE ISSUE WAS IDENTIFIED FOLLOWING THE DETECTION OF A SIMILAR DISCREPANCY ON ENGINE 602978 DURING A CONFIGURATION REVIEW. DISCUSSIONS WERE HELD WITH THE INVOLVED DISASSEMBLY INSPECTOR AND A TARGETED REVIEW OF THE INSPECTOR'S RECENT DELIVERIES WAS PERFORMED. THJul 31, 2026 · Boeing 737 · Engine (Turbine/Turboprop)SDR FDEA202607311070Seat Track · wornMAIN DECK CARGO COMPARTMENT SEAT TRACK AT STATION 1811, X=-27.5" FOUND CROWN WORN. SEAT TRACK EVALUATED AND FOUND EXCEEDED LIMIT IAW SRM 53-00-52-1A, FIGURE 101, ALLOWABLE DAMAGE 1. THE SEAT TRACK WAS REPAIRED BY SECTIONAL REPLACEMENT BS 1771 TO EXISTING SPJul 31, 2026 · N605FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA202607311069Seat Track · wornMAIN DECK CARGO COMPARTMENT SEAT TRACK AT STATION 5-0 TO 5-33, X=-75.25" FOUND CROWN WORN. EVALUATED AND FOUND EXCEEDED LIMIT IAW SRM 53-00-52-1A, FIGURE 101, ALLOWABLE DAMAGE 1. REPAIRED BY SECTIONAL REPLACEMENT AT BS 5-63 TO EXISTING SPLICE STATION 5-0/153Jul 31, 2026 · N605FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA202607311068Seat Track · wornMAIN DECK CARGO COMPARTMENT SEAT TRACK AT BETWEEN STATION 1421, X=-8.5" FOUND CROWN WORN. SEAT TRACK STATION 1421, X = - 8.5" EVALUATED AND FOUND EXCEEDED LIMIT AS PER MD-11 SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1.CROWN WORN SEAT TRACK REPAIRED BYJul 31, 2026 · N605FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA202607311067Seat Track · wornMAIN DECK CARGO COMPARTMENT SEAT TRACK AT STATION 1421, X=-27.5" FOUND CROWN WORN. EVALUATED AND FOUND EXCEEDED LIMIT AS PER MD-11 SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. SEAT TRACK REPAIRED BY SECTIONAL REPLACEMENT AT EXISTING SPLICES BS 1411- 143Jul 31, 2026 · N605FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA202607311066Seat Track · wornMAIN DECK CARGO BAY SEAT TRACK AT BS 1421, X=75.25", FOUND CROWN WORN. EVALUATED AND FOUND OUT OF LIMITS IAW SRM 53-00-52-1A, FIGURE 101, ALLOWABLE DAMAGE 1. THE SEAT TRACK WAS REPAIRED BY SECTIONAL REPLACEMENT AT EXISTING SPLICES BS 1351 - 1431, X = 47.5",Jul 31, 2026 · N605FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA202607311065Seat Track · wornMAIN DECK CARGO COMPARTMENT SEAT TRACK AT STATION 1341, X=-75.25" FOUND CROWN WORN. SEAT TRACK REAPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT AT STATION 1331 TO EXISTING SPLICE STATION 1371 X = - 47.5" AS PER MD - 11 SRM 53-00-52-2R FIGURE 201 REPAIR 1.Jul 31, 2026 · N605FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA202607311064Seat Track · wornMAIN DECK CARGO COMPARTMENT SEAT TRACK AT BETWEEN STATION 1300, X=8.5" FOUND CROWN WORN. THE SEAT TRACK EVALUATED & FOUND EXCEEDED LIMITS IAW SRM 53-00-52-1A, FIGURE 101, ALLOWABLE DAMAGE 1. THE SEAT TRACK WAS REPAIRED BY SECTIONAL REPLACEMENT AT EXISTINGJul 31, 2026 · N605FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA202607311063Seat Track · wornMAIN DECK CARGO COMPARTMENT SEAT TRACK AT BETWEEN STATION 1300, X=-8.5" FOUND CROWN WORN. REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT AT STATION 1269 STATION 1331, X =-8.5" AS PER SRM 53-00-52-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR PER GMM Jul 31, 2026 · N605FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA202607311062Seat Track · wornMAIN DECK CARGO COMPARTMENT SEAT TRACK AT BETWEEN STATION 1300, X=-75.25" FOUND CROWN WORN. SEAT TRACK STATION 1300, X = - 75.25 EVALUATED AND FOUND EXCEEDED LIMIT AS PER MD-11 SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CROWN WORN SEAT TRACK REPAIRED Jul 31, 2026 · N605FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA202607311061Floor Panel · brokenBROKEN 241WFF FLOOR PANEL, MAIN DECK CARGO COMPARTMENT FLOOR PANEL 241WFF, MAIN DECK CARGO COMPARTMENT WAS REPAIRED IAW B767 SRM 53-00- 50-2R PAR 4-B FIG 201 SHEET 2 REV 94 DEC 15/2025Jul 31, 2026 · N265FE · Boeing 767300 · Fuselage Floor PanelSDR IXXA20260731001Frame · chafedTHE UPPER CHORD IS DEEPLY CHAFED, ON THE BULKHEAD ON TOP OF THE RIGHT PYLON, LOCATED AT THE FWD O/B CORNER OF THE 441BT PANEL.Jul 31, 2026 · N379AZ · Boeing 767323 · Nacelle/Pylon, Main FrameSDR CALA2026073118137Power Supply · faultedEMERGENCY LIGHTS OPS TEST WITH THE TEST SWITCH PROCEDURE, LT AFT OVERWING EXIT IDENTIFIER NEEDS RELAMPED RELAMPED 3 INOP LAMPS REF AMM 33-51-10-962-040 OPS CK FAILED ALL LAMPS ON THIS ASSY INOP REPLACED FUSE F4 IN M11383POWER SUPPLY. LIGHTS OP CK GOOF REF AMMJul 31, 2026 · N75853 · Boeing 757324 · Emergency LightingSDR VNAA202610060027Rib · crackedCRACK ON MACHINED RIB LEADING EDGE SS58.41 AT LEFT WING. MACHINED RIB LEADING EDGE SS58.41 AT LEFT WING WAS REPPLACED PER CRJ-900 SRM 51-42-06-001-001-A01, SRM 51-42-10-001-001-A01 AND SRM 51-42-21-001-001-A01Jul 30, 2026 · N648NN · Cndair CL6002D24 · Wing, Rib/BulkheadSDR VNAA202610060026Rib · crackedCRACK ON MACHINED RIB LEADING EDGE SS58.41 AT RIGHT WING. MACHINED RIB LEADING EDGE SS58.41 AT RIGHT WING WAS REPLACED PER SRM 51-42-10-001-001-A01 AND SRM 51-42-21-001-001-A01Jul 30, 2026 · N648NN · Cndair CL6002D24 · Wing SparSDR VNAA202610060025Hinge · wornFREE PLAY ON BEARING OF RUDDER HINGE FITTING #2 #3 AT REAR SPAR OF HORIZONTAL STABILIZER. RUDDER HINGE FITTING #2 #3 AT REAR SPAR OF HORIZONTAL STABILIZER WERE REPLACED PER RIL #1213 REV. NCJul 30, 2026 · N648NN · Cndair CL6002D24 · Rudder StructureSDR VNAA202610060024Bolt · crackedCORROSION ON HARDWARE ON UPPER ATTACHMENT OF RH FLAP MOVEABLE VANE INBOARD ACTUATOR. HARDWARE WITH CORROSION ON UPPER ATTACHMENT OF RH FLAP MOVEABLE VANE INBOARD ACTUATOR WERE REPLACED PER MHIRJ CMM 57-52-02Jul 30, 2026 · N648NN · Cndair CL6002D24 · Wing Main, Frame StructureSDR HNAA2026092200885Rib · crackedRT WING, 1EA RIB 21 HAS A CRACK ON UPPER MID FLANGE. REPAIRED CRACK ON RIB 21 OF THE RT WING UPPER MID FLANGE WITH A CUTOUT FILLER AND DOUBLER IAW SRM 57-20-07-RE, AND EO 1-57-26-0404Jul 30, 2026 · N664MS · Emb EMB145LR · Wing, Rib/BulkheadSDR HNAA202609220085Rib · crackedRT WING, 1EA RIB 21 HAS A CRACK ON UPPER MID FLANGE. REPAIRED CRACK ON RIB 21 OF THE R/H WING UPPER MID FLANGE WITH A CUTOUT FILLER AND DOUBLER PER EMB 145 SRM 57-20-07-RE, AND PIEDMONT MAJOR EO-1-57-26-0404.Jul 30, 2026 · N664MS · Emb EMB145LR · Wing, Rib/BulkheadSDR SWIA2026073077222Window Post · crackedWINDSHIELD LT SIDE POST, AFTER NDT INSPECTION CRACK NOTED AND MARKED ON LH LOWER OB FITTING REMOVED AND REPLACED FITTING ON WINDSHIELD LH SIDE POST PN 601R33235-5S PO 2319 IAW CRJ200 SRM 53-11-35 SRM 51-42-21Jul 30, 2026 · N448SW · Cndair CL6002B19 · Fuselage Main, StructureSDR ASAA2026073068647Spar · corrodedLEFT HORIZONTAL STAB, I/B OF AFT SPAR, LOWER CORD ATTACHMENT FITTING AFT FACE HAS A LARGE AREA OF EXFOILIATINIG CORROSION. GROUNDED - YES. REMOVED CORROSION AND SUBMITTED TO ENGINEERING FOR DISPOSITION, REPAIRED CHORD LUG IAW EA CMPT-55EA-30655.W=1" O=2.046" RJul 30, 2026 · N569AS · Boeing 737890 · Horizontal Stabilizer, Spar/RibSDR REXA2026091101819Frame · corrodedCORROSION ON FRAME AT FS 333, BTW STGR 25 AND 26R ON MAIN AVIONICS COMPARTMENT CORROSION ON FRAME AT FS 333, BTW STGR 25 AND 26R ON MAIN AVIONICS COMPARTMENT WAS EVALUATED OUT OF LIMITS THEREFORE WAS REPAIRED PER CRJ-900 SRM 53-00-06-201-006-A01 AND CRJ 900 SRJul 30, 2026 · N930XJ · Cndair CL6002D24 · Fuselage Main, FrameSDR AALA202609109229Bottle · no testAIRCRAFT IN BASE MAINTENANCE: PASSENGER CREW DOOR 842 DAMPER AND EMERGENCY OPERATION CYLINDER DOES NOT PASS THE DAMPING FUNCTIONAL CHECK - REPLACED DAMPER AND EMERGENCY OPERATION CYLINDER PER AMM 52-13-00Jul 30, 2026 · N583UW · Airbus A321231 · Passenger/Crew DoorsSDR SWAA2026090809408Floorbeam · corrodedCORRODED FLOORBEAM, BS 986.5, LBL 42, WL 208.1. REPAIRED THE FLOORBEAM IAW SRM 53-70-51-2R-6, REPAIR 6.Jul 30, 2026 · N8652B · Boeing 7378H4 · Fuselage Main, Floor BeamSDR SWAA2026090849637Floor Support · crackedCRACK ON FLOOR SUPPORT BTW BS 344 TO BS 360 RBL 51 WL 208.1. REPLACED THE FLOOR SUPPORT IAW SRM 51-10-02, ITEM 9, SRM 51-40-02, AND DWG 141A5400, SHEET 14, REV -.Jul 30, 2026 · N8652B · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2026090804567Floor Support · corrodedCORRODED FLOOR SUPPORT, BS 947.5 - 967, LBL 50, WL 208.1. REPLACED THE FLOOR SUPPORT IAW SRM 51-10-02, ITEM 9, & DWG 147A5650, SHEET 55, REV A.Jul 30, 2026 · N8652B · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2026090823969Floor Support · corrodedCORROSION ON INTERCOSTAL LOCATED BTW BS 947.5 TO BS 967 RBL 50 WL 208.1 AT AFT GALLEY AREA . REPLACED INTERCOSTAL LOCATED BTW BS 947.5 TO BS 967 RBL 50 WL 208.1 AT AFT GALLEY ARE IAW B737-800 SRM 51-10-02 ITEM 9 SRM 51-40-02 AND DWG 147A5650 SHEET 71 REV A.Jul 30, 2026 · N8652B · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2026090875602Fitting · corrodedCORROSION ON FITTING LOCATED BTW BS 992.8 TO BS 1016 LBL 31 WL 208.1 AT AFT GALLEY AREA. REPLACED FITTING LOCATED BTW BS 992.8 TO BS 1016 LBL 31 WL 208.1 AT AFT GALLEY AREA IAW SRM 51-40-02 AND DWG 147A5700 SHEET 121 REV A.Jul 30, 2026 · N8652B · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SIMA20260730007Bracket · corrodedLEVEL 2 CORROSION AFT CARGO ? FR 80-81, STR 24R-27R CORROSION AT MULTIPLE LOCATIONS. (MAJOR REPAIR). AFT CARGO, FR80, STR 26R SHEAR CLIP REQUIRES REPLACEMENT DUE TO 100% MATERIAL LOSS. LOCATED AND DRILLED NEW SHEAR CLIP IAW E175-SRM 51-40-02 (PN# 170-85667-001Jul 30, 2026 · N212NN · Emb ERJ170200LR · Fuselage Miscellaneous StructureSDR SIMA20260730006Shear Tie · corrodedLEVEL 2 CORROSION (MAJOR REPAIR) AFT CARGO, FR 88, STR 27R, CORROSION AT SHEAR TIE FWD OF WASTE BOX. BLENDED SHEAR TIE AT FR 88, STR 27R HAS 100 % MATERIAL LOSS. LOCATED AND DRILLED NEW AFT CARGO- FR 88, STR 27R SHEAR TIE, FWD OF WASTE BOX IAW SRM 51-40-02 APJul 30, 2026 · N212NN · Emb ERJ170200LR · Fuselage Internal Mounting StructureSDR SWAA2026090768218Web · crackedCRACKED WEB LOCATED BTW BS 312 TO BS 328 LBL 47.5 WL 208.1. REPLACED THE WEB IAW SRM 51-10-02, ITEM 9, SRM 51-40-02, & DWG 141A5400, SHEET 26, REV -.Jul 30, 2026 · N8652B · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2026090775577Support Angle · crackedCRACK CARGO LINER SUPPORT ANGLE LOCATED BS 727B AND AT LBL 20 UPPER POSITION AT AFT CARGO COMPARTMENT. PERFORMED PERMANENT REPAIR ON CARGO LINER SUPPORT ANGLE LOCATED BS 727B AND AT LBL 20 UPPER POSITION AT AFT CARGO COMPARTMENT IAW SRM 51-70-11-2R-0 .Jul 30, 2026 · N8652B · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2026090796735Floor Support · crackedCRACKED FLOOR SUPPORT LOCATED BTW BS 277 - 294.5, RBL 1, WL 208.1, FWD GALLEY AREA. REPLACED THE FLOOR SUPPORT IAW SRM 51-40-02 SRM 51-10-02 PARAGRAPH 9, AND DWG 141A5400, SHEET 20, REV- .Jul 30, 2026 · N8652B · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2026090219233Shield · corrodedCORRODED SHIELD WEB, BS 500 - 500A, RBL 21, WL156 IN THE FWD CARGO BAY. REPLACED SHIELD WEB IAW SRM 51-10-02, ITEM 9, SRM 51-40-02, DWG 143A0080, SHEET 39, REV -.Jul 30, 2026 · N8648A · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2026090260355Bracket · crackedCRACK TRAILING EDGE BRACKET, DEFLECTOR AREA. ORSS 273 RT WING. REPLACED THE BRACKET IAW SRM 51-40-02, & DWG 115A6260, REV A.Jul 30, 2026 · N8648A · Boeing 7378H4 · Wing Main, Frame StructureSDR SWAA2026090260931Tie Clip · crackedCRACKED TIE CLIP, BILGE AREA BS 500I, STR26L. REPLACED THE TIE CLIP IAW SRM 51-40-02, AND DWG 143A1234, SHEET 19, & SHEET 20, REV-.Jul 30, 2026 · N8648A · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2026090235638Support Angle · corrodedCORRODED SUPPORT ANGLE, BS 500I LBL 21 - RBL21, WL 156 IN THE FWD CARGO BAY. REPLACED THE SUPPORT ANGLE IAW SRM 51-10-02, ITEM 9, & SRM 51-40-02.Jul 30, 2026 · N8648A · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2026090219089Attach Angle · crackedRIGHT BS 663 UPPER ATTACH ANGLE WAS CRACKED ON VAPOR BARRIER, RBL 11, WL 167.68. CRACK FOUND TO BE OUT OF LIMITS IAW SRM 57-10-10-1A-2. REPAIRED THE ATTACH ANGLE IAW EA-M-26-157-01143.Jul 30, 2026 · N8709Q · Boeing 7378 · Fuselage Main, Attach FittingsSDR SWAA2026090259031Support Angle · crackedCRACK CARGO LINER SUPPORT ANGLE BS 727B LBL 51 AT AFT CARGO COMPARTMENT. PERFORMED PERMANENT REPAIR ON CARGO LINER SUPPORT ANGLE BS 727B, LBL 51 IAW SRM 51-70-11-2R-0, SHEET 2, FIGURE 201.Jul 30, 2026 · N8648A · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2026090218272Tie Clip · crackedCRACKED TIE CLIP, BILGE AREA, BS 500I STR 26R IN THE FWD CARGO BAY. REPLACED THE TIE CLIP IAW SRM 51-40-02-0G, & DWG 143A1234, SHEET 20, REV -.Jul 30, 2026 · N8648A · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2026090278295Angle · crackedCRACKED ANGLE LOCATED FWD SIDE OF FRAME BS 500H, STR 26L IN THE FWD CARGO BAY. REPLACED THE ANGLE IAW SRM 51-40-02-0G-0, & DWG 143A7505, SHT 117, REV-.Jul 30, 2026 · N8648A · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2026090250385Support Angle · crackedCRACKED CARGO LINER SUPPORT ANGLE BS 727D, LBL 51 IN THE AFT CARGO BAY. PERFORMED A REPAIR OF THE SUPPORT ANGLE BS 727D, LBL 51 IAW SRM 51-70-11-2R-0, REPAIR GENERAL. SRM 51-40-02. SRM 51-10-02.Jul 30, 2026 · N8648A · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2026090289879Intercostal · crackedCRACKED INTERCOSTAL LOCATED BTW BS 500A TO 500B AND RBL21 FWD CARGO BAY. REPLACED INTERCOSTAL IAW SRM 51-40-02-0G, & DWG 143A7505, SHEET 137, REV -.Jul 30, 2026 · N8648A · Boeing 7378H4 · Fuselage Miscellaneous Structure