Service difficulty reports

1,771,708 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 2026FA0000341Skin · corrodedCORROSION WAS FOUND ON RIGHT HAND WING UPPER SKIN COMMON TO AFT SPARMay 8, 2026 · N376QS · Cessna 680CE · Wing, Plate/SkinSDR DALA2026050802922Socket · damagedWING/ENGINE SCAN LIGHTS INOP, 1 RH AFT UPPER AND 1 RH FWD LOWER AND 1 LH AFT LOWER HAD SOME HEAT DAMAGE. REPLACED RH AFT UPPER, RH FWD LOWER AND LH AFT LOWER LAMP SOCKET. OPS CHECK GOOD. (1582780) AIRCRAFT WAS GROUNDED.May 8, 2026 · N827NW · Airbus A330302 · Exterior LightingSDR DALA2026050802921Water Heater · failedLAVS AT 3 INBD ELECTRICAL ODOR. REPLACED HOT WATER HEATER PER A330 AMM 38-14. OK FOR SERVICE. (1583286) AIRCRAFT WAS GROUNDED.May 8, 2026 · N822NW · Airbus A330302 · Potable Water SystemSDR ABXA20260508191Isolation Valve · warning lightAFTER ENGINE START, L BLEED ISOLATION VALVE DISCRETE LIGHT AND YELLOW EICAS MESSAGE ON WHEN VALVE COMMANDED CLOSED. CREW RETURNED TO GATES (BTB). MTC SWAPPED L+C ISOLATION VALVES IAW B767 AMM 36-11-04 OPS/LEAK CHECK GOOD FOR L ISOLATION VALVE AC REMAINS NO ETOMay 8, 2026 · N762CK · Boeing 7673P6 · Pneumatic Distribution SystemSDR P5CA2026050800023Lamp · inoperativeDURING RON CHECK, FOUND MULTIPLE EMERGENCY LIGHTS INOP IN GALLEY AREA(<P>RELAMPED MULTIPLE LIGHTS IN GALLEY AREA PER AMM 33-51-01 & 33-51-03. OPS CHECK GOOD</P>)May 8, 2026 · N777SA · Boeing 777FZB · Emergency LightingSDR 2026F00101Fitting · corrodedAFTER REMOVAL OF NLG ACTUATOR FOUND CORROSION ON THE AFT FITTING ASSEMBLY. PERFORMED NLG SKIN CUTOUT, REMOVED EXISTING CORRODED NLG ACTUATOR FITTING P/N 7411213-5, S/N 31533942U AND INSTALLED A NEW CUSTOMER SUPPLIED FITTING P/N 7411213-5, S/N 34783587V, IN SAMMay 8, 2026 · N917QS · Cessna 680A · Fuselage Main, Attach FittingsSDR SWIA2026050777454Skin · corrodedCORROSION FOUND ON INNER FUSELAGE SKIN BETWEEN FS310 AND FS319 , STR25L TO STR26L. REPAIRED INNER SKIN IAW REO 670-53-21-2887 REV-.May 7, 2026 · N611SK · Cndair CL6002C10 · Fuselage Main, Plate/SkinSDR 4VAA202605070007Spar · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE LH FLAP LOWER FRONT SPAR IN TWO PLACES. THE LT FLAP LOWER FRONT SPAR WAS REPAIRED IN ACCORDANCE WITH SAAB STATEMENT 2000SDS060664.May 7, 2026 · N749SA · Saab 2000SAAB · Wing SparSDR SWIA2026050777014Skin · corroded640BB WING PLANK HAS CORROSION AROUND ENTIRE OPENING. (C-CHECK RO 08/28/2026)REPAIRED CORROSION DAMAGE AROUND FUEL PANEL 640BB OPENING IAW BOMBARDIER REO 601R-57-21-030, REV -L, DATED 2014-02-05. BOND AND LEAK CHECKS GOOD. COMPLETED AND ATTACHED TASKCARD 51-May 7, 2026 · N477CA · Cndair CL6002B19 · Wing, Plate/SkinSDR SWIA2026050776901Skin · corrodedAIRCRAFT SKIN AT PANEL 195BB HAS CORROSION AT FASTENER HOLES. REPAIRED CORROSION DAMAGE ON AIRCRAFT SKIN AT PANEL 195BB AT FASTENER HOLES IAW REO 601R-53-61-8546, REV--, SEE CONTINUE CARD FOR WORK PERFORMED, COMPLIED WITH 51-900-1003-SKY. LEAK CHKD OK.May 7, 2026 · N936EV · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR IPXA2026080258533Keelbeam · crackedMAJOR REPAIR, DURING HFEC INSPECTION, (2 EA) CRACK INDICATION NOTED AT THE LEVEL OF NLG CONNECTING FITTING ON THE LOWER STIFFENER BTW FR13A AND FR14, LH SIDE. MARKED IN RED. ACCOMPLISHED THE REPAIR PER EA#300-5312-27-A4499 REV -.May 7, 2026 · N141UP · Airbus A300F4622R · Fuselage Main, KeelSDR IPXA2026061658446Keelbeam · crackedMAJOR REPAIR, DURING ROTOTEST, (1 EA) CRACK INDICATION NOTED AT RH FWD LOWER HOLE OF THE KEEL BEAM BTW FR13A AND FR14 AT 4 O'CLOCK POSITION LOOKING I/B. ACCOMPLISHED THE REPAIR PER EA#300-5312-27-A4498 REV -.May 7, 2026 · N141UP · Airbus A300F4622R · Fuselage Main, KeelSDR SWAA2026061596478Skin · crackedCRACK OF 0.25' APPROX ON FORWARD ENTRY DOOR INTERNAL SKIN, MIDDLE, AT BS 344 AND WL 237. REPAIRED IAW EA 26-152-01267 WITH INSPECTION THRESHOLD TRACKED IN EA 26-152-01267-DTI.May 7, 2026 · N925WN · Boeing 7377H4 · Passenger/Crew DoorsSDR SWAA2026061596314Support Plate · corrodedCORROSION AFT CARGO BAY L/H FLOOR TO SIDEWALL SUPPORT PLATE MULTIPLE AREAS AROUND NUT PLATE HOLES, BS 727B - 767, LBL 22, WL 156. REMOVED AND REPLACED THE AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT, BS 727 - 847, LBL 22, WL 156, IAW SRM 51-40-05-0G-0, SRM 51-May 7, 2026 · N925WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2026061596316Cargo Track · crackedAFT CARGO BAY CARGO TRACK IS CRACKED BS 767 - 747, RBL 13, WL 156. REPAIRED IAW EA 26-153-01273.May 7, 2026 · N925WN · Boeing 7377H4 · Fuselage, Seat/Cargo Attach FittingsSDR SWAA2026061596315Sidewall Support · corrodedCORROSION AFT CARGO BAY RT FLOOR TO SIDEWALL SUPPORT PLATE HAD MULTIPLE AREAS AROUND NUT PLATE HOLES, BS 727B - 767, RBL 22, WL 156. EVALUATED, REMOVED, LOCATED, DRILLED, AND INSTALLED A NEW FLOOR TO SIDEWALL SUPPORT BS 727 - 767, RBL 22, WL 156, IAW SRM 51May 7, 2026 · N925WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2026061596317Sidewall Support · corrodedCORROSION FWD CARGO BAY LT FLOOR TO SIDEWALL SUPPORT PLATE AT MULTIPLE AREAS AROUND NUT PLATE HOLES, BS 460 - 500B, LBL 22, WL 156. CORROSION ON FWD CARGO BAY LT FLOOR TO SIDEWALL SUPPORT PLATE, BS 396 - 500D, LBL 22, WL 156, FOUND TO BE OUT OF LIMITS. REMay 7, 2026 · N925WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2026061596457Splice Strap · corrodedCORROSION AFT CARGO BAY FLOOR SPLICE STRAP AROUND NUT PLATE HOLE, BS 727D+6, RBL 11.5, WL 156. CORROSION ON STRAP WAS FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS ARE GIVEN IN THE SRM. RECEIVED A NEW CARGO BAY FLOOR SPLICE STRAP. THE NEW STRAP TO BE INSTALLEMay 7, 2026 · N925WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2026061596459Splice Strap · corrodedCORROSION AFT CARGO BAY FLOOR SPLICE STRAP AROUND NUT PLATE HOLE, BS 767+6, RBL 11.5, WL 156. CORROSION ON STRAP WAS FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS ARE GIVEN IN THE SRM. RECEIVED NEW CARGO BAY FLOOR SPLICE STRAP, THE NEW STRAP TO BE INSTALLED ONMay 7, 2026 · N925WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2026061596479Floor Panel · debondedFLOOR PANEL 231ZF UPPER SKIN HAS A LARGE DEBONDED AREA NEAR AFT EDGE. FABRICATED A NEW 231ZF FLOOR PANEL ACCOMPLISHED IAW SRM 53-00-50-2R-0.May 7, 2026 · N925WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2026061596480Floor Panel · debondedFLOOR PANEL 232SF UPPER SKIN HAS LARGE DEBONDED AREA NEAR AFT EDGE. FABRICATED A NEW 232SF FLOOR PANEL ACCOMPLISHED IAW SRM 53-00-50-2R-0.May 7, 2026 · N925WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2026061596481Floor Panel · pulledFLOOR PANEL 241CF UPPER SKIN HAS AREAS OF PULLED STRANDS. REPLACEMENT FLOOR PANEL 241CF WAS FABRICATED IAW SRM 53-00-50-2R-0.May 7, 2026 · N925WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2026061596470Fastener · looseAFT ENTRY DOOR SLIDE COVER AFT GIRT BAR RETAINER FASTENERS ARE LOOSE. REMOVED AND REPLACED FASTENERS ON AFT ENTRY DOOR SLIDE COVER AFT GIRT BAR IAW SRM 51-40-02-0G-0 .May 7, 2026 · N925WN · Boeing 7377H4 · Emergency EquipmentSDR SWAA2026061596483Scuff Plate · crackedFWD SERVICE DOOR SCUFF PLATE CRACKED AT AFT EDGE. REMOVED THE COATINGS AND OTHER UNWANTED MATERIALS FROM THE SCUFF PLATE BEFORE WELDING IAW SRM 53-10-15-2R-2 STEP 4.B.(3). REFERRED TO SOPM 20-30-03, WELDED THE DAMAGED AREA ON SCUFF PLATE IAW SRM 53-10-15-2R-May 7, 2026 · N925WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2026061596087Former · crackedWING TO BODY FAIRING FORMER IS CRACKED BS 500D BETWEEN STRINGER 19 AND 20 L/H. REMOVED DAMAGED FAIRING FORMER AND INSTALLED NEW WING TO BODY FAIRING FORMER AT BS 500D BETWEEN STRINGER 19 AND 20 R/L PER SRM 51-40-02-0G-0; AND DWG 116A3010 REV: -.May 7, 2026 · N925WN · Boeing 7377H4 · Aerodynamic FairingsSDR REXA2026070301058Fitting · corrodedCORROSION AND WEAR WAS FOUND ON LUG BORE ON AIL STA .336.4015 (LUG L1) AND 337.657 (LUG L2) AT LH AILERON. LUG BORE L 1=(STA=336.4015), L2=(STA=337.657), L5=(STA=342.911) & L6=(STA=344.1665) ON CENTTER FITTING AT LH AILERON WERE REPAIRED PER REO 670-57-61-237 May 7, 2026 · N927XJ · Cndair CL6002D24 · AileronsSDR SWIA2026050776438Roller · excess playLEFT SLAT TRACK 3-2 OUTBOARD FWD ROLLER EXCESSIVE FREE PLAY. INSTALLED NEW LEFT SLAT TRACK 3-2 OUTBOARD FWD ROLLER IAW 27-81-44-400-803-A01 ,EXTENSION/RETRACTION OF SLATS GOOD AT THIS TIME.May 7, 2026 · N770SK · Cndair CL6002C10 · Leading Edge DevicesSDR SWIA2026050776437Roller · stuckRH SLAT TRACK 2-2 OUTBOARD FWD ROLLER DOES NOT TURN FREELY. INSTALLED NEW RH SLAT TRACK 2-2 OTBD FWD, ROLLER IAW AMM 27-81-44-400-802-A01. EXTENSION/RETRACTION OF SLATS GOOD AT THIS TIME.May 7, 2026 · N770SK · Cndair CL6002C10 · Leading Edge DevicesSDR SWIA2026050776436Roller · excess playRH SLAT TRACK 2-2 INBOARD AFT ROLLER EXCESSIVE FREE PLAY. (CAMP 32216895). (C-CHECK RO 07/01/2026)INSTALLED NEW RH SLAT TRACK 2-2 INBD AFT, ROLLER REF CRJ700 AMM 27-81-44-400-802-A01 CAL TOOL TUC5598 CAL DUE: 31-MAR-27,,EXTENSION/RETRACTION OF SLATS GOOD AT TMay 7, 2026 · N770SK · Cndair CL6002C10 · Leading Edge DevicesSDR SWIA2026050776435Roller · excess playRH SLAT TRACK 1-2 OUTBOARD FWD, ROLLER EXCESSIVE FREE PLAY. INSTALLED NEW RT SLAT TRACK 1-2 OUTBOARD FWD, ROLLER IAW AMM 27-81-44-400-801-A01. OPS TEST GOOD AT THIS TIME.May 7, 2026 · N770SK · Cndair CL6002C10 · Leading Edge DevicesSDR SWIA2026050776434Roller · out of limitsRIGHT SLAT TRACK 1-2 OUTBOARD AFT ROLLER FLAT SPOTS OUT OF LIMITS. INSTALLED NEW RT SLAT TRACK 1-2 OTBD AFT, ROLLER IAW AMM 27-81-44-400-801-A01. EXTENSION/RETRACTION OF SLATS GOOD AT THIS TIME.May 7, 2026 · N770SK · Cndair CL6002C10 · Leading Edge DevicesSDR SWIA2026050776433Roller · excess playRIGHT SLAT TRACK 1-2 INBOARD FWD ROLLER EXCESSIVE FREE PLAY. INSTALLED NEW RT SLAT TRACK 1-2 INBD FWD, ROLLER IAW AMM 27-81-44-400-801-A01. EXTENSION/RETRACTION OF SLATS GOOD AT THIS TIME.May 7, 2026 · N770SK · Cndair CL6002C10 · Leading Edge DevicesSDR SWIA2026050776432Roller · excess playRIGHT SLAT TRACK 1-2 INBD AFT ROLLER EXCESSIVE FREE PLAY. INSTALLED NEW RT SLAT TRACK 1-2 INBD AFT, ROLLER IAW AMM 27-81-44-400-801-A01. ,EXTENSION/RETRACTION OF SLATS GOOD AT THIS TIME.May 7, 2026 · N770SK · Cndair CL6002C10 · Leading Edge DevicesSDR HNAA2026061700535Bulkhead · cracked00300 CRACK IN THE RH WHEEL WELL WEB AT RIB 3. FABRICATED AND INSTALLED DOUBLER OVER CRACK IN THE RH WHEEL WELL WEB AT RIB 3 IAW EMB 145 SRM 53-23-12-RE SEE MINOR EO# EO1-05-26-0228May 7, 2026 · N657AE · Emb EMB145LR · Fuselage Main, BulkheadSDR HNAA2026061700534Floor Support · corrodedRH FLOOR SILL FROM FR 32 FR 35 HAS CORROSION. REMOVED AND REPLACED WITH NEW MID CABIN RH FLOOR SILL FROM FR 32 TO FR 35 IAW EMB 145 SRM 51-40-02-PR, SECTION 2May 7, 2026 · N657AE · Emb EMB145LR · Fuselage Miscellaneous StructureSDR HNAA2026061700533Floor Support · corrodedMID OMEGA BEAM GUSSET FROM FR 32 TO FR 36 HAS CORROSION. REMOVED AND REPLACED WITH NEW MID CABIN MID OMEGA BEAM GUSSET FROM FR 32 TO FR 36 IAW EMB 145 SRM 51-40-02-PRMay 7, 2026 · N657AE · Emb EMB145LR · Fuselage Miscellaneous StructureSDR HNAA2026061700532Floor Support · corrodedLH OMEGA BEAM GUSSET FROM FR 29 TO FR 34 HAS CORROSION. REMOVED AND REPLACED MID CABIN L/H FLOOR SILL FROM FR 29 - FR 34 PER EMB 145 SRM 51-40-02-PR.May 7, 2026 · N657AE · Emb EMB145LR · Fuselage Miscellaneous StructureSDR HNAA2026061700531Floor Support · corrodedRH FLOOR SILL FROM FR 36 TO FR 41 HAS CORROSION. REMOVED AND REPLACED WITH NEW RH FLOOR SILL FROM FR 36 TO FR 41 IAW EMB 145 SRM 51-40-02May 7, 2026 · N657AE · Emb EMB145LR · Fuselage Miscellaneous StructureSDR HNAA2026061700530Floor Support · corrodedMID OMEGA BEAM GUSSET FROM FR 36 TO FR 38 HAS CORROSION. REMOVED AND REPLACED WITH NEW MID CABIN MID OMEGA BEAM GUSSET FROM FR 36 TO FR 38 IAW EMB 145 SRM 51-40-02-PRMay 7, 2026 · N657AE · Emb EMB145LR · Fuselage Miscellaneous StructureSDR HNAA2026061700529Floor Support · corroded00272 LH OMEGA BEAM GUSSET FROM FR 36 TO FR 38 HAS CORROSION. REMOVED AND REPLACED WITH NEW LH OMEGA BEAM GUSSET FROM FR 36 TO FR 38 IAW EMB 145 SRM 51-40-02 STEP 2, B.May 7, 2026 · N657AE · Emb EMB145LR · Fuselage Miscellaneous StructureSDR HNAA2026061700528Floor Support · corroded00271 LH FLOOR SILL FROM FR 36 TO FR 39 HAS CORROSION. FABRICATED AND INSTALLED DOUBLER ON MID CABIN LH FLOOR SILL AT FR39 IAW ETD 2026-145-008549 REV: B. SEE PIEDMONT MAJOR EO# EO1-53-26-0243May 7, 2026 · N657AE · Emb EMB145LR · Fuselage Miscellaneous StructureSDR HNAA2026061700527Floor Support · corrodedLT OMEGA BEAM GUSSET FROM FR 38 TO FR 44 HAS CORROSION. REMOVED CORROSION FROM MID CABIN, 1EA LH OMEGA BEAM GUSSET FROM FR 38 TO FR 44. FOUND IN LIMITSMay 7, 2026 · N657AE · Emb EMB145LR · Fuselage Miscellaneous StructureSDR HNAA2026061700526Floor Support · corrodedRT FLOOR SILL FROM FR 41 TO FR 48 HAS CORROSION. REMOVED AND REPLACED MID CABIN RT FLOOR SILL FROM FR 41 - FR 48 PER EMB 145 SRM 51-40-02-PR.May 7, 2026 · N657AE · Emb EMB145LR · Fuselage Miscellaneous StructureSDR HNAA2026061700525Floor Support · corroded00254 LH OMEGA BEAM GUSSET FROM FR 50 TO FR 53 HAS CORROSION. REMOVED AND REPLACED MID CABIN LH OMEGA BEAM GUSSET FROM FR 50 TO FR 53 IAW SRM 51-40-02-PRMay 7, 2026 · N657AE · Emb EMB145LR · Fuselage Miscellaneous StructureSDR HNAA2026061700524Floor Support · corroded00253 CORROSION RH SILL BETWEEN FRAMES 65 AND 66. REMOVED AND REPLACED RH FLOOR SILL FROM FR 65 - FR 66 PER EMB 145 SRM 51-40-02-PR.May 7, 2026 · N657AE · Emb EMB145LR · Fuselage Miscellaneous StructureSDR HNAA2026061700523Floor Support · corroded00249 RH FLOOR SILL AT FR 48 HAS CORROSION. REMOVED AND REPLACED MID CABIN RH FLOOR SILL AT FR 48 IAW EMB 145 SRM 51-40-02-PRMay 7, 2026 · N657AE · Emb EMB145LR · Fuselage Miscellaneous StructureSDR HNAA202606170522Floor Support · corroded00248 MID OMEGA BEAM GUSSET FROM FR 44 TO FR 52 HAS CORROSION. REMOVED AND REPLACED WITH NEW MID CABIN MID OMEGA BEAM GUSSET FROM FR 44 TO FR 52 IAW EMB 145 SRM 51-40-02-PRMay 7, 2026 · N657AE · Emb EMB145LR · Fuselage Miscellaneous StructureSDR HNAA2026061700521Door Frame · gouged00238 SERVICE DOOR INNER FRAME STRUCTURE ON RH SIDE MIDDLE OF DOOR IS GOUGED/SCRATCHED ON PREVIOUS REPAIR. CUTOUT AND INSTALLED FILLER AND DOUBLER ON SERVICE DOOR INNER FRAME STRUCTURE RH SIDE MIDDLE OF DOOR IAW EMB 145 SRM 52-43-01 STEP 7 FIG. 208. SEE PIEDMay 7, 2026 · N657AE · Emb EMB145LR · Fuselage Main, StructureSDR HNAA2026061700520Floor Support · corroded00237 LH OMEGA BEAM FLANGE FROM FR 53 TO FR 59 HAS CORROSION. REMOVED CORROSION BY BLENDING ON AFT WET AREA, 1EA LH OMEGA BEAM FLANGE FROM FR 53 TO FR 59. FOUND WITHIN MAXIMUM ALLOWABLE LIMITS IAW EMB 145 53-24-10-AD.May 7, 2026 · N657AE · Emb EMB145LR · Fuselage Miscellaneous StructureSDR HNAA2026061700519Floor Support · corroded00236 MID OMEGA BEAM FLANGE FROM FR 53 TO FR 59 HAS CORROSION. REMOVED CORROSION BY BLENDING ON AFT WET AREA, 1EA MID OMEGA BEAM FLANGE FROM FR 53 TO FR 59. FOUND TO BE WITHIN MAXIMUM ALLOWABLE LIMITS IAW EMB 145 SRM 53-24-01-ADMay 7, 2026 · N657AE · Emb EMB145LR · Fuselage Miscellaneous Structure