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 VNAA202610300012Hinge · wornIN REF TO TRFKE00EQGMU: PERM REPAIR - PASSENGER DOOR SURROUND STRUCTURE - HINGE REPLACEMENT REPLACE THE PASSENGER DOOR HINGE IAW SRM 53-21-23-201-007-A01. AFTER HINGE REPLACEMENT. ENGINEERING
COMMENTS: PAX DOOR HINGE MUST BE REPLACED. TRFKE00EQGMU. PASSENGSDR IPXA2026102336717Support Bracket · crackedAFTER REMOVAL OF ACCESS PANELS 144CR AND 144AR, FOUND SUPPORT BRACKET BROKEN. REMOVED ADN REPLACED SUPPORT BRACKET UNDERNEATH THE PANELS144CR AND 144AR IAW SRM 51-40-21.SDR VNAA202610230062Hinge · wornPERM REPAIR - PASSENGER DOOR SURROUND STRUCTURE - HINGE REPLACEMENT REPLACE THE PASSENGER DOOR HINGE IN ACCORDANCE WITH SRM 53-21-23-201-007-A01. DOOR SURROUND STRUCTURE PASSENGER DOOR HINGE WERE REPLACED PER SRM 53-21-23-201-007-A01.SDR IPXA2026101627405Angle · corrodedAPU INLET SURROUND STRUCTURE FWD STRAP, UPPR AND LWR MID ANGLES, AND UPPR AND LWR FWD CORNER ANGLES HAVE EXFOLIATING CORROSION. VERIFIED STEP 32. REF. RII GMM 04-02.SDR HNAA2026100900970Skin · corrodedCARGO DOOR CUTOUT, THERE IS CORROSION ON THE LOWER EDGE OF THE DOOR CUTOUT, IN-LINE WITH FR 66. REMOVED AND REPLACED CARGO DOOR LOWER CUTOUT SILL IAW SRM 51-40-02.SDR SWIA2026082677540Skin · dentedCOMPLY WITH SCHEDULED MAINTENANCE CODE RA103394-SRM 53-10-01-AD01 MXCODEID113882-PR - COMPLY WITH PERMANENT REPAIR ON RA ID 103394DENT ON LEFT FUSELAGE ABOVE SKYWEST LOGO INSPECTED REPORTED DENT ON LEFT FUSELAGE BETWEEN FR 18 - FR20 STGR12L - STGR 15L FOUND TOSDR HNAA2026100700956Stub Beam · crackedLH WING STUB, FUSE TO WING BOS STUB CRACKED AT BTW FR40-46. REPAIRED IAW ETD 2026-145-015085 AND EO 1-53-26-0436SDR HNAA2026100700954Angle · corrodedRH WING STUB, FUSE TO WING-BOX ANGLE CORRODED AT FR46. RAR ANGLE IAW ETD 2024-145-015085SDR SWAA2026092917117Support Angle · crackedCRACKED SUPPORT ANGLE, BS 500I, STR 28L. REPLACED THE SUPPORT ANGLE IAW SRM 51-10-02, ITEM 9, SRM 51-40-02, AND DWG 143A7902, SHEET 320, REV-.SDR SWAA2026092973065Web · crackedCRACKED WEB TRAILING EDGE PANEL, RT WING, ORSS 266. REPLACED THE WEB AND FASTENERS IAW SRM 51-10-02, ITEM 9, SRM 51-40-02, AND DWG 115A2512, SHEET 16, REV-.SDR SWAA2026092956153Support Angle · crackedCRACKED SUPPORT ANGLE, RT WING, ORSS 261. REPLACED THE SUPPORT ANGLE IAW SRM 51-10-02, ITEM 9, SRM 51-40-02, & DWG 115A2512, SHEET 13, REV- .SDR SWAA2026092933487Support Angle · crackedCRACKED SUPPORT ANGLE, ORSS 271, RT WING. REPLACED THE SUPPORT ANGLE IAW SRM 51-10-02, ITEM 9, AND DWG 115A6200, SHEET 17, REV A.SDR SWAA2026092956067Support Angle · crackedCRACKED SUPPORT ANGLE AT THE FIXED TRAILING EDGE PANEL, ORSS 261, LT WING. REPLACED THE SUPPORT ANGLE IAW RM 51-10-02, PARAGRAPH 9, SRM 51-40-02, DWG 115A2512, SHEET 16, REV-.SDR R61A2026092600262Strap · corrodedDURING HEAVY CHECK, MAINTENANCE FOUND CORRODED FWD WTB FAIRING TO FUSELAGE STRAP FOUND ON CFII AT FR 27-28, STR 24R-28L. THE FWD WTB FAIRING TO FUSELAGE STRAP WAS REPLACED IAW SRM 51-42-02, SRM 51-43-04 AND SRM 51-41-02.SDR HNAA2026092500908Shear Tie · corrodedCARGO UNDERFLOOR, THERE IS CORROSION ON A SHEAR TIE, IN-LINE WITH FR 65, STR 20L-21L. R & R SHEAR TIE IN-LINE WITH FR65 AT STR 20L-21L IAW SRM 51-40-02.SDR HNAA2026092500907Door Frame · corrodedCARGO DOOR CUTOUT, THERE IS CORROSION ON THE LOWER EDGE OF THE DOOR CUTOUT, IN-LINE WITH FR 66. REMOVED AND REPLACED CARGO DOOR LOWER CUTOUT SILL IAW SRM 51-40-02.SDR HNAA2026092100864Floor Support · crackedLEFT OMEGA BEAM OTBD ANGLE CRACKED AT BTWN FR 46-50. R & R ANGLE IAW SRM 51-40-02.SDR HNAA2026092100863Skin · crackedLT WING LEADING EDGE NR 2 LWR SKIN CRACKED AND CORRODED. R & R IAW TASK 866SDR MASA202609142043Service Panel · corrodedDURING HEAVY CHECK CFIII, CORRODED LOWER SKIN WATER SERVICE PANEL REMOVED AND REPLACED IAW AMM 20-10-01-910-801-A, TABLE 201 AND TABLE 206. NRC 4502706-3000-0023. REV 103.SDR MASA202609142041Seat Track · corrodedDURING HEAVY CHECK OF CF ILL AFT WET AREA, CORROSION ON R/H, I/B AFT SEAT TRACK FR 84 R/H, REMOVED BY BLENDING AND AREA REPROTECTED IAW EDT 2026-170-014429, DISPOSITION 001, PERMNENT REPAIR, SEE AWS AND NOT REPORT FOR DETAILS, "NO CRACK FOUND". MAX MATRL REMOVSDR SWAA2026091439838Stringer · deformedSTRINGER 24R, BS 380+11.5, STRINGER DEFORMED. REMOVED AND REPLACED THE DAMAGED STRINGER 24R BTWN BS 362 - 436 IAW SRM 51-40-02-0G-0, IAW DWG 143A0070, REV -.SDR SWAA2026091458223Stringer · crackedSTRINGER 23R, AT BS 380+13, STRINGER IS DEFORMED WITH 3.5 CRACK. STRINGER REMOVED AND REPLACED IAW SRM 51-40-02-0G-0, & DWG 143A3250, REV -.SDR CALA2026090919315Web · corrodedFWD CARGO, LOWER MAIN SILL WEB HAD TWO POINTS OF POSSIBLE CORROSION. REMOVED THE FWD CARGO LOWER MAIN SILL WEB, LOCATED, DRILLED, COUNTERSANK, APPLIED ALODINE, PRIMER, INSTALLED NUTPLATES AND INSTALLED NEW WEB IAW SRM 53-30-15-1A-1, SRM 51-10-02-0G-0, SRM 51SDR CALA2026090719250Support · corrodedLEFT WING LE O/B LOWER PANEL SUPPORT HAS CORROSION AT STA SS 67.53 RH SIDE. REMOVED SUPPORT ON LEFT WING LE O/B LOWER PANEL AT STA. SS 67.53 RH SIDE, RECEIVED NEW SUPPORT TAG A462489 P/N. 116A5301U37, LOCATED AND DRILL NEW SUPPORT, APPLIED ALODINE ON NEW HOLSDR IPXA2026090428170Support Angle · crackedFOUND FWD CARGO DOORWAY CEILING SUPPORT CRACK AT BS 600. REMOVED DAMAGE SUPPORT ANGLE IAW SRM 51-40-02-0G, REV. 96. INSTALLED NEW SUPPORT ANGLE IAW SRM 51-40-02-0G, REV. 96 AND DWG 143T8540, SHT 2, REV B.SDR U5QA202608260178Hydraulic Line · leakingHYD FLUID FROM RT MLG ACTUATOR HOSE. REMOVED RT BRACE ACTUATOR'S PRESSURE & RETURN LINES, INSTALLED NEW HYD LINES IAW GIV-MSG-3 AMM. 32-01-00. COMPLIED WITH SYSTEM BLEEDS, OPS & LEAK CHKD WITH NO FURTHER DISCREPANCIES NOTED.SDR SWAA2026090334823Retainer · missingMISSING RETAINER OF ESCAPE STRAP ON LT EMERGENCY EXIT. INSTALLED THE RETAINER IAW SOPM 20-50-12 REV.58.SDR SWAA2026090356940Retainer · missingMISSING RETAINER FOR ESCAPE STRAP ON THE RT EMERGENCY EXIT. INSTALLED THE RETAINER IAW SOPM 20-50-12 REV.58.SDR SWAA2026090343518Support · corrodedSUPPORT ZEE ASSY CORRODED, FROM BS 727 - 847, LBL 22, WL 156.1. REPLACED THE SUPPORT ZEE IAW SRM 51-40-02-0G, DWG 146A7500, SHEET 173, REV-, & DWG 146A7500, SHEET 176, REV-.SDR N6WA2026090301Seat Track · corrodedCORROSION ON LT FLOOR SEAT TRACK FROM FS349 TO FS477.40. INSTALLED NEW LT FLOOR SEAT TRACK FROM BS 349 - 477.40 IAW AMM 53-00-49.SDR SWIA2026082676962Unknown · odorBURNING PLASTIC SMELL FROM FRONT OF THE CABIN TO AROUND ROW 10. (FLIGHT 6414) PERFORMED PERMANENT DOUBLER REPAIR INSTALLATION TO FUSLEAGE SKIN LOCATED BETWEEN FS 1000.00 - FS 1015.00 AND STRG 25R - STRG 26R IN REF. GOGO REPAIR DWG NO. 601-2365-02-343 AND STRSDR IPXA2026090324513Bulkhead · crackedCRACKED BULKHEAD, NR 1 PYLON AFT FAIRING PANEL 437DD, INNER AREA. REMOVED DAMAGE BULKHEAD IAW SRM 51-40-02-0G, REV. 96. INSTALLED NEW BULKHEAD IAW SRM 51-40-02-0G, REV 96 AND DWG 313T3360, SHT 15, REV B.SDR IPXA2026090324466Bracket · crackedCRACKED BRACKET, NR 1 AFT FAIRING INNER DRAIN TUBE SUPPORT BRACKET. REPLACEED. REMOVED DAMAGE BRACKET IAW SRM 51-40-02-0G, REV 96. INSTALLED A NEW BRACKET IAW SRM 51-40-02-0G, REV 96 AND DWG 272T0333, SHT 8, REV-.SDR IPXA2026090236478Floor Panel · corrodedAFT CARGO FOOR PANEL 153AF HAS CORROSION. LOCATED & DRILLED NEW FLOOR PANEL 153AF AFT CARGO IAW SRM 51-40-05. TREATES & PRIMED NEW FLOOR PANEL 153AF IAW SRM 51-20-01.SDR UIEA2026082600800Seal · brokenCAPT LIFE VEST TAMPER SEAL BROKEN. REMOVED AND REPLACED THE LIFE VEST IAW AMM 25-62-01-960-005. OPS CHKD OK.SDR DALA2026090104934Elec Connector · misinstalledEMERGENCY LIGHT AT SEAT 8A INOPERATIVE. DEFERRED TO MEL 33-50-07A. CONFIRMED 28VDC. FOUND MISSING GND AT P-J3 (988017). T/S FOUND CONNECTOR PARTIALLY INSTALLED T SEAT 7A INTERCONNECT TO 8A REF A350 WDM 33 -51. OPS CHECKS GOOD AFTER SEATING CONNECTOR FOR 7A. SDR IPXA2026090126837Bracket · chafedCHAFED BRACKET, NR 1 ENG RT CORE COWL INNER OPEN ROD STOW AREA. REMOVED THE DAMAGE BRACKET IAW SRM 51-40-02-0G, REV 96. INSTALLED A NEW BRACKET IAW SRM 51-40-02-0G, REV 96, & CMM IPL 71-13-24, REV 51.SDR IPXA2026090123388Bracket · chafedCHAFED BRACKET, NR 2 ENG LT CORE COWL OPEN HOLE ROD BRACKET. REMOVED DAMAGE BRACKET IAW SRM 51-40-02-0G, REV 96. INSTALLED A NEW BRACKET IAW SRM 51-40-02-0G, REV 96, & CMM IPL 71-13-23, REV 47.SDR IPXA2026090123395Bracket · chafedCHAFED BRACKET, NR 2 ENG RT CORE COWL OPEN HOLD ROD BRACKET. REMOVED THE DAMAGED BRACKETS IAW SRM 51-40-02-0G, REV 96. INSTALLED A NEW BRACKET IAW SRM 51-40-02-0G, REV 96, & CMM IPL 71-13-24, REV 51.SDR AALA202609018676Attach Angle · corrodedAIRCRAFT IN BASE MAINTENANCE: LOWER AFT CENTER BULKHEAD ATTACH ANGLE FOUND CORRODED. REMOVED AND INSTALLED Z ANGLE IAW AARD 51-00-05-1 AND BOEING DRAWING 143A9485 AND SRM 51-40-02.SDR DALA2026090104921Light · inoperativeSEAT 10D EMERGENCY LIGHT INOP. R & R 10D EMER ESCAPE PATH LIGHT IAW AMM 33-51-19. LIGHT OPERATES NORMALLY, OKAY FOR SERVICE. (LP: 8828773, AIRCRAFT WAS GROUNDED)SDR DALA2026083104918Skin · corrodedCORROSION UPPER SURFACE IB AFT FLAP LT WING. PERFORMED PERMANENT REPAIR ON UPPER SURFACE IB AFT FLAP LT WING AS PER B767-300 SRM 57-53-01 (1778910)(AIRCRAFT GROUNDED)SDR SWAA2026082756964Transmitter · faultedON FINAL APPROACH DURING FLAP EXTENSION, FLAP INDICATOR WAS AT FLAPS 10 WITH FLAPS LEVER AT 30. RAN THE TRAILING EDGE FLAP DISAGREE QRH CHECKLIST. USED THE ALTERNATE FLAPS SWITCH TO GET FLAPS TO 15_ NO EXISTING FAULTS ON SMYD 1 OR SMYD 2FLIGHT LEG 0 DISPLAYED SDR SWAA2026083189435Light · inoperativeCENTER AISLE AFT 2 SECTIONS OF PHOTOLUMINESCENT STRIPS WILL NOT GLOW R&R CENTER AISLE AFT 2 SECTIONS OF PHOTOLUMINESCENT STRIPS REFERENCE AMM 33-51-15SDR SWAA2026083137585Seal · crackedRIGHT HORIZONTAL STABILIZER FWD UPPER SLIDING SEAL CRACKED ALONG SEAL TRACK EDGE. REMOVED AND REPLACED RIGHT HORIZONTAL STABILIZER FWD UPPER SLIDING SEAL. REF AMM 53-31-31.SDR SWAA2026083159001Lens · missingFWD SERVICE DOOR EXIT IDENTIFIER LENS MISSING INSTALLED LENS REF AMM 33-51-01SDR SWAA2026083100148Flashlight · no testFWD F/A FLASHLIGHT WILL NOT TEST. R & R FORWARD F/A FLASHLIGHT IAW AMM 25-64-00 OPS TEST PASSED.SDR SWAA2026083167183Panel · crackedCRACKED RETAINER INSTALLED ON PANEL ASSY 332AB OBTAINED NEW PANEL FROM STOCK. LOCATED AND DRILLED HOLES PER SRM 51-40-05 AND COUNTERSUNK HOLES PER SRM 51-40-08. C/WSDR SWAA2026083151036Engine · fireUPON POST FLIGHT WALK AROUND, 5 MINUTES AFTER SHUTDOWN, FLAMES WERE OBSERVED INSIDE ENG#2 EXHAUST NOZZLE. EVENTUALLY, FLAMES WENT OUT BY THEMSELVES._ 02 - INSPECTED PER [AMM 71-00-00-800-803-F00-NG (INSPECTION AFTER AN ENGINE FIRE USE OF FIRE EXTINGUISHING AGESDR SWAA2026083146667Stiffener · crackedLEFT MAIN LANDING GEAR MIDDLE DOOR HAS A CRACK IN THE LOWER FWD STIFFENER REMOVED AND REPLACED CENTER DOOR UP TO REF AMM 32-13-11 STEP 3H(4). REQUIRES MAIN LANDING GEAR SHOCK STRUTS DOOR ADJUSTMENT ADJUSTED LH MLG INNER DOOR PER AMM 32-13-11. OPS CHECK GOOD. A