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 SCN2026F00001Light · unsecureCABIN WRITE UP SEAT 11& 12 DEF EMERGENCY STRIP ON FLOOR PEELING OFF. INSPECTED EMERGENCY LIGHT PHOTOLUMINESCENT STRIP AT 11& 12 DEF. FOUND TO BE SECURE AND FUNCTIONAL REF AMM 33-51-15SDR SCNA20260629267Light · unsecureROW 15D EMERGENCY LIGHT STRIP IS TOR AND ON FLOOR. RESECURED LIGHTSTRIP AT 15D REF AMM 33-50-07 OKAY FOR SERVICESDR SCNA20260629265Girt Bar · damagedR2 DOOR GIRT BAR LEFT HAND SIDE OF BAR, THE PLASTIC PIECE IS BROKEN, DEBRIS FOUND WAS FROM AN OLD PIECE. RENTENSION CLIP IS INSTALLED AND SECURED AT 2R DOOR GIRT BAR. OK FOR SERVICE REF 25-66-01.SDR SIMA20260627004None · noneON FINAL APPROACH WHEN THE LANDING GEAR WAS EXTENDED THE FLIGHT ATTENDANT REPORTED SMELLING OF BURNING RUBBER NO FIRE OR SMOKE WAS OBSERVED IN THE CABIN .BY THE TIME WE HAD PARKED AT THE GATE, THE ODOR HAD DISSIPATED. THERE WAS NO FIRE SMOKE OBSERVED IN THE CASDR SIMA20260627001Unknown · odorHARD BOIL EGG/SULFUR SMELL DURING START OF DESCENT FROM FL240, SLOWING DOWN, AND APU START FOR APPROX 1 MINUTE AT A TIME. PRESSURIZED AT THE TIME OF FIRST SMELLING ODOR. FAS DID A SWEEP THROUGH OF CABIN, NO ONE WAS EATING EGGS AND THERE WE'RE NONE IN THE OVERHSDR JJBA20260629020Battery · inoperativeALL FWD EMERGENCY LIGHTS MOMENTARILY COME ON THEN DIM OFF. REMOVED AND REPLACED NR 1 EMERGENCY LIGHT BATTERY. OPS CHECK SAT.SDR SIMA20260627002Indication Sys · faultedHYD (2) LO PRESS [CAUTION] AND HYD (2) LO QTY ADVISORY RECEIVED IN FLIGHT. PRESS WAS 0 AND QTY SHOWED 0 WHEN EICAS MESSAGES RECEIVED. RAN QRH. DECLARED EMERGENCY AND DIVERTED TO KBIL AS PRECAUTION. PERFOMRED HYD LOW FIM TASK 29-11-00-810-806-A. INSPECTED SERVSDR CALA2026062917382Housing · damagedEMERGENCY LIGHTS - OPERATIONAL CHECK EMERGENCY LIGHTS OPERATIONAL CHECK - ROW 29 ABC EPL SHROUD IS DAMAGED AND NOT SECURED TO SEAT REMOVED AND REPLACED THE BROKEN SHROUD. REF CMM 25-21-56.SDR CALA2026062917381Battery · faultedEMERGENCY FUEL SHUTOFF BATTERY ASSY REQUIRES RESTORATION. REMOCED AND REPLACED EMERGENCY FUEL SHUTOFF BATTERY ASSY IAW BOEING 737 MAX AMM 28-22-14 OPS CHECK GOOD.SDR CALA2026062917380Battery · no testEMERGENCY LIGHTING EPSU FAILED BITE TEST PER TASK CARD 18-3351-1-0003. FAULT CODE 10WL DISPLAYED AS A RESULT OF THE TEST. INSTALLED SERVICABLE EPSU BATTERY P/N 3214-31 REF AMM 33-51-38-400-002-A. OPS CHECK NORMAL.SDR FDEA202606270817Battery Pack · failedR1 EMERGENCY LIGHT DOESN'T STAY ON FOR THE COMPLETE LIGHT TEST. L1 LIGHT NORMAL. AMM 33-51-07-2 REMOVED POWER SUPPLY BATTERY PACK, HAS POWER AT POWER SUPPLY, REPLACED BATTERY PACK, OPS NORMAL. OK TO CONTINUE.SDR FDEA202606270812Floor Panel · puncturedMAIN DECK CARGO COMPARTMENT, L/H FLOOR PANEL 241KFFHAS PUNCTURE DAMAGE. JM10 FABRICATED NEW FLOOR PANEL 241KFF, MPN: 145T5876-8, LBL 77.5 - LBL 89.5, STA 821 - 933 IN REF. TO BOEING DWG 145T5876-8, AND SR67-53-009. SEE JPF FOR ALL THE WORK PERFORMED. THIS SDR FDEA202606270811Floor Panel · damagedMAIN DECK CARGO COMPARTMENT, R/H OUTBD FLOOR PANEL 232NFF HAS PUNCTURE DAMAGE. FABRICATED NEW FLOOR PANEL 232NFF, RBL 86.5 - RBL 77.5, BS 654 22 - 675 IAW DWG 143T5876-20, AND SRM 67-53-009. PERFORMED. THIS IS A MAJOR REPAIR. FOR INSTALLATION OF THIS PANESDR JR2R20260627898Doubler · corrodedFWD FLOOR DOUBLER AT FR16 BETWEEN LBL12 TO LBL40 IS CORRODED. REPAIRED PER ETD.SDR JR2R20260627900Doubler · corrodedFWD FLOOR DOUBLER AT FR16 BETWEEN LBL12 TO LBL40 IS CORRODED. REPAIRED PER ETD.SDR JR2R202606279946Floorbeam · corrodedUPON REMOVAL OF RT FWD FLOOR DOUBLER AT FR12-FR14, FOUND CORROSION ON FR 14 CROSSBEAM BETWEEN RBL 30 AND RBL 42. REPAIRED IAW ETD.SDR JR2R20260627903Seat Track · corrodedFWD SEAT TRACK AT LBL 11 FR 17 IS CORRODED. REPAIRED PER SRM.SDR JR2R20260627902Floorbeam · corrodedFLOORBEAM AT FR 17 BETWEEN LBL5 TO LBL10 IS CORRODED. REPAIRED IAW SRM.SDR JR2R20260627893Floorbeam · corrodedFWD WET AREA CROSSBEAM AT FR 14, RBL 30 IS CORRODED. REPAIRED PER ETD.SDR JR2R20260627879Strap · corrodedFLOOR SUPPORT UPPER STRAP AT LBL 11 BETWEEN FR 85 - FR 86 IS CORRODED. REPLACED PER SRM.SDR JR2R20260627882Doubler · corrodedAFT WET AREA FLOOR GUSSET TEXAS DOUBLER AT FR90 RBL24 IS CORRODED. REPLACED PER SRM.SDR ABXA20260627287Fire Loop · warning messageRIGHT ENGINE FIRE LOOP NR 1 ILLUMINATED, CREW DEFERRAL IAW MEL 26-11-1-1. MTX PERFORMED VISUAL INSP AND OPS TEST OF ENGINE FIRE DETECTION SYSTEM IAW AMM 26-11-00 NO DEFECTS NOTED AT THIS TIME OPS CHECK GOOD.AND RETURNED ACFT TO SERVICESDR JR2R20260627079Fitting · chafedNR 1 ENGINE PYLON INBOARD AND OTBD UPPER LINK FITTINGS ARE CHAFED & GOUGED. REPAIRED PER ETD.SDR JR2R20260627851Fitting · chafedNR 2 ENGINE PYLON INBOARD AND OUTBOARD UPPER LINK FITTINGS ARE CHAFED & GOUGED. REPAIRED PER ETD.SDR IXXA20260627002Stiffener · crackedNUMBER 2 PYLON AFT SECTION V-WEB HAS OUTBOARD VERTICAL STIFFENER CRACKEDSDR IXXA20260627001Stiffener · crackedNUMBER 2 PYLON AFT SECTION V-WEB AREA HAS INBOARD VERTICAL STIFFENER CRACKEDSDR SWIA2026062677615Door Frame · corrodedPAX DOOR FRAME BS 313.56 BTWN DD4 AND DD5 WAS CORRODED. REPLACED WITH A NEW PASSENGER DOOR FRAME BS 313.56 IAW SRM 51-42-06-001-001-A01, SRM 51-42-21-001-001-A01, AND DWG 601R31702, REV N. COMPLIED WITH SKYWEST TASK CARD 51-900-1002-SKY. PRESSURE LEAK CHECKSDR SWIA2026062677550Floorbeam · corrodedRIGHT BS 280 FLOORBEAM WAS CORRODED INSIDE OF SCRW HOLES. REMOVED AND REPLACED FLOORBEAM IAW SRM 51-42-06-001-001-A01, 51-42-13-001-001-A01, 51-42-21-001-001-A01, AND 51-42-22-001-001-A01.SDR SWIA2026062677239Skin · dentedCOMPLY WITH SCHEDULED MAINTENANCE CODE RA27400-STS EA 25-2015-093 969SW-DTI, DAMAGE TOLERANCE INSPECTION. REPAIRED A DENT LOCATED AFT OF BS 250 AND BTWN STRS 25R AND 26R, NDT PERFORM NDT LFEC GVI PER EA 25-2015-093, REV B, SEC II DTA, PER CUSTOMER REQUEST CSDR SWIA2026062677235Skin · dentedCOMPLY WITH SCHEDULED MAINTENANCE CODE RA27402-STS EA 30-2015-160 969SW-DTI, DAMAGE TOLERANCE INSPECTION. REPAIRED LOWER FUSELAGE SKIN DENT JUST AFT OF BS 605, BTWN STR 24L - 26L, NDT PERFORM NDT LFEC GVI IAW EA 30-2015-160, REV A, SEC II DTA, COMPLIED WITSDR IPXA2026082980480Support · corrodedAFT CARGO COMP LH SIDEWALL PANEL STRUCTURE HAS SURFACE CORROSIONS BETWEEN FR.57.3 TO FR.59. INSTALLED NEW PROFILE IAW SRM 51-40-21-001.SDR IPXA2026082980668Sidewall Support · corrodedAFT CARGO COMP. RH SIDEWALL PANEL SUPPORT FITTING HAS SURFACE CORROSION AT FR.57. INSTALLED NEW RH SIDEWALL PANEL SUPPORT FITTING IAW A300-600 SRM 51-40-21-001.SDR IPXA2026082980617Sidewall Panel · corrodedAFT CARGO COMP. RT SIDEWALL PANEL STRUCTURE CORRODED AT UPPER LT CORNER BS 3353. FR.54. INSTALLED NEW CORNER PROFILE IAW SRM 51-40-21-001.SDR REXA2026082601684Latch · crackedAFTER COAMING LATCH REMOVAL, CRACK ON SKIN AT LH UPPER TRANSCOWL WAS FOUND. SKIN AT LH UPPER TRANSCOWL WAS REPAIRED PER EA NO: CRJ954-22469 REV ASDR REXA2026082401613Bracket · corrodedCORROSION ON UPPER AND LOWER MLG HYD LINES SUPPORT PLATE (IN BK, LG EXT, LG RET) AT LH/RH WHEEL WELL AREA, APROX RBL 39/LBL 39. DUE TO EXCESSIVE CORROSION ON UPPER AND LOWER MLG HYD LINES SUPPORT PLATE (IN BK, LG EXT, LG RET) AT LH/RH WHEEL WELL AREA, APROX RBSDR REXA2026082401612Plate · corrodedCORROSION ON UPPER AND LOWER MLG HYD LINES SUPPORT PLATE (IN BK, LG EXT, LG RET) AT LH/RH WHEEL WELL AREA, APROX RBL 39/LBL 39. DUE TO EXCESSIVE CORROSION ON UPPER AND LOWER MLG HYD LINES SUPPORT PLATE (IN BK, LG EXT, LG RET) AT LH/RH WHEEL WELL AREA, APROX RBSDR REXA2026082401611Bracket · corrodedCORROSION ON UPPER AND LOWER MLG HYD LINES SUPPORT PLATE (IN BK, LG EXT, LG RET) AT LH/RH WHEEL WELL AREA, APROX RBL 39/LBL 39. DUE TO EXCESSIVE CORROSION ON UPPER AND LOWER MLG HYD LINES SUPPORT PLATE (IN BK, LG EXT, LG RET) AT LH/RH WHEEL WELL AREA, APROX RBSDR REXA2026082401610Bracket · corrodedCORROSION ON UPPER AND LOWER MLG HYD LINES SUPPORT PLATE (IN BK, LG EXT, LG RET) AT LH/RH WHEEL WELL AREA, APROX RBL 39/LBL 39. DUE TO EXCESSIVE CORROSION ON UPPER AND LOWER MLG HYD LINES SUPPORT PLATE (IN BK, LG EXT, LG RET) AT LH/RH WHEEL WELL AREA, APROX RBSDR REXA2026082401563Diaphragm · crackedCRACK AND BROKEN DIAPHRAGMS ON LT & RT WHEEL WELL AREA APROX RBL 34 - LBL 34. DIAPHRAGMS ON LT & RT WHEEL WELL AREA APROX RBL 34 - LBL 34 WERE REPLACED PER SRM 51-41-02-001-001-A01SDR REXA2026082401562Diaphragm · crackedCRACK AND BROKEN DIAPHRAGMS ON LH/RH WHEEL WELL AREA APROX RBL 34 / LBL 34. DIAPHRAGMS ON LH/RH WHEEL WELL AREA APROX RBL 34 / LBL 34 WERE REPLACED PER CRJ 900 SRM 51-41-02-001-001-A01SDR REXA2026082401561Rib · crackedCRACK ON MACHINED RIB OF LEADING EDGE SS 57.16 AT LH WING. MACHINED RIB OF LEADING EDGE SS 57.16 AT LH WING WAS REPAIRED PER REO 690-57-41-240 REV. --SDR FXTA20260626001Bolt · looseFLAP ACTUATOR ATTACHMENT HARDWARE FOUND LOOSESDR 3EJA865JS062926Outflow Valve · failedAFTER DEPARTURE FROM KSLC PASSING THROUGH 8000’, NOTICED THE CABIN WAS NOT PRESSURIZING.SDR SWIA2026062676814Angle · corrodedUPON REMOVAL OF INNER SKIN, FOUND BS 320.163 INTERCOSTAL DD4 FWD SIDE ANGLE CORRODED. REMOVED AND INSTALLED A NEW BS 320.163 DD4 FWD SIDE INTERCOSTAL ANGLE IAW SRM 51-42-06-001-001-A01, AND DWG 601R31702, REV N. COMPLIED WITH TASK CARD 51-900-1002-SKY. SEE CSDR SWIA2026062676806Frame · corrodedUPON REMOVAL INNER SKIN FOUND FORMER, BS 320.163 CORRODED. REMOVED AND INSTALLED A NEW PAX DOOR FORMER AT BS 320.163 IAW SRM 51-42-06-001-001-A01, SRM 51-42-21-001-001-A01, AND DWG 601R31702, REV N. PERFORMED PRESSURE LEAK TEST OF THE REPAIR AREA IAW AMM 21-SDR SWIA2026062676798Angle · corrodedUPON REMOVAL OF INNER SKIN FOUND BOTTOM FWD SIDE ANGLE BS 338.963 CORRODED. REMOVED AND IINSTALLED A NEW BOTTOM FWD SIDE ANGLE BS 338.963 IAW SRM 51-42-06-001-001-A01, SRM 51-42-21-001-001-A01, AND DWG 601R31702, REV N. PERFORMED PRESSURE LEAK TEST OF THE RESDR SWIA2026062676783Doubler · crackedUPON REMOVED INNER SKIN FOUND DOUBLER PULL IN CAM BS 338.963 POSSIBLY CRACKED. REMOVED AND INSTALLED A NEW PAX DOOR PULL IN CAM DOUBLER IAW SRM 51-42-06-001-001-A01, SRM 51-42-21-001-001-A01, AND DWG 601R31702, REV. N. COMPLIED WITH TASK CARD 51-900-1002-SKYSDR SWIA2026062676779Angle · corrodedUPON REMOVAL OF INNER SKIN FOUND BOTTOM AFT SIDE ANGLE BS 338.963 CORRODED. REMOVED AND INSTALLED NEW PAX DOOR BOTTOM AFT SIDE ANGLE BS 338.963 IAW SRM 51-42-06-001-001-A01, SRM 51-42-21-001-001-A01, AND DWG 601R31702, REV N. PERFORMED PRESSURE LEAK TEST OFSDR IPXA2026063066815Strut · wornFOUND RH WING OUTBD FLAP SUPPORT STRUT LOWER INSERT, COVE ATTACH WORN OUT, WBL 695. REVIEWED PER GMM-MTX 09.05.01.09. IAW CMM 57-52-55 601, REPAIR PARAGRAPH 1.F.(4), REV 212. REFER TO SRM 57-53-01-2R-1 AND SRM 51-70-07-0G-0 REV. 107 PERFORMED REPAIR.SDR IPXA2026072970144Splice Plate · crackedDURING PERFORM EO-76733-JIC2 STEP 247, FOUND NR 2 FASTENER HOLE CRACK. ACCOMPLISHED REPAIR IAW EO-98163-REQ1 REV.1 AND EGAT EI F2026A57M-1371 REV 3.