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 CALA2026092119565Light Sys · faultedEMERGENCY EXIT LIGHTS MOMENTARILY CAME ON OVER ALL FOUR OVERWING EXITS RIGHT BEFORE TAKEOFF ROLL. LIGHTS WENT OUT ON THEIR OWN. EMER EXIT LIGHT SWITCH TESTED GOOD. F/A VERIFIED ONLY RT OVERWING EMERG AND SURROUNDING LIGHTS CAME ON. ACCESSSED M1695 AND VERIFIEDSDR CALA2026092119564Power Supply · faultedDURING EMERGENCY LIGHT TEST FAIL MESSAGE EPSU INT LOAD EMER RT APPEARED. IAW FIM 33-51-00-810-807-A, REMOVED AND REPLACED EPSU AND BATTERY 12WL IAW AMM 33-51-38-000-001-A. NO FIX. SUGGEST FURTHER TROUBLESHOOTING OF WIRING PER FIM. CONFIRMED ALL EXIT MARKERS SDR CALA2026092119563Flashlight Assy · dischargedGALLEY 6 FLIGHT ATTENDANT SEAT EMERGENCY FLASHLIGHT INOP. FLASHLIGHT AT G6 FLIGHT ATTENDANT SEAT REMOVED & REPLACED PER TASK 25-60-00-210-801-C1. OP CHECK OKAY.PARTS USED: 78-2500-3-0845, QTY :1SDR CALA2026092119559Hydraulic Line · leakingHYDRAULIC FLUID STREAKS AND SHIMMERY FLUID PRESENT ON LT WING LOWER SIDE OF FLAPS AND FLAP SEALS BETWEEN OUTERMOST PYLON COVER AND MIDDLE PYLON COVER INSPECTED SUSPECTED AREA. FOUND MOIST LINES/ AND HYDRAULIC SMELL. UNABALE PINT POINT SUSPECTED LEAK. CLEANED LSDR CALA2026092119558Packing · leakingODOR IN A/C APU SUPPLYING PACKS FOUND APU FUEL CONTROL CLUSTER LEAKING. O-RINGS NEED TO BE REPLACED. EIGHT O-RINGS WERE CHANGED ON THE APU FUEL CONTROL UNIT IAW AMM 49-11-00. OK TO CONTINUE.SDR CALA2026092119557Filter · cloggedMUSTY ODOR FROM PACKS ON TAKEOFF/CLIMB. DISAPPEAR ED IN CRUISE. CAME BACK ON DESCENT. REMOVED AND REPLACED RECIRCULATOIN AIR FILTERS IAW AMM TASK21-25-01-400-801. CONFIRMED WITH TOMC ENGINE WASH ACCOMPLISHED ON SNA ON 09/19/26 OPERATED PACKS NO MUSTY SMELL NOTSDR CALA2026092119556Potable Water · contaminatedWATER FROM REAR COFFEE MACHINE SMELLS AND TASTES BAD. DRAINED AND REFILLED POTABLE WATER SYSTEM IN REF TO AMM 12-14-00. OPS CHECK BOTH REAR COFFEE MAKERS IN THE REAR OF THE AIRCRAFT IN REF TO AMM 25-32-01. THE WATER NO LONGER SMELLS.SDR QMLA2026092120071Outlet · odorUPON APPROACH AND LANDING BACK TO BASE, CREWMEMBER IN REAR OF AIRCRAFT NOTICED A BURNING ODOR COMING FROM THE ELECTRICAL COMPARTMENT IN THE NR 1 SIDE WALL OF THE AIRCRAFT. LANDED AND EXAMINED THE AREA, THEN REMOVED ELECTRICAL POWER FROM CIRCUIT AND ODOR DISSIPSDR DALA2026091905237Battery Pack · inoperativeFOUND R1 DOOR AND FIRST CLASS SEAT EMERGENCY LIGHTS INOP. REPLACED M2816 EMERGENCY LIGHT BATTERY PACK PER B737 AMM 33-51. OPS CHECK GOOD. (LP 7531551 - AIRCRAFT WAS GROUNDED)SDR DALA2026091905239Battery Pack · inoperativeFOUND L2 DOOR AND AFT OVERHEAD EMERGENCY EXIT SIGNS INOP. REPLACED M1673 EMERGENCY LIGHT BATTERY PACK PER B737 AMM 33-51. OPS CHECK GOOD. (LP 7531552 - AIRCRAFT WAS GROUNDED)SDR JR2R20260919603Shear Tie · corrodedAFT CARGO SHEAR TIE AT FR81 BETWEEN STR27R-STR28R IS CORRODED. REPLACED PER SRM.SDR JR2R20260919599Shear Tie · corrodedAFT CARGO SHEAR TIE AT FR74 BETWEEN STR29L-STR28L IS CORRODED. REPLACED PER SRM.SDR JR2R20260919602Shear Tie · corrodedAFT CARGO SHEAR TIE AT FR81 BETWEEN STR28R-STR29R IS CORRODED. REPLACED PER SRM.SDR JR2R20260919606Shear Tie · corrodedAFT CARGO SHEAR TIE AT FR83 BETWEEN STR27R-STR28R IS CORRODED. REPLACED PER SRM.SDR 2026FA0000745Stringer · debondedRT WING STRINGER #3, (CWS 201.25) DEBONDED AT END (INSIDE PANEL 631DB)SDR 2026FA0000744Stringer · debondedRT WING STRINGER NR 2 (CWS 117.60) IS DEBONDED AT END (INSIDE PANEL 621CB)SDR REXA2026110402043Cam Fitting · wornWEAR ON FWD CAM FITTING AT PASSENGER DOOR SURROUND STRUCTURE. FWD CAM FITTING AT PASSENGER DOOR SURROUND STRUCTURE WAS REPLACED PER SRM 51-42-21-001-001-A01SDR REXA2026110402042Angle · corrodedCORROSION ON ANGLE MID CAP AT PASSENGER DOOR SURROUND STRUCTURE. ANGLE MID CAP AT PASSENGER DOOR SURROUND STRUCTURE REPLACED PER CRJ900 SRM 51-41-02-001-001-A01SDR REXA2026110402041Handle · crackedCRACK ON FWD/AFT CORNERS AT PASSENGER DOOR OUTER FLAP HANDLE. PASSENGER DOOR OUTER FLAP HANDLE WAS REPLACED PER CRJ 900 S.R.M. 51-42-06-001-001-A01SDR REXA2026110402040Support · crackedCRACKS ON SUPPORT BASE MAIN BATTERY DIRECT BUS (JB6) AT FWD EQUIPMENT COMPARTMENT. SUPPORT BASE MAIN BATTERY DIRECT BUS (JB6) AT FWD EQUIPMENT COMPARTMENT WAS REPLACED PER CRJ900 SRM 51-42-06-001-001-A01SDR REXA2026110402039Support Plate · corrodedCORROSION ON HYDRAULIC LINES SUPPORT PLATES (IN BK, LG EXT, LG RET) LBL 45 AT LH MLG WHEEL WELL HYDRAULIC LINES SUPPORT PLATES (IN BK, LG EXT, LG RET) LBL 45 AT LH MLG WHEEL WELL WAS REPLACED PER CRJ-900 AMM 20-21-00.SDR REXA2026110402038Support Angle · crackedCRACK ON ANGLE SUPPORTS IN STA. FS= 797 AND STA. WS= 15 AT LH/RH MLG W/W FWD FACE. ANGLE SUPPORTS IN STA. FS= 797 AND STA. WS= 15 AT LH/RH MLG W/W FWD FACE WERE REPLACED PER CRJ 900 SRM 51-42-21-001-001-A01.SDR REXA2026110402037Support Angle · crackedCRACK ON ANGLE SUPPORTS IN STA. FS= 797 AND STA. WS= 15 AT LH/RH MLG W/W FWD FACE. ANGLE SUPPORTS IN STA. FS= 797 AND STA. WS= 15 AT LH/RH MLG W/W FWD FACE WERE REPLACED PER CRJ 900 SRM 51-42-21-001-001-A01.SDR REXA2026110402026Rib · crackedCRACKED RIB, LEADING EDGE SS27.75 RT WING. THE RIB WAS REPLACED IAW SRM 51-42-06-001-001-A01, SRM 51-42-10-001-001-A01, & SRM 51-42-21-001-001-A01SDR REXA2026110402020Angle · corrodedCORROSION ON THE ANGLE OF THE LOWER SILL, LOCATED BTWN BS 319 AND 349, WL 72.50 AT THE GALLEY SERVICE DOOR EXTERNAL SURROUND STRUCTURE. THE ANGLE WAS REPLACED IAW SRM 51-42-06-001-001-A01, & SRM 51-42-21-001-001-A01.SDR REXA2026110402013Floorbeam · chafedCRACKED PREVIOUS REPAIR ANGLE (TWO) ON THE FLOORBEAM, RBL 12, BS 280. THE FLOORBEAM WAS REPAIRED IAW REO 690-53-11-1221 REV-.SDR REXA2026110402007Angle · corrodedCORROSION ON ANGLE LOWER SILL LOCATED BETWEEN FS 319.00 AND 349.00 WL 72.50 AT GALLEY SERVICE DOOR EXTERNAL SURROUND STRUCTURE. CORROSION ON ANGLE LOWER SILL LOCATED BETWEEN FS 319.00 AND 349.00 WL 72.50 AT GALLEY SERVICE DOOR EXTERNAL SURROUND STRUCTURE WAS RSDR REXA2026110402006Seal Retainer · chafedINTIAL INSPECTION: WEAR AND BEND ON SEAL RETAINER LOWER AT FWD AND CENTER BAGGAGE BAY DOOR. SEAL RETAINER LOWER AT FWD AND CENTER BAGGAGE BAY DOOR WERE EVALUATED OUT LIMITS PER CRJ/900 SRM 52-35-07-201-001-A01 THEREFORE WERE REPLACED IAW SRM 51-42-06-001-001-SDR REXA2026110402004Panel · crackedCRACK ON AFT SIDE PANEL AT PASSENGER DOOR STRUCTURE. AFT SIDE PANEL AT PASSENGER DOOR STRUCTURE WAS REPAIRED IAW SRM 52-11-04-201-004-A01SDR IPXA2026103106921Skin · dentedDENT ON RT INBD SLAT #(7), INBD COVE SKIN, OUTBD END NEXT TO KRUGER FLAP. REF ITEM 5 DET II OF SRM 57-43-01-0I-1. I.A.W CMM 57-43-37 REV.51 INSTALL THE SKIN COVE WITH NEW P/N: 114T3161-12. 2.I.A.W DWG 114T3162 SHEET 01 REV. F REPLACED THE BRACKET. REVIEWEDSDR VNAA202610310018Bracket · corrodedBRACKETS (02EAS) P/N CC670-75268-1 WERE FOUND DAMAGED. BRACKETS (02EAS) WERE REPLACED IAW SRM 51-42-21-001-001-A01.SDR VNAA202610310017Bracket · corrodedCORROSION ON BRACKET (02EA) P/N CC670-75269-1 (LH) AND P/N CC670-75269-2 (RH) AT MLG WHEEL WELL AREA. BRACKET (02EA) P/N CC670-75269-1 (LH) AND P/N CC670-75269-2 (RH) AT MLG WHEEL WELL AREA WERE REPLACED IAW SRM 51-42-06-001-001-A01.SDR VNAA202610310016Drag Angle · crackedCRACK ON RIGHT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT DRAG ANGLE BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATUM (TRACE AT BL0.00). (SM) CRACK ON RIGHT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT DRAG ANGLE WAS REPAIRED IAW SRM 55-31-00-201-001-A01SDR SWIA2026091877814Skin · demodificationCOMPLY WITH FWD ATG ANTENNA PERMANENT REPAIR IAW DRAWING 170-2365-02-RS, M-93 ERJ175-53-26-03, & EA ERJ4111-44. COMPLIED WITH FWD ATG ANTENNA PERMANENT REPAIR IAW DRAWING 170-2365-02-RS, M-93 ERJ175-53-26-03, & EA ERJ4111-44.SDR SWIA2026091877813Skin · demodificationCOMPLY WITH AFT ATG ANTENNA PERMANENT REPAIR IAW DRAWING 170-2365-02-RS, AND M-93, ERJ175-53-26-03 & EA ERJ4111-44. COMPLIED WITH AFT ATG ANTENNA PERMANENT REPAIR REF DWG 170-2365-02-RS AND M-93 ERJ175-53-26-03 EA ERJ4111-44.SDR SWIA2026091877811Skin · demodificationCOMPLY WITH RH SIDE ATG ANTENNA PERMANENT REPAIR REF DRAWING 170-2365-02-RS AND M-93 ERJ175-53-26-03 EA ERJ4111-44 C-CHECK RO 10272026COMPLIED WITH RH SIDE ATG ANTENNA PERMANENT REPAIR REF DRAWING 170-2365-02-RS AND M-93 ERJ175-53-26-03 EA ERJ4111-44 WEIGHSDR SWIA2026091877808Skin · demodificationCOMPLY WITH LH SIDE ATG ANTENNA PERMANENT REPAIR REF DRAWING 170-2365-02-RS AND M-93 ERJ175-53-26-03 EA ERJ4111-44 C-CHECK RO 10272026COMPLIED WITH LH SIDE ATG ANTENNA PERMANENT REPAIR REF DRAWING 170-2365-02-RS AND M-93 ERJ175-53-26-03 EA ERJ4111-44SDR AALA202610294440Handle · excess playAIRCRAFT IN BASE MAINTENANCE: FWD ENTRY DOOR HANDLE HAS PLAY. REMOVED AND REPLACED NEW HANDLE MECHANISM ASSY AT L1 ENTRY DOOR IAW AMM 52-11-11.SDR IPXA2026102413332Skin Panel · delaminatedLOWER AFT APU PANEL BETWEEN STA 1963 TO 1992 IS DELAMINATED. INSTALLED/BONDED ALL REPAIR DOUBLERS AND FILLERS ON INNER SIDE OF LOWER AFT APU PANEL BETWEEN STA 1963 TO 1992 AND CURED AT 310'F DEGS FOR 360 MINUTES REF 51-70-10-2R-0 REPAIR 4 PARA,4 AND SRM 51-70-SDR HNAA2026102801046Skin · crackedLT RF2 AT FR78 AND BTW STR6-7L CRACKED AROUND ONE RIVET. REPAIRED IAW SRM 53-32-01 RE FIG 213 SHEET 3SDR VNAA202610230072Seat Track · corrodedCORROSION ON SEAT RAIL IN STGR 15L AND STA 409-469 , 485-553, 661-720 AT CPAX. DUE TO EXCESSIVE CORROSION ON SEAT RAIL IN STGR 15L AND STA 409 TO 720 AT CPAX WAS REPLACED PER
CRJ900 SRM 53-31-49-101-001-A02 AND PER CRJ900 AMM 53-00-49 (CONFIG A12)SDR VNAA202610230068Seat Track · corrodedCORROSION ON SEAT RAIL IN LBL 9 AND STA 847+32-969 AT CPAX. DUE TO EXCESSIVE CORROSION ON SEAT RAIL IN LBL 9 AND STA 847+32-969 AT CPAX WAS REPLACED PER SRM 53-31-49-101-001-A02 AND CRJ900 AMM 53-00-49 (CONFIG A12).SDR IPXA2026102409508Housing · delaminatedAPU AIR INLET DOOR HOUSING INNER SURFACE HAS AREAS OF DELAMINATION AS VIEWED WITH DOOR REMOVED. ACCOMPLISHED PERMANENT REPAIR AT COM. APU AIR INLET DOOR HOUSING PER EO-98936-REQ1 AND EA 757-4915-01-B0856, REV. I/R.SDR HNAA2026102601032Skin · dentedRIGHT LEADING EDGE 1, NOSE SKIN DENTED BTW YS1526.50-YS1259. REPAIRED IAW SRM 57-40-00SDR AALA202610230574Frame · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK INDICATION ON FRAME 16 LEFT SIDE UPPER DOUBLE JOGGLE AREA OPEN FASTENER HOLE 6, CRACK DIRECTION IS 3 O'CLOCK, CRACK DEPTH IS 0.120 INCH APROXIMATELY AT FORWARD GALLEY AREA. MAINTENANCE PERFORMED TIME LIMITED REPAIR ON FRAME SDR AALA202610225556Tee Fitting · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ALONG UPPER FLANGE OF 947.5 BEAM. REMOVED AND REPLACED TEE-CHORD IAW EA 379184, SRM 53-70-51-2R-5 REPAIR 5.SDR SIMA20260918013Floor Support · corrodedAFT WET AREA FLOOR STRUCTURE - CORROSION ON INTERCOSTAL A FR 90-91 Y. (LEVEL 2 CORROSION) REMOVED AND INSTALLED NEW AFT WET AREA FLOOR INTERCOSTAL AT FR 90-91 Y+11" PER EMB 175 SRM 51-40-00.SDR SIMA20260918014Floor Support · corrodedAFT WET AREA FLOOR STRUCTURE - CORROSION ON SPLICE AS MARKED FR 90 Y+11. (LEVEL 2 CORROSION) REMOVED AND REPLACED WITH NEW AFT WET AREA FLOOR STRUCTURE SPLICE AT FR 90 Y+11 IAW EMB 175 SRM 51-40-08.SDR SIMA20260918012Floor Support · corrodedSSI# 53-23-005 AFT WET AREA FLOOR STRUCTURE - CORROSION ON PANEL SUPPORT AS MARKED FR 89-90 Y+36". (LEVEL 2 CORROSION) REMOVED AND REPLACED WITH NEW PANEL SUPPORT FROM FR 89-90 Y+36" IAW EMB 175 SRM 51-40-08.SDR SWAA2026102154393Stop Fitting · crackedCRACKED STOP PAD, EMERGENCY DOOR 833, FWD POSITION, LOWER SURFACE. REPLACED STOP PAD IAW SOPM 20-50-12, REV 58.