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.
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 F3LA202605100412Battery · failedACFT WAS ON SCHEDULED MAINTENANCE REFERENCE LP477859 #2 EPSU 16WL TEST FAIL BATTERY FAULT. REMOVED AND REPLACED EPSU BATTERY AT 16WL REF AMM 33-51-38-400-002-A. A/C OK FOR SERVICE.SDR F3LA202605100411Battery · failedACFT WAS ON SCHEDULED MAINTENANCE REFERENCE LP477859 #1 EPSU 13WL TEST FAIL BATTERY FAULT. REMOVED AND REPLACED EPSU BATTERY AT 13WL REF AMM 33-51-38-400-002-A. A/C OK FOR SERVICE.SDR IXXA20260510001Frame · crackedFRAME AT REAR OF HYD BAY NAC 375, IB ANGLE ON AFT SIDE OF FRAME IS CRACKED.SDR F3LA202605100410Battery · failedACFT WAS ON SCHEDULED MAINTENANCE REFERENCE LP477858 #3 EPSU 10WL TEST FAIL BATTERY FAULT. REMOVED AND REPLACED EPSU BATTERY AT 10WL REF AMM 33-51-38-400-002-A. A/C OK FOR SERVICE. /END/.SDR R61A2026051000121Skin · crackedLH WING MAIN BOX LOWER SKIN CLOSE TO RIB 3A AND SPAR II - CRACK - PERMANENT REINFORCING REPAIRSDR SWIA2026050977288Skin · damagedLEFT APRON SKIN PANEL ASSY HAD CHAFE AND GOUGE DAMAGE. REPAIRED THE APRON ASSY SKIN PANEL, IAW REO 601R-53-41-3446, REV-.SDR 4VAA202605090018Fairing · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE LEFT WING SKIN DOUBLER AILERON ACTUATOR FAIRING. THE LEFT HAND WING SKIN DOUBLER AILERON ACTUATOR FAIRING WAS REPAIRED IN ACCORDANCE WITH SAAB STATEMENT 2000SDS060701.SDR SWIA2026050977016Skin · scratchedWHILE INVESTIGATING DAMAGE TO FUSELAGE SKIN ASSOCIATED WITH CP 32002666 FOUND 2 OFF SCRATCHES ON EXTERIOR SURFACE OF FUSELAGE SIDE SKIN P/N 601R38327-52 AT FS559.00 +5.00, BETWEEN STR 8R AND STR 10R. (C-CHECK RO 08/28/2026)PERFOMED MAJOR REPAIR TO 2 SCRATCHESDR SWIA2026050976899Channel · corrodedCHANNEL ASSY OF FWD DRAIN MAST CORRODED. REMOVED THE DAMAGE FROM CHANNEL ASSY OF FWD DRAIN MAST, & EVALUATED AS OUT-OF-LIMITS. REPLACED CHANNEL WITH SERVICEABLE CHANNEL IAW DWG 601R43210, REV D, SRM 51-42-06-00 & SRM 51-42-10, REV 39. COMPLIED WITH TASK CARDSDR SWAA2026061597014Floor Panel · damagedAFT FLOOR PANEL 242WF HAS MISSING PLIES ON LOWER SURFACE. DUE TO THE EXTENT OF DAMAGE, REPLACED THE AFT FLOOR PANEL 242WF IAW SRM 51-10-02-0G-0, PARA 9, AND AIPC 53-21-00-26, ITEM 195.SDR SWAA2026061597013Floor Panel · delaminatedAFT FLOOR PANEL 241AEF UPPER SURFACE DELAMINATED. AFT FLOOR PANEL 241AEF WAS REPAIRED IAW SRM 53-00-50-2R-1.SDR REXA2026070301056Hinge Fitting · corrodedAFTER BUSHINGS REMOVAL, CORROSION WAS FOUND ON LH/RH NLG AFT DOOR HINGE FITTING (2 EAS) AND CORROSION ON RH/LH AIRFRAME HINGE FITTING (2 EAS) AT NLG. LH/RH NLG AFT DOOR HINGE FITTING (2 EAS) AND RH/LH AIRFRAME HINGE FITTING (2 EAS) AT NLG WERE REPLACED PER CRJSDR REXA2026070301055Hinge Fitting · corrodedAFTER BUSHINGS REMOVAL, CORROSION WAS FOUND ON LH/RH NLG AFT DOOR HINGE FITTING (2 EAS) AND CORROSION ON RH/LH AIRFRAME HINGE FITTING (2 EAS) AT NLG. LH/RH NLG AFT DOOR HINGE FITTING (2 EAS) AND RH/LH AIRFRAME HINGE FITTING (2 EAS) AT NLG WERE REPLACED PER CRJSDR REXA2026070301054Hinge Fitting · corrodedAFTER BUSHINGS REMOVAL, CORROSION WAS FOUND ON LH/RH NLG AFT DOOR HINGE FITTING (2 EAS) AND CORROSION ON RT & LT AIRFRAME HINGE FITTING (2 EAS) AT NLG. LH/RH NLG AFT DOOR HINGE FITTING (2 EAS) AND RH/LH AIRFRAME HINGE FITTING (2 EAS) AT NLG WERE REPLACED PER CSDR VNAA202606300001Skin · dentedTHREE DENTS ON UPPER SKIN OF SLAT NR 3 AT LT WING BTW SS 407-425. THE DENTS ON UPPER SKIN OF SLAT NR 3 AT LT WING BTW SS 407- 425 WERE REPAIRED IAW REO 670-57-42-2510.SDR SWAA2026061896842Fitting · deterioratedDETERIORATED HARDWARE ENTRY AND SERVICE GIRT BAR FITTING AT AFT GALLEY AREA. REPLACED HARDWARE ENTRY AND SERVICE GIRT BAR FITTING AT AFT GALLEY AREA IAW AMM 25-66-02-400-801 THE INSTALLATION WILL BE ACCOMPLISHED ON TASK CARD TTG8R007DGB8 STEP 13.SDR HNAA2026061700537Skin · gouged00413 FUSELAGE EXTERNAL SKIN AT FR 7, STR 15L, UNDER GPU ACCESS DOOR HAS A GOUGE. PERFORMED CUTOUT AND INSTALLED FABRICATED FILLER AND DOUBLER TO FUSELAGE EXTERNAL SKIN AT FR 7 STR 15L UNDER GPU ACCESS DOOR IAW EMB 145 SRM M53-12-01-RE STEP 2 FIGURE 201 SEE PSDR AALA202606163144Web · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CARGO COMPARTMENT DOOR THRESHOLD WEB BETWEEN STA 807 AND STA 847 AT S25R. REPLACED WEB PER AARD 51-00-05-1.SDR IPXA2026061205245Seat Track · gougedSTR, MAIN DECK CARGO COMPARTMENT LOWER SILL AREA, SEAT TRACK HAS MULTIPLE GOUGES, APPROX BTW BS 520 AND BS 600, LBL 62.20, ID STICKER NUM. (085-063). ATA 53-10. INSTALLED 1 EA NEW SEAT TRACK SECTION AT MAIN CARGO COMPARTMENT DOOR LOWER STA:520 TO 540 LBL 62.SDR VNAA202606120003Skin · damagedLIGHTNING STRIKE ON SEVERAL FASTENERS BTW STR 23L AND BS 210 - 265. LIGHTNING STRIKE ON SEVERAL FASTENERS BTW STGR 23L AND BS 210 - 265 WERE REPAIRED IAW SRM 53-00-00-201-003-A01.SDR SWAA2026061197111Rod End · corrodedTHE RIGHT WING AILERON TAB ATTACH (HINGE) ROD ENDS ALL HAVE EVIDENCE OF EXTERNAL SURFACE CORROSION.. REMOVED RT AILERON TRIM TAB PER AMM 27-11-21. R & R RIGHT WING AILERON TAB ATTACH ROD ENDS IAW CMM 57-50-26. REINSTALLED RT AILERON TRIM TAB IAW AMM 27-11-SDR SWAA2026061097046Access Panel · elongatedELONGATED HOLE ON ACCESS PANEL 561AB, LT WING. REPAIRED THE ACCESS PANEL 561AB IAW SRM 51-70-04-2R-10, REPAIR 10.SDR IPXA2026052405432Control Wheel · corrodedCOPILOTS CONTROL WHEEL OUTER SKIN CORRRODED RH SIDE. INSTALLED SERVICEABLE COPILOTS AILERON CONTROL WHEEL AND ADAPTER IAW AMM 27-11-02-424-010 TW ID:19-983 DD:09/03/2026SDR IPXA2026051105596Angle · corrodedBS 1790 - 1820, RBL 3R, APU INTAKE DOOR SURROUND UPPER ANGLE IS CORRODED VERIFIED REMOVAL OF UPPER ANGLE AT FS 1790 - 1820 RBL S-3R IAW SRM 51-40-02-0G.SDR REXA2026060900955Tube · corrodedCORROSION ON TUBE BTW FS 310.00 AND FS333.00 AT PASSENGER DOOR SURROUND STRUCTURE CORROSION ON TUBE BTW FS 310.00 AND FS333.00 AT PASSENGER DOOR SURROUND STRUCTURE WAS REMOVED AND EVALUATED OUT LIMITS PER CRJ-900 SRM 53-00-00-101-001, SRM 51-21-00-001-001-A0SDR REXA2026060800957Fitting · corrodedCORROSION ON CLOSING FITTING ON FS342 (PASSENGER DOOR LOWER SILL AREA) AT PAX CABIN FLOOR STRUCTURE DUE TO EXCESSIVE DAMAGE ON FITTING, CLOSING ON FS342 (PASSENGER DOOR LOWER SILL AREA) AT PAX CABIN FLOOR STRUCTURE WAS REPLACED PER SRM 51-42-06-001-001-A01SDR REXA2026060800952Seat Track · corrodedCORROSION ON SEAT TRACK ON RBL9 FROM FS349 TO FS409 AT PAX CABIN FLOOR STRUCTURE DUE TO EXCESSIVE DAMAGE ON SEAT TRACK ON RBL9 FROM FS349 TO FS409 AT PAX CABIN FLOOR STRUCTURE WAS REPLACED PER CRJ900 SRM 51-10-06-001-001-A01 AND AMM 53-00-49SDR REXA2026060800950Angle · crackedCRACKED SUPPORT ANGLE OF SHEAR BOX BTW FS 280 AND RBL 12.0 MAIN AVIONICS COMPARTMENT. SUPPORT ANGLE OF SHEAR BOX BTW FS 280 AND RBL 12.0 MAIN AVIONICS COMPARTMENT WAS REPLACED PER CRJ900 SRM 51-42-21-001-001-A01SDR REXA2026060800948Angle · crackedCRACK ON LH VERTICAL STABILIZER TO FUSELAGE ATTACHMENT FWD & AFT DRAG ANGLE BTW 61.56% STRG DATUM TO 67.5% REAR SPAR DATUM CRACK ON LH VERTICAL STABILIZER TO FUSELAGE ATTACHMENT FWD & AFT DRAG ANGLE BTW 61.56% STRG DATUM TO 67.5% REAR SPAR DATUM WERE REPAIRED SDR REXA2026060800940Angle · corrodedCORROSION ON MID CAP ANGLE FROM FS310 TO FS349 (PASSENGER DOOR LOWER SILL AREA) AT PAX CABIN FLOOR STRUCTURE MID CAP ANGLE FROM FS310 TO FS349 (PASSENGER DOOR LOWER SILL AREA) AT PAX CABIN FLOOR STRUCTURE WAS REPLACED PER CRJ-900 SRM 51-41-02-001-001-A01SDR REXA2026060800939Door Frame · crackedCRACK ON UPPER FRAME AT AFT RH/LH & FWD RH/LH OVERWING EMERGENCY EXIT DOORS CRACK ON UPPER FRAME AT AFT RH/LH & FWD RH/LH OVERWING EMERGENCY EXIT DOORS WERE REPAIRED PER REO 670-52-21-103 REV. - -SDR AALA202606086993Angle · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CARGO COMPARTMENT DOOR THRESHOLD INNER CHORD ANGLE BETWEEN STA 807 AND STA 847 AT S25R. REMOVED / BLENDED CORROSION PER SRM 51-10-02.SDR AALA202606057730Shield · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CARGO COMPARTMENT SHIELD BETWEEN STA 767 AND STA 807 AT S25R. REPLACED SHIELD PER AARD 51-00-05-1.SDR REXA2026060400904Lug · corrodedCORROSION AND WEAR WAS FOUND ON LUG BORE ON AIL STA 337.657 (LUG L2) AND 342.911 (LUG L5) LUG BORE ON AIL STA 337.657 (LUG L2) AND 342.911 (LUG L5) WERE REPAIRED PER REO 690-57-61-521 REV. - - AND REO 670-57-61-237 REV - -SDR AALA202606040568Transition Panel · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CARGO COMPARTMENT TRANSITION PANEL BETWEEN STA 727D AND STA 727E AT S25L. REPAIRED TRANSITION PANEL PER SRM 53-00-53-1A.SDR AALA202606048316Transition Panel · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CARGO COMPARTMENT TRANSITION PANEL BETWEEN STA 727E AND STA 727F AT S25L. REPAIRED TRANSITION PANEL PER SRM 53-00-53-1A.SDR AALA202606047255Transition Panel · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CARGO COMPARTMENT TRANSITION PANEL BETWEEN BS 727G AND 727H AT S25L. REPAIRED TRANSITION PANEL PER SRM 53-00-53-1A.SDR R61A2026060400157Seat Track · corrodedRH I/B SEAT TRACK HAS 3 CORRODED RIVETS ON I/B FLANGE AT FR59.TECHNICIAN REPAIRED RH I/B SEAT TRACK SECTION BETWEEN FR56 AND FR60 .REF. EMB SRM 53-00-10 REPAIR 01SDR R61A2026060400156Seat Track · corrodedCORROSION - LT INBD SEAT TRACK AT FR18.MECHANIC PERFORMED CUTOUT AT LH I/B SEAT TRACK AT FR18 IAW REF. SRIIM CH. 51, REF. EMB SRM 53-10-10 /REPAIR 01PSDR R61A2026060400155Seat Track · corrodedCORROSION - RT INBD SEAT TRACK AT FR15.REPAIRED RT INBD SEAT TRACK AT FR15 IAW SRM 53-10-10 /REPAIR 01PSDR AALA202606037102Transition Panel · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON FORWARD CARGO COMPARTMENT TRANSITION PANEL BETWEEN STA 500 AND STA 500I AT LBL 35. REPLACED TRANSITION PANEL PER AARD 51-00-05-1.SDR IPXA2026060205494Skin · crackedNR 2 ENG FIRE LOOP ACCESS PANEL L/E SKIN CRACKED . INSTALLED EXTERNAL REPAIR DOUBLER AT #2 ENG FIRE LOOP ACCESS PANEL IAW E.A.# 757-5741-01-B0742 REV P1 STEP 7. ACCOMPLISHED PERMANENT REPAIR PER EO-97550-REQ1 AND VT-SAA EA 757-5741-01-B0742, REV. I/R.SDR J7SA2026060200482Fce · unserviceableCREW RECEIVED GND SPLR FAIL AND SPOILER FAIL CAS MESSAGES ON LANDING WHILE BRAKING. REPLACED #2 FCE IAW EMB-505 AMM 27-03-01. RIGGING AND OPS CHECKS GOOD.SDR SWAA2026060197036Seat Track · corrodedCORROSION SEAT TRACK LOCATED BS 360 PLUS 14 INCH AND LBL 45.5 WL 208.1 PASSENGER CABIN. REPLACED SEAT TRACK LOCATED BS 360 TO BS 480 AND LBL 45.5 WL 208.1 PASSENGER CABIN IAW SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DWG: 143A5300; SHEET 54, REV -, DWG: 141A5300SDR SWAA2026060197185Access Panel · crackedCRACK ANGLE ACCESS PANEL 551GB AT LT WING. REPLACED ANGLE AND FASTENERS LOCATED ACCESS PANEL 551GB AT LT WING IAW SRM B737-700 51-10-02, ITEM 9 AND SRM B737-700 51-40-02. MEASUREMENT OF CRACK: L 1.087.SDR AALA202606017848Skin · delaminatedAIRCRAFT IN BASE MAINTENANCE: LEFT HAND OUTBOARD TRAILING EDGE FLAP TOPSIDE DELAMINATED. REPAIRED FLAP PER CMM 57-53-08.SDR AALA202606012326Transition Panel · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON FORWARD CARGO COMPARTMENT TRANSITION PANEL BETWEEN STA 500 AND STA 500I AT S25L. REPLACED TRANSITION PANEL PER SRM 53-00-53-2R-5.SDR SCNA20260529225Web · crackedCRACK IN LOWER HOLE AT 9 HRS POSITION ON THE WEB, STA 727 AND S-18A (IN REF. CARD 737-53A1402-01-GRP1-CFG1-RH-INIT, ITEM 12: FIG. 4 - STEP 3). OPENSDR CALA2026052916620Frame · dentedFWD CARGO, RT SIDE, BS 680, LOWER SIDEWALL, FRAME HAS A DENT. ACCOMPLISHED WORK PER UAL EC/RA:5330-07770 AND VT MAE EA: 757-53 30-13-A4488 REV-.SDR AALA202605288504Bottle · leakingAIRCRAFT IN BASE MAINTENANCE: PASSENGER / CREW DOOR 832 DAMPER AND EMERGENCY OPERATION CYLINDER PRESSURE LOW. REPLACED DOOR DAMPER AND EMERGENCY OPERATION CYLINDER PER AMM 52-13-14.