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 REXA2026073001341Bracket · corrodedCORROSION ON INTERNAL ANGLES IN REFUEL/DEFUEL PANEL AT INTERNAL AREA OF FAIRING 192AR. CORROSION ANGLE (1 EA) IN REFUEL/DEFUEL PANEL AT INTERNAL AREA OF FAIRING 192AR WERE REMOVED PER CRJ-900 SRM 51-21-06-001-001-A01 AND WAS FOUND WITHIN OF LIMITS PER CRJ-900SDR REXA2026073001324Stringer · corrodedCORROSION ON STGR 21 RH BTWN FS 364.00 TO FS 379.00 CORROSION ON STGR 21 RH BTWN FS 364.00 TO FS 379.00 WAS REMOVED PER CRJ-900 SRM 51-21-06-001-001-A01 EVALUATED OUT LIMITS PER CRJ-900 SRM 53-21-03-101-006-A04 THEREFORES WAS REPLACED PER CRJ 900 SRM 51-42-21-SDR REXA2026073001323Angle · corrodedCORROSION ON MOUNITNG ANGLE OF SERVICE DOOR BTW FS 319 TO 349 AT CPAX MOUNITNG ANGLE OF SERVICE DOOR BTW FS 319 TO 349 AT CPAX WAS EVALUATED OUT OF LIMITS DUE TO EXCESIVE CORROSION PER CRJ-900 SRM 53-00-00-101-001-A01, THEREFORE WAS REPLACED PER CRJ-900 SRM 51SDR AALA202607226500Skin · debondedAIRCRAFT IN BASE MAINTENANCE: RIGHT WING INBOARD TRAILING EDGE FLAP LOWER SKIN PANEL IS DEBONDED AT THE TRAILING EDGE OF THE FLAP 45 INCHES FROM THE FUSELAGE BETWEEN FLAP RIBS 4 AND 5. REPAIRED FLAP PER EA 360105D AND SRM 57-52-00-300-093,SDR AALA202607221642Skin · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CARGO COMPARTMENT INTERNAL SKIN PANEL BETWEEN FR 59 AND FR 60, BETWEEN S42L AND S43L. REPAIRED SKIN PANEL PER EA 376515.SDR SWAA2026061510533Battery · no testFWD INBD EMERGENCY FLASHLIGHT WILL NOT TEST. REPLACED FWD INBD FLASHLIGHT BATTERY IAW AMM 25-64-00. OPS TESTED GOOD.SDR SWAA2026061510867Flashlight · inoperativeAFT RT INBD FLASHLIGHT WILL NOT TEST. R & R THE AFT RT INBD FLASHLIGHT IAW AMM 25-64-00.SDR SWAA2026061510856Flashlight · not seatedAFT GALLEY EMERGENCY FLASHLIGHT INOPERATIVE. SECURED THE FLASHLIGHT IN CRADLE IAW SIP. OPS CHECKED NORMAL.SDR SWAA2026061510221Isolator · crackedAFT ENTRY DOOR FWD LOWER SLIDE ISOLATOR IS CRACKED. R & R AFT ENTRY DOOR FWD LOWER SLIDE ISOLATOR IAW SRM 51-40-02.SDR SWAA2026061510181Light · faultedROW 15 ABC SIDEWALL LIGHT FLICKERING. OK TO CONT MEL 33-21-01A. REMOVED AND REPLACED 15ABC SIDEWALL LIGHT IAW AMM 33-51-04.SDR SWAA2026061510387Battery Pack · inoperativeEMERGENCY LIGHT ON LEFT OVER WING EXIT DOOR IS INOPERATIVE. REMOVED AND AND REPLACED THE BATTERY PACK IAW AMM 33-51-06. OPS CHECKED GOOD.SDR SWAA2026061510272Seal · crackedRIGHT HORIZONTAL STAB FORWARD UPPER SLIDING SEAL HAS A 4 VERTICAL CRACK ALONG THE FORWARD SEAL TRACK. R & R RT HORIZONTAL STAB FWD UPPER SLIDING SEAL IAW AMM 53-31-31.SDR SWAA2026061510271Seal · crackedL/H HORIZONTAL STABILIZER FORWARD UPPER SLIDING SEAL HAS A 3 VERTICAL CRACK ALONG THE FORWARD SEAL TRACK.<[01] REMOVED AND REPLACED L/H HORIZONTAL STABILIZER FORWARD UPPER SLIDING SEAL IAW AMM 53-31-31.SDR SWAA2026072001893Scuff Plate · crackedFWD SERVICE DOOR SCUFFPLATE AFT CORNER IS CRACKED. WELDED FWD SERVICE DOOR SCUFFPLATE AFT CORNER PER SRM 53-10-15-2R-2.SDR AALA202607204148Web · corrodedAIRCRAFT IN BASE MAINTENANCE: INTERGRAINULAR CORROSION ON K-WEB AT STA 986, RBL 40. MAINTENANCE REPLACED K-WEB AT STA 986, RBL 40 IAW AARD 51-00-05-1.SDR SWAA2026071784671Access Panel · damagedELONGATED HOLES ACCESS PANEL 661CB AT RT WING. REPAIRED ACCESS PANEL 661CB AT RT WING IAW SRM 51-70-04-2R-9, REPAIR 9.SDR SWAA2026071772442Floorbeam · corrodedCORROSION ON FLOOR BEAM LOCATED BS 328 RBL 45.5 WL 208.1 AT FWD GALLEY AREA. REPAIRED FLOORBEAM LOCATED BS 328 WL 208.1 BTW BL 0 TO RBL 60 AT FWD GALLEY AREA IAW SRM 53-10-51-2R-7, REPAIR 7.SDR SWAA2026071773765Access Panel · damagedELONGATED HOLES ACCESS PANEL 661BB AT RT WING. REPAIRED ACCESS PANEL 661BB AT RT WING IAW SRM 51-70-04-2R-9, REPAIR 9.SDR SWAA2026071787897Floorbeam · corrodedCORROSION ON FLOORBEAM LOCATED BS 986.5 LBL 42 WL 208.1 AT AFT GALLEY AREA. REPAIRED THE FLOORBEAM LOCATED BS 986.5 LBL 42 WL 208.1 AT AFT GALLEY AREA IAW SRM 53-70-51-2R-6, REPAIR 6, ALTERNATIVE 4.SDR SWAA2026071748282Rib · crackedCRACK ANGLE DEFLECTION CONTROL RIB TRAILING EDGE AT LEVEL ORSS 277 LT WING CRACK ANGLE DEFLECTION CONTROL RIB TRAILING EDGE AT LEVEL ORSS 277 LT WING. REPLACED ANGLE (CLIP) LOCATED DEFLECTION CONTROL RIB TRAILING EDGE AT LEVEL ORSS 277 LT WING IAW SRM 51-40-0SDR SWAA2026071786882Support Angle · crackedCRACKED SUPPORT ANGLE, BS 695, RBL 24.75 AT PASSENGER CABIN. REPLACED THE SUPPORT ANGLE IAW SRM 51-10-02, ITEM 9, AND DRAWING 273A9110, SHEET 6, REV A, DWG 111A6000, SHEET 304, REV-.SDR SWAA2026071736110Access Panel · damagedELONGATED HOLES ON ACCESS PANEL 661AB AT RT WING. REPAIRED ACCESS PANEL 661AB AT RT WING IAW SRM 51-70-04-2R-10 REPAIR 10.SDR SCNA20260715304Skin · crackedWO 94270 NR00178: CRACK ON LOWER SKIN STAB STA = 101.90 AT RH HORIZONTAL STABILIZER. - - CRACK ON LOWER SKIN STAB STA = 101.90 AT RH HORIZONTAL STABILIZER WAS REPAIRED PER B737-800 SRM 55--10-01-2R-11 REPAIR 11SDR SCNA20260715303Stringer · corrodedWO 94270 NR0179: CORROSION ON STRINGER AT STA 847+10IN, S-23R. AFT CARGO COMPT. - - REJECT: PHYSICAL: WORK SIGNED OFF BUT NOT ACCOMPLISHED/OR PARTIALLY ACCOMPLISHED - IN REFERENCE TO WIP #2 WAS FOUND ELONGATED HOLES (6 LOCATIONS) ON EXTERNAL SKIN BTW STA 887+5SDR VNAA202607120020Hinge · wornEXCCESSIVE FREE PLAY (LATERAL AND LONGITUDINAL) OF BEARINGS FOUND ON BOTH 2 CENTRAL RUDDER HINGES OF VERTICAL STABILAZER REAR SPAR. HINGE 3 WAS REPAIRED PER RIL #1213 REV. A. AND HINGE 2 WAS REPLACED PER RIL #2103 REV. B.SDR VNAA202607120019Rib · crackedCRACK ON OUTB MACHINED RIB OF FLS 168.07 TRAILING EDGE AREA AT WING RH. RIB OF FLS 168.07 TRAILING EDGE AREA AT RH WING WAS REPAIRED PER REO 690-57-51-542 REV. - -SDR VNAA202607120018Floorbeam · crackedCRACK ON CENTER FLOOR BEAM RBL12.0 BTW 221.73 TO FS 229.00 AT FWD FUSELAGE INTERNAL STRUCTURE (FLIGHT COMPARTMENT FLOOR STRUCTURE BELOW WL79.50). CENTER FLOOR BEAM RBL12.0 BTW 221.73 TO FS 229.00 AT FWD FUSELAGE INTERNAL STRUCTURE (FLIGHT COMPARTMENT FLOOR SSDR AALA202607113398Transition Panel · corrodedAIRCRAFT IN BASE MAINTENANCE: EXFOLIATION CORROSION ON TRANSITION PANEL AT STA 727H TO 767, RBL 22. MAINTENANCE REPLACED TRANSITION PANEL AT STA 727H TO 767, RBL 22 IAW BOEING DRAWING 1467500 & AARD 51-00-05-01.SDR SWAA2026071010750Floorbeam · corrodedCORROSION ON FLOORBEAM LOCATED BS 986.5 RBL 43 WL 208.1 AT AFT GALLEY AREA. REPAIRED FLOORBEAM LOCATED BS 986.5 RBL 43 WL 208.1 AT AFT GALLEY AREA IAW SRM 53-70-51-2R-6, REPAIR 6, ALTERNATIVE 4.SDR AALA202607109267Mount · corrodedAIRCRAFT IN BASE MAINTENANCE: L1 ENTRY DOOR GIRT BAR MOUNT CORRODED. MAINTENANCE REPLACED 1 ENTRY DOOR GRT BAR MOUNT IAW AARD 51-00-05-1.SDR AALA202607106399Transition Panel · corrodedAIRCRAFT IN BASE MAINTENANCE: LH TRANSITION PANEL HAS CORROSION FROM BS 727C TO 727J AT LBL22. MAINTENANCE REPLACED TRANSITION PANEL IAW AARD 51-00-05-01 AND OEING DWG 146A7500.SDR AALA202607108772Web · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON THRESHOLD WEB AT 983 AND LBL 55 UNDER CREASE ANGLE. MAINTENANCE REPLACED WEB AT 983 AND LBL 55 IAW DWG 147A8501 AND AAARD 51-00-05-1.SDR AALA202607101879Web · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON OUTER WEB AFT OF L2 THREASHOLD AT STA 994, LBL 54. MAINTENANCE REPLACED OUTER WEB AT STA 994, LBL 54 IAW AARD 51-00-05-1 AND BOEING DWG 147A8510.SDR CALA2026070717571Floorbeam · corrodedFOUND DAMAGE CORROSION AT AFT WET AREA FLOORBEAM BS 947 RBL 50 TO BE OUT OF LIMITS , REPAIRED WET AREA FLOORBEAM STA 947 BETWEEN LBL 7.8 TO RBL 55 IAW SRM 53-70-51-2R-5 THIS REPAIR IS CATEGORY A REPAIR NO FOLLOW ACTION REQUIRE.SDR HNAA2026070700583Floor Support · corrodedLAVATORY FLOOR SUPPORT BETWEEN FR60 AND FR61 IS CORRODED AROUND SINK DRAIN FITTING. REMOVED AND REPLACED LAVATORY FLOOR SUPPORT BETWEEN FR60 AND FR61 IAW EMB 145 SRM 51-40-02.SDR HNAA2026070700582Bearing · corrodedNLG LEG LT HALF BEARING CORRODED. R & R NLG LEG LT HALF BEARING IAW AMM 32-10-01. SEE W/C 53-20-06 FOR INSTALLATION.SDR HNAA2026070700581Seat Track · corrodedRT UPPER SEAT TRACK NR 4 HAS CORROSION IN MULTIPLE AREAS. REMOVED AND REPLACED RT UPPER SEAT TRACK NR 4 IAW AMM 53-01-06.SDR SWAA2026070610461Access Panel · damagedELONGATED HOLES ACCESS PANEL 661BB AT RT WING. REPAIRED ACCESS PANEL 661BB AT RT WING IAW SRM 51-70-05-2R-9 REPAIR 9.SDR SWAA2026070110468Pressure Deck · crackedCRACK NOTED ON LH HORIZONTAL PRESSURE DECK BS 663+9.5; LBL 37.5; WL 202.5; L: 0.3'. PERFORMED REPAIR AT HORIZONTAL PRESSURE DECK BETWEEN BS 663 TO BS 675 LBL 30 TO LBL 60 PER SRM 53-40-51-2R-2 REP 2.SDR IPXA2026063081398Skin · dentedRIGHT WING AILERON UPPER SURFACE TRAILING EDGE WEDGE HAS HAIL DAMAGE WITH NUMEROUS DENTS. NOT LISTED ON ADM OR DEFERRAL LOG. REMOVED R/H WING ALL SPEED AILERON IAW A300-600 AMM 27-11-28/401. INSTALLED RT WING ALL SPEED AILERON IAW AMM 27-11-28/401.SDR SWAA2026063010342Skin · delaminatedRIGHT OTBD AFT FLAP LOWER INBD END DELAMINATED. RECEIVED A NEW RT OTBD AFT FLAP, INSTALLATION WILL BE ACCOMPLISHED ON CC TTG8Q01CM9EG.SDR SWAA2026063010344Wedge · delaminatedLEFT INBD MID FLAP OTBD T/E EDGE WEDGE DELAMINATED AT TRAILING EDGE. REMOVED AND REPLACED LEFT INBD MID FLAP OTBD T/E EDGE WEDGE IAW SRM 51-40-02-0G-0, SRM 51-40-05-0G-0, 51-40-02-0G-0, DWG 113A2100 REV. C, & AMM 51-31-00.SDR REXA2026062900987Drag Angle · crackedTHERE IS A POSSIBLE CRACK IN THE RIGHT-HAND VERTICAL STABILIZER DRAG ANGLE. STRIPPED PAINT FROM FWD DRAG ANGLE IAW CRJ900 SRM 51-26-01-001-001-A01. FOUND FWD DRAG ANGLE TO BE VISUALLY CRACKED 2.35"L, REMOVED FASTENERS FOR ACCESS FOR REPAIR IAW SRM 51-42-06-0SDR REXA2026062600979Bushing · damagedUPON REMOVAL OF THE LT WING SIDE AILERON BUSHINGS, IT WAS FOUND THAT THE LUG -C- (HINGE NR 2 INBD) WAS PREVIOUSLY O/S & CURRENTLY MEASURES (0.8965"). COMPLIED WITH STEPS NR 1 & 2 OF IAW REO 690-57-51-541, REV -. ENSURED NO PREVIOUS BLENDING ON WING SIDE AILSDR IPXA2026062381318Web · crackedINTERCOSTAL LOCATED ON RT WING TRAILING EDGE ABOVE #2 OUTBD FLAP CARRIAGE FWD LOWER CORNER IS CRACKED. AA010. REMOVED WEB AND BRACKET ON RH WING TRAILING EDGE ABOVE #2 OUTBD FLAP IAW A300 SRM 51-40-21. INSTALLED NEW WEB IN RH WING TRAILING EDGE ABOVE #2 OUTBD SDR IPXA2026062388115Carriage · crackedINTERCOSTAL LOCATED ON LEFT WING TRAILING EDGE ABOVE THE NR 2 OTBD FLAP CARRIAGE IS CRACKED AT THE LOWER FWD AND AFT CORNERS. REMOVED INTERCOSTAL AND BRACKET AT ZONE 500 LT WING TRAILING EDGE ABOVE THE NR 2 OTBD FLAP CARRIAGE IAW SRM 51-40-21. INSTALLED INTERSDR AALA202606253516Access Panel · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT WING ACCESS PANEL 640JB COUNTERSINK HOLES. REPLACED ACCESS PANEL 640JB PER JOB CARD 26C64057007.SDR AALA202606257367Access Panel · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT WING ACCESS PANEL 640RB COUNTERSINK HOLES. REPLACED ACCESS PANEL 640RB PER JOB CARD 26C64057020.SDR AALA202606256197Access Panel · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT WING ACCESS PANEL 640LB COUNTERSINK HOLES. REPLACED ACCESS PANEL 640LB PER JOB CARD 26C64057020.SDR IPXA2026062381140Skin · corrodedMULTIPLE AREAS OF CORROSION ON RT WING OUTBD FIXED TRAILING EDGE UPPER SURFACE IN ADDITION TO WHAT WAS ALREADY IDENTIFIED BY QC. AA008. REMOVED DAMAGED AT RT WING OUTBD FIXED TRAILING EDGE UPPER SURFACE SECTION WAS FOUND TO BE OUT OF LIMITS (75% LOSS MATERIAL,