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 IPXA2026090366928Circuit Breaker · trippedAIR TURN BACK, WHILE ENROUTE, EICAS MSG GND EQUIPMENT COOLING RAN QRH AND PUT GND EQUIPMENT IN ALT. PROBE HEAT EICAS MSG. RT FWD FUEL PUMP AND L AFT FUEL PUMP EICAS MSGS. STATUS MSG EQPT COOLING FAN. RESET CB 310 AND RAN ALL SYSTEMS COMING OF AC BUS L SECTIOSDR DALA2026090304983Girt Bar · fodON DEPARTURE, L2 DOOR NOT INDICATING ARMED ON FAP. CLEANED DEBRIS FROM GIRT BAR & CYCLED DOOR IAW AMM 52-12. OK FOR SERVICE. (9135270) AIRCRAFT WAS GROUNDED.SDR DALA2026090304981Wire · damagedEMERGENCY LIGHT AT SEAT 50JH INOPERATIVE. REPAIRED WIRING IAW AMM 33-51. OK FOR SERVICE. (9319280) AIRCRAFT WAS GROUNDED.SDR UIEA2026090300850Test Light · inoperativeFO FLASHLIGHT TEST LIGHT INOPERATIVE. OPS CHECK PERFORMED IAW AMM 25-64-01-710-801. OPS CHECKED GOOD, NO ISSUES NOTED.SDR 2026FA0000680Motor · defectiveELEVATOR PITCH TRIM MOTOR HOUSING ATTACH SCREWS ARE WORKING LOOSE AND CAUSING EXCESSIVE MOVEMENT IN THE ELEVATOR CONTROL SYSTEM. THIS HAS BEEN AN ONGOING ISSUE WILL ALL OF OUR 24 SR20 AIRCRAFT. CIRRUS HAS BEEN NOTIFIED OF THE DEFECT (4/2/26) BUT HAS YET TO TAKSDR DALA2026090304980Flap · no discrepancyEVIDENCE OF RUBBING ON LEADING EDGE OF LEFT INBOARD FLAP LOCATED JUST ABOVE MAIN LANDING GEAR. PAINT SHOWING BARE METAL IN THAT AREA, INSPECTED LT INBD FLAP AND FOUND NO EVIDENCE OF RUBBING OR CHAFING PER B717 AMM 27-50. (9116531) (AIRCRAFT GROUNDED).SDR QR9R2026090300002Gcu · failedON APPROACH, GEN DISCON ON CAD AND GEN AMPS DROPPED TO 0.0 ON SYSTEM #2. TROUBLESHOOTING CONFIRMED THE #2 GCU TO BE BAD. REMOVED AND REPLACED GCU IAW AMM 24-30-00, 4-1; MOC SUCCESSFULLY COMPLETED.SDR ABXA20260903393Module · faultedRUDDER RATIO EICAS MSG APPEARED AFTER BLOCK OUT. CREW RETURNED TO THE GATE (BTB). MTC PERFORMED B767 FIM 27-09 FT 803 CLEARED FAULT BALLS ON RUDDER RATIO CHANGING MODULES. RAN BOTH ENGINES IAW B767AMM 71-00-00 MESSAGE DID NOT RETURN NO FURTHER ACTION REQUIREDSDR DXTR2026090302Blades · crackedBLADE S/N PMOXM75 SUCTION SIDE CRACK .155 INCH. PRESSURE SIDE CRACK .407 INCH (OPEN) THROUGH COOLING HOLE WITH CRACK PRESENT ON TOP OF COOLING HOLE R&R ENGINE.SDR QR9R2026090300001Transceiver · faultyDURING FLIGHT, #4 RADIO COULD RECEIVE BUT WAS INTERMITTENT ON TRANSMIT. REMOVED AND REPLACED TRANSCEIVER IAW CMM BK 117 C-2 COM/NAV MM.SDR DXTR2026090301Rib · crackedFOUND CRACK ON THE PYLON RIB RT AFT FIREWALL REMOVED THE CRACKED RIB IAW SRM 51-40-05. MATCH DRILLED HOLES IN NEW RIB IAW SRM 51-40-05. COMPLETED MATCH DRILL OF NEW RIB AND INSTALLED IAW SRM 51-40-05.SDR DXTR2026090300192Rib · crackedFOUND CRACK IN PYLON RIB RIGHT AFT FIREWALL. REMOVED CRACKED RIB IAW SRM 51-40-05. MATCH DRILLED HOLES IN NEW RIB IAW SRM 51-40-05. COMPLETED MATCH DRILL OF NEW RIB AND INSTALLED TO RIGHT PYLON IAW SRM 51-40-05.SDR 2A6R2026090375403Frame · corrodedFOUND CORROSION DAMAGE ON FRAME 1, REQUIRING REPLACEMENT OF THE FRAME.SDR HNAA2026102901055Skin · delaminatedRIGHT ENGINE THRUST REVERSER OTBD SKIN HAS MULTIPLE AREAS OF UNDERLYING DELAMINATION AND CORROSION. COMPLIED WITH PERMANENT REPAIR OF THE RT THRUST REVERSER EXHAUST O/B BEAM SKIN IAW ETD2026-145-015884 REV.: A AND EO1-05-26-0438.SDR HNAA2026102901054Skin · delaminatedLT ENGINE THRUST REVERSER OTBD SKIN HAD MULTIPLE AREAS OF UNDERLYING DELAMINATION AND CORROSION. COMPLIED WITH PERMANENT REPAIR OF THE LT THRUST REVERSER EXHAUST OTBD BEAM SKIN IAW ETD2026-145-015762 REV.: A AND EO1-05-26-0438.SDR IPXA2026101448502Frame Splice · corrodedRH ELEVATOR LOWER SURFACE O/B CONDUCTIVE FRAME SPLICE HAS BULGING, EVIDENCE OF CORROSION UNDERNEATH. INSTALLED RH ELEVATOR LOWER SPLICE PLATE AND RH ELEVATOR LOWER SURFACE CONDUCTIVE FRAME IAW B757-200PF SRM 51-40-02-0G-0. AND DWG 183N2003 REV G.SDR AALA202610263863Seat Track · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON MID CABIN FLOOR SEAT TRACK AT FR 35 AND Y765 LEFT - REPLACED SEAT TRACK PER SRM 51-72-11SDR VNAA202610230058Skin Panel · damagedSKIN, LOWER, PANEL WITHIN 6718.97 FLIGHT HOURS AFTER SECTION I, ACCOMPLISH A PERMANENT REPAIR AT DISCREPANT AREA IN ACCORDANCE WITH APPROVED PROCEDURES OR REPLACE PART. LIGHTNING STRIKE DAMAGE TO LOWER FUSELAGE SKIN AT FS437.00 BETWEEN STR22L - STR23L WAS RESDR VNAA202610230051Rib · crackedCRACK ON STRIP WS163.00 BELOW I/B MULTI-FUNCTION SPOILER AT RH WING. CRACK MACHINED RIB (STRIP) FLAP STA 168.07 TRAILING EDGE, BELOW I/B MULTI-FUNCTION SPOILER AT RH WING WAS REPAIRED PER
REO 690-57-51-561 REV -.SDR IPXA2026101448482Frame · corrodedRH ELEVATOR O/B UPPER SURFACE AROUND O/B STATIC DISCHARGER HAS LIGHT CORROSION. INSTALLED NEW UPPER CONDUCTIVE FRAME AND UPPER SPLICE PLATE AT R/H ELEVATOR O/B AREA IAW B757-200PF SRM 51-40-02-0G-0. AND DWG 183N2003 REV G. TOOL ID: 18-1041 DUE: 11/04/2026.SDR IPXA2026101448406Adapter · corrodedRH ELEVATOR STATIC DISCHARGER BASE, 2ND FROM O/B, HAS CORROSION. INSTALLED ADAPTER PLATE RH ELEVATOR STATIC DISCHARGER ON RH ELEVATOR UPPER SURFACE. IAW B757-200PF SRM 51-40-02-0G-0. AND DWG 183N2229 REV A.SDR REXA2026102001978Retainer · corrodedSECONDARY NRC, AFTER SEAL REMOVAL IAW NRC 00119, CORROSION FOUND ON THE AFT LOWER RETAINER SEAL, AFT RETAINER, FWD RETAINER & LOWER RETAINER SEAL. CORROSION ON AFT LOWER RETAINER SEAL, AFT RETAINER, FWD RETAINER & LOWER RETAINER SEAL WAS REMOVED IAW SRM 51-2SDR REXA2026102001977Retainer · corrodedSECONDARY NRC, AFTER SEAL REMOVAL IAW NRC 00119, CORROSION FOUND ON THE AFT LOWER RETAINER SEAL AFT RETAINER, FWD RETAINER AND LOWER RETAINER SEAL. THE CORROSION ON AFT LOWER RETAINER SEAL, AFT RETAINER, FWD RETAINER, & LOWER RETAINER SEAL WAS REMOVED IAW SRMSDR REXA2026102001976Support · crackedCRACKED JUCTION BOX SUPPORT IN THE FWD E/E BAY. JUCTION BOX SUPPORT WAS REPLACED IAW SRM 51-42-06-001-001-A01.SDR REXA2026102001962Drag Angle · crackedCRACKED VERTICAL STABILIZER TO FUSELAGE RT AFT DRAG ANGLE BTW, 55.62% DATUM TO 67.5% REAR SPAR DATUM. THE VERTICAL STABILIZER TO FUSELAGE DRAG ANGLE WAS REPAIRED IAW SRM 55-31-00-201-001-A01.SDR REXA2026102001949Floorbeam · corrodedCORROSION ON FLOORBEAM BS 280. FLOORBEAM BS 280 RT WAS REPLACED IAW SRM 51-10-06-001-001-A01, AND SRM 51-42-06-001-001-A01, SRM 51-42-21-001-001-A01 AND SRM 51-42-10-001-001-A01.SDR SWAA2026101961048Pressure Deck · dentedPREVIOUS REPAIR ON THE FLIGHT DECK FLOOR DENTED AT BS 255, RBL 4 - LBL 14, WL 207.54. REMOVED AND INSTALLED A REPLACEMENT FLIGHT DECK FLOOR WEB, BS 250 - 270, LBL 21- RBL 8 IAW SRM 51-40-02, AND EA 21-153-00734, REV A.SDR SWAA2026101472427Floor Panel · delaminatedDELAMINATED FLOOR PANEL 241AF. REPAIRED THE FLOOR PANEL IAW SRM 53-00-50-2R-7, REPAIR 7.SDR SWAA2026101433575Floor Panel · delaminatedDELAMINATED FLOOR PANEL 232SF. REPAIRED THE FLOOR PANEL IAW SRM 53-00-50-2R-7, REPAIR 7.SDR HNAA2026100900964Floor Support · crackedUPPER OMEGA PROFILE CRACKED. R & R PROFILE IAW SRM 51-40-02SDR HNAA2026100700955Pressure Blkhd · crackedFWD PX BULKHEAD, RH WEB CRACKED. REPAIRED IAW ETD 2026-145-015239 AND EO 1-53-26-0451SDR HNAA2026100700952Frame · crackedCOCKPIT, LEFT UPPER FRAME CRACKED. REPAIRED IAW ETD 2026-145-015252 AND EO 1-53-26-0462.SDR HNAA2026100700951Pressure Blkhd · crackedFWD PX BULKHEAD, LT WEB CRACKED. REPAIRED WEB IAW ETD 2026-145-015239 REV. A AND EO 1-53-26-0451SDR SWAA2026100627071Support Angle · crackedCRACKED BS 663.75 SUPPORT ANGLE, RBL 8. REPLACED THE SUPPORT ANGLE IAW SRM 51-40-02, DWG 111A1322, SHEET 13, REV A, DWG 111A1000, SHEET 387, REV -.SDR SWAA2026100505878Support Angle · crackedCRACKED SUPPORT ANGLE, BTWN BS 500C - 500D, BL 0, WL 208.1. REPLACED THE SUPPORT ANGLE IAW SRM 51-10-02, ITEM (8), AND DWG 143A5400, SHEET 231, REV-.SDR HNAA2026100200940Angle · crackedBATTERY COMPARTMENT, UPPER ANGLE CRACKED AT BTW FR 6-7. REPAIRED ANGLE IAW ETD 2026-145-015574 AND EO 1-53-26-0453SDR AALA202609307114Fitting · excess playAIRCRAFT IN BASE MAINTENANCE: NOSE LANDING GEAR AFT LEG DOOR LOWER LEFT ATTACH POINT HAS PLAY. REPLACED LEG DOOR FITTING AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK WITH NO ISSUES NOTEDSDR SWAA2026092967557Support Angle · crackedCRACKED SUPPORT ANGLE, BTWN BS 500I - 520, BL 0, WL 208.1. REPLACED THE SUPPORT ANGLE AND FASTENERS IAW SRM 51-10-02, ITEM 8, SRM 51-40-02, & DWG 143A5400, SHEET 229, REV -.SDR SWAA2026092942419Attach Angle · crackedBS 663, RBL 34 VAPOR BARRIER ATTACH ANGLE WAS CRACKED. REPAIRED THE ATTACH ANGLE IAW EA EA-M-26-157-01481.SDR SWAA2026092987379Support Angle · crackedCRACKED SUPPORT ANGLE, BTWN BS 380 - 400, LBL 13, WL 208.1. REPLACED THE SUPPORT ANGLE IAW SRM 51-40-02, SRM 51-10-02, DWG 143A5400, SHEET 184, REV -, & DWG 143A5400, SHEET 182, REV-.SDR SWAA2026092976230Attach Angle · crackedBS 663, RBL 30.5 VAPOR BARRIER ATTACH ANGLE WAS CRACKED. THE ATTACH ANGLE WAS REPAIRED IAW EA M-26-157-01481.SDR SWAA2026092956029Support Bracket · crackedCRACKED SUPPORT BRACKET, BS 867, STR 2R - 3R. REPLACED THE SUPPORT BRACKET IAW SRM 51-10-02-0G-0, ITEM 8, SRM 51-40-02-0G-2, & DWG 146A7901, SHEET 66, REV A.SDR J7SA2026092900521Fce · faultedFLAPS FAIL ON STARTUP. REPLACED # 1 FCE IAW EMB PHENOM 300 AMM 27-03-01.SDR R61A2026092600270Skin · crackedDURING HEAVY CHECK MAINTENANCE FOUND LT WING FIXED LEADING EDGE SLAT 2 IB TRACK UPPER CUT OUT CRACKED. LT WING FIXED LEADING EDGE SLAT 2 IB TRACK UPPER CUT OUT REPAIRED IAW ETD2026-170-015333.SDR R61A2026092600269Skin · crackedDURING HEAVY CHECK MAINTENANCE FOUND RH WING FIXED LEADING EDGE SLAT #2 IB TRACK UPPER CUT OUT CRACKED. RH WING FIXED LEADING EDGE SLAT #2 IB TRACK UPPER CUT OUT HAS BEEN REPAIRED IAW EMB ETD2026-170-015335.SDR SWAA2026092565083Bracket · crackedACCESS PANEL 651FB HAD A CRACKED BRACKET. REMOVED AND REPLACED THE BRACKET ON THE RT WING ACCESS PANEL 651FB IAW SRM 51-40-02-0G-0.SDR REXA2026092501880Lug · damagedFOUND L/H AILERON SIDE LUG LABELED G TO BE OVERSIZED. COMPLIED WITH STEP F(8) OF REO 670-57-61-237 REV. --, FABRICATED (QTY. 1) O/S AILERON BUSHING. LPI PERFORMED IAW STEP F(9) OF REO 670-57-61-237 REV--. NO INDICATIONS NOTED. APPLIED BRUSH CAD-PLATING TSDR REXA2026092501879Lug · damagedFOUND LT AILERON SIDE LUG LABELED B TO BE OVERSIZED. FABRICATED (QTY. 1) O/S AILERON BUSHING. LPI PERFORMED IAW STEP F(9) OF REO 670-57-61-237 REV. --. NO INDICATIONS NOTED. APPLIED BRUSH CAD-PLATING TO NEW BUSHING LABELED B IAW STEP F(8) OF REO 670-57-61-SDR REXA2026092501876Lug · damagedFOUND LT AILERON SIDE LUG LABELED I TO BE OVERSIZED. COMPLIED WITH SECTION I UPPER LUG ONLY IAW STEPS 1-3 OF REO 690-57-61-556 REV --(P2). PERFORMED EDDY CURRENT OF LT AILERON LUG IAW REO 690-57-61-556 REV -- P2. NO INDICATIONS NOTED. COMPLIED WITH SECTION ISDR REXA2026092501875Lug · damagedFOUND L/H AILERON SIDE LUG LABELED -H- TO BE OVERSIZED. COMPLIED WITH SECTION LOWER LUG ONLY IAW STEPS 1-3 OF REO 690-57-61-556 REV --(P2). PERFORMED EDDY CURRENT OF LT AILERON LUG LABEL H IAW REO 690-57-61-556 REV -- P2. NO INDICATIONS NOTED. COMPLIED WITH