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 SIMA202602176001Door · bindingL1 DOOR BINDING WHEN CLOSING. GATE AGENT ALSO SAID WAS DIFFICULT TO OPEN FROM OUTSIDE. TRANSFERRED TO NRWC 771-DFW-02680. OPEN.SDR ABXA20260216066Lock · installedPER MXC, A/C BACK TO GATE (BTB) TO REMOVE CENTER WING LOCK INSTALLED ON L/P 39114-88/1 (LOADING CREW REPORTED CTR WING LOCK MISSING RT MCD STA 1490, BL0). REMOVED PREVIOUSLY INSTALLED CENTER WING LOCK AT STA 1490, BL 0 PER IAI CMM -50-20-21 AND ABX CLS B767 MSDR 2026FA0000127Fuel Sys · contaminatedPOLLUTION FOUND IN FUEL TANKS AFTER REMOVAL OF BOTH WINGS - FOLLOWING REMOVAL OF BOTH WINGS FOR REPLACEMENT OF LOWER PANELS AFTER 2C INSPECTION PERFORMED IN 2025, WE FOUND CONTAMINATION IN THE WINGS, IN THE CENTRE TANK, IN THE THREE FEEDERS’ TANKS, IN THE FILTSDR CALA2026021713836Lens · missingPROXIMITY LIGHT OF THE SEAT 4F WITH LENS MISSING. FLOOR PROXIMITY LIGHT REMOVED IAW AMM DMC-B787-A-33-51-06-00A-520A-A AND INSTALLED IAW AMM DMC-B787-A-33-51-06-00A-720A-A AND ITEM OK. GOOD FOR FLIGHT.SDR CALA2026021713834Light · inoperativeEMERGENCY AISLE LIGHT INOPERATIVE AT SEAT 24C. REMOVED AND REPLACED LIGHT FIXTURE PATH FINDER AT SEAT 24C REF CMM 25-23-54. EMERGENCY LIGHT TEST OK IAW AMM 33-51-00.SDR CALA2026021713832Bulb · inoperativeEMERGENCY DOME LIGHT INOP IN FLIGHT DECK COMPARTMENT. REMOVED AND REPLACED THE SECONDARY LAMP OF THE LEFT DOME LIGHT REF AMM 33-14-00-960-804. EMERGENCY DOME LIGHT TEST OK REF AMM 33-51-00.SDR QXEA2026021600033Brake Assy · malfunctionedON LANDING ROLLOUT APPLIED BRAKES A/C SKIPPED A FEW TIMES. LET OFF BRAKES AND REAPPLIED AND A/C "SKIPPED" A FEW MORE TIMES. REMOVED FROM SERVICE. PERFORMED GVI OF BRAKES. NO DEFECTS NOTED. TAXID WITH CREW TO PERFORM HIGH SPEED TAXI. COULD NOT DUPLICATE SKIPPINSDR JJBA20260216026Shear Tie · crackedFRAME 61 RH SHEAR TIE CRACKED. REMOVED AND REPLACED SHEAR TIE.SDR AALA202602167300Slide · low pressureAIRCRAFT WAS NOT GROUNDED: SLIDE RAFT NUMBER 3 PRESSURE BOTTLE LOW. REMOVED AND REPLACED SLIDE RAFT NUMBER 3. PER AMM 25-64-00.SDR AALA202602167198Wire Harness · no testAIRCRAFT WAS NOT GROUNDED: SEAT 1C EMERGENCY WHITE LIGHT INOPERATIVE. MAINTENANCE FOUND THE EMERGENCY LIGHTING HARNESS INSIDE OF THE SEAT ENDBAY WAS DEFECTIVE AND REPLACED THE SEAT END BAY WITH A SERVICABLE UNIT THAT ALSO CONTAINED A SERVICEABLE HARNESS PER CMSDR AALA202602164433Bottle · low pressureAIRCRAFT WAS GROUNDED: R2 DOOR DAMPER AND EMERGENCY OPERATION CYLINDER PRESSURE LOW. SERVICED DOOR DAMPER AND EMERGENCY OPERATION CYLINDER PER AMM 52-22-00.SDR AALA202602161475Bottle · low pressureAIRCRAFT WAS GROUNDED: L2 DOOR DAMPER AND EMERGENCY OPERATION CYLINDER PRESSURE LOW. SERVICED DOOR DAMPER AND EMERGENCY OPERATION CYLINDER PER AMM 52-22-00.SDR AALA202602169766Bottle · low pressureAIRCRAFT WAS GROUNDED: R4 DOOR DAMPER AND EMERGENCY OPERATION CYLINDER PRESSURE LOW. SERVICED DOOR DAMPER AND EMERGENCY OPERATION CYLINDER PER AMM 52-10-00.SDR AALA202602168513Bottle · low pressureAIRCRAFT WAS GROUNDED: L1 DOOR DAMPER AND EMERGENCY OPERATION CYLINDER PRESSURE LOW. SERVICED DOOR DAMPER AND EMERGENCY OPERATION CYLINDER PER AMM 52-10-00.SDR DALA2026021601053Uplock Sensor · faultedATB DUE TO NOSE LANDING GEAR WOULD NOT RETRACT (L/G DOORS NOT CLOSED ECAM WARNING). REPLACED NLG UPLOCK PROXIMITY SENSOR (13GA). (LP 8129952)SDR FDEA202602160217Safety Wire · wrong partLEFT SLIDE ASSY. SN 3359, FOUND BREAK AWAY WIRE SECURES THE RELEASE MECHANISM NOT TO BE CLAD-PLATED COPPER WIRE. RELEASED FOR SERVICE PER MEL : 52-11-01-02 CATEGORY : C EXPIRATION : 22FEB26 "MEL 52-11-01-02: DOOR _L1__ DOOR - INOP. IF SLID E/RAFT TO BE SDR FDEA202602160216Safety Wire · wrong partFOUND L1 DOOR SLIDE SAFETY WIRE NON-COMPATIBLE, NEEDS REPLACING. REPLACED SAFETY WIRE WITH PART NO. MS20995CY16 CAD PLATED COPPER. REF. AMM 25-66-01-4. AC OK FOR SERVICE.SDR FDEA202602160215Safety Wire · wrong partRH SLIDE - REPLACE THE BREAKAWAY WIRE SECURING THE RELEASE CABLE TO THE PACKBOARD RELEASE MECHANISM ON THE PACKBOARD WITH MS20995CY16 CAD-PLATED COPPER WIRE PER SMIS 25-60/5696 (F.E.A.# G-2560-F0386294 C PART 1) RH SLIDE - REPLACE THE BREAKAWAY WIRE SESDR FDEA202602160214Safety Wire · wrong partLH SLIDE - REPLACE THE BREAKAWAY WIRE SECURING THE RELEASE CABLE TO THE PACKBOAR RELEASE MECHANISM ON THE PACKBOARD WITH MS20995CY16 CAD-PLATED COPPER WIRE PER SMIS 25-60/3937 (FEA G-2560-F0386282 C P1). REMOVED AND REPLACED BREAKAWAY WIRE SECURING RELESDR FDEA202602160213Safety Wire · wrong partL1 DOOR SLIDE HAS INCORRECT LOCK WIRE INSTALLED ON PACKBOARD RELEASE CABLE TO RELEASE MECHANISM. REF WRI 25-60 6781 MOD TYPE F MOD NO. G-2560-F0386282 REV NO. C PS P1. SAFTIED L1 DOOR SLIDE WITH CAD-COPPER BREAKAWAY LOCK WIRE INSTALLED ON PACKBOARD RELEASDR 2026FA0000125Angle · corrodedNOSE TUNNEL CORROSION.SDR 2026FA0000124Fastener · interferenceHI-LOC CLEARANCE AND INTERFERENCE.SDR SWIA2026021576174Skin · ground damageTECH HIT AIRCRAFT WITH MAN LIFT ON RH SKIN PANEL AND DENT AND GOUGED SKIN FROM BS 1000 TO BS 1015 BETWEEN STRG 15R AND 17R. RECEIVED AND COMPLIED WITH FINAL MHIRJ REO 670-53-61-2685 REV -. THE REPAIR OF DAMAGE FROM FS 1000 TO FS 1015 RH SKIN PANEL BETWEEN STSDR REXA2026052700691Stand Off · crackedPARTS RACK: CRACKED INNER SUPPORT ANGLE (STANDOFF 1 EA) ON LH LOWER TRANSCOWL. INNER SUPPORT ANGLE (STANDOFF 1 EA) ON LH LOWER TRANSCOWL WAS REPAIRED AND REPLACED PER CRJ-900 SRM 51-42-21-001-001-A01, CRJ-900 SRM 51-42-28-001-001-A01, EA CRJ954-21413 REV A, CSDR 3EJA202603250004Acm · false indicationDURING TAKEOFF AT 100 FEET ACM OVERHEAT LIGHT ILLUMINATED ALONG WITH AN ODOR OF PLASTIC MELTING. TROUBLE SHOT AND COULD NOT DUPLICATE.SDR SWAA2026032371183Skin · crackedCRACK INDICATION FOUND ON LT HORIZONTAL STAB LOWER SKIN PANEL. HSS 193.9, RIB & 8 INCHES FROM REAR SPAR. INBD SIDE OF RIB. PERFORMED MAJOR REPAIR ON LT HORIZONTAL STAB LOWER SKIN PANEL IAW EA 26-155-00655-WIP1, EA 26-155-00655-WIP2, & EA 26-155-00655.SDR SWAA2026032370948Nut · deterioratedDETERIORATED HANDLE NUT ON ENTRY AND SERVICE DOORS. REPLACED THE NUT IAW SOPM 20-50-01, REV.40.SDR SWAA2026032371181Crossbeam · crackedCRACKED CROSSBEAM, BS 540 BTWN BL 0 - LBL 24.75, WL 208.1. REPLACED THE CROSSBEAM IAW SRM 51-10-02, ITEM 9, & SRM 51-40-02.SDR SWAA2026032371180Crossbeam · crackedCRACKED CROSSBEAM, BS 540 BTWN BL 0 - RBL 24.75, WL 208.1. REPLACED THE CROSSBEAM IAW SRM 51-40-02, & SRM 51-10-02, PARAGRAPH 9.SDR SWAA2026032370959Nut Plate · corrodedCORROSION RAIL NUT PLATE LOCATED ON INTERNAL CAVITY LEADING EDGE OFSS308 AT RT WING. REPLACED RAIL NUT PLATE LOCATED ON INTERNAL CAVITY LEADING EDGE OFSS308 AT RT WING IAW SRM 51-10-02 ITEM 9, & DWG 112A4402, SHEET 8, REV. B.SDR SWIA2026031875544Mount · crackedCARGO DOOR, FWD AND AFT BALANCE SPRING BOXES MOUNTING PLATES CRACKED AROUND BALANCE SPRING BOX MOUNTING BOLTS. REMOVED AND INSTALLED NEW AFT CARGO DOOR BALANCE SPRING BOX FWD AND AFT MOUNTING PLATE IAW DWG 601R35055, REV T AND SRM 51-42-06. OPS TEST GOOD.SDR SWAA2026031677316Strap · out of adjustBS 328 FRAME STRAP FROM STR 22R TO STR 20R DOES NOT MATCH WITH CONFIGURATION TASK 5311-I-17336-NG FIGURE 15, AS PER EA 26-153-00455, THE CONFIGURATION IS ACCEPTABLE.SDR CALA2026030914406Floor Skin · dentedCOCKPIT AFT OF PEDESTAL FLOOR PANEL, SKIN HAS SEVERAL DENTS AND BARE METAL. REPAIRED COCKPIT FLOOR SKIN IAW REO-G25794, REV IR, & EC/RA 5310-08803.SDR CALA2026030914404Pressure Web · crackedREAR SPAR VERTICAL PRESSURE WEB BETWEEN LBL 45.64 AND LBL 40.00 CRACKED. REPAIRED CENER WING REAR SPAR VERTICAL PRESSURE WEB BETWEEN LBL45.64 AND LBL40.SDR IPXA2026030523252Fitting · crackedFOUND RT SPOILER NR 7 INBD SIDE SUPPORT RIB FITTING CRACKED, WBL 255. IAW AMM 20-51-01-912-008, REV 115 INSTALLED THE SUPPORT ROD. CONDITION CHECKED NORMAL.SDR IPXA2026030223147Web · crackedFOUND LT NR 5 SPOILER OTBD SIDE, SUPPORT WEB CRACKED, WBL 432. REMOVED THE DAMAGED WEB IAW SRM 51-40-02-0G, REV 105, INSTALLED A NEW WEB IAW SRM 51-40-02-0G, REV 106, DWG 65B10865, SHT 2, REV N, & DWG 65B11629, SHT 2, REV E.SDR IPXA2026030223284Bracket · crackedFOUND MAIN DECK CARGO TRIM AIR DUCT SUPPORT BRACKET CRACKED, BS 1180 LT. REMOVED THE DAMAGED BRACKET IAW SRM 51-40-02-0G, REV 106, INSTALLED A NEW BRACKET IAW SRM 51-40-02-0G, REV 106, & DWG 214U2177, SHT 2, REV C.SDR IPXA2026030222795Door · brokenBROKEN PANEL, LOWER FACE OF LT WING NR 3 SLAT OTBD SEAL DOOR. INSTALL NEW SEAL DOOR IAW SRM 51-40-02-0G, REV 94, AND AIPC 57-41-51-15 REV. 141.SDR DALA2026030201422Ils System · unreliableILS IS SOMEWHAT NOT RELIABLE, THEREFORE, AN STC FOR "ILS LOOK-ALIKE" LPV IS BEING DEVELOPED AS A BACK UP FOR ILS. ACCOMPLISHED ER/A 632398-14 (1452682)SDR SIMA20260215003Seat Track · corrodedCORROSION - FWD WET AREA - LEFT TRACK AT FRAME 17 THRU 20 (MAJOR REPAIR) (LEVEL 2 CORROSION) BLENDED CORRODED AREA ON FWD WET AREA LEFT TRACK AT FRAME 17 THRU 20 -17 PER EMB-175 SRM 51-10-03. DEEPEST BLENDED AREA MEASURES (L=1?,W=.5?,.039? ). ORIGINAL MATERIALSDR SIMA20260215002Seat Track · corrodedSSI 53-10-027-0392CORROSION - FWD WET AREA - RIGHT TRACK AT FRAME 17 (MAJOR REPAIR) (LEVEL 2 CORROSION). BLENDED CORRODED AREA ON FWD WET AREA RIGHT TRACK AT FRAME 17 PER EMB-175 SRM 51-10-03. BLENDED AREA MEASURES (L=1.2?,W=.8?,H=.025?). ORIGNAL MATERIAL THICSDR SIMA20260215004Seat Track · corrodedAFT WET AREA - RH TRACK - AT FRAME 85 Y + 10 " (MAJOR REPAIR) (LEVEL 2 CORROSION). DAMAGED AREA ON AFT WET AREA - RH TRACK - AT FRAME 85 Y + 10 " IS FOUND TO BE CORRODED PER EMB-175 SRM 51-10-02. AFTER FURTHER EVAL PART IS FOUND TO BE OUT OF ALLOWABLE LIMITS PSDR IPXA2026022622496Former · crackedCRACK-FORMER, FWD SIDE OF L/H WING OUTBD L/E NOSE BEAM, OSS 717.29 (REPLACE). INSTALL NEW NOSE FORMER IAW SRM 51-40-02-0G REV.94 AND BOEING DWG NO. 114T2164 SH 6 REV - AND UPS EO-96624-REQ1 REV1 .SDR IPXA2026022320352Angle · crackedFOUND THE ANGLE CRACK AT STA 1578 RBL 80 OUTBOARD IN BULK CARGO COMPARTMENT RIGHT AREA. (REPLACE). I.A.W SRM 51-40-02-0G REV. 94 AND BOEING DWG NO.146T5650 SH.5 REV.C INSTALLED NEW ANGLE.SDR IPXA2026022320306Angle · crackedFOUND THE ANGLE CRACK AT STA 1578 LBL 80 OUTBOARD IN BULK CARGO COMPARTMENT LEFT AREA. (REPLACE). I.A.W SRM 51-40-02-0G REV. 94 AND BOEING DWG NO.146T5650 SH.5 REV.C INSTALLED NEW ANGLE.SDR AALA202602265992Angle · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK IN FORWARD CARGO COMPARTMENT FLOOR STRUCTURE BAFFLE CLIP AT BS 500G, RBL 25. REPLACED BAFFLE CLIP PER AARD 51-00-05-1.SDR AALA202602264813Angle · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK IN FORWARD CARGO COMPARTMENT FLOOR STRUCTURE BAFFLE CLIP AT BS 500H, RBL 25. REPLACED BAFFLE CLIP PER AARD 51-00-05-1.SDR IPXA2026022320466Angle · crackedFAULT - FOUND THE ANGLE CRACK AT STA 1578 RBL 80 INBOARD IN BULK CARGO COMPARTMENT RIGHT AREA. (REPLACE). I.A.W SRM 51-40-02-0G REV. 94 AND BOEING DWG NO.146T5650 SH.5 REV.C INSTALLED NEW ANGLE. REVIEW COMPLETESDR IPXA2026022320039Angle · crackedFAULT - FOUND THE ANGLE CRACK AT STA 1578 LBL 80 INBOARD IN BULK CARGO COMPARTMENT LEFT AREA. (REPLACE). I.A.W SRM 51-40-02-0G REV. 94 AND BOEING DWG NO.146T5650 SH.5 REV.C INSTALLED NEW ANGLE. REVIEW COMPLETESDR FDEA202602150250Reservoir · failedPREFLIGHT CHECK FOUND LEFT ENTRY DOOR EPAS RESERVOIR PRESSURE DROP TO 0. REMOVED AND REPLACED LH EPAS RESERVOIR REF B777 AMM 52-11-22-4.