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.

SDR SWAA2026033076730Sidewall Support · corrodedAFT CARGO SIDEWALL SUPPORT AT LBL 22, BS 727 - 847 WAS CORRODED AT SEVERAL LOCATIONS. REMOVED AND REPLACED SIDEWALL SUPPORT IAW SRM 51-40-02-0G-0, & DWG 146A7500, REV-.Mar 4, 2026 · N249WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2026033076731Sidewall Support · corrodedAFT CARGO SIDEWALL SUPPORT AT RBL 22, BS 727 - 767 CORRODED AT SEVERAL LOCATIONS. REMOVED AND REPLACED THE SIDEWALL SUPPORT IAW SRM 51-40-02-0G-0, & DWG 146A7500, REV -.Mar 4, 2026 · N249WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2026033076732Sidewall Support · corrodedAFT CARGO SIDEWALL SUPPORT AT BS 727A, LBL 22, WL 155 CORRODED. SIDEWALL SUPPORT RESOLVED ON CUSTOMER CARD TTG8Q01ASTYM.Mar 4, 2026 · N249WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2026033076808Pressure Blkhd · crackedAFT PRESSURE BULKHEAD HAD A CRACK INDICATION, EMANATING FROM RIVET AT STRINGER 7R LOWER GROUP OF FIVE, CLOSEST TO APEX. APPROX. 1/8' LONG. REJECTED STEP 43 FOR EDGE MARGIN IS OUT OF LIMITS OF -1 FILLER AND -2 FILLER. REFABRICATED -1 AND -2 REPAIR PARTS TO MMar 4, 2026 · N486WN · Boeing 7377H4 · Fuselage Main, BulkheadSDR IPXA2026032721947Floor Panel · corrodedEXFOLIATION FLOOR PANEL RT SIDE AFT CARGO BS 1600-1560, STR 27 AND 28R. REMOVED CORROSION FROM FLOOR PANEL RT SIDE AFT CARGO. MAT LOSS MORE THAN 50%. MAX ALLOWABLE IS 10%. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-1A-1 FIG 101. INSTALLED REPAIR DOUBLER IN Mar 4, 2026 · N451UP · Boeing 75724APF · Fuselage Floor PanelSDR IPXA2026031919295Tee Angle · corrodedLOWER HALF OF FUSELAGE TEE ANGLE BETWEEN BS 1040 & 1060, AROUND STRINGER 25R HAD CORROSION. INSTALLED A NEW TEE ANGLE BTWN BS 1040 - 1060, STRINGER 25R IAW SRM 51-40-02-0G-0.Mar 4, 2026 · N416UP · Boeing 75724APF · Fuselage Miscellaneous StructureSDR IPXA2026032119365Angle · corrodedLOWER HALF OF FUSELAGE RH PACK HOT AIR EXHAUST FRONT STRUCTURE ANGLE BETWEEN STR 1040 AND STR 1060 HAS CORROSION DOT 115-004. INSTALLED NEW INTERCOSTAL AND REINSTALLED COVER SUPPORT HOT AIR EXHAUST, IAW B757-200PF, SRM 51-40-02.Mar 4, 2026 · N416UP · Boeing 75724APF · Fuselage Miscellaneous StructureSDR SWAA2026032076727Support · corrodedFWD CARGO COMPARTMENT FLOOR TO BULKHEAD SUPPORT CORRODED, BS 500D, LBL22 - RBL 22, WL 156. REMOVED AND REPLACED THE FLOOR TO BULKHEAD SUPPORT IAW SRM 51-40-02-0G, AND DRAWING 143A9481, REV -.Mar 4, 2026 · N924WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2026032076725Sidewall Support · corrodedFWD CARGO BAY FLOOR TO SIDEWALL SUPPORT CORRODED, BS 500A+6, 500A+10, 500A+14, & 500A+18, RBL 25, WL 156. REMOVED AND REPLACED THE SIDEWALL SUPPORT IAW SRM 51-40-02-0G, AND DRAWING 143A7500, REV -.Mar 4, 2026 · N924WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2026032076726Sidewall Support · corrodedCORROSION ON FWD CARGO COMPARTMENT FLOOR TO SIDEWALL SUPPORT BS 400-500D; LBL22; WL 156. REMOVED AND REPLACED FWD. CARGO FLOOR TO SIDEWALL SUPPORT IAW SRM 51-40-02-0G AND DRAWING 143A7500 REV -.Mar 4, 2026 · N924WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR IPXA2026031816555Seat Track · corrodedMAJOR REPAIR, DURING PANEL CLOSE ON MDC FLOOR, FR 75, Y794.3, SEAT TRACK WITH CORROSION. REMOVED CORROSION WITH ABRASION BY HAND AT MCD FLOOR FR 75, Y794.3, IAW SRM 51-74-10-201. INSTALLED SEAT TRACK SECTION AND U-SECTION SPLICE FITTINGS (04EA), IAW A300-600Mar 4, 2026 · N135UP · Airbus A300F4622R · Fuselage, Seat/Cargo Attach FittingsSDR SWAA2026031676607Receiver · brokenOWE LT FWD EMERGENCY LIGHT ASSY RECEPTACLE IS BROKEN. REMOVED AND REPLACED IAW AMM 33-21-00-960-805-NG.Mar 4, 2026 · N8611F · Boeing 7378H4 · Emergency LightingSDR J7SA2026031200476Acm · faultedREJECTED TAKEOFF DUE TO PACK TEMP HIGH CAS, PACK FAIL CAS, AND VISIBLE SMOKE IN CABIN. CREW TAXIED BACK TO THE FBO WITHOUT INCIDENT. FOUND BROKEN BLADE ON ACM. REPLACED ACM AND PRECOOLER. PERFORMED OPS AND BLEED CHECKS. ALL CHECKS SATISFACTORY AT THIS TIME. WOMar 4, 2026 · N531FX · Bombdr BD1001A10 · Cabin Cooling SystemSDR AALA202603128966Angle · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK IN WING CENTER SECTION REAR SPAR VAPOR BARRIER ATTACH ANGLE AT BS 663, S23L, AND LBL 9. REPAIRED ANGLE PER SRM 57-10-10-2R-5.Mar 4, 2026 · N990AN · Boeing 737823 · Wing, Center BoxSDR AALA202603126437Rib · wornAIRCRAFT IN BASE MAINTENANCE: RIGHT WING OUTBOARD FLAP OUTBOARD DEFLECTION CONTROL RIB WORN. REPLACED RIB PER AARD 51-00-05 AND EA 372815.Mar 4, 2026 · N983AN · Boeing 737823 · Trailing Edge FlapsSDR AALA202603121287Shock Absorber · abnormalAIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED AND THE AIRCRAFT RETURNED TO LAX DUE TO THE FLIGHT CREW REPORTING A LANDING GEAR NOT UPLOCKED / SHOCK ABSORBER ECAM FAULT DISPLAYED AFTER LIFT OFF. THE AIRCRAFT L/G GEAR NOT UPLOCKED SHOCK ABSORBER FAULT AFTER LMar 4, 2026 · N435AN · Airbus A321253NX · Landing Gear Position and WarningSDR AALA202603117620Fitting · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON KEEL BEAM LATTICE FITTING AT STA 882 BETWEEN LBL 11.5 AND RBL 11.5. REPLACED LATTICE FITTING PER DWG 450Z4110-19.Mar 4, 2026 · N819AN · Boeing 7878 · Fuselage Main, KeelSDR AALA202603109974Heatshrink · missingAIRCRAFT WAS NOT GROUNDED: THE RED INDICATORS ON THE GIRT BAR ON THE R1 DOOR MISSING. : INSTALLED HEAT SHRINK TUBE. PER J/C 2523J012-001.Mar 4, 2026 · N819NN · Boeing 737823 · Emergency EquipmentSDR ASAA2026030464793Battery Pack · dischargedEMERGENCY LIGHTS OUT ON THE FOLLOWING: R/H OVERWING EXIT, ROWS 8L, 11L, CABIN CEILING EXIT LIGHT. GROUNDED - YES. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY S/N 411270 AT ROW 7LH, OPS CHECK GOOD IAW B737-900 AMM 33-51-06-960-805.Mar 4, 2026 · N494AS · Boeing 737990ER · Emergency LightingSDR DALA2026031001638Skin · damagedSHIP 9500 ELONGATED HOLE (1EA) AND TOOL MARKS (1EA ) ON INNER/OUTER SKIN FROM FUEL ACCESS PANEL 620JB AT RH WING. CORRECTIVE ACTION: REPAIRED PER PRI 632126-14 (1479482)Mar 4, 2026 · N949AT · Boeing 717200 · Wing, Plate/SkinSDR DALA2026031001637Doubler · crackedCRACK ON INTERNAL PRODUCTION DOUBLER INSIDE OF AFT ACCESSORY COMPARMET IN LONGERON 3 RH,CANTED STA Y= 1178.225 APPROX. CORRECTIVE ACTION: REPAIRED PER B717-200 SRM 53-30-08-2R-9 PROCEDURE 9 REPAIR 9 (1478843)Mar 4, 2026 · N949AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2026031001648Not Reported · not reportedER/A 627199-14AD REV F REQUIRES STAGE 2 DTA APPROVAL. REPAIRED PER ER/A 00-627199. (1478991)Mar 4, 2026 · N986AT · Boeing 717200 · Standard Practices/StructuresSDR CALA2026031014460Wire · exposed31D EMERGENCY PATH LIGHT WIRE EXPOSED. WIRES THAT WERE EXPOSED ARE FOR OUTLET IN USE LIGHTS. TRIM PIECE AT SEAT 31D INSERTS RIPED OUT SECURED TRIM PIECE IN PLACE NO HAZARD TO PAX. TOMC APPROVED NEF 2500BX FOR SEAT 31D TRIM SECURED IN PLACE NEF APPLIED CONFIRMEMar 4, 2026 · N17336 · Boeing 7378 · Light System WiringSDR DALA2026031001628Fitting · out of limitsDTE ERA 631653-14AD REV ORIGINAL. REPAIR AT THE MIRROR FITTING & LHS HOLE D1 IS TIME LIMITED, REQUIRING DTE FOLLOW UP PRIOR TO 91,114 TFC. C/A: REVISE AND UPDATE ERA 631653-14AD WITH DTE RESULTS PRIOR TO 91,114 TFC. ASSOCIATED AA 5311-01226 ADDED FOR AC 3277 AMar 4, 2026 · N377NW · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA2026031001627Window Frame · noneINSPECTION ERA 631653-14AD REV ORIGINAL. WINDSHIELD FRAMING ( AREA 2) REQUIRES FOLLOW UP INSPECTIONS PRIOR TO 58,114 TFC AND EVERY 4,700 FC THEREAFTER. C/A: ACCOMPLISH FOLLOW UP INSPECTIONS PER ERA 631653-14AD, SECTION II , PRIOR TO 58,114 TFC AND EVERY 4,700 Mar 4, 2026 · N377NW · Airbus A320211 · Standard Practices/StructuresSDR DALA2026031001626Fitting · not reportedCONTINUITY FITTINGS REPLACEMENT IS TIME LIMITED, REQUIRING DTE FOLLOW UP PRIOR TO 60,614 TFC. REVISE AND UPDATE ERA 631768-14AD WITH DTE RESULTS PRIOR TO 60,614 TFC ASSOCIATED AA 5311-01226 ADDED FOR AC 3277 ASSOCIATED ER/A 14-631768 ADDED FOR AC 3277. (LP: 1Mar 4, 2026 · N377NW · Airbus A320211 · Fuselage Main, StructureSDR SWIA2026030475429Skin · damagedSKIN DAMAGE IS OUT OF LIMITS AND IS LOCATED ON FRAME 08 TO FRAME 09 AND ALONG STRG 19L. (FLIGHT 3064) REASSESSED DAMAGE ON FWD LEFT SIDE OF AIRCRAFT JUST UNDER CAPTS WINDOW, CONFIRMED DAMAGE LOCATION TO BE LOCATED ON FRM 08 TO FRM 09 AND JUST BELOW STRG 15LMar 4, 2026 · N406SY · Emb ERJ170200LR · Fuselage Main, Plate/SkinSDR SWAA2026030976578Scuff Plate · crackedCRACK MEASURING 0.5 IN. ON DENT MEASURING L=0.625; W=0.5; D=0.054, ON THE FWD CARGO SCUFF PLATE. R & R THE SCUFF PLATE IAW AMM 53-11-01, & 53-11-02,Mar 4, 2026 · N286WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2026030976352Battery Pack · no testTHE AFT LEFT EMERGENCY LIGHT BATTERY PACK FAILED A CAPACITY CHECK. REMOVED & REPLACED THE BATTERY PACK IAW MM 33-51-06.Mar 4, 2026 · N8309C · Boeing 7378H4 · Emergency LightingSDR SWAA2026030976573Lamp · inoperativeRIGHT FWD OVERWING EXIT SIGN HAD 3 BULBS INOPERATIVE. R & R THE LAMPS IAW AMM 33-51-01-960-801-NG.Mar 4, 2026 · N8321D · Boeing 7378H4 · Emergency LightingSDR SWAA2026030976833Sign · crackedFWD ENTRY DOOR EMERGENCY EXIT SIGN CRACKED. R & R FWD ENTRY DOOR EMERGENCY EXIT SIGN IAW AMM 33-51-01.Mar 4, 2026 · N8610A · Boeing 7378H4 · Emergency LightingSDR SWAA2026030976364Support Bracket · crackedRIGHT ECS BAY, FWD KEEL BEAM CROSS BLEED SUPPORT BRACKET CRACKED. R & R THE SUPPORT BRACKET IAW SRM 51-40-02.Mar 4, 2026 · N8632A · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2026030976362Slider · crackedLEFT HORIZONTAL STAB, FWD UPPER SLIDER CRACKED. REMOVED AND REPLACED IAW AMM 53-31-31-401, CONFIG 2.Mar 4, 2026 · N8309C · Boeing 7378H4 · Horizontal Stabilizer Miscellaneous StructureSDR DXTA2026030907127Battery · faultedAPPROACH INTO KBZN AT ABOUT 14,000' THE EMER LIGHTS BEGAN TO FLICKER. EMER LIGHTS ARE OFF WITH THE SWITCH IN THE OFF POSITION. WITH THE SWITCH IN THE ARM POSITION AND POWER OFF, THE LIGHTS ILLUMINATED AND WERE STEADY. WITH THE SWITCH IN THE ON POSITION AND Mar 4, 2026 · N333QS · Emb EMB505 · Emergency LightingSDR IPXA2026030919342Floorboard · wornMAJOR REPAIR, FLOORBOARD INSIDE L1 DOOR THRESHOLD IS WORN AND IS SHOWING CORE MATERIAL. INSTALLED NEW FLOORBOARD INSIDE L1 DOOR THRESHOLD IAW AMM 53-21-02.Mar 4, 2026 · N575UP · Boeing 74744AF · Fuselage Floor PanelSDR IPXA2026030908993Door Frame · damagedFOUND DAMAGE ON UNDERLYING STRUCTURE BEHIND SEAL DEPRESSOR SPLICE AT FS 615 APPROX WL 170. ALL STEPS ARE COMPLETE EO-96726-REQ1.Mar 4, 2026 · N575UP · Boeing 74744AF · Fuselage Main, StructureSDR IPXA2026030906568Support Bracket · crackedCRACKED TORQUE TUBE SUPPORT BRACKET OF THE LT WING LEADING EDGE COMPARTMENT. INSTALLED A NEW BRACKET IAW SRM 51-40-02-0G, REV 94, & DWG 114T1240, SHT 6, REV -.Mar 4, 2026 · N348UP · Boeing 76734AF · Wing, Attach FittingsSDR DALA2026030901617Snubber · out of toleranceSHIP 5656 ROTATORY SNUBBER OUT LIMITS ON TORQUE TUBE OF PASSENGER DOOR L2. CORRECTIVE ACTION: SUMMARY OF NRC 00063: ROTATORY SNUBBER ON TORQUE TUBE OF PASSENGER DOOR L2 WAS REPLACED PER B757-200 AMM 52-11-10. (1478891)Mar 4, 2026 · N556NW · Boeing 757251 · Passenger/Crew DoorsSDR DALA2026030901613Support · corrodedSHIP 5804 CORROSION ON LOWER SILL SETTLEMENT AREA OF THRESHOLD (UPPER/LOWER FACE) BTW STA 1360 TO STA 1460 AT AFT CARGO COMPARTMENT. CORRECTIVE ACTION: SUMMARY OF NRC 00217: CORROSION LEVEL 2. LOWER SILL SETTLEMENT AREA OF THRESHOLD (UPPER/LOWER FACE) BTW STA Mar 4, 2026 · N584NW · Boeing 757351 · Fuselage Miscellaneous StructureSDR DALA2026030901612Strap · crackedSHIP 5804 CRACK ON STABILIZATION STRAP BTW STA 1640 AND LBL 24 AT AFT CARGO COMPARTMENT. CORRECTIVE ACTION: SUMMARY OF NRC 00336: STABILIZATION STRAP BTW STA 1640 AND LBL 24 AT AFT CARGO COMPARTMENT WAS REPAIRED PER B 757-300 SRM 53-00- 51-2R PROCEDURE REPAIR Mar 4, 2026 · N584NW · Boeing 757351 · Fuselage Miscellaneous StructureSDR DALA2026030901605Guide Arm · faulted(LOG 8253804) UNABLE TO OPEN L1 DOOR. REMOVED DAMAGED ENTRY DOOR GUIDE ARM AND ROLLER. INSTALLED NEW FWD ENTRY DOOR GUIDE ARM AND ROLLER IAW B737 AMM 52-11. FIT AND OPS CHECK GOOD.Mar 4, 2026 · N3746H · Boeing 737832 · Passenger/Crew DoorsSDR DALA2026030901603Floorbeam · corroded(LOG 1479152) CORROSION ON UPPER FLANGE BEAM STA 947 LBL 21 TO LBL 29 AT AFT PASSENGER CABIN (W2). UPPER FLANGE BEAM STA 947 LBL 8 TO LBL 60 AT AFT PASSENGER CABIN (W2) WAS REPAIRED PER B737-900 SRM 53-70-51-2R PROCEDURE 5 REPAIR 5 AND ER/A 632805-14 PRI REV. Mar 4, 2026 · N883DN · Boeing 737932ER · Fuselage Main, Floor BeamSDR DALA2026030901602Battery Pack · inoperative(LOG 8254571) DURING EMERGENCY LIGHT CHECK OF CABIN FOUND FLOOR PORXIMITY LIGHTS OUT AT ROW 28-32. REPLACED BATTERY PACK REF B737AMM 33-51-06. OPS CHECK GOOD.Mar 4, 2026 · N926DZ · Boeing 737932ER · Emergency LightingSDR ANCF20260309007None · noneOUTER WING REAR SPAR FWD FACE DETAILED INSPECTION OF OUTER WING, REAR SPAR FORWARD FACE, BETWEEN RIB 11 AND RIB 27, INCLUDING JOINT AT RIB 22 AND TOP AND BOTTOM FLANGES, REINFORCING ANGLE AT RIB 20 AND JOINT ANGLES BETWEEN RIB 24 AND RIB 25Mar 4, 2026 · N957AV · Airbus A320214 · Standard Practices/StructuresSDR U2RA202603090001Hydraulic Line · crackedAPPROXIMATELY 30 MINUTES AFTER TOP OF CLIMB, CRUSING AT FLIGHT LEVEL 34,000, EICAS MESSAGE "HYD QTY LOW 1" QUANTITY OBSERVED DECREASING REPIDLY ON HYD SYNOPTIC PAGE. SHORTLY AFTER, QUANTITY AT 0.00. EICAS "HYD PRESS SYS 1". NON NORMAL CHECKLIST ACTIONED. - RMar 4, 2026 · N756CA · Boeing 747446 · Hydraulic System, MainSDR CALA2026030914410Door Frame · crackedCRACKED: MAIN CABIN R1 DOOR CUTOUT CRACKED AT FWD LOWER DOOR FRAME. REMOVED AND REPLACED NEW FRAME ASSY AT MAIN CABIN R1 DOOR CUTOUT FWD AND LOWER SRM 51-40-02-0G-0 AND DWG 141A8370.Mar 4, 2026 · N14250 · Boeing 737824 · Fuselage Main, StructureSDR CALA2026030914408Fmu · unserviceableEGT REACHED 597C DURING ENGINE START NR 2 PILOT DEBRIEFED UPON RTB EVENT, THEY CONFIRMED THAT START PROCEDURE WAS NORMAL UP UNTIL THE LATER STAGE WHEN THEY NOTICED THE EGT WAS GETTING OUT OF PARAMETERS, LIGHT UP WAS WITHIN SECONDS AS PER NORMAL, THEY CONFIRM TMar 4, 2026 · N684UA · Boeing 7673CB · Fuel Controlling SystemSDR DALA2026030801597Indication Sys · malfunctionedRT OVERWING SLIDE NOT SHOWING ARMED ON ECAM. TRANSFER TO A320 MEL 25-60-04F DURING M PROCEDURE HAD TO C/W STEP 11. M PROCEDURE C/W. DISPATCH APPROVED. PLACARDS INSTALLED. CYCLED LATCH PIN ON FWD RT OVERWING EXIT DOOR. PERFORMED A320 TSM 52-21-00-810-809. ALL Mar 4, 2026 · N355NW · Airbus A320212 · Door Warning SystemSDR DALA2026030801596Fitting · noneCONFIRM DT EVALUATION FOR POSSIBLE FCS REPAIR INTERNAL STRUCTURE REINFORCE FITTING LOCATED BTW FR 42 TO FR 43 AND -Y1292 TO -Y 1650.0 TORSION BOX LOWER SHELL IN MAIN WHEEL WELL (REFERENCE AA CARD 5100-01821- 01A). CONFIRMED DT EVALUATION FOR POSSIBLE FCS REPAIMar 4, 2026 · N377NW · Airbus A320211 · Standard Practices/StructuresSDR DALA2026030801595Stringer · noneCONFIRM DT EVALUATION FOR POSSIBLE FCS REPAIR STRINGER 42L LOCATED BTW FR 55 TO FR 58 IN AFT CARGO COMPARTMENT (REFERENCE AA CARD 5100-0182 1-01A). CONFIRMED DT EVALUATION FOR POSSIBLE FCS REPAIR STRINGER 42L LOCATED BTW FR 55 TO FR 58 IN AFT CARGO COMPARTMENMar 4, 2026 · N377NW · Airbus A320211 · Standard Practices/Structures