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 IPXA2026041087635Guide · wornFOUND MAIN DECK CARGO HANDLING LATERAL GUIDE ASSY DAMPER WORN AT: STA 500 RBL 66.50 AND STA 620 LBL 66.50 TOTAL:2EA I.A.W AMM 25-57-08-004-015 AND AMM 25-57-08-404-020 REV.147 REPLACED LATERAL GUIDE ASSY. C/W REVIEWApr 8, 2026 · N352UP · Boeing 76734AF · Cargo CompartmentsSDR IPXA2026041087549Roller · deformedFAULT-FOUND MAIN DECK CARGO HANDLING SHAFT OF ROLLER RAIL ASSY DEFORM TOTAL:1EA AT STA 977 LBL 77.50 (REPLACE). I.A.W AMM 25-57-05-004-001 AND AMM 25-57-05-404-006 REV.147 REPLACED ROLLER RAIL ASSY. C/W REVIEWApr 8, 2026 · N352UP · Boeing 76734AF · Fuselage Main, StructureSDR AALA202604244240Hinge Fitting · excess playAIRCRAFT IN BASE MAINTENANCE: RIGHT HAND HORIZONTAL STABILIZER ELEVATOR #6 HINGE ARM END FITTING HAS EXCESSIVE PLAY. REPLACED HINGE ARM END FITTING PER AMM 55-16-42.Apr 8, 2026 · N572UW · Airbus A321231 · Elevator StructureSDR AALA202604249253Hinge Fitting · excess playAIRCRAFT IN BASE MAINTENANCE: RIGHT HAND HORIZONTAL STABILIZER ELEVATOR #4 HINGE ARM END FITTING HAS EXCESSIVE PLAY. REPLACED HINGE ARM END FITTING PER AMM 55-16-42.Apr 8, 2026 · N572UW · Airbus A321231 · Elevator StructureSDR AALA202604242018Hinge Fitting · excess playAIRCRAFT IN BASE MAINTENANCE: RIGHT HAND HORIZONTAL STABILIZER ELEVATOR #1 HINGE ARM END FITTING HAS EXCESSIVE PLAY. REPLACED HINGE ARM END FITTING PER AMM 55-16-42.Apr 8, 2026 · N572UW · Airbus A321231 · Elevator StructureSDR ASAA2026040865644Floor Support · corrodedCORROSION ON THE STRINGER ON THE RIGHT HAND SIDE OF THE AFT CARGO PIT BETWEEN STATIONS 767 AND 787 12 INCHES FROM THE BUTT LINE. GROUNDED - YES. REMOVED CORROSION FROM THE AFT PIT FLOOR RAIL AT STA 772, RBL 13.84 IAW B737-800 SRM 53-00-53-1A-2.2.D ORIG THICKNEApr 8, 2026 · N528AS · Boeing 737890 · Fuselage Miscellaneous StructureSDR ASAA2026040865640Channel · corrodedMULTIPLE SPOTS OF CORROSION ON THE LEFT HAND TRANSITION STRAP IN THE AFT CARGO PIT BETWEEN STATIONS 787 AND THE FORWARD BULKHEAD. GROUNDED - YES. REMOVED CORROSION FROM THE L/H AFT PIT TRANSITION PANEL AT STA 787 TO FWD BULKHEAD IAW B737-800 SRM 53-00-53-1A-2.Apr 8, 2026 · N528AS · Boeing 737890 · Fuselage Miscellaneous StructureSDR IPXA2026042200417Frame Angle · crackedBULK CGO COMP STA 1640 LBL 16" FLOOR AREA ANGLE FRAME HAS CRACKED. REMOVED FLOOR ANGLE FRAME AT AFT CARGO COMP AT STA 1640 LBL 16" IAW B757 SRM 51-40-02-0G-0. INSTALLED NEW ANGLE AT CARGO COMP. STA. 1640 LOWER IAW SRM 51-40-02-0G-0 AND RESTORE ACCESS AS REApr 8, 2026 · N454UP · Boeing 75724APF · Fuselage Main, FrameSDR IPXA2026042104911Tee Angle · corrodedR/H WHEEL WELL FAIRING SUPPORT STRUCTURE TCHORD HAS CORROSION, BTWN STA 1040 AND STA 1060 AT RBL 62. LOCATED AND DRILLED NEW T-CHORD I.A.W. B757-200PF SRM 51-40-05.Apr 8, 2026 · N421UP · Boeing 75724APF · Aerodynamic FairingsSDR IPXA2026042205165Ball Mat · corrodedMAIN DECK BALL MAT 231BM3 UNDER SIDE SKIN HAS CORROSION AT ALL BALL CUTOUTS. OUT OF SEQUENCE STEP 6 INSPECTED FABRICATIN OF NEW SKIN FOR BALLMAT 231BM3 IAW B757 GMM09-08-01-04 SREO 11648-RQ002.Apr 8, 2026 · N421UP · Boeing 75724APF · Fuselage Miscellaneous StructureSDR AALA202604233203Hinge Fitting · excess playAIRCRAFT IN BASE MAINTENANCE: LEFT HAND HORIZONTAL STABILIZER ELEVATOR #5 HINGE ARM END FITTING HAS EXCESSIVE PLAY. REPLACED HINGE ARM END FITTING PER AMM 55-16-42.Apr 8, 2026 · N572UW · Airbus A321231 · Elevator StructureSDR AALA202604234017Hinge Fitting · excess playAIRCRAFT IN BASE MAINTENANCE: LEFT HAND HORIZONTAL STABILIZER ELEVATOR #3 HINGE ARM END FITTING HAS EXCESSIVE PLAY. REPLACED HINGE ARM END FITTING PER AMM 55-16-42.Apr 8, 2026 · N572UW · Airbus A321231 · Elevator StructureSDR AALA202604234680Hinge Fitting · excess playAIRCRAFT IN BASE MAINTENANCE: LEFT HAND HORIZONTAL STABILIZER ELEVATOR #2 HINGE ARM END FITTING HAS EXCESSIVE PLAY. REPLACED HINGE ARM END FITTING PER AMM 55-16-42.Apr 8, 2026 · N572UW · Airbus A321231 · Elevator StructureSDR AALA202604235994Hinge Fitting · excess playAIRCRAFT IN BASE MAINTENANCE: LEFT HAND HORIZONTAL STABILIZER ELEVATOR #6 HINGE ARM END FITTING HAS EXCESSIVE PLAY. REPLACED HINGE ARM END FITTING PER AMM 55-16-42.Apr 8, 2026 · N572UW · Airbus A321231 · Elevator StructureSDR AALA202604238084Hinge Fitting · excess playAIRCRAFT IN BASE MAINTENANCE: LEFT HORIZONTAL STABILIZER ELEVATOR #1 HINGE ARM END FITTING HAS EXCESSIVE PLAY. REPLACED HINGE ARM END FITTING PER AMM 55-16-42.Apr 8, 2026 · N572UW · Airbus A321231 · Elevator StructureSDR IPXA2026042205156Ball Mat · corrodedMAIN DECK BALL MAT 232BM2 UNDER SIDE SKIN HAS CORROSION AT ALL BALL CUTOUTS DOT 07586-05. REMOVED BALL MAT LOWER SKIN I.A.W SREO-11648-REQ002 AND B757-200 SRM 51-40-02-OG. TREATED AND PRIMED EXTERNAL SURFACE OF LOWER SKIN AND INSTALLED NEW LOWER SKIN ON BALL Apr 8, 2026 · N421UP · Boeing 75724APF · Fuselage Miscellaneous StructureSDR IPXA2026042105195Adapter · corrodedCLS ADAPTER AT Y0 FRAME 57.2 RT WITH CORROSION. REMOVED AND REPLACED CLS ADATPER AT ZONE 200. MAIN CABIN COMPARTMENT FLOOR STRUCTURE FR 57.2, Y0 RT IAW SRM 51-40-21-001.Apr 8, 2026 · N141UP · Airbus A300F4622R · Fuselage, Seat/Cargo Attach FittingsSDR IPXA2026041492530Bushing · wornWORN BUSHING, NR 2 ENGINE RT CORE COWL PRESSURE RELIEF DOOR INNER AREA. INSTALLED A NEW BUSHING IAW SRM 51-40-02-0G, REV 94, AND CMM IPL 71-13-24, REV 50.Apr 8, 2026 · N352UP · Boeing 76734AF · Nacelle/Pylon, Main FrameSDR IPXA2026041192806Seal · brokenBROKEN SEAL, NR 1 PYLON RT SIDE PANEL 436CR. INSTALLED A NEW SEAL STRIP IAW SRM 51-40-02-0G, REV 94, AND DWG 311T2570, SH 16, REV -.Apr 8, 2026 · N352UP · Boeing 76734AF · Nacelle/Pylon, Main FrameSDR IPXA2026041203053Floor Support · corrodedAFT CARGO COMPARTMENT FLOOR SUPPORT UPPER FLANGE HAS EVIDENCE OF CORROSION APPROX BTW BS 1460 AND BS 1480, LBL 10.45 AND RBL 10.45, ID STICKER NUM, (085-040) ATA 53-10 VERIFIED TOOLING. VERIFIED STEP 7.Apr 8, 2026 · N454UP · Boeing 75724APF · Fuselage Miscellaneous StructureSDR IPXA2026041202987Floor Support · corrodedAFT CARGO COMPARTMENT FLOOR SUPPORT UPPER FLANGE HAS EVIDENCE OF CORROSION APPROX BTW BS 1460 AND BS 1480, LBL 7.55 AND RBL 7.55, ID STICKER NUM, (085-039) ATA 53-10 VERIFIED TOOLING. VERIFIED STEP 4 AND 5.Apr 8, 2026 · N454UP · Boeing 75724APF · Fuselage Miscellaneous StructureSDR IPXA2026041705118Structure · corrodedMAIN DECK BALL MAT 232BM1 UNDER SIDE SKIN HAS CORROSION AT ALL BALL CUTOUTS . . INSTALLED SKIN ON BALL MAT 232BM1 IAW SRM 51-40-02 AND SERO-11648 -REQ002. REVIEWED.Apr 8, 2026 · N421UP · Boeing 75724APF · Fuselage Miscellaneous StructureSDR IPXA2026041803176Floor Support · corrodedAFT CARGO COMPARTMENT FLOOR STRINGER UPPER FLANGE HAS CORROSION APPROX BTW BS 1460 AND BS 1480, RBL 16.10, ID STICKER NUM, (085-041) ATA 53-10 VERIFIED STEP 6. OK TO INSTALL.Apr 8, 2026 · N454UP · Boeing 75724APF · Fuselage Miscellaneous StructureSDR HNAA2026042100321Attach Fitting · gougedF111356 LH AILERON DAMPER ATTACHMENT FITTING IS GOUGED 2 EACH. RAR LH AILERON DAMPER ATTACHMENT FITTING IAW EMB 145 SRM 51-40-02Apr 8, 2026 · N905JH · Emb EMB145LR · Wing, Attach FittingsSDR MASA20260420088Shear Plate · corrodedDURING HEAVY CHECK INSPECTIONS ON CFIII FUSELAGE FLOOR STRUCTURE, CORROSION FOUND ON LH SHEAR PLATE BETWEEN FR 87-88, LH SHEAR PLATE BETWEEN FR 137-88, REMOVED AND REPLACED IAW ERJ-175 SRM 51-42-01 REV 45Apr 8, 2026 · N87353 · Emb ERJ170200LR · Fuselage Miscellaneous StructureSDR IPXA2026041493823Rub Strip · chafedCHAFED WEAR STRIP, NR 2 ENG R/H CORE COWL INNER AFT UPPER EDGE. INSTALLED NEW WEAR STRIP I.A.W SRM 51-40-02-0G REV.94 AND CMM IPL 71-13-24 REV. 50Apr 8, 2026 · N352UP · Boeing 76734AF · Nacelle/Pylon, Main FrameSDR CALA2026041715429Oven · dirtyOVEN 205 FA SHUT OFF DUE BURNING SMELL PERFORMED AMM 05-51-58 REV 139. FOUND FOOD SPILLAGE IN OVEN 205 FWD GALLEY. COMPLIED WITH, CB PULLED AND COLLARED. OVEN 205 DEFERRED IAW NEF 2520P. CLEANED LARGE BURNT FOOD FROM BOTTOM OF OVEN. STILL SMELLS DURING OPS Apr 8, 2026 · N14120 · Boeing 757224 · Buffet/GalleysSDR IPXA2026040994656Skin · debondedDEBONDED SKIN, INBD AFT EDGE OF LT WING T/E OUTBD FLAP T/E SKIN, WBL 289.45. PERFORMED NDT/UT FOR THE REWORKED AREA & PLUS 2 INCHES HEATED AREA , IAW NDT MANUAL PART, 1 51-01-01 REV:143Apr 8, 2026 · N352UP · Boeing 76734AF · Trailing Edge FlapsSDR IPXA2026041094116Former · crackedCRACKED FORMER, FWD SIDE OF LT WING OTBD L/E NOSE BEAM, OSS 499.6. INSTALL NEW FORMER IAW SRM 51-40-02-0G REV.95 AND DWG 114T2511 SH 1 REV: DApr 8, 2026 · N352UP · Boeing 76734AF · Wing Main, Frame StructureSDR IPXA2026041094070Former · crackedCRACKED FORMER, FWD SIDE OF LT WING OTBD L/E NOSE BEAM, OSS 441.6. INSTALLED NEW FORMER I.A.W SRM 51-40-02-0G REV.94 AND BOEING DWG NO. 114T2241 SH 4 REV - AND UPS SREO-54290-REQ1 REV2Apr 8, 2026 · N352UP · Boeing 76734AF · Wing Main, Frame StructureSDR IPXA2026041094681Former · crackedCRACKED FORMER, RT WING OTBD LE WS 510. INSTALL NEW FORMER I.A.W SRM 51-40-02-0G REV.94 AND BOEING DWG NO. 114T2161 SH 6 REV - AND UPS SREO-50900-REQ001 REV2.Apr 8, 2026 · N352UP · Boeing 76734AF · Wing Main, Frame StructureSDR IPXA2026041192577Bracket · gougedGOUGED BRACKET, NR 1 ENG RT CORE COWL HOLD-OPEN ROD RECEIVER. INSTALLED A NEW BRACKET IAW SRM 51-40-02-0G, REV 94, AND CMM IPL 71-13-24, REV 50.Apr 8, 2026 · N352UP · Boeing 76734AF · Nacelle/Pylon, Main FrameSDR IPXA2026041590371Beam · crackedDURING PERFORMANCE OF EO-63801-JIC001, FOUND LEFT WING TRAILING EDGE SUPPORT BEAM CRACKED AT WS 1079.95. INSTALLED A NEW BEAM IAW SRM 51-40-02-0G, REV.94 AND DWG 113T1913, SHT 1, REV A, DWG 113T1657, SHT 1, REV C, AND DWG 113T1676, SHT 2, REV -.Apr 8, 2026 · N352UP · Boeing 76734AF · Wing Main, Frame StructureSDR IPXA2026041492581Adapter · chafedCHAFED ADAPTER AND BRACKET, NR 2 ENG LT CORE COWL HOLD OPEN ROD SUPPORT BRACKET AREA. INSTALLED A NEW BRACKET AND ADAPTER IAW SRM 51-40-02-0G, REV 94, AND CMM IPL 71-13-23, REV 47.Apr 8, 2026 · N352UP · Boeing 76734AF · Nacelle/Pylon, Main FrameSDR IPXA2026041492647Bracket · chafedCHAFED ADAPTER & BRACKET, NR 2 ENG, RT CORE COWL HOLD OPEN ROD SUPPORT BRACKET AREA. INSTALLED A NEW BRACKET & ADAPTER IAW SRM 51-40-02-0G, REV 94, AND CMM IPL 71-13-24, REV 50.Apr 8, 2026 · N352UP · Boeing 76734AF · Nacelle/Pylon, Main FrameSDR IPXA2026041590118Bracket · crackedNR 2 ENGINE LT CPRSR REAR FRAME SENSOR SUPPORT BRACKET CRACKED, NEAR 10 O'CLOCK. REPLACED THE BRACKET IAW AMM 70-50-00-912-001-H00, REV 147.Apr 8, 2026 · N352UP · Boeing 76734AF · Engine (Turbine/Turboprop)SDR IPXA2026041590099Clamp · brokenBROKEN CLAMP, NR 1 ENGINE LOWER -D- SUMP OIL SUPPLY TUBE, FWD SUPPORT. REPLACED THE CLAMP IAW AMM 20-11-00-910-802, REV 147,Apr 8, 2026 · N352UP · Boeing 76734AF · Turbine Engine Oil SystemSDR IPXA2026041192828Bracket · brokenNR 1 ENG, LT THRUST REVERSER COWL INNER DRAIN TUBE SUPPORT CLAMP ATTACH PLATE BROKEN AT 11:00 O'CLOCK. INSTALLED A NEW BRACKET IAW SRM 51-40-02-0G, REV 94, AND IPC 78-32-51, REV 96.Apr 8, 2026 · N352UP · Boeing 76734AF · Engine Thrust ReverserSDR IPXA2026041492935Support Angle · crackedNR 2 PYLON AFT FAIRING R/H AFT STIFFENER SUPPORT ANGLE CRACKED. INSTALLED A NEW SUPPORT ANGLE IAW SRM 51-40-02-0G, REV 94, AND DWG 313T2303, SHT 131, REV- , AND SHT 136 REV -.Apr 8, 2026 · N352UP · Boeing 76734AF · Nacelle/Pylon Miscellaneous StructureSDR IPXA2026041193805Bracket · gougedGOUGED BRACKET, NR 1 ENG RT CORE COWL PRESSURE RELIEF DOOR LOWER LATCH STOP PAD. INSTALLED A NEW BRACKET IAW SRM 51-40-02-0G, REV 94, AND CMM IPL 71-13-24, REV 50.Apr 8, 2026 · N352UP · Boeing 76734AF · Nacelle/Pylon Miscellaneous StructureSDR IPXA2026041394644Support · crackedRT WING NR 6 FLAP TRACK SUPPORT FAIRING INBD AFT SIDE CRACKED. PERFORMED NDT/UT FOR THE REWORKED AREA AND PLUS 6 INCHES, AROUND HEATED AREA IAW NDT MANUAL PART 1 51-01-01, REV 143, NO DEFECT FOUND IAW AMM 20-11-00-910-802, REV.147. INSTALLED THE SEAL & RETAApr 8, 2026 · N352UP · Boeing 76734AF · Trailing Edge FlapsSDR IPXA2026041393757Plate · chafedCHAFED PLATE STRIKE , RT BODY L/G W/W INBD DOOR LOWER SIDE. REMOVE DAMAGE PLATE I.A.W SRM 51-40-02-0G REV.48.INSTALL NEW PLATE I.A.W SRM 51-40-02-0G REV.48 AND BOEING DWG NO.149U1608 SH2 REV.-Apr 8, 2026 · N610UP · Boeing 7478F · Fuselage Miscellaneous StructureSDR IPXA2026041393769Plate · chafedCHAFED PLATE STRIKE, LT BODY L/G W/W INBD DOOR LOWER SIDE EDGE. REMOVE DAMAGE PLATE I.A.W SRM 51-40-02-0G REV.48. INSTALL NEW PLATE I.A.W SRM 51-40-02-0G REV.48 AND BOEING DWG NO.149U1608 SH2 REV.-Apr 8, 2026 · N610UP · Boeing 7478F · Fuselage Miscellaneous StructureSDR DALA2026041502392Frame · corrodedER/A 633493-14; A220-100 / FWD AND CNTR WING TO BODY FAIRING / FRAME / FR40, LBL 15 - RBL 15 / FR36, LBL 20 - RBL 20 / CORROSION. SUBJECT REPAIR REQUIRES FOLLOW-ON ACTION. ACCOMPLISH 633493-14, SECTION II REPETITIVE INSPECTION WITHIN EVERY 1,000 FLIGHT HOURS FApr 8, 2026 · N135DQ · Airbus BD5001A10 · Aerodynamic FairingsSDR IPXA2026041106001Profile · crackedTEE PROFILE AT FRAME 80 LT CORNER WITH CRACK. REMOVED AND REPLACED THE TEE PROFILE.Apr 8, 2026 · N141UP · Airbus A300F4622R · Fuselage Miscellaneous StructureSDR AALA202604146568Scuff Plate · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON THE BOTTOM OF R2 DOOR SCUFF PLATE PROTECTOR. MAINTENANCE REMOVED AND REPLACED R2 DOOR SCUFF PLATE SUPPORT PN D5348004820303 IAW AIRBUS SRM 53-41-69-028.Apr 8, 2026 · N9025B · Airbus A319115 · Fuselage Miscellaneous StructureSDR AALA202604141454Scuff Plate · corrodedAIRCRAFT IN BASE MAINTENANCE: AFTER REMOVAL OF SCUFF PLATE FOUND CORROSION ON CORNER SHAPE SILL AT FR68 STGR 23RH. MAINTENANCE REPLACED CORNER SHAPE SILL AT FR68 STGR 23RH PER SRM 53-41-69-283-008, SRM 51-44-11-08, AND SRM 51-42-11-001.Apr 8, 2026 · N9025B · Airbus A319115 · Fuselage Miscellaneous StructureSDR DALA2026041402369Skin · crackedFUSELAGE SKIN, BS 1087, L13R - 14R CRACKED. ASSOCIATED ER/A 00-633468 (1536411) (AIRCRAFT GROUNDED)Apr 8, 2026 · N939AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR HNAA2026041300284Angle · crackedRIGHT WING TOP SURFACE, ANGLE NR 1 FROM FWD AND AT RIB 1A FOUND CRACKED AT FWD AND AFT SIDE. CUT OUT DAMAGED, FABRICATED IAW SRM 57-20-01, REPAIRED IAW SRM 57-20-01 ITEM 3.Apr 8, 2026 · N909AE · Emb EMB145LR · Wing Miscellaneous StructureSDR DALA2026041302319Acm · contaminatedFUME/SMKE - ON TAXI IN WITH RT PACK ON, WET SOCK SMELL WITH VISIBLE FOG/SMOKE. CORRECTIVE ACTION: FOUND APU WITH NO OIL IN OIL TANK AND EXTENSIVE OIL CONTAMINATION IN BLEED DUCT. APU CHANGE COMPLETED AND BLEED DUCTS CLEANED. STILL HAVE ODOR AND HAZE ON APU BLEApr 8, 2026 · N943AT · Boeing 717200 · Cabin Cooling System