N11FQ

Service difficulty reports · 22

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

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'
  WHERE n_number = 'N11FQ' AND registry_match = 'registration'
  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 2A6D20240614001Attach Angle · crackedDAMAGE TO THE BAGGAGE COMPARTMENT LH FWD LOWER ANGLE (P/N: 350A210053.28) IN THE FORM OF GOUGE/CRACK. THE GOUGE/CRACK DAMAGE MEASURED TO BE APPROXIMATELY 0.13” IN DIAMETER.Jun 14, 2024 · N11FQ · Urocop EC130T2 · Fuselage Main, Attach FittingsSDR 2A6D20240528001Frame · corrodedDAMAGE TO THE AFT UPPER FRAME (P/N: 350A21-1242.35) IN THE FORM OF CORROSION. THE CORROSION DAMAGE IS ON THE UPPER FLANGE OF FRAME AT LH AND RH BOTTOM SIDE NEAR THE AFT LOWER FRAME. THE LH SIDE CORROSION DAMAGE MEASURED TO BE APPROXIMATELY 0.71: X 2.05” AND THMay 28, 2024 · N11FQ · Urocop EC130T2 · Fuselage Main, FrameSDR 2A6D20240509003Floorbeam · corrodedDAMAGE IS ON THE LH CABIN FLOOR EDGE FITTING (P/N: 350A214753.20) IN THE FORM OF CORROSION AND CRACKS. THE LH FITTING PLATE IS EXCESSIVELY CORRODED AND THE CRACK DAMAGES AT TWO FASTENER HOLES TO EOP WHICH RESULTS IN REPLACEMENT OF LH FITTING.May 9, 2024 · N11FQ · Urocop EC130T2 · Fuselage Main, Floor BeamSDR 2A6D20240509002Bonding Plate · corrodedDAMAGE IS ON THE TAIL BOOM VHF ANTENNA BASE PLATE (P/N: 350A65-1707.00) IN THE FORM OF CORROSION. THE BASE PLATE IS EXCESSIVELY CORRODED AND DEPTH OF THE DAMAGE IS ALL THE WAY THROUGH THICKNESS WHICH RESULTS IN REPLACEMENT OF ANTENNA BASE PLATE.May 9, 2024 · N11FQ · Urocop EC130T2 · Fuselage Main, StructureSDR 2A6D20240509001Bulkhead · corrodedTHE UPPER 7° BULKHEAD DOUBLER (PN: 350A21-0849.20) IS CORRODED AT THE LOCATION OF A PASS-THRU HOLE. THE DAMAGE AREA WAS REPORTED TO BE 0.80” X 0.50” AND 0.030” DEEP AT THE DEEPEST POINTMay 9, 2024 · N11FQ · Urocop EC130T2 · Fuselage Main, BulkheadSDR 2A6D20240508003Crosstube · corrodedTHE AFT LANDING GEAR CROSSTUBE FITTING (PN: 350A21-0960.20) IS CORRODED IN MULTIPLE AREAS ON THE LOWER SURFACE. THE DEEPEST DAMAGE AREA WAS REPORTED TO BE 0.022” DEEP AND THE LARGEST AREA IS APPROXIMATELY 0.40” WIDE WITH VARIOUS LENGTHSMay 8, 2024 · N11FQ · Urocop EC130T2 · Fuselage Main, StructureSDR 2A6D20240508002Crossbeam · corrodedTHE RH X2244 CROSSBEAM (PN: 350A21-0861.20) IS CORRODED IN AN AREA ON THE LOWER OUTBOARD CORNER OF THE CROSSBEAM. THE DAMAGE WAS REPORTED TO BE 0.572” X 0.179” AND 0.028” DEEPMay 8, 2024 · N11FQ · Urocop EC130T2 · Fuselage Structure (General)SDR 2A6D20240508001Crossbeam · corrodedTHE RH X1790 CROSSBEAM (PN: 350A21-0572.20) IS CORRODED IN AN AREA WHERE IT CONTACTS THE RH Y400 BEAM (PN: 350A21-0587.20)May 8, 2024 · N11FQ · Urocop EC130T2 · Fuselage Main, StructureSDR 2A6D20240425009Skin Panel · corrodedCORROSION DAMAGE ON THE FWD UPPER SKIN MEASURED TO BE APPROXIMATELY 0.80” X 0.60” X 0.003”Apr 25, 2024 · N11FQ · Urocop EC130T2 · Fuselage Main, Plate/SkinSDR 2A6D20240425008Stiffener · corrodedDAMAGE TO THE TAIL BOOM LH FWD STIFFENER MEASURED TO BE APPROXIMATELY 0.85” X 0.85” X 0.0125” IN THE FORM OF CORROSION.Apr 25, 2024 · N11FQ · Urocop EC130T2 · Rotorcraft Tail BoomSDR 2A6D20240425007Attach Angle · corrodedREAR LANDING GEAR ATTACHMENT LOWER ANGLE HAS DAMAGE IN THE FORM OF CORROSION. THE DAMAGE NEAR THE ANGLE OVERLAPS WITH MACHINED FRAME AND AFT LOWER BELLY FAIRING. THE DAMAGE IS ON THE VERTICAL FACE OF THE ANGLE AT PREVIOUS REPAIR LOCATION AND IS MEASURED TO BE Apr 25, 2024 · N11FQ · Urocop EC130T2 · Fuselage, Landing Gear Attach FittingsSDR 2A6D20240425006Cradle · corrodedRH AFT FUEL CRADLE REINFORCEMENTS HAS DAMAGE IN THE FORM OF CORROSION. THE RH AFT CORROSION DAMAGE MEASURED TO BE APPROXIMATELY 2.1” X 0.80” X 0.009”.Apr 25, 2024 · N11FQ · Urocop EC130T2 · Fuel StorageSDR 2A6D20240425005Cradle · corrodedTHE LH FWD FUEL CRADLE REINFORCEMENTS HAD DAMAGE IN THE FORM OF CORROSION. THE LH FWD CORROSION DAMAGE MEASURED TO BE APPROXIMATELY 1.0” X 0.80” X 0.008”.Apr 25, 2024 · N11FQ · Urocop EC130T2 · Fuel StorageSDR 2A6D20240425004Skin Panel · corrodedDAMAGE IS ON THE AFT FUSELAGE RH SIDE SKIN PANEL (P/N: 350A210046-21 IN THE FORM OF CORROSION. THE RH SIDE SKIN DAMAGE IS NEAR TOP EDGE WHERE ENGINE DECK OVERLAPS AND MEASURED TO BE APPROXIMATELY 0.15” X 0.20” X 0.011”.Apr 25, 2024 · N11FQ · Urocop EC130T2 · Fuselage Main, Plate/SkinSDR 2A6D20240425003Skin Panel · corrodedFIRST DAMAGE IS ON THE AFT FUSELAGE LH SIDE SKIN PANEL IN THE FORM OF CORROSION. THE LH SIDE SKIN DAMAGE IS NEAR TOP EDGE WHERE ENGINE DECK OVERLAPS AND MEASURED TO BE APPROXIMATELY 0.15” X 0.35” X 0.009”.Apr 25, 2024 · N11FQ · Urocop EC130T2 · Fuselage Main, Plate/SkinSDR 2A6D20240425002Brace · corrodedDAMAGE TO THE LH VERTICAL ANGLE (PN: 350A62-1148.21) ON THE AFT SECTION FWD LOWER FRAME IN THE FORM OF CORROSION. THE CORRODED AREA IS LOCATED AT THE BOTTOM END OF THE ANGLE, AND WAS MEASURED TO BE APPROXIMATELY 0.875” X 0.875” IN SIZE THROUGH THE FULL THICKNEApr 25, 2024 · N11FQ · Urocop EC130T2 · Fuselage Miscellaneous StructureSDR 2A6D20240425001Web · corrodedDAMAGE TO THE LOWER CENTER WEB IN THE FORM OF CORROSION. THE CORROSION DAMAGE IS TOWARDS THE AFT SIDE OF THE WEB NEAR LIGHTENING HOLES AND MEASURED TO BE THROUGH THICKNESS IN DEPTH.Apr 25, 2024 · N11FQ · Urocop EC130T2 · Fuselage Miscellaneous StructureSDR 2A6D20240320001Support Angle · corrodedEXFOLIATION CORROSION LOCATED ON FWD. L/H SIDE STIFFENER OF MASTER ELECTRICAL BOX.Mar 20, 2024 · N11FQ · Urocop EC130T2 · Fuselage Miscellaneous StructureSDR 2A6D20240201002Web · corrodedDAMAGE TO THE LOWER CENTER WEB (P/N: 350A21-4300.20) IN THE FORM OF CORROSION. THE CORROSION DAMAGE IS TOWARDS THE AFT SIDE OF THE WEB NEAR LIGHTENING HOLES AND MEASURED TO BE THROUGH THICKNESS IN DEPTH.Feb 1, 2024 · N11FQ · Urocop EC130B4 · Fuselage Miscellaneous StructureSDR 2A6D20240201001Angle · corrodedDAMAGE TO THE LH VERTICAL ANGLE (PN: 350A62-1148.21) ON THE AFT SECTION FWD LOWER FRAME IN THE FORM OF CORROSION. THE CORRODED AREA IS LOCATED AT THE BOTTOM END OF THE ANGLE, AND WAS MEASURED TO BE APPROXIMATELY 0.875” X 0.875” IN SIZE THROUGH THE FULL THICKNEFeb 1, 2024 · N11FQ · Urocop EC130B4 · Fuselage Miscellaneous StructureSDR HCMA201407170001Bolt · looseTHE DIGITAL NR READING WAS FLUCTUATING IN FLIGHT. AFTER TROUBLESHOOTING OF THE NR PICKUP ON THE NR GAUGE, IT WAS DECIDED TO INSPECT THE PHONIC WHEEL FOR SECURITY. UPON REMOVAL OF THE EPICYCLIC, IT WAS FOUND THAT SIX ATTACHMENT BOLTS, 2 WERE TORQUED TO 100 INJul 15, 2014 · N11FQ · Urocop EC130T2 · Main Rotor Mast/SwashplateSDR HCM2014F00000Engine · making metalDURING FLIGHT, ENGINE CHIP LIGHT ILLUMINATED AND PILOT MADE A PRECAUTIONARY LANDING. MECHANIC INSPECTED ENGINE CHIP PLUGS. A SIGNIFICANT AMOUNT OF METAL WAS FOUND ON THE ELECTRIC PLUG, MODULE 01 CHIP PLUG AND THE ENGINE OIL TANK CHIP PLUG. IT WAS DETERMINEMay 2, 2014 · N11FQ · Urocop EC130T2 · Engine (Turbine/Turboprop)
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