N430Z, cancelled Feb 14, 2007
Service difficulty reports · 21
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 = 'N430Z' AND deregistration_id = 'N430Z-2007-02-14' 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' WHERE n_number = 'N430Z' AND deregistration_id = 'N430Z-2007-02-14' 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 OZI2003F00001Floorbeam · corrodedFORWARD SIDE OF LAVATORY FLOORBEAM (FRAME 35) CORRODED.SDR OZIA200343001Floor Support · corrodedFORWARD SIDE OF LAVATORY FLOOR SUPPORT (FRAME 35) CORRODED.SDR OZI2003F00002Sill · corrodedBAGGAGE COMPARTMENT DOOR SILL, AT THE FLOORBOARD ATTACH HOLES CORRODED.SDR OZI2003F00000Longeron · corrodedBAGGAGE COMPARTMENT LONGERON CORRODED.SDR OZIA200343003Longeron · corrodedBAGGAGE COMPARTMENT LONGERON CORRODED.SDR OZIA200343002Sill · corrodedBAGGAGE COMPARTMENT DOOR SILL, AT THE FLOORBOARD, ATTACH HOLES CORRODED.SDR OZIA200243009Lamp · burned outRight main gear "green down arrow" not illuminated when gear selected down.SDR OZIA200243008Turbine Blades · missingENGINE SHOWED SHIFT IN ITT AND N2 PARAMETERS ON ECTM. BORESCOPE FOUND HP TURBINE MISSING TWO BLADES AND OTHER BLADES WITH CRACKS.SDR OZIA200243007Actuator · contaminatedELEVATOR MISTRIM CAS MESSAGE. ELEVATOR TRIM MOTOR FAIL MESSAGE ON SYC MAINT PAGE. NORMAL OR STANDBY PITCH TRIM WOULD NOT WORK ON DESCENT. RETURNED BELOW FREEZING LEVEL.SDR OZIA200243006Speed Switch · seizedOn landing roll out norm anti-skid and alt anti-skid degrade CAS message, OB LH MLG tire flat spotted.SDR OZIA200243005Warning System · activatedINTERMITTENT RT FUEL FILTER BYPASS INDICATION.SDR OZIA200243004Dau · failedMultiple CAS miscompares--FWC, Misc CPCS10XX, Misc Fuel, Misc Engine.SDR OZIA200243003Computer · failedGLIDESLOPE ON CAPTAIN'S SIDE FAILED.SDR OZIA200243002Lever · failedAfter takeoff, Pilot had multiple warning indications, "takeoff config, landing gear warning horn". Pilot elected to return to airport. When elected to extend landing gear, the gear did not come down. Pilot used emergency landing gear extension procedures to lSDR OZIA200243001Pseu · failedAfter takeoff, Pilot had multiple warning indications, "takeoff config, landing gear warning horn". Pilot elected to return to airport. When elected to extend landing gear, the gear did not come down. Pilot used emergency landing gear extension procedures to lSDR OZIA200143005Control Unit · miswiredDURING REMOVE AND REPLACE OF AILERON DISCONNECT UNIT, FOUND UNIT TO BE WIRED INCORRECTLY (PINS B & C WERE INCORRECT). SWAPPED WIRES B & C ON THE AILERON DISCONNECT UNIT TO CONFORM WITH THE AIRCRAFT WIRING MANUAL IAW DORNIER SPR RESPONSE A00025599. UNIT INSTASDR OZIA200143004Pseu · failedApproximately 2 minutes after takeoff, had gear tone and other failures: 1) norm anti-skid fail, 2) proxy system "A" fail, 3) HYD qty "A" fail, 4) ground spoilers not stowed. Apparent proxy system "A" fail or total proxy computer fial. Normal landing extensionSDR OZIA013127003Wire · reversedUPON COMPLYING WITH SB 328J-31-097, FOUND PITCH AND ROLL INPUTS TO THE DAUS TO BE INCORRECT (REVERSED WIRING). CORRECTED WIRING.SDR OZIA013127001Engine · overtempHIGH ITT ON TAKEOFF ROLL. REJECTED TAKEOFF. ENGINE EXCEEDANCE PAGE INDICATED 930 DEGREES. NO FURTHER ACTION NEEDED PER 328 MANUAL.SDR 31270922528Actuator · failedFLAP CONTROL UNIT AND FLAP ASYM INDICATIONS ON EICAS SCREEN. RIGHT FLAP INDICATED 27 DEGREES AND LEFT FLAP INDICATED 0 DEGREES. BOTH FLAPS ACTUALLY AT 0 DEGREES. REMOVED AND REPLACED RIGHT FLAP ACTUATOR. OPS CHECK GOOD ON GROUND.SDR OZIA013127002Solenoid Valve · defectiveRT ENGINE EXCEEDANCE, ZONE B, AT 935.8 DEGREES FOR 20.2 SECONDS. REMOVED AND REPLACED SOLENOID VALVES UPPER AND LOWER. OPS CHECK GOOD.
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