# Service difficulty reports: N430Z, cancelled Feb 14, 2007 A list on [N430Z, cancelled Feb 14, 2007](https://openairdocs.org/deregistered/N430Z-2007-02-14.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. - [SDR OZI2003F00001](https://openairdocs.org/sdr/OZI2003F00001.md): Floorbeam · corroded · Jan 2, 2003 · N430Z · Dorner DO328300 · Fuselage Main, Floor Beam > FORWARD SIDE OF LAVATORY FLOORBEAM (FRAME 35) CORRODED. - [SDR OZIA200343001](https://openairdocs.org/sdr/OZIA200343001.md): Floor Support · corroded · Jan 2, 2003 · N430Z · Dorner DO328300 · Fuselage Miscellaneous Structure > FORWARD SIDE OF LAVATORY FLOOR SUPPORT (FRAME 35) CORRODED. - [SDR OZI2003F00002](https://openairdocs.org/sdr/OZI2003F00002.md): Sill · corroded · Dec 31, 2002 · N430Z · Dorner DO328300 · Fuselage Main, Structure > BAGGAGE COMPARTMENT DOOR SILL, AT THE FLOORBOARD ATTACH HOLES CORRODED. - [SDR OZI2003F00000](https://openairdocs.org/sdr/OZI2003F00000.md): Longeron · corroded · Dec 31, 2002 · N430Z · Dorner DO328300 · Fuselage Main, Longeron/Stringer > BAGGAGE COMPARTMENT LONGERON CORRODED. - [SDR OZIA200343003](https://openairdocs.org/sdr/OZIA200343003.md): Longeron · corroded · Dec 31, 2002 · N430Z · Dorner DO328300 · Fuselage Main, Longeron/Stringer > BAGGAGE COMPARTMENT LONGERON CORRODED. - [SDR OZIA200343002](https://openairdocs.org/sdr/OZIA200343002.md): Sill · corroded · Dec 31, 2002 · N430Z · Dorner DO328300 · Fuselage Main, Structure > BAGGAGE COMPARTMENT DOOR SILL, AT THE FLOORBOARD, ATTACH HOLES CORRODED. - [SDR OZIA200243009](https://openairdocs.org/sdr/OZIA200243009.md): Lamp · burned out · Sep 24, 2002 · N430Z · Dorner DO328300 · Flight Compartment Lighting > Right main gear "green down arrow" not illuminated when gear selected down. - [SDR OZIA200243008](https://openairdocs.org/sdr/OZIA200243008.md): Turbine Blades · missing · Sep 10, 2002 · N430Z · Dorner DO328300 · Turbine Section > ENGINE SHOWED SHIFT IN ITT AND N2 PARAMETERS ON ECTM. BORESCOPE FOUND HP TURBINE MISSING TWO BLADES AND OTHER BLADES WITH CRACKS. - [SDR OZIA200243007](https://openairdocs.org/sdr/OZIA200243007.md): Actuator · contaminated · Aug 31, 2002 · N430Z · Dorner DO328300 · Elevator Control System > ELEVATOR 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 OZIA200243006](https://openairdocs.org/sdr/OZIA200243006.md): Speed Switch · seized · Jun 15, 2002 · N430Z · Dorner DO328300 · Brake > On landing roll out norm anti-skid and alt anti-skid degrade CAS message, OB LH MLG tire flat spotted. - [SDR OZIA200243005](https://openairdocs.org/sdr/OZIA200243005.md): Warning System · activated · May 20, 2002 · N430Z · Dorner DO328300 · Engine Fuel Indicating System > INTERMITTENT RT FUEL FILTER BYPASS INDICATION. - [SDR OZIA200243004](https://openairdocs.org/sdr/OZIA200243004.md): Dau · failed · May 7, 2002 · N430Z · Dorner DO328300 · Central Computers > Multiple CAS miscompares--FWC, Misc CPCS10XX, Misc Fuel, Misc Engine. - [SDR OZIA200243003](https://openairdocs.org/sdr/OZIA200243003.md): Computer · failed · May 6, 2002 · N430Z · Dorner DO328300 · Integrated Flight System > GLIDESLOPE ON CAPTAIN'S SIDE FAILED. - [SDR OZIA200243002](https://openairdocs.org/sdr/OZIA200243002.md): Lever · failed · Jan 30, 2002 · N430Z · Dorner DO328300 · Landing Gear Position and Warning > After 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 l - [SDR OZIA200243001](https://openairdocs.org/sdr/OZIA200243001.md): Pseu · failed · Jan 30, 2002 · N430Z · Dorner DO328300 · Landing Gear Position and Warning > After 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 l - [SDR OZIA200143005](https://openairdocs.org/sdr/OZIA200143005.md): Control Unit · miswired · Sep 15, 2001 · N430Z · Dorner DO328300 · Aileron Control System > DURING 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 INSTA - [SDR OZIA200143004](https://openairdocs.org/sdr/OZIA200143004.md): Pseu · failed · Jul 12, 2001 · N430Z · Dorner DO328300 · Landing Gear Retraction/Extension System > Approximately 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 extension - [SDR OZIA013127003](https://openairdocs.org/sdr/OZIA013127003.md): Wire · reversed · Apr 24, 2001 · N430Z · Dorner DO328300 · Instrument System Wiring > UPON COMPLYING WITH SB 328J-31-097, FOUND PITCH AND ROLL INPUTS TO THE DAUS TO BE INCORRECT (REVERSED WIRING). CORRECTED WIRING. - [SDR OZIA013127001](https://openairdocs.org/sdr/OZIA013127001.md): Engine · overtemp · Feb 19, 2001 · N430Z · Dorner DO328300 · Engine (Turbine/Turboprop) > HIGH ITT ON TAKEOFF ROLL. REJECTED TAKEOFF. ENGINE EXCEEDANCE PAGE INDICATED 930 DEGREES. NO FURTHER ACTION NEEDED PER 328 MANUAL. - [SDR 31270922528](https://openairdocs.org/sdr/31270922528.md): Actuator · failed · Sep 22, 2000 · N430Z · Dorner DO328300 · Trailing Edge Flap Actuator > FLAP 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 OZIA013127002](https://openairdocs.org/sdr/OZIA013127002.md): Solenoid Valve · defective · Feb 20, 2000 · N430Z · Dorner DO328300 · Engine Fuel Distribution > RT ENGINE EXCEEDANCE, ZONE B, AT 935.8 DEGREES FOR 20.2 SECONDS. REMOVED AND REPLACED SOLENOID VALVES UPPER AND LOWER. OPS CHECK GOOD. ## The whole list in SQL Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS: ```sql 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 ``` This list as a web page: https://openairdocs.org/deregistered/N430Z-2007-02-14/reports --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.