N889US, cancelled Jul 22, 2004

Service difficulty reports · 23

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 = 'N889US' AND deregistration_id = 'N889US-2004-07-22'
  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 USAAF02001Battery · dischargedGSO - THE FLOOR TRACK EMERGENCY LIGHTS BETWEEN SEAT ROWS 8 TO 12 WERE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERY SUPPLY. (M)Jan 18, 2002 · N889US · Fokker F28MK0100 · Emergency LightingSDR USAAF01057Light · inoperativePIT - THE EMERGENCY EXIT TRACK LIGHTING AT ROWS 9 AND 10 WERE INOPERATIVE. MAINTENANCE REPLACED THE TRACK LIGHTING STRIP. OPERATIONALLY CHECKED OK. (M)Jul 27, 2001 · N889US · Fokker F28MK0100 · Emergency LightingSDR USAAF01013Battery · dischargedPIT - THE FORWARD ENTRANCE DOOR AND SERVICE DOOR EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE REPLACED THE BATTERY SUPPLY ASSEMBLY. OPERATIONALLY CHECKED OK. (M)Mar 30, 2001 · N889US · Fokker F28MK0100 · Emergency LightingSDR USAAF01010Unknown · odorCLT-MEM - FLT 896 - A LOUD NOISE, WITH SUBSEQUENT VIBRATION AND METAL BURNING ODOR , WAS HEARD DURING FLIGHT. THE FLIGHT DIVERTED TO CHA AND LANDED WITHOUT INCIDENT. (M)Mar 23, 2001 · N889US · Fokker F28MK0100 · Air Distribution SystemSDR USAAF00041Battery · dischargedGSO - FOUND THE RIGHT TRAILING EDGE FAIRING LIGHT INOPERATIVE. MAINTENANCE REPLACED THE NR 7 EMERGENCY POWER SUPPLY. OPS CHECKS NORMAL. (M)Jun 2, 2000 · N889US · Fokker F28MK0100 · Emergency LightingSDR USAAF99038Windshield · failedBNA - FLT 793 - EN ROUTE CLT-STL, AT FL310, CREW DETECTED A NOXIOUS SMELL AND THEN SAW SMOKE IN THE COCKPIT. CREW DESELECTED WINDOW HEAT AND THE ODOR STOPPED. FLIGHT DIVERTED TO BNA AND LANDED WITH NO FURTHER INCIDENT. MAINTENANCE REPLACED THE WINDSHIELD. Aug 3, 1999 · N889US · Fokker F28MK0100 · Flight Compartment WindowsSDR USAAF98082Coffee Maker · overheatedBWI - FLT 1192 - EN ROUTE TO BWI AT FL230, SMOKE SMELL ENTERED THE COCKPIT. CREW STATED THAT SMOKE WAS NOT VISIBLE AND FLIGHT ATTENDANTS ALSO SMELLED SMOKE AND COULD SEE IT COMING FROM ABOVE COFFEE MAKERS. THE FLIGHT CREW PULLED THE COFFEE MAKER CIRCUIT BREAOct 4, 1998 · N889US · Fokker F28MK0100 · Buffet/GalleysSDR USAAF98070Battery · dischargedGSO - FOUND FORWARD EMERENCY EXIT LIGHT INOPERATIVE. MAINTENANCE REPLACED THE BATTERY POWER SUPPLY. (X)Aug 20, 1998 · N889US · Fokker F28MK0100 · Emergency LightingSDR USAA980239Floorbeam · corrodedPIT - DURING Q-CHECK, FOUND .3750 INCH BY .50 INCH CORRODED AREA AT BEAM AT STA 3870, BL 1127R. BLENDED OUT CORROSION ON FLOOR BEAM TO SMOOTH CONTOUR, ALODINE NR 1200S PRIME AND TOP COAT REWORKED AREAS, SEALED TOP SURFACE BEAM WITH PR 1436G PER EA 49760. (X)Jun 5, 1998 · N889US · Fokker F28MK0100 · Fuselage Main, Floor BeamSDR USAA980238Floorbeam · corrodedPIT - DURING Q-CHECK, FOUND SEVERAL .25 INCH BY .25 INCH CORRODED AREAS AT STA 3870 AND STA 4610 BL 1127L BEAM. BLENDED CORROSION TO SMOOTH CONTOUR. ALODINED AND PRIMED. SEALED TOP SURFACE WITH 1436G PER EA 49760. (X)Jun 5, 1998 · N889US · Fokker F28MK0100 · Fuselage Main, Floor BeamSDR USAA980237Floorbeam · corrodedPIT - DURING Q-CHECK, FOUND 1 INCH BY .50 INCH CORRODED AREA AT BEAM AT STA 3870 FORWARD BEAM BL 1127L. BLENDED OUT CORROSION ON FLOORBEAM, INSTALLED L-ANGLE DOUBLER WET WITH PR 1436G USMS MS20426AD5 AND MS047AD5 FASTENERS PER EA 49771. (X)Jun 5, 1998 · N889US · Fokker F28MK0100 · Fuselage Main, Floor BeamSDR USAAF98031Stop · out of adjustCLT 1856 - CREW RECEIVED LEFT MAIN LANDING GEAR WARNING MESSAGE DURING RETRACTION ON THE MFDU. CREW LOWERED THE GEAR AND RECEIVED A NORMAL DOWN AND LOCKED INDICATION. THE FLIGHT THEN RETURNED TO CLT WHERE LANDING WAS WITHOUT FURTHER INCIDENT. MAINTENANCE FOMar 25, 1998 · N889US · Fokker F28MK0100 · Landing Gear Door Retract SectionSDR USAA980150Floorbeam · corrodedPIT - DURING UNSCHEDULED MAINTENANCE, PILOT REPORT, FOUND BL 0 CORRODED AT STATION 3870 TO AFT OF 5305. MANUFACTURED NEW BEAM AND INSTALLED PER SRM 53-12-10 FIG 8 ITEM 390. (M)Feb 21, 1998 · N889US · Fokker F28MK0100 · Fuselage Main, Floor BeamSDR USAA980149Web · corrodedPIT - DURING UNSCHEDULED MAINTENANCE, PILOT REPORT, FOUND BL 0 SUPPORT WEB CORRODED AT STATION 5305. MANUFACTURED AND INSTALLED NEW WEB PER SRM 53-12-10 FIG 8 ITEM 840. (M)Feb 21, 1998 · N889US · Fokker F28MK0100 · Fuselage Miscellaneous StructureSDR USAAF97090Temp Valve · failedFLT 1543 - CLT-MSP - DURING CLIMB AT FL 220, NR 2 BLEED FAULT ILLUMINATED AND WAS RESET. LATER, AT FL340, THE RIGHT PACK BECAME VERY NOISY AND BEGAN TO VIBRATE. PACK WAS SHUT DOWN AND AIRCRAFT DESCENDED TO FL 250. AT THIS TIME AN ELECTRICAL SMELL WAS NOTED,Nov 12, 1997 · N889US · Fokker F28MK0100 · Cabin Pressure Control SystemSDR 97ZZZM1174Pack · failedFLT 1543 - CLT-MSP - DURING CLIMB AT FL 220, NR 2 BLEED FAULT ILLUMINATED AND WAS RESET. LATER, AT FL340, THE RIGHT PACK BECAME VERY NOISY AND BEGAN TO VIBRATE. PACK WAS SHUT DOWN AND AIRCRAFT DESCENDED TO FL 250. AT THIS TIME AN ELECTRICAL SMELL WAS NOTED,Nov 12, 1997 · N889US · Fokker F28MK0100 · Cabin Pressure Control SystemSDR 97ZZZM1173Shutoff Vlv · failedFLT 1543 - CLT-MSP - DURING CLIMB AT FL 220, NR 2 BLEED FAULT ILLUMINATED AND WAS RESET. LATER, AT FL340, THE RIGHT PACK BECAME VERY NOISY AND BEGAN TO VIBRATE. PACK WAS SHUT DOWN AND AIRCRAFT DESCENDED TO FL 250. AT THIS TIME AN ELECTRICAL SMELL WAS NOTED,Nov 12, 1997 · N889US · Fokker F28MK0100 · Cabin Pressure Control SystemSDR USAAF97058Switch · stickingPIT/CRW - FLT 1017 - ON CLIMB-OUT FROM PIT, 'RUDDER 2' FAULT ILLUMINATED. WHILE GOING THROUGH APPROPRIATE CHECK LIST, 'RUDDER 1' FAULT ILLUMINATED, AUTOPILOT DISENGAGED, AND 'STAB TRIM' FAULT ILLUMINATED. CREW ELECTED TO RETURN TO PIT BECAUSE CRW IS A NON-MJul 11, 1997 · N889US · Fokker F28MK0100 · Rudder Control SystemSDR USAAF97028Line · loosePIT - FL 305 - CREW NOTED MFDU MESSAGE WING ANTI-ICE LOW CAPACITY. SHORTLY THEREAFTER, THE TAIL ANTI-ICE FAULT ILLUMINATED. FLIGHT RETURNED TO PIT AND LANDED WITH NO FURTHER INCIDENT. MAINTENANCE FOUND THE LINE FROM THE LEFT ENGINE TMSOV TO THE PNEUMATIC THMar 14, 1997 · N889US · Fokker F28MK0100 · Pneumatic Distribution SystemSDR USAAF97022Battery · dischargedDURING AN ANNUAL EMERGENCY SLIDE OPERATIONAL CHECK, THE FORWARD SERVICE DOOR EMERGENCY SLIDE LIGHTS DID NOT ILLUMINATE WHEN SLIDE WAS DEPLOYED. THE SLIDE DID DEPLOY NORMALLY, HOWEVER, NONE OF THE SLIDE LIGHTS ILLUMINATED. (M)Feb 17, 1997 · N889US · Fokker F28MK0100 · Emergency LightingSDR USAAF96081Windshield · failedSYR - FL 1052 - AT FL 280 NEAR ABL, CAPTAIN'S WINDSHIELD OUTER PANE SHATTERED. FLIGHT DIVERTED TO SYR AND LANDED WITH NO FURTHER INCIDENT. MAINTENANCE REPLACED THE WINDSHIELD AND THE HEAT CONTROLLER. (M)Jul 28, 1996 · N889US · Fokker F28MK0100 · Flight Compartment WindowsSDR 96ZZZM1240Heat Controller · failedSYR - FL 1052 - AT FL 280 NEAR ABL, CAPTAIN'S WINDSHIELD OUTER PANE SHATTERED. FLIGHT DIVERTED TO SYR AND LANDED WITH NO FURTHER INCIDENT. MAINTENANCE REPLACED THE WINDSHIELD AND THE HEAT CONTROLLER. REFERENCE USAAF96081.Jul 28, 1996 · N889US · Fokker F28MK0100 · Windshield/Door Rain/Ice RemovalSDR USAAF96039Strobe Light · faultyLGA - FL 866 - UPON LANDING IN LGA, BRAKE PEDALS WENT TO FLOOR, GRABBED AND CYCLED. MAINTENANCE REPLACED THE LOWER FUSELAGE STROBE LIGHT DUE TO ELECTROMAGNETIC INTERFERENCE WITH THE ANTI-SKID SYSTEM. ANTI-SKID TEST ACCOMPLISHED, CHECKED NORMAL. (M)May 4, 1996 · N889US · Fokker F28MK0100 · Exterior Lighting
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