# Service difficulty reports: N889US, cancelled Jul 22, 2004 A list on [N889US, cancelled Jul 22, 2004](https://openairdocs.org/deregistered/N889US-2004-07-22.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. - [SDR USAAF02001](https://openairdocs.org/sdr/USAAF02001.md): Battery · discharged · Jan 18, 2002 · N889US · Fokker F28MK0100 · Emergency Lighting > GSO - THE FLOOR TRACK EMERGENCY LIGHTS BETWEEN SEAT ROWS 8 TO 12 WERE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERY SUPPLY. (M) - [SDR USAAF01057](https://openairdocs.org/sdr/USAAF01057.md): Light · inoperative · Jul 27, 2001 · N889US · Fokker F28MK0100 · Emergency Lighting > PIT - THE EMERGENCY EXIT TRACK LIGHTING AT ROWS 9 AND 10 WERE INOPERATIVE. MAINTENANCE REPLACED THE TRACK LIGHTING STRIP. OPERATIONALLY CHECKED OK. (M) - [SDR USAAF01013](https://openairdocs.org/sdr/USAAF01013.md): Battery · discharged · Mar 30, 2001 · N889US · Fokker F28MK0100 · Emergency Lighting > PIT - THE FORWARD ENTRANCE DOOR AND SERVICE DOOR EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE REPLACED THE BATTERY SUPPLY ASSEMBLY. OPERATIONALLY CHECKED OK. (M) - [SDR USAAF01010](https://openairdocs.org/sdr/USAAF01010.md): Unknown · odor · Mar 23, 2001 · N889US · Fokker F28MK0100 · Air Distribution System > CLT-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) - [SDR USAAF00041](https://openairdocs.org/sdr/USAAF00041.md): Battery · discharged · Jun 2, 2000 · N889US · Fokker F28MK0100 · Emergency Lighting > GSO - FOUND THE RIGHT TRAILING EDGE FAIRING LIGHT INOPERATIVE. MAINTENANCE REPLACED THE NR 7 EMERGENCY POWER SUPPLY. OPS CHECKS NORMAL. (M) - [SDR USAAF99038](https://openairdocs.org/sdr/USAAF99038.md): Windshield · failed · Aug 3, 1999 · N889US · Fokker F28MK0100 · Flight Compartment Windows > BNA - 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. - [SDR USAAF98082](https://openairdocs.org/sdr/USAAF98082.md): Coffee Maker · overheated · Oct 4, 1998 · N889US · Fokker F28MK0100 · Buffet/Galleys > BWI - 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 BREA - [SDR USAAF98070](https://openairdocs.org/sdr/USAAF98070.md): Battery · discharged · Aug 20, 1998 · N889US · Fokker F28MK0100 · Emergency Lighting > GSO - FOUND FORWARD EMERENCY EXIT LIGHT INOPERATIVE. MAINTENANCE REPLACED THE BATTERY POWER SUPPLY. (X) - [SDR USAA980239](https://openairdocs.org/sdr/USAA980239.md): Floorbeam · corroded · Jun 5, 1998 · N889US · Fokker F28MK0100 · Fuselage Main, Floor Beam > PIT - 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) - [SDR USAA980238](https://openairdocs.org/sdr/USAA980238.md): Floorbeam · corroded · Jun 5, 1998 · N889US · Fokker F28MK0100 · Fuselage Main, Floor Beam > PIT - 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) - [SDR USAA980237](https://openairdocs.org/sdr/USAA980237.md): Floorbeam · corroded · Jun 5, 1998 · N889US · Fokker F28MK0100 · Fuselage Main, Floor Beam > PIT - 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) - [SDR USAAF98031](https://openairdocs.org/sdr/USAAF98031.md): Stop · out of adjust · Mar 25, 1998 · N889US · Fokker F28MK0100 · Landing Gear Door Retract Section > CLT 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 FO - [SDR USAA980150](https://openairdocs.org/sdr/USAA980150.md): Floorbeam · corroded · Feb 21, 1998 · N889US · Fokker F28MK0100 · Fuselage Main, Floor Beam > PIT - 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) - [SDR USAA980149](https://openairdocs.org/sdr/USAA980149.md): Web · corroded · Feb 21, 1998 · N889US · Fokker F28MK0100 · Fuselage Miscellaneous Structure > PIT - 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) - [SDR USAAF97090](https://openairdocs.org/sdr/USAAF97090.md): Temp Valve · failed · Nov 12, 1997 · N889US · Fokker F28MK0100 · Cabin Pressure Control System > FLT 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, - [SDR 97ZZZM1174](https://openairdocs.org/sdr/97ZZZM1174.md): Pack · failed · Nov 12, 1997 · N889US · Fokker F28MK0100 · Cabin Pressure Control System > FLT 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, - [SDR 97ZZZM1173](https://openairdocs.org/sdr/97ZZZM1173.md): Shutoff Vlv · failed · Nov 12, 1997 · N889US · Fokker F28MK0100 · Cabin Pressure Control System > FLT 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, - [SDR USAAF97058](https://openairdocs.org/sdr/USAAF97058.md): Switch · sticking · Jul 11, 1997 · N889US · Fokker F28MK0100 · Rudder Control System > PIT/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-M - [SDR USAAF97028](https://openairdocs.org/sdr/USAAF97028.md): Line · loose · Mar 14, 1997 · N889US · Fokker F28MK0100 · Pneumatic Distribution System > PIT - 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 TH - [SDR USAAF97022](https://openairdocs.org/sdr/USAAF97022.md): Battery · discharged · Feb 17, 1997 · N889US · Fokker F28MK0100 · Emergency Lighting > DURING 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) - [SDR USAAF96081](https://openairdocs.org/sdr/USAAF96081.md): Windshield · failed · Jul 28, 1996 · N889US · Fokker F28MK0100 · Flight Compartment Windows > SYR - 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) - [SDR 96ZZZM1240](https://openairdocs.org/sdr/96ZZZM1240.md): Heat Controller · failed · Jul 28, 1996 · N889US · Fokker F28MK0100 · Windshield/Door Rain/Ice Removal > SYR - 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. - [SDR USAAF96039](https://openairdocs.org/sdr/USAAF96039.md): Strobe Light · faulty · May 4, 1996 · N889US · Fokker F28MK0100 · Exterior Lighting > LGA - 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) ## 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 = 'N889US' AND deregistration_id = 'N889US-2004-07-22' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/deregistered/N889US-2004-07-22/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.