# Service difficulty reports: N863US, cancelled Jul 22, 2003 A list on [N863US, cancelled Jul 22, 2003](https://openairdocs.org/deregistered/N863US-2003-07-22.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. - [SDR USAAF00079](https://openairdocs.org/sdr/USAAF00079.md): Wire · broken · Nov 20, 2000 · N863US · Fokker F28MK0100 · Light System Wiring > IND - THE LAST SECTION OF FIRST CLASS FLOOR LEVEL EMERGENCY LIGHTS WERE FOUND INOPERATIVE. MAINTENANCE REPAIRED A BROKEN WIRE. OPERATIONALLY CHECKED GOOD. (M) - [SDR USAAF00080](https://openairdocs.org/sdr/USAAF00080.md): Battery Pack · discharged · Nov 20, 2000 · N863US · Fokker F28MK0100 · Emergency Lighting > IND - THE LEFT OVERWING EMERGENCY EXIT LIGHTS, WERE FOUND INOPERATIVE BETWEEN THE EXITS. MAINTENANCE REPLACED A BATTERY AND POWER SUPPLY PACK. OPERATIONALLY CHECKED GOOD. (M) - [SDR USAAF00050](https://openairdocs.org/sdr/USAAF00050.md): Battery · discharged · Jul 10, 2000 · N863US · Fokker F28MK0100 · Emergency Lighting > CLT - FOUND THE FIRST CLASS FLOOR LEVEL EMERGENCY EXIT LIGHTS INOPERATIVE. MAINTENANCE REPLACED THE POWER SUPPLY FOR THE FIRST CLASS EMERGENCY EXIT LIGHTS. OPS CHECK OK. (M) - [SDR USAAF00044](https://openairdocs.org/sdr/USAAF00044.md): Slide · detached · Jun 4, 2000 · N863US · Fokker F28MK0100 · Escape Slide > CLT - FOUND FORWARD SERVICE DOOR SLIDE FALLING OUT OF SLIDE PACK. MAINTENANCE REPLACED SLIDE ASSY. OK FOR SERVICE. (M) - [SDR USAAF98008](https://openairdocs.org/sdr/USAAF98008.md): Shutoff Valve · inoperative · Jan 19, 1998 · N863US · Fokker F28MK0100 · Engine Anti-Icing System > GSO - FLT 875 - FLT EN ROUTE RIC TO CLT, WHEN NR 2 ENGINE ANTI-ICE FAILURE OCCURRED. CREW RESET CIRCUIT BREAKER AND IT POPPED. DUE TO WEATHER CONDITIONS IN CLT, FLIGHT DIVERTED TO GSO. FLT LANDED GSO WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED RIGHT ENG - [SDR USAAF98004](https://openairdocs.org/sdr/USAAF98004.md): Indicator Module · failed · Jan 13, 1998 · N863US · Fokker F28MK0100 · Landing Gear Position and Warning > CLT - FLT 220 - THE GREEN LEFT MLG LIGHT STAYED ON AFTER RETRACTION, NO OTHER ABNORMAL INDICATIONS WERE PRESENT. THE AIRCRAFT RETURNED TO CLT. THE AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE LANDING GEAR INDICATION MODULE. GROUND CHE - [SDR USAAF97061](https://openairdocs.org/sdr/USAAF97061.md): Seal · failed · Jul 17, 1997 · N863US · Fokker F28MK0100 · Airborne Auxiliary Power Unit (APU) System > CLT/TYS - FLT 589 - DURING DESCENT INTO CLT AFTER STARTING THE APU, CREW ACTIVATED THE SPEED BRAKE AND RECEIVED A MOMENTARY 'APU FIRE' WARNING. THE APU AUTO-SHUTDOWN AND FIRED THE BOTTLE. THE FLIGHT LANDED AT TYS WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECT - [SDR 97ZZZX4222](https://openairdocs.org/sdr/97ZZZX4222.md): Seal · failed · Jul 17, 1997 · N863US · Fokker F28MK0100 · Airborne Auxiliary Power Unit (APU) System > CLT/TYS - FLT 589 - DURING DESCENT INTO CLT AFTER STARTING THE APU, CREW ACTIVATED THE SPEED BRAKE AND RECEIVED A MOMENTARY 'APU FIRE' WARNING. THE APU AUTO-SHUTDOWN AND FIRED THE BOTTLE. THE FLIGHT LANDED AT TYS WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECT - [SDR 97ZZZX4221](https://openairdocs.org/sdr/97ZZZX4221.md): Seal · failed · Jul 17, 1997 · N863US · Fokker F28MK0100 · Airborne Auxiliary Power Unit (APU) System > CLT/TYS - FLT 589 - DURING DESCENT INTO CLT AFTER STARTING THE APU, CREW ACTIVATED THE SPEED BRAKE AND RECEIVED A MOMENTARY 'APU FIRE' WARNING. THE APU AUTO-SHUTDOWN AND FIRED THE BOTTLE. THE FLIGHT LANDED AT TYS WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECT - [SDR USAAF97049](https://openairdocs.org/sdr/USAAF97049.md): Control Unit · failed · Jun 18, 1997 · N863US · Fokker F28MK0100 · External Power System > PIT/STL - FLT 1531 - EN ROUTE TO STL APPROXIMATELY 90NM EAST OF IND, ESSENTIAL AC POWER BUS FAILED. FLIGHT DIVERTED TO IND FOR MAINTENANCE PURPOSES. NO EMERGENCY WAS DECLARED. FLIGHT LANDED IND WITHOUT INCIDENT. MAINTENANCE REPLACED GROUND POWER CONTROL UN - [SDR USAAF97036](https://openairdocs.org/sdr/USAAF97036.md): Outflow Valve · stuck open · Apr 8, 1997 · N863US · Fokker F28MK0100 · Pressure Regulator/Outflow Valve > FLT 1227 - CLT-IAD - AFTER TAKEOFF FROM CLT, THE AIRCRAFT WOULD NOT PRESSURIZE. FLIGHT RETURNED TO CLT. MAINTENANCE REPLACED THE PRIMARY OUTFLOW VALVE. (M) - [SDR USAAF97027](https://openairdocs.org/sdr/USAAF97027.md): Air Distribution · odor · Mar 9, 1997 · N863US · Fokker F28MK0100 · Air Distribution System > DURING THE LAST FORTY MINUTES OF FLIGHT, CREW NOTED ACRID ODOR IN THE COCKPIT. MAINTENANCE INSPECTED THE AREA AND FOUND NO PROBLEM. THE EQUIPMENT COOLING AIR FILTER WAS CHANGED. (M) - [SDR USAA970026](https://openairdocs.org/sdr/USAA970026.md): Skin · damaged · Jan 20, 1996 · N863US · Fokker F28MK0100 · Fuselage Main, Plate/Skin > PIT - DURING Q-1 CHECK, FOUND 18 INCH BY 20 INCH AREA OF DISBONDED AND HEAT DAMAGED SKIN AT RT STUBWING FUSELAGE SKIN BETWEEN FRAMES 24011 AND 24611 AND BETWEEN STRINGER 21A AND UPPER CONTACT ANGLE. CUT OUT DAMAGED AREA OF SKIN AND INSTALLED AN EXTERNAL DOUBL - [SDR USAA970025](https://openairdocs.org/sdr/USAA970025.md): Skin · damaged · Jan 20, 1996 · N863US · Fokker F28MK0100 · Fuselage Main, Plate/Skin > PIT - DURING Q-1 CHECK, FOUND 18 INCH BY 24 INCH AREA OF DISBONDED AND HEAT DAMAGED SKIN AT LT STUBWING FUSELAGE SKIN BETWEEN FRAMES 24011 AND 24611 AND BETWEEN STRINGER 21A AND UPPER CONTACT ANGLE. CUT OUT DAMAGED AREA OF SKIN AND INSTALLED AN EXTERNAL DOUBL - [SDR USAA970024](https://openairdocs.org/sdr/USAA970024.md): Bulkhead · cracked · Jan 20, 1996 · N863US · Fokker F28MK0100 · Fuselage Main, Bulkhead > PIT - DURING Q-1 CHECK, FOUND TWO.5 INCH CRACK (LT SIDE) OF CENTER FUEL TANK PRESSURE BULKHEAD AT FRAME 14911 AND STATION 11. STOP DRILLED AND CUT OUT CRACKED AREA. INSTALLED FILLER AND NEW ANGLES PER EA NR 34272. (M) - [SDR USAA970023](https://openairdocs.org/sdr/USAA970023.md): Bulkhead · cracked · Jan 20, 1996 · N863US · Fokker F28MK0100 · Fuselage Main, Bulkhead > PIT - DURING Q-1 CHECK, FOUND 3 INCH CRACK (RT SIDE) OF CENTER FUEL TANK PRESSURE BULKHEAD AT FRAME 14911 AND STATION 64. STOP DRILLED AND CUT OUT CRACKED AREA. INSTALLED FILLER AND NEW ANGLES PER EA NR 34272. (M) - [SDR USAA970022](https://openairdocs.org/sdr/USAA970022.md): Beam · corroded · Jan 20, 1996 · N863US · Fokker F28MK0100 · Fuselage Miscellaneous Structure > PIT - DURING Q-1 CHECK, FOUND 2 INCH BY 2 INCH AREA OF CORROSION (.068 INCH DEEP) IN MID CARGO DOOR LATCH BEAM TOP SURFACE BETWEEN STATION 11333-12791, STATION 72. CUT OUT CORRODED AREA AND INSTALLED A BATH TUP REPAIR FITTING PER EA NR 46074. CORROSION LEVEL - [SDR USAA951248](https://openairdocs.org/sdr/USAA951248.md): Floor Beam · corroded · Dec 6, 1995 · N863US · Fokker F28MK0100 · Fuselage Main, Floor Beam > PIT - DURING APU MODIFICATION TRACK, FOUND CORROSION ON FLOOR BEAM, BETWEEN STATION 4850 AND 5305 AND BL 0. CUT OUT CORRODED SECTION OF BEAM AND SPLICED IN NEW 'T' EXTENSION PER SRM 51-70-06. (M) - [SDR USAA950752](https://openairdocs.org/sdr/USAA950752.md): Valve · leaking · Jul 11, 1995 · N863US · Fokker F28MK0100 · Cabin Pressure Control System > RDU - FLT 109 - THE CABIN PRESSURE WOULD NOT CLIMB WITH ALTITUDE. THE CAPTAIN DECLARED AN EMERGENCY AND DIVERTED TO RDU. MAINTENANCE INSTALLED A NEW VALVE AT THE RT SIDE EXTERNAL AIR CONNECTION. OPERATIONS CHECKED GOOD. (W) ## 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 = 'N863US' AND deregistration_id = 'N863US-2003-07-22' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/deregistered/N863US-2003-07-22/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.