N863US, cancelled Jul 22, 2003

Service difficulty reports · 19

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 = 'N863US' AND deregistration_id = 'N863US-2003-07-22'
  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 USAAF00079Wire · brokenIND - THE LAST SECTION OF FIRST CLASS FLOOR LEVEL EMERGENCY LIGHTS WERE FOUND INOPERATIVE. MAINTENANCE REPAIRED A BROKEN WIRE. OPERATIONALLY CHECKED GOOD. (M)Nov 20, 2000 · N863US · Fokker F28MK0100 · Light System WiringSDR USAAF00080Battery Pack · dischargedIND - THE LEFT OVERWING EMERGENCY EXIT LIGHTS, WERE FOUND INOPERATIVE BETWEEN THE EXITS. MAINTENANCE REPLACED A BATTERY AND POWER SUPPLY PACK. OPERATIONALLY CHECKED GOOD. (M)Nov 20, 2000 · N863US · Fokker F28MK0100 · Emergency LightingSDR USAAF00050Battery · dischargedCLT - 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)Jul 10, 2000 · N863US · Fokker F28MK0100 · Emergency LightingSDR USAAF00044Slide · detachedCLT - FOUND FORWARD SERVICE DOOR SLIDE FALLING OUT OF SLIDE PACK. MAINTENANCE REPLACED SLIDE ASSY. OK FOR SERVICE. (M)Jun 4, 2000 · N863US · Fokker F28MK0100 · Escape SlideSDR USAAF98008Shutoff Valve · inoperativeGSO - 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 ENGJan 19, 1998 · N863US · Fokker F28MK0100 · Engine Anti-Icing SystemSDR USAAF98004Indicator Module · failedCLT - 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 CHEJan 13, 1998 · N863US · Fokker F28MK0100 · Landing Gear Position and WarningSDR USAAF97061Seal · failedCLT/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 INSPECTJul 17, 1997 · N863US · Fokker F28MK0100 · Airborne Auxiliary Power Unit (APU) SystemSDR 97ZZZX4222Seal · failedCLT/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 INSPECTJul 17, 1997 · N863US · Fokker F28MK0100 · Airborne Auxiliary Power Unit (APU) SystemSDR 97ZZZX4221Seal · failedCLT/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 INSPECTJul 17, 1997 · N863US · Fokker F28MK0100 · Airborne Auxiliary Power Unit (APU) SystemSDR USAAF97049Control Unit · failedPIT/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 UNJun 18, 1997 · N863US · Fokker F28MK0100 · External Power SystemSDR USAAF97036Outflow Valve · stuck openFLT 1227 - CLT-IAD - AFTER TAKEOFF FROM CLT, THE AIRCRAFT WOULD NOT PRESSURIZE. FLIGHT RETURNED TO CLT. MAINTENANCE REPLACED THE PRIMARY OUTFLOW VALVE. (M)Apr 8, 1997 · N863US · Fokker F28MK0100 · Pressure Regulator/Outflow ValveSDR USAAF97027Air Distribution · odorDURING 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)Mar 9, 1997 · N863US · Fokker F28MK0100 · Air Distribution SystemSDR USAA970026Skin · damagedPIT - 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 DOUBLJan 20, 1996 · N863US · Fokker F28MK0100 · Fuselage Main, Plate/SkinSDR USAA970025Skin · damagedPIT - 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 DOUBLJan 20, 1996 · N863US · Fokker F28MK0100 · Fuselage Main, Plate/SkinSDR USAA970024Bulkhead · crackedPIT - 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)Jan 20, 1996 · N863US · Fokker F28MK0100 · Fuselage Main, BulkheadSDR USAA970023Bulkhead · crackedPIT - 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)Jan 20, 1996 · N863US · Fokker F28MK0100 · Fuselage Main, BulkheadSDR USAA970022Beam · corrodedPIT - 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 LEVELJan 20, 1996 · N863US · Fokker F28MK0100 · Fuselage Miscellaneous StructureSDR USAA951248Floor Beam · corrodedPIT - 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)Dec 6, 1995 · N863US · Fokker F28MK0100 · Fuselage Main, Floor BeamSDR USAA950752Valve · leakingRDU - 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)Jul 11, 1995 · N863US · Fokker F28MK0100 · Cabin Pressure Control System
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