N867US, cancelled Feb 3, 2004

Service difficulty reports · 16

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 = 'N867US' AND deregistration_id = 'N867US-2004-02-03'
  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 USAAF01074Battery · dischargedRIC - THE FIRST CLASS EMERGENCY TRACK LIGHTING AND NR 1 CEILING EMERGENCY LIGHT WERE FOUND INOPERATIVE. MAINTENANCE REPLACED THE NR 9 SUPPLY BATTERY. OPERATIONALLY CHECKED OK. (M)Sep 21, 2001 · N867US · Fokker F28MK0100 · Emergency LightingSDR USAAF01047Battery Pack · inoperativeIND - THE RIGHT OVERWING EMERGENCY EXIT LIGHTS AND THE FLOOR EMERGENCY LIGHTS IN ROW 4-8 WERE FOUND INOPERATIVE. MAINTENANCE REPLACED BATTERY PACKS. OPS CHECKED OK. (M)Jul 15, 2001 · N867US · Fokker F28MK0100 · Airborne Auxiliary Power Unit (APU) SystemSDR USAAF01041Power Supply · dischargedIND - THE EMERGENCY LIGHTS WERE FOUND INOPERATIVE IN THE MIDDLE CABIN AREA. MAINTENANCE REPLACED THE NR 5 POWER SUPPLY UNIT. OPERATIONALLY CHECK OK. (M)Jul 3, 2001 · N867US · Fokker F28MK0100 · Emergency LightingSDR USAAF01036Battery Pack · inoperativeGSO - THE EMERGENCY LIGHTS WERE INOPERATIVE IN THE CENTER CABIN. MAINTENANCE REPLACED THE BATTERY PACK. OPERATIONALLY CHECKED OK. (M)Jun 27, 2001 · N867US · Fokker F28MK0100 · Emergency LightingSDR USAAF00051Sign · inoperativeIND- FOUND THE RIGHT SIDE EXIT SIGN, BETWEEN OVERWING EXITS, INOPERATIVE. MAINTENANCE REPAIRED BROKEN WIRE AT SIGN. SYSTEM CHECKED OK. (M)Jul 7, 2000 · N867US · Fokker F28MK0100 · Emergency LightingSDR USAAF99035Brakes · delaminatedILM - FLT 573 - DURING LANDING, THE NR 1 BRAKE CAUGHT FIRE. CFR RESPONDED AND EXTINGUISHED THE FIRE. PASSENGERS WERE EVACUATED VIA ESCAPE SLIDE. NO MAJOR INJURIES REPORTED. MINOR INJURIES (SCRATCHES) REPORTED DUE TO EVACUATION. MAINTENANCE CARRIED OUT AN Jun 26, 1999 · N867US · Fokker F28MK0100 · BrakeSDR USAAF98022Hyd System · failedFLT 861 - BHM - EN ROUTE TO BHM AT APPROXIMATELY 11,000 FT, CAPTAIN BELIEVED AIRCRAFT SUSTAINED A LIGHTNING STRIKE. AIRCRAFT LOST SYSTEM 2 HYDRAULIC PRESSURE SHORTLY AFTERWARDS. DURING APPROACH TO BHM AFTER FLAPS AND LANDING GEAR WERE EXTENDED THE SYSTEM 1 HFeb 26, 1998 · N867US · Fokker F28MK0100 · Hydraulic System, MainSDR USAAF98011Battery Pack · dischargedIND - EMERGENCY EXIT LIGHT ABOVE MAIN ENTRY DOOR WAS INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK. (M)Feb 2, 1998 · N867US · Fokker F28MK0100 · Emergency LightingSDR USAAF97096Power Supply · inoperativeIND - FOUND CENTER RIGHT OVERWING EXIT SIGN INOPERATIVE. REPLACED THE POWER SUPPLY AND BATTERY. (M)Nov 21, 1997 · N867US · Fokker F28MK0100 · Emergency LightingSDR USAAF97079Door · out of adjustFLT 1455 - PHL-MSP - EN ROUTE TO MSP, FUEL WOULD NOT TRANSFER FROM THE CENTER TANK TO THE WING TANKS. FLIGHT DIVERTED TO PIT FOR MAINTENANCE AND LANDED WITHOUT INCIDENT. MAINTENANCE RESET THE FUELING PANEL POWER SWITCH TO OFF AND ADJUSTED THE MECHANISM ON THOct 10, 1997 · N867US · Fokker F28MK0100 · Aircraft Fuel Distribution SystemSDR USAAF97070Socket · shortedCLRT/GSO - FLT 846 - ON APPROACH TO GSO, CREW DID NOT RECEIVE ANY GREEN DOWN AND LOCKED INDICATIONS ON THE GEAR HANDLE MODULE. THE INTRANSIT LIGHTS WORKED NORMALLY, AND THERE WERE NO GEAR UNSAFE MESSAGES ON THE MULTI-FUNCTION DISPLAYS. CREW DECLARED AN EMERGAug 26, 1997 · N867US · Fokker F28MK0100 · Landing Gear Position and WarningSDR USAA970183Skin · delaminatedPIT - DURING Q-1 CHECK, VISUAL AND CONDUCITVITY TEST FOUND FUSELAGE SKIN DELAMINATION/DISBONDED AT L/R SKIN, STATION 14011 AND 24611, STRINGER 52-53A AREA AND 21A-23 AREA. CUT OUT AND INSTALLED DOUBLER REPAIR PER US AIRWAYS EA NR 28690A. (M)May 8, 1997 · N867US · Fokker F28MK0100 · Fuselage Main, Plate/SkinSDR USAA970182Angle · crackedPIT - DURING Q-1 CHECK, VISUAL AND NDT INSPECTION DETECTED CRACKS ON SKIN CONNECTIN ANGLES, LEFT 1 INCH, RIGHT .375 INCH AT STATION 14911, STRINGER NR 11LHS, STRINGER NR 64 RHS. INSTALLED DOUBLER REPAIR PER US AIRWAYS EA NR 32204A. (M)May 8, 1997 · N867US · Fokker F28MK0100 · Fuselage Miscellaneous StructureSDR USAA970181Panel · crackedPIT - DURING Q-1 CHECK, VISUAL INSPECTION DETECTED .157 INCH SKIN CRACK AT RT NLG SIDE WALL PANEL, AFT OF FORWARD AIRCO PACK SUPPORT BRACKET. INSTALLED DOUBLER REPAIR 6 INCH BY 8 INCH PER US AIRWAYS EA NR 46923. (M)May 8, 1997 · N867US · Fokker F28MK0100 · Fuselage Miscellaneous StructureSDR USAA950090Pack · malfunctionedLGA - FLT 1156 - DURING FLIGHT THERE WAS DEPRESSURIZATION. THE NR 1 PACK FAULTED. CAPTAIN GOT THE CABIN PRESSURE UNDER CONTROL. ACFT DIVERTED AND LANDED WITHOUT INCIDENT. MAINTENANCE OPERATED NR 1 PACK WITH ENGINE BLEED AND APU AIR. CHECKS SATISFACTORY. Feb 6, 1995 · N867US · Fokker F28MK0100 · Cabin Cooling SystemSDR USAA950045Pin · shearedCLT - FLT 685 - AFTER TAKEOFF, BOTH MLG WOULD NOT RETRACT WHEN SELECTED UP. ACFT RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE RT GEAR SEQUENCE VALVE BRACKET LEVER ATTACH PIN. CHECKS OK ON GEAR RETRACTION. (W)Jan 27, 1995 · N867US · Fokker F28MK0100 · Landing Gear Retraction/Extension System
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