N882US, cancelled Oct 7, 2003

Service difficulty reports · 22

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 = 'N882US' AND deregistration_id = 'N882US-2003-10-07'
  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 USAAF01090Light · inoperativePIT - THE RIGHT FAIRING EMERGENCY LIGHT WAS INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT ASSEMBLY. (M)Dec 28, 2001 · N882US · Fokker F28MK0100 · Emergency LightingSDR USAAF01075Actuator · failedRIC-CLT - FLT 1008 - AFTER TAKEOFF, THE NOSE LANDING GEAR FAILED TO RETRACT. THE GEAR WAS CYCLED WITH NO CHANGE. THE AIRCRAFT RETURNED TO THE FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE GEAR AND FOUND SAFE TO FERRY TO PIT WITH THE GEAR DOWNOct 6, 2001 · N882US · Fokker F28MK0100 · Landing Gear Door ActuatorSDR USAAF01024Light · inoperativeIND - THE EMERGENCY EXIT LIGHT ON THE MAIN ENTRY DOOR HINGE WAS INOPERATIVE. MAINTENANCE REPLACED THE LIGHT ASSEMBLY. FUNCTIONALLY CHECKED OK. (M)May 15, 2001 · N882US · Fokker F28MK0100 · Emergency LightingSDR USAAF99055Unknown · odorORD - FLT 1999 - STRONG OIL BURNING ODOR DETECTED DURING TAKEOFF AND CLIMB-OUT. ODOR WENT AWAY ONCE THE NR 2 PACK WAS TURNED OFF. MAINTENANCE OPS CHECKED NR 2 PACK FOR OIL ODOR, BUT DID NOT DETECT ANY ODOR. PACK OK FOR SERVICE. (X)Dec 1, 1999 · N882US · Fokker F28MK0100 · Air Distribution SystemSDR USAAF99027Pump · failedSBN - FLT 1240 EN ROUTE PIT-SBN, CREW EXPERIENCED TOTAL HYDRAULIC FAILURE. FLIGHT PROCEEDED TO SBN. UPON LANDING, THE NR 3 TIRE BLEW, CAUSING LOSS OF DIRECTIONAL CONTROL OF THE AIRCRAFT. THE AIRCRAFT CAME TO A STOP APPROXIMATELY 6000 FEET DOWN THE RUNWAY ANMay 21, 1999 · N882US · Fokker F28MK0100 · Hydraulic Pump (Electric/Engine), MainSDR USAAF98063Hydraulic System · failedCLT - FLT 281 - ON CLIMB-OUT FROM CLT, SYSTEM 1 HORIZONTAL STABILIZER HYDRAULICS FAILED. SEVERAL MINUTES LATER, SYSTEM 2 HORIZONTAL STABILIZER HYDRAULICS FAILED. FLIGHT RETURNED TO CLT WITHOUT DECLARING AN EMERGENCY AND LANDED WITHOUT FURTHER INCIDENT. MAINJul 30, 1998 · N882US · Fokker F28MK0100 · Hydraulic Power SystemSDR USAAF98057Mlg · failedPIT - FLT 671 - ON APPROACH TO CRW WHEN THE LANDING GEAR WAS SELECTED DOWN, THE MAIN LANDING GEAR DID NOT EXTEND. CREW RECYCLED THE GEAR HANDLE WITH THE SAME RESULT. FLIGHT RETURNED TO PIT. ON APPROACH TO PIT, CREW USED THE ALTERNATE GEAR EXTENSION PROCEDURJul 18, 1998 · N882US · Fokker F28MK0100 · Landing Gear Retraction/Extension SystemSDR 98ZZZX2863Door · damagedPIT - FLT 671 - ON APPROACH TO CRW WHEN THE LANDING GEAR WAS SELECTED DOWN, THE MAIN LANDING GEAR DID NOT EXTEND. CREW RECYCLED THE GEAR HANDLE WITH THE SAME RESULT. FLIGHT RETURNED TO PIT. ON APPROACH TO PIT, CREW USED THE ALTERNATE GEAR EXTENSION PROCEDURJul 18, 1998 · N882US · Fokker F28MK0100 · Landing Gear DoorsSDR USAAF98053Pseu · failedCLT - FLT 1458 - AFTER TAKEOFF, 'GND/FLT CONTROL' MESSAGE ALONG WITH MASTER CAUTION LIGHT WOULD INTERMITTENTLY APPEAR EVERY 2-3 MINUTES. FLIGHT RETURNED TO CLT AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE PROXIMITY SWITCHING ELECTRONIC UNIT,Jun 17, 1998 · N882US · Fokker F28MK0100 · Landing Gear Position and WarningSDR 98ZZZX2831Sensor · failedCLT - FLT 1458 - AFTER TAKEOFF, 'GND/FLT CONTROL' MESSAGE ALONG WITH MASTER CAUTION LIGHT WOULD INTERMITTENTLY APPEAR EVERY 2-3 MINUTES. FLIGHT RETURNED TO CLT AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE PROXIMITY SWITCHING ELECTRONIC UNIT,Jun 17, 1998 · N882US · Fokker F28MK0100 · Landing Gear Position and WarningSDR 98ZZZX2830Sensor · failedCLT - FLT 1458 - AFTER TAKEOFF, 'GND/FLT CONTROL' MESSAGE ALONG WITH MASTER CAUTION LIGHT WOULD INTERMITTENTLY APPEAR EVERY 2-3 MINUTES. FLIGHT RETURNED TO CLT AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE PROXIMITY SWITCHING ELECTRONIC UNIT,Jun 17, 1998 · N882US · Fokker F28MK0100 · Landing Gear Position and WarningSDR 98ZZZX2829Harness · failedCLT - FLT 1458 - AFTER TAKEOFF, 'GND/FLT CONTROL' MESSAGE ALONG WITH MASTER CAUTION LIGHT WOULD INTERMITTENTLY APPEAR EVERY 2-3 MINUTES. FLIGHT RETURNED TO CLT AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE PROXIMITY SWITCHING ELECTRONIC UNIT,Jun 17, 1998 · N882US · Fokker F28MK0100 · Landing Gear Position and WarningSDR USAAF97075Battery Pack · dischargedDURING ROUTINE OVERNIGHT MAINTENANCE INSPECTION, MAIN ENTRY DOOR EXIT SIGN WOULD NOT ILLUMINATE. MAINTENANCE REPLACED THE BATTERY PACK. (X)Sep 22, 1997 · N882US · Fokker F28MK0100 · Emergency LightingSDR USAAF97057Aux Power Unit · failedPIT/ERI - FLT 502 - ON DESCENT INTO ERI, THE APU SHUT DOWN AUTOMATICALLY WHEN THE SPEED BRAKE WAS DEPLOYED. A 'LOW AGENT' FOR THE APU FIRE SYSTEM ALSO ILLUMINATED. THE FLIGHT LANDED ERI WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE APU ASSY. US AIRWAYJul 9, 1997 · N882US · Fokker F28MK0100 · APU Core EngineSDR USAAF97052Swivel Joint · leakingRDU/CLT - FLT 1614 - ON APPROACH TO CLT, APPROXIMATELY 15 MILES FROM AIRPORT, APU FIRE WARNING ILLUMINATED, ALONG WITH AUTOMATIC APU SHUT DOWN AND FIRE BOTTLE DISCHARGE. CAPTAIN DECLARED AN EMERGENCY. FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE FOUNJun 26, 1997 · N882US · Fokker F28MK0100 · APU Bleed Air SystemSDR 97ZZZX3180Fire Contl Unit · malfunctionedRDU/CLT - FLT 1614 - ON APPROACH TO CLT, APPROXIMATELY 15 MILES FROM AIRPORT, APU FIRE WARNING ILLUMINATED, ALONG WITH AUTOMATIC APU SHUT DOWN AND FIRE BOTTLE DISCHARGE. CAPTAIN DECLARED AN EMERGENCY. FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE FOUNJun 26, 1997 · N882US · Fokker F28MK0100 · Fire DetectionSDR USAAF97033Battery Pack · dischargedIND - FORWARD OVERHEAD EXIT SIGN AND AREA EMERGENCY LIGHT INOP. MAINTENANCE REPLACED THE BATTERY PACK. (M)Mar 22, 1997 · N882US · Fokker F28MK0100 · Emergency LightingSDR USAAF97026Windshield · failedPIT - FL 8565 - EN ROUTE MCO-PIT - CREW NOTED STRONG ELECTRICAL SMELL IN COCKPIT. CREW DONNED OXYGEN MASKS. FLIGHT LANDED AT PIT WITH NO FURTHER INCIDENT. MAINTENANCE REPLACED THE RIGHT WINDSHIELD. (M)Mar 8, 1997 · N882US · Fokker F28MK0100 · Flight Compartment WindowsSDR USAAF96115Bulb · failedEMERGENCY EXIT LIGHT AT 12A IS OUT OF SERVICE. MAINTENANCE RELAMPED EXIT LIGHT. (M)Nov 5, 1996 · N882US · Fokker F28MK0100 · Emergency LightingSDR USAAF96097Bypass Vlv · failedRDU-PIT - FLT 1423 - ON CLIMB GOING THROUGH FL 100, PACK CABIN SUPPLY TEMP WENT TO 100F EVEN WITH TEMP SELECT FULL COLD. ONE PACK WAS ON MEL AS WELL AS APU BLEED AIR. AIRCRAFT DIVERTED TO GSO. NO FURTHER INCIDENTS. MAINTENANCE REPLACED LEFT BYPASS VALVE. Sep 8, 1996 · N882US · Fokker F28MK0100 · Cabin Cooling SystemSDR USAAF96025Windshield · crackedFLT NR 275 - RDU - OUTER PANE OF CAPTIANS WINDSHIELD SHATTERED IN FLIGHT AT 29,000 FEET PRECAUTIONARY LANDING MADE AT RDU. REPLACED L1 WINDOW. (M)Feb 24, 1996 · N882US · Fokker F28MK0100 · Flight Compartment WindowsSDR USAAF96008Shutoff Valve · inoperativeCLT - FL 1295 - EN ROUTE PIT - LGA, CREW RECEIVED TAIL ANTI-ICING FAULT SHORTLY AFTER SELECTING TAIL ANTI-ICE. FLIGHT DIVERTED TO CLT AND LANDED WITH NO FURTHER INCIDENT. MAINTENANCE REPLACED THE TAIL ANTI-ICE SHUTOFF VALVE. (M)Jan 12, 1996 · N882US · Fokker F28MK0100 · Airfoil Anti/De-ice System
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