N857US, cancelled Feb 23, 2005

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 = 'N857US' AND deregistration_id = 'N857US-2005-02-23'
  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 USAAF01087Odor · detectedILM-CLT - FLT 1546 - DURING CLIMB-OUT THERE WERE STRONG FUMES IN THE CABIN AND THE LAV SMOKE DETECTORS SOUNDED. THE AIRCRAFT RETURNED TO THE FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE APU, AIR CONDITIONING PACKS, AND ENGINES. NO ABNORMAL IDec 23, 2001 · N857US · Fokker F28MK0100 · Air Distribution SystemSDR USAAF01054Door · unserviceableFLT 835 - EN ROUTE PIT-STL, DURING CLIMB-OUT, THE RIGHT OVERWING EMERGENCY EXIT DOORS BEGAN TO MAKE NOISE, THEN THE COVERS FOR THE EMERGENCY DOOR EMERGENCY RELEASE HANDLE FELL OFF. THE PASSENGERS IN THE EXIT ROWS WERE RESEATED AND THE FLIGHT CONTINUED TO STL.Jul 26, 2001 · N857US · Fokker F28MK0100 · Emergency ExitsSDR USAAF01055Door · unserviceableCLT - FLT 9281 - EN ROUTE STL-CLT - DURING THE FLIGHT, THE RIGHT OVER-WING EMERGENCY EXIT DOORS BECAME UNLATCHED. AFTER LANDING, THE EMERGENCY EXIT DOORS FELL OUT OF THE EMERGENCY EXIT OPENINGS ONTO THE EMERGENCY ROW SEATS. MAINTENANCE REPLACED THE RIGHT SIDJul 26, 2001 · N857US · Fokker F28MK0100 · Emergency ExitsSDR USAA010934Frame · crackedPIT - FOUND FRAME CRACKED 4 INCHES, FS 21736 BETWEEN STRINGER 3 AND THROUGH UPPER C-CHANNEL. INSTALLED TWO REPAIR ANGLES PER EA 71597. (M)Jul 25, 2001 · N857US · Fokker F28MK0100 · Fuselage Structure (General)SDR USAAF01053Door · unsecurePIT - FLT 1472 - EN ROUTE PIT-SDF, DURING CLIMB-OUT, THE COVER FOR THE EMERGENCY DOOR EMERGENCY RELEASE HANDLE AND SOME SAFETY WIRE FELL OFF. THE EMERGENCY DOOR EMERGENCY RELEASE HANDLE WAS FOUND TO BE IN THE INCORRECT POSITION. THE FLIGHT RETURNED TO FIELD Jul 25, 2001 · N857US · Fokker F28MK0100 · Emergency ExitsSDR USAA010802SkinPIT - FOUND SKIN WITH HEAT DAMAGE 8 INCH BY 12 INCH AREA, STATION 27026-27526 STRINGER 46-50. REMOVED HEAT DAMAGE, INSTALLED REPLACEMENT SKIN/DOUBLER PER EA 54649 AND TYP REPAIR 53-40-01. (M)Jul 1, 2001 · N857US · Fokker F28MK0100 · Fuselage Structure (General)SDR USAAF01029Tube · crackedPIT-CLT - FLT 347 - AFTER TAKEOFF, A VERY STRONG ODOR OF SKYDROL WAS NOTED IN THE CABIN. FLIGHT RETURNED TO THE FIELD IN PIT AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND A CRACKED FLAIR ON THE RIGHT HYDRAULIC LINE TO THE PRESSURE FILTER. REPLACED May 26, 2001 · N857US · Fokker F28MK0100 · Hydraulic Power SystemSDR USAAF01028Coalescer Bag · dirtySTL-PIT - FLT 288 - UPON APPLICATION ON TAKEOFF THRUST, A STRONG, ACRID, MUSTY ODOR DEVELOPED IN THE COCKPIT AND AFT CABIN AREAS. FLIGHT LANDED IN PIT WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED LEFT AND RIGHT COALESCER BAGS. LEAK CHECKED GOOD. RAN THE May 25, 2001 · N857US · Fokker F28MK0100 · Humidity Control SystemSDR USAAF00048Controller · faultyCLT-IND - FLT 235 - DURING CLIMB, SMOKE ODOR WAS PRESENT IN THE COCKPIT. ODOR DISSIPATED WHEN THE WINDOW HEAT WAS TURNED OFF. THE FLIGHT RETURNED TO THE FIELD DUE TO THE DEACTIVATED SYSTEM AND THE WEATHER EN ROUTE. FLIGHT LANDED WITHOUT INCIDENT. MAINTENANJun 24, 2000 · N857US · Fokker F28MK0100 · Windshield/Door Rain/Ice RemovalSDR USAAF00006Light · inoperativeIND - THE RIGHT AFT OVERWING EXTERIOR EMERGENCY LIGHT WAS INOPERATIVE. MAINTENANCE REPAIRED A BROKEN WIRE BEHIND THE SOCKET ASSEMBLY. (M)Jan 25, 2000 · N857US · Fokker F28MK0100 · Emergency LightingSDR USAAF99028Wire · brokenRDU - FOUND THE PASSENGER DOOR AND FORWARD SERVICE DOOR EMERGENCY EXIT MARKERS AND FLIGHT COMPARTMENT DOME LIGHT REMAIN ILLUMINATED AT ALL TIMES. AIRCRAFT FERRIED TO PIT WHERE MAINTEANCE REPAIRED A BROKEN WIRE AT THE FORWARD EMERGENCY EXIT LIGHT. (X)May 23, 1999 · N857US · Fokker F28MK0100 · Light System WiringSDR USAAF99013Tire · failedPIT - FLT 7881 - AFTER LANDING PIT DURING ROLLOUT, BOTH LEFT MAIN GEAR TIRES BLEW OUT WHEN MODERATE BRAKING WAS APPLIED. MAINTENANCE REPLACED BOTH LEFT MAIN GEAR TIRE ASSEMBLIES AND THE LEFT GEAR GROUND/FLIGHT SWITCH. THE ANTI-SKID SYSTEM AND THE NOSE GEAR SMar 12, 1999 · N857US · Fokker F28MK0100 · TireSDR USAAF98055Light · malfunctionedPIT - FLT 671 - AFTER TAKEOFF FROM PIT, THE EMERGENCY EXIT LIGHTS REMAINED ILLUMINATED AFTER LANDING GEAR WAS RETRACTED. MAINTENANCE RESEATED RELAY K2618A AND THE SYSTEM OPERATED NORMALLY. THEY PROGRAMMED THE RELAY FOR CHANGE AS A PRECAUTIONARY MAINTENANCE AJul 13, 1998 · N857US · Fokker F28MK0100 · Emergency LightingSDR USAAF98016Handle · looseCLE - FLT 598 - ON CLIMB-OUT OF CLE, CAPTAIN RECEIVED A MID CABIN DOOR WARNING LIGHT. FLIGHT RETURNED TO CLE WHERE LANDING WAS WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND MID CARGO HANDLE OPEN. CLOSED HANDLE. WARNING LIGHTS OPS NORMAL. (M)Feb 17, 1998 · N857US · Fokker F28MK0100 · Cargo/Baggage DoorsSDR USAAF97055Supply Unit · failedRDU/PHL - FLT 1408 - ON APPROACH TO PHL WHEN LANDING GEAR WAS SELECTED DOWN, IN-TRANSIT LIGHT ILLUMINATED BUT NONE OF THE THREE GREEN 'DOWN AND LOCKED' INDICATIONS ILLUMINATED. CREW RECYCLED THE GEAR WITH THE SAME RESULT. ATC CONFIRMED THAT ALL GEARS WERE DOJul 5, 1997 · N857US · Fokker F28MK0100 · Landing Gear Position and WarningSDR USAAF96078Flt Cntrl Comptr · failedPIT - FL 1601 - AFTER TAKEOFF, CREW RECEIVED 'NO AUTOLAND'MESSAGE. NEITHER AUTOPILOT WOULD TURN ON. FLIGHT RETURNED TO PIT ANDLANDED WITH NO FURTHER INCIDENT. MAINTENANCE REPLACED THE NR 1 FCC.(M)Jul 17, 1996 · N857US · Fokker F28MK0100 · Flight ControllerSDR USAA950940Skin · delaminatedPIT - DURING Q-1 INSPECTION, FOUND FUSELAGE SKIN DELAMINATED APPROXIMATELY 10 INCH BY 24 INCH AREA BETWEEN RIGHT STUB WING UPPER AND LOWER CONNECTION ANGLE FROM STATION 24011 TO STATION 24611. CUT OUT DAMAGED AREA AND INSTALLED DOUBLER REPAIR PER USAIR EA NR Aug 16, 1995 · N857US · Fokker F28MK0100 · Fuselage Main, Plate/SkinSDR USAA950939Skin · delaminatedPIT - DURING Q-1 INSPECTION, FOUND FUSELAGE SKIN DELAMINATED BETWEEN LEFT STUBWING UPPER AND LOWER CONNECTION ANGLES. AREA APPROXIMATELY 10 INCHES BY 24 INCHES AT STATION 24011 TO STATION 24611. CUT OUT DAMAGED AREA INSTALLED DOUBLER REPAIR PER USAIR EA NR 3Aug 16, 1995 · N857US · Fokker F28MK0100 · Fuselage Main, Plate/SkinSDR USAA9509937Angle · corrodedPIT - DURING Q-1 INSPECTION, FOUND CORROSION AT ATTACH ANGLE NR 2 RADIO RACK FLOOR PANEL. FABRICATED REPAIR ANGLE AND INSTALLED PER SRM 53-12-10. (M)Aug 11, 1995 · N857US · Fokker F28MK0100 · Fuselage Miscellaneous StructureSDR USAA950936Stringer · crackedPIT - DURING Q-1 INSPECTION, FOUND .5 INCH CRACK IN STRINGER NR 68 RIGHT SIDE 4 INCHES AFT OF FRAME 3870. INSTALLED DOUBLER REPAIR PER SRM 51-70-06 FIG 202. (M)Aug 2, 1995 · N857US · Fokker F28MK0100 · Fuselage Main, Longeron/StringerSDR USAA950941Fitting · crackedPIT - DURING Q-1 INSPECTION, FOUND .5 INCH CRACK BETWEEN STATION 8305 AND STATION 8805 AT STRINGER NR 2 FITTING. INSTALLED DOUBLER ANGLE PER SRM 53-00-02. (M)Jul 31, 1995 · N857US · Fokker F28MK0100 · Fuselage Miscellaneous StructureSDR USAA950520Spinner · moistureMEM - FLT 0358 - THE CREW RECEIVED AN ENGINE VIBRATION READING FROM THE NR 2 ENGINE. THE CAPTAIN CUT THE ENGINE BACK TO IDLE AND DECLARED AND EMERGENCY. FLIGHT LANDED WITH NO FURTHER INCIDENTS. MAINTENANCE REMOVED THE SPINNER DUE TO THE PRESENCE OF MOISTUREMay 18, 1995 · N857US · Fokker F28MK0100 · Turbine Engine Air Inlet Section
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