N856US, cancelled Jul 18, 2003

Service difficulty reports · 29

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 = 'N856US' AND deregistration_id = 'N856US-2003-07-18'
  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 USAAF00076Slide · inoperativeGSO - FOUND THE FORWARD GALLEY SERVICE DOOR EMERGENCY EVACUATION SLIDE HAD LOW PRESSURE. MAINTENANCE REPLACED THE FORWARD GALLEY SERVICE DOOR EMERGENCY EVACUATION SLIDE. OK FOR SERVICE. (M)Oct 26, 2000 · N856US · Fokker F28MK0100 · Escape SlideSDR USAAF00058Battery Pack · dischargedPIT - FOUND THE EMERGENCY EXIT LIGHTS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED A BATTERY PACK. OK FOR SERVICE. (M)Aug 4, 2000 · N856US · Fokker F28MK0100 · Emergency LightingSDR USAAF00049Control Valve · out of adjATL-PIT - FLT 545 - FULL BRAKE PEDAL APPLICATION REQUIRED TO RECEIVE MINIMAL BRAKING ACTION. MAINTENANCE BLED THE BRAKES AND ADJUSTED THE RIGHT NORMAL BRAKE CONTROL VALVE. TAXI CHECKS OK. (M)Jun 28, 2000 · N856US · Fokker F28MK0100 · Landing Gear Brake SystemSDR USAAF00045Fire Loop · failedIND-DCA - FLT 1212 - ON CLIMB-OUT, NR 2 ENGINE FIRE WARNING ILLUMINATED AT FL 100. THE NR 2 ENGINE WAS SHUTDOWN AND BOTH FIRE EXTINGUISHING BOTTLES WERE FIRED. FLIGHT RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. TOTAL SINGLE ENGINE TIME WAS 8 MINUTES. MAJun 8, 2000 · N856US · Fokker F28MK0100 · Fire DetectionSDR USAAF00032Slide · dischargedPHL - FOUND SLIDE PACK ON DOOR 1L APPEARING TO BE LOW. MAINTENANCE REPLACED FORWARD LEFT ENTRY DOOR ESCAPE SLIDE. CHECKS GOOD. (M)Apr 24, 2000 · N856US · Fokker F28MK0100 · Escape SlideSDR USAAF99046Power Supply · inoperativeIND - FOUND AFT SECTION OF LOW LEVEL EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK AND POWER SUPPLY. (M)Sep 19, 1999 · N856US · Fokker F28MK0100 · Emergency LightingSDR USAAF99021Door · crackedCLT - FLT 2276 - AFTER TAKEOFF FROM CLT, THE LEFT AND RIGHT MAIN LANDING GEAR WOULD NOT RETRACT. FLIGHT RETURNED TO CLT AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND THE RIGHT MAIN LANDING GEAR DOOR CRACKED. THE DOOR WAS REMOVED AND THE AIRCRAFT OPApr 3, 1999 · N856US · Fokker F28MK0100 · Landing Gear Door Retract SectionSDR USAAF99019Valve · failedCLT - FLIGHT 861 - AFTER TAKEOFF FROM CLT, A BLEED NR 2 DUCT FAULT OCCURRED. THE FLIGHT RETURNED TO CLT AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE APU CHECK VALVE AND THE OPSOV SEALS. THEY ALSO PERFORMED A BLEED SYSTEM BALANCING ADJUSTMENApr 2, 1999 · N856US · Fokker F28MK0100 · Pneumatic Distribution SystemSDR 99ZZZM263Seal · failedCLT - FLIGHT 861 - AFTER TAKEOFF FROM CLT, A BLEED NR 2 DUCT FAULT OCCURRED. THE FLIGHT RETURNED TO CLT AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE APU CHECK VALVE AND THE OPSOV SEALS. THEY ALSO PERFORMED A BLEED SYSTEM BALANCING ADJUSTMENApr 2, 1999 · N856US · Fokker F28MK0100 · Pneumatic Distribution SystemSDR USAAF98067Battery Pack · dischargedIND - FORWARD ENTRY DOOR EXIT SIGN INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK. (M)Aug 11, 1998 · N856US · Fokker F28MK0100 · Emergency LightingSDR USAAF97100Fuel Pump · failedFLT 1283 - PHL-MSP - TEN MINUTES AFTER DEPARTURE FROM PHL THE NR 1 CENTER FUEL TANK BOOST PUMP FAILED. THE CAPTAIN SWITCHED TO CENTER CROSSFEED BUT IT DID NOT OPERATE. IN THE VICINITY OF DTW THERE WAS A 700 POUND FUEL IMBALANCE. CAPTAIN ELECTED TO DIVERT THDec 8, 1997 · N856US · Fokker F28MK0100 · Fuel Boost PumpSDR USAAF97069Idg Generator · failedFLT 245 - CLT-DTW - WHILE EN ROUTE TO DTW, THE APU SHUT DOWN DUE TO A LOW OIL PRESSURE WARNING. THE NR 2 IDG WAS ON MEL. THE CREW ELECTED TO DIVERT TO PIT FOR MAINTENANCE. THE FLIGHT LANDED PIT WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE NR 2 IDG. Aug 11, 1997 · N856US · Fokker F28MK0100 · AC Generator-AlternatorSDR USAAF97032Breaker · trippedBUF - EMERGENCY EXIT SIGN LIGHTS DO NOT COME ON AFTER GEAR EXTENSION. MAINTENANCE RESET BREAKER FOR RELAY K2618A. OPERATIONAL CHECKED GOOD. (M)Mar 24, 1997 · N856US · Fokker F28MK0100 · Emergency LightingSDR USAAF96080Indicator Module · malfunctionedFLT NR 503 - CLT-DAY - LEFT MAIN GEAR GREEN LIGHT REMAINS ON WITH GEAR RETRACTED. RETURNED TO FIELD. MAINTENANCE REPLACED THE LANDING GEAR INDICATOR MODULE. (M)Jul 21, 1996 · N856US · Fokker F28MK0100 · Landing Gear Position and WarningSDR USAAF96014Sequencing Vlv · failedCHS - AFTER TAKEOFF, CREW WOULD NOT GET THE MAIN GEAR TO RETRACT. THE GEAR WAS CYCLED TWICE. FLIGHT RETURNED TO CHS AND LANDED WITH NO FURTHER INCIDENT. AIRCRAFT FERRIED TO CLT FOR REPAIR. MAINTENANCE REPLACED THE RIGHT GEAR DOOR SEQUENCING 'A' VALVE. GEAJan 24, 1996 · N856US · Fokker F28MK0100 · Landing Gear Door Retract SectionSDR USAA960005Floor Beam · corrodedPIT - DURING Q-1 INSPECTION, FOUND CORROSION .005 INCH TO .053 INCH ON FLOOR BEAM AT STATION 1127R FWD OF FRAME 4850. REPLACED SECTION OF BEAM FROM STATION 4850 TO 5305 PER SRM 53-21-10. (M)Jan 3, 1996 · N856US · Fokker F28MK0100 · Fuselage Main, Floor BeamSDR USAA960003Skin · delaminationPIT - DURING Q-1 INSPECTION, FOUND SKIN DELAMINATION LEFT STUB WING TO FUSELAGE AT STATION 24011 TO 26011. INSTALLED DOUBLER REPAIR PER USAIR EA NR 29492B AND EA NR 31703. (M)Jan 3, 1996 · N856US · Fokker F28MK0100 · Nacelle/Pylon, Plate/SkinSDR USAA960002Skin · lightning strikePIT - DURING Q-1 INSPECTION, FOUND LIGHTNING STRIKE DAMAGE ABOVE CO-PILOTS SLIDING WINDOW IN FUSELAGE SKIN PITTED. INSTALLED FLUSH REPAIR PER USIAR EA NR 31049. (M)Jan 3, 1996 · N856US · Fokker F28MK0100 · Fuselage Main, Plate/SkinSDR USAA960001Floor Beam · corrodedPIT - DURING Q-1 INSPECTION, FOUND CORROSION ON FLOOR BEAM BLO AT STATION 3845 T-CAP. REMOVED SECTION OF CORRODED T-CAP FROM STATION 3845 TO 5315 AND SPLICED IN NEW SECTION PER SRM 53-21-10. (M)Jan 3, 1996 · N856US · Fokker F28MK0100 · Fuselage Main, Floor BeamSDR USAA960000Skin · delaminationPIT - DURING Q-1 INSPECTION, FOUND SKIN DELAMINATION RIGHT STUB WING TO FUSELAGE AT STATION 24011-26011. INSTALLED DOUBLER REPAIR PER USAIR EA NR 29492B AND EA NR 31703. (M)Jan 3, 1996 · N856US · Fokker F28MK0100 · Nacelle/Pylon, Plate/SkinSDR USAA951355Stringer · corrosionPIT - Q1/C2 INSPECTION, FOUND CORROSION ON STRINGER NR 3 STATION 11257. SPLICED IN NEW SECTION OF STRINGER PER SRM 51-70-06 REPAIR NR 5. (M)Dec 27, 1995 · N856US · Fokker F28MK0100 · Fuselage Main, Longeron/StringerSDR USAA951354Stringer · corrodedPIT - Q1/C2 INSPECTION, FOUND CORROSION ON STRINGER NR 3 AT STATION 12791 TO STATION 13851. SPLICED IN NEW SECTION OF STRINGER NR 3 PER SRM 51-70-06 REPAIR NR 5. (M)Dec 27, 1995 · N856US · Fokker F28MK0100 · Fuselage Main, Longeron/StringerSDR USAA950409Fuel Vent Valve · failedDCA - FLT 200 - ON TAKEOFF, TOWER ADVISED FLIGHT THAT FUEL WAS BEING SIPHONED OUT OF WING. FLIGHT RETURNED TO DCA WHERE LANDING WAS WITHOUT INCIDENT. MAINTENANCE REPLACED LT O/B FUEL VENT VALVE. NO LEAKS NOTED. (Z)Apr 25, 1995 · N856US · Fokker F28MK0100 · Aircraft Fuel Distribution SystemSDR USAA950201Prsov · malfunctionedPHL - FLT 0244 - CABIN PRESSURE CONTINUED TO CLIMB AT FL 330. CREW DECLARED AN EMERGENCY TO GET LOWER PRESSURE. FLIGHT LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED TO RIGHT PRSOV AND THE RIGHT PACK FLOW VALVE. OPERATIONS CHECKED GOOD. REFERENCE 95ZZZZ155Mar 1, 1995 · N856US · Fokker F28MK0100 · Cabin Pressure Control SystemSDR 95ZZZZ155Valve · inoperativePHL - FLT 0244 - CABIN PRESSURE CONTINUED TO CLIMB AT FL 330. CREW DECLARED AN EMERGENCY TO GET LOWER PRESSURE. FLIGHT LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED TO RIGHT PRSOV AND THE RIGHT PACK FLOW VALVE. OPERATIONS CHECKED GOOD. REFERENCE USAA95020Mar 1, 1995 · N856US · Fokker F28MK0100 · Cabin Pressure Control SystemSDR USAA950211Valve · inoperativeTPA - FLT 8003 - THE GEAR WOULD NOT RETRACT AFTER TAKEOFF. CREW TRIED TO RECYCLE GEAR. GEAR REMAINED EXTENDED AND CREW RETURNED TO TPA. MAINTENANCE REPLACED THE RIGHT MAIN LANDING GEAR DOOR VALVE. (Z)Feb 26, 1995 · N856US · Fokker F28MK0100 · Landing Gear Door Retract SectionSDR USAA950218Switch · intermittentCLT - FLT 2188 - AIRCRAFT LOST PRESSURIZATION AT FL 330 AND CABIN ALTITUDE WAS INCREASING. FLIGHT DIVERTED TO CLT AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE RIGHT ENGINE CHANGE OVER SWITCH AND CARGO DOOR SEALS AND ADJUSTED THE LEFT ENGINE CHANGE OFeb 23, 1995 · N856US · Fokker F28MK0100 · Cabin Pressure Control SystemSDR 95ZZZZ154Seals · leakingCLT - FLT 2188 - AIRCRAFT LOST PRESSURIZATION AT FL 330 AND CABIN ALTITUDE WAS INCREASING. FLIGHT DIVERTED TO CLT AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE RIGHT ENGINE CHANGE OVER SWITCH AND CARGO DOOR SEALS AND ADJUSTED THE LEFT ENGINE CHANGE OFeb 23, 1995 · N856US · Fokker F28MK0100 · Cargo/Baggage DoorsSDR USAA950149Valve · stickingPIT - FLT 428 - AT FL 330 GOT EXCESSIVE CABIN ALTITUDE MESSAGE. CABIN WAS APPROACHING 11,000 FEET. CREW DID EMERGENCY DESCENT IAW PROCEDURES. ALSO, TRIED MANUAL PRESSURIZATION BUT HAD NO RESPONSE. ACFT DIVERTED AND LANDED WITHOUT INCIDENT. MAINTENANCE PREFeb 20, 1995 · N856US · Fokker F28MK0100 · Pressure Regulator/Outflow Valve
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