N859US, cancelled Mar 25, 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 = 'N859US' AND deregistration_id = 'N859US-2003-03-25'
  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 USAAF01080Battery · dischargedCLT - THE EMERGENCY FLOOR LIGHTS WERE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERIES. (M)Nov 1, 2001 · N859US · Fokker F28MK0100 · Emergency LightingSDR USAAF01058Battery Pack · inoperativeGSO - THE EMERGENCY MARKER LIGHTS IN THE ENTRY AREA WOULD NOT ILLUMINATE. MAINTENANCE REPLACED THE NR 1 BATTERY PACK. OPERATIONALLY CHECKED OK. (M)Jul 28, 2001 · N859US · Fokker F28MK0100 · Emergency LightingSDR USAAF00072Downlock Switch · failedSTL-CLT - FLT 1276 - THE LEFT LANDING GEAR LIGHT STAYS GREN WITH GEAR UP. THE FLIGHT LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE LEFT LANDING GEAR PRIMARY DOWN LOCK SWITCH. OPS CHECK NORMAL. (M)Sep 30, 2000 · N859US · Fokker F28MK0100 · Landing Gear Position and WarningSDR USAAF00055Engine · malfunctionedLEX-PIT - FLT 280 - THE NR 2 ENGINE WAS SHUTDOWN, APPROX 66 MILES FROM PIT, DUE TO SEVERE VIBRATION. ENCOUNTERED MODERATE RAIN AND ENGINE ANTI-ICE WAS IN USE DURING THE VIBRATION EVENT. QRH PROCEDURES WERE ACCOMPLISHED, AN EMERGENCY DECLARED, AND AN UNEVENTFJul 29, 2000 · N859US · Fokker F28MK0100 · Engine (Turbine/Turboprop)SDR USAAF99042Power Supply · inoperativeRDU - FOUND FORWARD FLOOR PROXIMITY LIGHTS AND NR 1 AISLE CEILING LIGHT INOPERATIVE DURING EMERGENCY LIGHT TEST. MAINTENANCE REPLACED THE BATTERY PACK AND SUPPLY UNIT. (M)Aug 28, 1999 · N859US · Fokker F28MK0100 · Emergency LightingSDR USAAF99029Battery Pack · dischargedIND - FOUND FORWARD ENTRY EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERY PACK. (X)May 28, 1999 · N859US · Fokker F28MK0100 · Emergency LightingSDR USAAF99018Air Dist · odorALB - FLT 701 - WHILE CLIMBING THROUGH 2000 FEET, A FLIGHT ATTENDANT INFORMED THE FLIGHT CREW OF A BURNING ODOR IN THE CABIN AROUND LEFT ROW 17. THE CREW DECLRED AN EMERGENCY AND ELECTED TO DIVERT THE FLIGHT TO ALB. ON APPROACH TO ALB, THE DOOR DISSIPATED. Apr 1, 1999 · N859US · Fokker F28MK0100 · Air Distribution SystemSDR USAAF99005Switch · malfunctionedPIT - FLT 1534 - AFTER TAKEOFF FROM PIT, THE AIRCRAFT SUSTAINED A LIGHTNING STRIKE. THE LEFT ENGINE OIL PRESSURE INDICATOR DROPPED TO ZERO AND THE FLIGHT CREW SHUT DOWN THE LEFT ENGINE. THE FLIGHT RETURNED TO PIT AND LANDED WITHOUT FURTHER INCIDENT. SINGLE Jan 17, 1999 · N859US · Fokker F28MK0100 · Engine Oil PressureSDR 99ZZZM156Transmitter · malfunctionedPIT - FLT 1534 - AFTER TAKEOFF FROM PIT, THE AIRCRAFT SUSTAINED A LIGHTNING STRIKE. THE LEFT ENGINE OIL PRESSURE INDICATOR DROPPED TO ZERO AND THE FLIGHT CREW SHUT DOWN THE LEFT ENGINE. THE FLIGHT RETURNED TO PIT AND LANDED WITHOUT FURTHER INCIDENT. SINGLE Jan 17, 1999 · N859US · Fokker F28MK0100 · Engine Oil PressureSDR USAAF97085Power Supply · inoperativeIND - DURING ROUTINE MAINTENANCE VISIT, THE EMERGENCY EXIT LIGHT LOCATED ABOVE THE MAIN ENTRY DOOR WAS FOUND INOPERATIVE. MAINTENANCE REPLACED THE POWER SUPPLY. (M)Oct 28, 1997 · N859US · Fokker F28MK0100 · Emergency LightingSDR USAAF97051Control Unit · failedFLT 854 - CLT-PNS - ON SHORT FINAL APPROACH TO PNS, AT APPROXIMATELY 200 FT, UPON COMPLETION OF APU START, CREW RECEIVED RED 'APU FIRE' WARNING. APU AUTO SHUTDOWN, AND FIRE BOTTLE WAS FIRED. NO EMERGENCY WAS DECLARED. FLIGHT LANDED PNS WITHOUT FURTHER INCIDJun 24, 1997 · N859US · Fokker F28MK0100 · Fire DetectionSDR USAAF97025Radome · damagedMDT - FL 1861 - AFTER TAKEOFF FROM PHL, CREW NOTED BIRD STRIKE ON LEFT SIDE OF NOSE. NO ADVERSE EFFECTS WERE NOTED ON COCKPIT GAUGES. FLIGHT CONTINUED. AT APPROXIMATELY 17,500 FEET, CREW NOTED THAT THE LEFT SIDE OF THE RADOME BEGAN TO COLLAPSE AND THE AIRSPMar 5, 1997 · N859US · Fokker F28MK0100 · Aerodynamic FairingsSDR USAA960612Frame · crackedPIT - DURING Q-1 CHECK, FOUND 3 INCH CRACKS (2 EACH) AND .075 INCH CRACKS (2 EACH) AT FUSELAGE CENTER WING FRONT SPAR FRAME AND ANGLES AT STA 11 (LHS) AND STA 64 (RHS). ROUTED OUT CRACK AREAS IN FRAME AND INSTALLED NEW ANGLES PER EA NR 33430 AND EA NR 32077. Sep 17, 1996 · N859US · Fokker F28MK0100 · Fuselage Main, FrameSDR USAA960611Skin · delaminatedPIT - DURING Q-1 CHECK, FOUND 4 INCH BY 4 INCH DENT/DELAMINATION LT ELEVATOR BETWEEN RIB 215 AND RIB 1265. REPLACED AND REPAIRED DAMAGED SKIN AND HONEYCOMB CORE AND INSTALLED A DOUBLER PER SRM 51-70-03. (X)Sep 17, 1996 · N859US · Fokker F28MK0100 · Elevator, Plate/SkinSDR USAA960610Skin · delaminatedPIT - DURING Q-1 CHECK, FOUND 3 INCH BY 3 INCH DENT/DELAMINATION AT RT ELEVATOR JUST INBOARD OF RIB 1265. REPAIRED AND REPLACED DAMAGED SKIN AND HONEYCOMB CORE AND INSTALLED A DOUBLER PER SRM 51-70-03. (X)Sep 17, 1996 · N859US · Fokker F28MK0100 · Elevator, Plate/SkinSDR USAA951038Fire Warning · activatedCLT - FL 1229, ON APPROACH, CREW RECEIVED APU FIRE WARNING LIGHT AND APU AUTO SHUTDOWN. THE APU FIRE BOTTLE DISCHARGED AUTOMATICALLY. THE APPROACH CONTINUED AND THE FLIGHT LANDED WITH NO FURTHER INCIDENT. NO INDICATION OF FIRE WAS FOUND. MAINTENANCE CHECKESep 27, 1995 · N859US · Fokker F28MK0100 · Fire DetectionSDR USAA950450Sensor · faultyMCO - FLT 0244 - AFTER TAKEOFF, THE CAPTAIN RECEIVED A FLAP DISAGREEMENT LIGHT. THE FLAPS WERE RECYCLED BUT THE INDICATAION STILL REMAINED. MAINTENANCE REPLACED THE FLAP LEVER RVDT. ALL TEST CHECKED GOOD. (M)May 7, 1995 · N859US · Fokker F28MK0100 · Leading Edge Slat Control SystemSDR USAA950408Actuators · failedSRQ-TPA - FLT 2030 - ON TAKEOFF CREW RECEIVED RIGHT LANDING ALERT AFTER GEAR UP SELECTION, GEAR INDICATIONS NORMAL. RECYCLED GEAR SEVERAL TIMES AND DIVERTED FLIGHT TO TPA WHERE LANDING WAS WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED BOTH MAIN LANDING GEARApr 23, 1995 · N859US · Fokker F28MK0100 · Landing Gear ActuatorSDR USAA950359Control Rod · out of adjustMCO - FLT 1203 - FLIGHT RETURNED TO MCO DUE TO GEAR DOOR RETRACT PROBLEM. FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE ADJUSTED THE CONTROL ROD. OPERATIONS CHECKED GOOD. (W)Apr 6, 1995 · N859US · Fokker F28MK0100 · Landing Gear Door Retract Section
Back to N859US, cancelled Mar 25, 2003