N886US, cancelled Jun 19, 2013

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 = 'N886US' AND deregistration_id = 'N886US-2013-06-19'
  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 USAAF01031Battery Pack · dischargedRDU - THE AFT CABIN AND LAVATORY EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE BATTERY IN THE AFT EMERGENCY LIGHTS BATTERY PACK. OPS CHECKED OK. (M)May 31, 2001 · N886US · Fokker F28MK0100 · Emergency LightingSDR USAAF01025Battery Pack · corrodedRDU - THE AFT LAVATORY AREA EMERGENCY LIGHTS WERE FOUND INOPERATIVE. MAINTENANCE CLEANED CORROSION FROM BATTERY PACK CONTACTS IN NR 8 EMERGENCY POWER SUPPLY. OPERATIONALLY CHECKED OK. (M)May 15, 2001 · N886US · Fokker F28MK0100 · Emergency LightingSDR USAAF01012Wire · brokenRDU - THE RIGHT SERVICE DOOR EXIT LIGHT WAS INOPERATIVE IN STANDBY AND EMEGENCY LIGHTING. MAINTENANCE REPAIRED TWO BROKEN WIRES ON THE BACK OF THE EXIT LIGHT ASSEMBLY. OPERATIONALLY CHECKED OK. (M)Mar 26, 2001 · N886US · Fokker F28MK0100 · Light System WiringSDR USAAF00036Unknown · odorTYS-CLT - FLT 1731 - BURNING SMELL NOTED BY F/O, FLIGHT ATTENDANTS AND CAPTAIN DURING CLIMB-OUT. SMELL DIMINISHED CLIMBIN THROUGH 10,000, BUT STILL NOTICEABLE IN CRUISE FLIGHT. MAINTENANCE GROUND RAN ENGINES AT HIGH AND COULD NOT SMELL BURNING SMELL. GROUNDMay 8, 2000 · N886US · Fokker F28MK0100 · Air Distribution SystemSDR USAAF99041Battery Pack · dischargedCLT - FOUND THE NR 8 EMERGENCY BATTERY PACK INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK. (M)Aug 23, 1999 · N886US · Fokker F28MK0100 · Emergency LightingSDR USAAF98071Warning System · activatedPIT - FLT 274 - EN ROUTE LGA-SDF, CREW RECEIVED THREE CHIME WARNING FROM THE MFDU AND NOTED THAT THE CABIN ALTITUDE WAS CLIMBING THROUGH 10,000 FT. CREW PERFORMED AN EMERGENCY DESCENT. THE FLIGHT DIVERTED TO PIT AND LANDED WITH NO FURTHER INCIDENT. (M)Aug 20, 1998 · N886US · Fokker F28MK0100 · Central WarningSDR USAAF98065Detector · malfunctionedTYS - FLT 1633 - ON APPROACH TO TYS DESCENDING THROUGH 4000 FEET, WHEN SPEEDBRAKES WERE DEPLOYED THE APU FIRE WARNING ANNUNCIATED. THE APU AUTOMATICALLY SHUT DOWN AND THE FIRE BOTTLE DISCHARGED. THE APU WAS BEING RUN BECAUSE THE NR 1 GENERATOR WAS ON MEL. FAug 4, 1998 · N886US · Fokker F28MK0100 · Fire DetectionSDR 98ZZZM607Gcu · failedTYS - FLT 1633 - ON APPROACH TO TYS DESCENDING THROUGH 4000 FEET, WHEN SPEEDBRAKES WERE DEPLOYED THE APU FIRE WARNING ANNUNCIATED. THE APU AUTOMATICALLY SHUT DOWN AND THE FIRE BOTTLE DISCHARGED. THE APU WAS BEING RUN BECAUSE THE NR 1 GENERATOR WAS ON MEL. FAug 4, 1998 · N886US · Fokker F28MK0100 · AC Generation SystemSDR 98ZZZM606Idg · failedTYS - FLT 1633 - ON APPROACH TO TYS DESCENDING THROUGH 4000 FEET, WHEN SPEEDBRAKES WERE DEPLOYED THE APU FIRE WARNING ANNUNCIATED. THE APU AUTOMATICALLY SHUT DOWN AND THE FIRE BOTTLE DISCHARGED. THE APU WAS BEING RUN BECAUSE THE NR 1 GENERATOR WAS ON MEL. FAug 4, 1998 · N886US · Fokker F28MK0100 · AC Generator-AlternatorSDR USAAF98034Controller · malfunctionedCLT - FLT 1079 - EN ROUTE FROM MDT TO CLT WHILE DESCENDING FROM 350 TO 310, AIRCRAFT EXPERIENCED A LOSS OF CABIN PRESSURE. A RAPID DESCENT TO 10,000 FEET WAS MADE. MASKS DID NOT DROP. FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE NR 1 AUApr 1, 1998 · N886US · Fokker F28MK0100 · Cabin Pressure ControllerSDR USAAF96043Flap Synchro · failedPIT - FL 8075 - DURING DESCENT INTO AVP, THE CREW COULD NOT GET THE FLAPS TO EXTEND. A DECISION WAS MADE TO DIVERT TO PIT WHERE MAINTENANCE IS AVAILABLE TO MAKE REPAIRS. THE CAPTAIN DECLARED AN EMERGENCY FOR PRECAUTIONARY MEASURES. THE FLIGHT LANDED WITHOUTMay 13, 1996 · N886US · Fokker F28MK0100 · Trailing Edge Flap Control SystemSDR USAAF96004AHarness · faultyCLT - AFTER TAKEOFF, CREW RECEIVED GND/FLT FAULT, LIFT DUMPER FAULT, TCAS FAULT AND PROX SW SYS INOP. FLIGHT RETURNED TO CLT AND LANDED WITH NO FURTHER INCIDENT. MAINTENANCE REPLACED THE LEFT MAIN LANDING GEAR HARNESS AND THE SENSOR. (M)Jan 5, 1996 · N886US · Fokker F28MK0100 · Landing Gear Position and WarningSDR USAAF96004Ground Sense · malfunctionedFLT NR 1007 - CLT - THE FLIGHT RETURNED TO FIELD DUE TO A GROUND SENSE PROBLEM. (M)Jan 5, 1996 · N886US · Fokker F28MK0100 · Landing Gear Position and WarningSDR USAAF96003AProx Sensor · out of adjustFLT NR 1488 - RIC - SHORTLY AFTER GEAR RETRACTION THE FOLLOWING ALERTS, 'LD FAULT', 'STAB TRIM CONFIG' AND 'TCAS'. WHEN GEAR EXTENDED, LOUD RELAY CLICKING FOLLOWED BY ALL MESSAGES CLEARING. MAINTENANCE ADJUSTED THE LEFT MAIN GEAR NR 3 PROXIMITY SENSOR AND SWJan 5, 1996 · N886US · Fokker F28MK0100 · Landing Gear Position and WarningSDR USAAF95008Pack · failedFLT NR 689 - PIT - WHILE AT FL 350 THE AIRCRAFT PRESSURIZATION STARTED TO CLIMB TO 10K FEET. THE CAPTAIN REQUESTED DESCENT TO FL 100 AND RECEIVED SAME FROM ATC. THE FLT WAS DIVERTED TO PIT. NO EMERGENCY WAS DECLARED. THE FLT LANDED IN AT PIT WITH NO FURTHEDec 28, 1995 · N886US · Fokker F28MK0100 · Cabin Cooling SystemSDR USAA950024Nut · loosePIT - FLT 1025 - AFTER TAKEOFF, THE CREW GOT A 'HYD SYS 2 LO QTY' ALERT. ACFT RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND PRESSURE LINE 'B' NUT ON UPPER PUMP LOOSE AT QUICK DISCONNECT. MAINTENANCE TIGHTENED FITTING. SERVICED, RAN ENGINJan 19, 1995 · N886US · Fokker F28MK0100 · Hydraulic System, Main
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