N897US, cancelled Jan 17, 2018

Service difficulty reports · 20

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 = 'N897US' AND deregistration_id = 'N897US-2018-01-17'
  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 USAAF01061Fire Detector · malfunctionedTRI - FLT 896 - EN ROUTE PIT-CLT, AT FL310, RECEIVED AN APU FIRE WARNING. THE FIRE EXTINGUISHING SYSTEM AUTOMATICALLY DISCHARGED. THE FLIGHT DIVERTED TO TRI AND LANDED SAFELY. MAINTENANCE INSPECTED THE APU ENCLOSURE AND THE TAIL COMPARTMENT. NO SIGNS OF A Jul 30, 2001 · N897US · Fokker F28MK0100 · Fire DetectionSDR USAAF01051Extinguisher · dischargedCLT-IND - FLT 476 - THE WATER FIRE EXTINGUISHER DISCHARGED INTO THE LAVATORY TRASH BIN IN FLIGHT. NO SMOKE OR FIRE WAS DETECTED. THE FLIGHT LANDED WITHOUT INCIDENT IN IND. MAINTENANCE REPLACED THE WATER BOTTLE EXTINGUISHER. OK FOR SERVICE. (M)Jul 24, 2001 · N897US · Fokker F28MK0100 · Fire Protection SystemSDR USAAF01048Odor · detectedSTL-CLT - FLT 1249 - THE LAVATORY SMOKE ALARM BEGAN TO CHIME AND AN ODOR OF SMOKE WAS PRESENT IN THE AFT CABIN AREA DURING CLIMB. THE FLIGHT RETURNED TO FIELD IN STL AND LANDED WITHOUT INCIDENT. MAINTENANCE RAN ENGINES AND APU. NO ODOR WAS DETECTED. THE TAJul 17, 2001 · N897US · Fokker F28MK0100 · Air Distribution SystemSDR USAAF01049Timer · malfunctionedSTL-PIT - FLT 9281 - SLIGHT FUMES WERE NOTICED COMING FROM BOTH LAVATORIES, AND SMOKE DETECTORS ACTIVATED FOR A BRIEF TIME DURING CRUISE FLIGHT. FLIGHT LANDED IN PIT WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED LEFT AND RIGHT LAVATORY FAUCET TIMERS. LEAK Jul 17, 2001 · N897US · Fokker F28MK0100 · Potable Water SystemSDR USAAF00069Strut · dischargedPIT-BNA - FLT 1532 - THE NOSE LANDING GEAR FAILED TO COME DOWN DURING APPROACH. RECEIVED A GEAR UNSAFE WARNING. THE FLIGHT PERFORMED A GO-AROUND AND CYCLED THE LANDING GEAR AGAIN. THE LANDING GEAR THEN OPERATED NORMALLY AND THREE GREEN LANDING GEAR INDICATISep 15, 2000 · N897US · Fokker F28MK0100 · Nose/Tail Landing Gear Strut/AxleSDR USAAF00043Brake Assy · malfunctionedCMH-PHL - FLT 835 - ON LANDING ROLL, EXCESSIVE BRAKE PRESSURE REQUIRED TO STOP AIRCRAFT ON CAPTAINS SIDE. FIRST OFFICERS BRAKES SEEM NORMAL AT TAXI SPEED. MAINTENANCE INSPECTED PEDAL TORQUE TUBES, SPRINGS, AND ROD ENDS. OPERATIONALLY CHECKED BRAKES. LUBED Jun 4, 2000 · N897US · Fokker F28MK0100 · Landing Gear Brake SystemSDR USAAF00040Brake · malfunctionedBHM-CLT - FLT 1511 - DURING ROLL OUT, MUCH MORE THAN NORMAL BRAKE PEDAL FORCE SEEMED TO BE REQUIRED FOR NORMAL BRAKING EFFORT. MAINTENANCE BLED NR 3 AND NR 4 BRAKE ASSEMBLIES. LEAK AND OPS CHECKS OK. (M)Jun 1, 2000 · N897US · Fokker F28MK0100 · BrakeSDR USAAF00034Spring · brokenCLT - FOUND SERVICE DOOR GIRT BAR SLIDER HAS BROKEN SPRING. MAINTENANCE REPLACED THE SPRING IN SLIDER. CHECKS NORMAL. (M)May 3, 2000 · N897US · Fokker F28MK0100 · Escape SlideSDR USAA991233Fitting · crackedPIT - DURING RON VISIT, FOUND 1.125 INCH CRACK IN T-FITTING (W/O JOGGLE) AT BOTTOM END OF T-FITTING AFT SIDE APBH BL 1027L. STOP DRILLED CRACK PER CD. REINSTALLED BLIND FASTENERS PER CD 53F00703. (M)Nov 1, 1999 · N897US · Fokker F28MK0100 · Fuselage Miscellaneous StructureSDR USAAF99048Battery Pack · dischargedGSO - EMERGENCY LIGHT STRIP NEAR CENTER EXIT INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK. (M)Sep 28, 1999 · N897US · Fokker F28MK0100 · Emergency LightingSDR USAAF99044Battery Pack · dischargedIND - FOUND FLOOR EMERGENCY LIGHTS INOPERATIVE FROM ROW 12 THROUGH 17. MAINTENANCE REPLACED THE NR 7 BATTERY PACK. (M)Sep 13, 1999 · N897US · Fokker F28MK0100 · Emergency LightingSDR USAAF99012Window · crackedCLT - FLT 8076 - EN ROUTE TO CLT AT FL240, THE OUTER PANE OF THE LEFT COCKPIT SLIDING WINDOW CRACKED. FLIGHT WAS A NON-REVENUE FERRY FLIGHT. AIRCRAFT LANDED CLT WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE LEFT SLIDING WINDOW. (M)Mar 13, 1999 · N897US · Fokker F28MK0100 · Flight Compartment WindowsSDR USAAF00003Anti-Skid System · malfunctionedCLT-BHM - FLT 1252 - ON TAXI OUT FOR TAKEOFF, WHEN BRAKES WERE APPLIED (20 KNOTS), ANTI-SKID WOULD RELEASED BRAKES, MAKING IT HARD TO SLOW DOWN. MAINTENANCE ACTION PENDING. AIRCRAFT WAS RELEASED ON MEL. (M)Jan 7, 1999 · N897US · Fokker F28MK0100 · Brake Anti-Skid SectionSDR USAAF98093Bulb · failedCRW - FLT 435 - ON APPROACH TO CRW WHEN LANDING GEAR WAS SELECTED DOWN, THERE WAS NO GEAR DOWN AND SAFE INDICATION. CREW RECYCLED LANDING GEAR BUT THERE WAS STILL NO GEAR SAFE INDICATION. PROBLEM APPEARED TO BE AN INDICATION PROBLEM. CAPTAIN DID NOT DECLARENov 30, 1998 · N897US · Fokker F28MK0100 · Landing Gear Position and WarningSDR USAAF98066Battery Pack · dischargedGSO - FORWARD EMERGENCY LIGHTS WEAK. MAINTENANCE REPLACED THE BATTERY PACK. (M)Aug 2, 1998 · N897US · Fokker F28MK0100 · Emergency LightingSDR USAAF96026Bulb · failedFLT 578 - CLT - RIGHT MAIN GEAR FAILED TO INDICATE DOWN AND GREEN. RECYCLED GEAR, CHANGED BULBS WITH NO CHANGE. LANDED NORMALLY, TAXIED WITH GEAR PINNED. PERFORMED BITE USING THE PSEU WITH NO DEFECTIVE SWITCHES OR TARGETS. INSPECTED INDICATION PACK ON FORWFeb 25, 1996 · N897US · Fokker F28MK0100 · Landing Gear Position and WarningSDR USAA950451Lines · uninstalledPIT - FLT 8554 - DURING TAKEOFF AT ROTATION, THE AC LOST ALL INSTRUMENTATION. THE CAPTAIN DECLARED AN EMERGENCY AND RETURNED TO PIT. MAINTENANCE REINSTALLED THE PITOT AND STATIC LINES. OPERATIONS CHECKED GOOD. (W)May 6, 1995 · N897US · Fokker F28MK0100 · Pitot/Static SystemSDR USAA950580Stringer · crackedPIT - DURING SCHEDULED INSPECTION OF USAIR CD 53F00762 HFEC INSPECTION OF STRINGERS NR 6, 7, 68 AFT OF FRAME STATION 3870, FOUND .5 INCH CRACK (RADICAL) AT STRINGER NR 68 RT SIDE FRAME 3870. INSTALLED SPLICE REPAIR TO STRINGER 68 RT SIDE AFT OF FRAME STATION May 5, 1995 · N897US · Fokker F28MK0100 · Fuselage Main, Longeron/StringerSDR USAA950579Stringer · crackedPIT - DURING SCHEDULED INSPECTION USAIR PCI 289 CD 53F00762, FOUND A .5 INCH CRACK IN STRINGER 68 RT SIDE AFT OF FRAME 3870. INSTALLED SPLICE REPAIR TO STRINGER 68 PER SRM 51-70-06. (M)May 5, 1995 · N897US · Fokker F28MK0100 · Fuselage Main, Longeron/StringerSDR USAA950232Pump · inoperativePIT - FLT 0141 - THE R1 FUEL BOOST PUMP FAULT LIGHT ILLUMINATED IN-FLIGHT. FLIGHT DIVERTED TO PIT AND LANDED WITHOUT INCIDENT. MAINTEANCE REPLACED THE R1 AND R2 BOOST PUMPS AND COCKPIT OVERHEAD PANEL. OPERATIONS CHECKED GOOD. (X)Mar 13, 1995 · N897US · Fokker F28MK0100 · Fuel Boost Pump
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