N869US, cancelled Jul 9, 2003

Service difficulty reports · 17

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 = 'N869US' AND deregistration_id = 'N869US-2003-07-09'
  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 USAAF01006Inverter · inoperativeIND - MAIN ENTRANCE DOOR, SERVICE DOOR AND GALLEY AISLE FLOOR PROXIMITY LIGHTS WERE INOPERATIVE. MAINTENANCE REPLACED INVERTER A AND THE OUTBOARD MARKER LIGHT ASSEMBLY. OPS CHECKED OK. (M)Feb 19, 2001 · N869US · Fokker F28MK0100 · Emergency LightingSDR USAAF00078Relay · failedCMH-PIT - FLT 2004 - DURING FLIGHT, AN ELECTRIC ODOR WAS NOTICED THROUGHOUT AIRCRAFT. THE ODOR THEN DISSIPATED AFTER TEN MINUTES. FLIGHT LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED RELAY K0933A. AIRCRAFT AND EQUIPMENT COOLING FAN OPS CHECKED OK. (M)Oct 27, 2000 · N869US · Fokker F28MK0100 · Air Distribution SystemSDR USAAF00027Girt Bar · damagedRIC - FOUND THE FORWARD SERVICE DOOR WILL NOT ARM PROPERLY. MAINTENANCE FOUND ARMING MECHANICAL LINKAGE BOUND AT DOOR OPEN/CLOSING HANDLE INTERFACE POINT. FREED LINKAGE AT INTERFACE/STICKING POINT. DOOR OPS CHECKED OK. (M)Mar 25, 2000 · N869US · Fokker F28MK0100 · Escape SlideSDR USAAF00014Uplock Bracket · looseCLT-PIT - FLT 1422 - DURING APPROACH, LANDING GEAR WAS SELECTED TO EXTEND. ALL LANDING GEAR INDICATED DOWN AND LOCKED, HOWEVER, THE RT MAIN GEAR DOOR INDICATED NOT CLOSED. GEAR WAS RECYCLED WITH THE SAME RESULT. THE APPROPRIATE HYDRAULIC SYSTEM WAS SHUTDOWNFeb 14, 2000 · N869US · Fokker F28MK0100 · Landing Gear Retraction/Extension SystemSDR USAAF98061Slide · malfunctionedPIT - DURING AN ANNUAL ESCAPE SLIDE OPERATIONAL CHECK SAMPLING PROGRAM, THE FORWARD ENTRY DOOR ESCAPE SLIDE DID NOT FULLY INFLATE. ACCORDING TO THE INSPECTOR THAT WITNESSED THE DEPLOYMENT, THE SLIDE INITIALLY WAS HUNG UP IN THE DOORWAY. WHEN THE MANUAL HANDLJul 19, 1998 · N869US · Fokker F28MK0100 · Escape SlideSDR USAAF98056Engine · failedPIT - FLT 8079 - EN ROUTE TO PHL AT FL33 AND ON DESCENT TO FL29, AS N1 CAME BACK THROUGH 50 PERCENT, NR 1 ENGINE VIBRATION INDICATION WENT TO TOP OF ORANGE BAND. THE VIBRATION WAS FELT IN THE COCKPIT FLOOR AND THROTTLE QUADRANT. ALSO, AN AUDIBLE RUMBLE WAS HJul 18, 1998 · N869US · Fokker F28MK0100 · Engine (Turbine/Turboprop)SDR USAA970257Angle · crackedPIT - DURING Q-1 CHECK, FOUND CRACK IN RADIUS AT FUSELAGE CTR PRESS BULKHEAD ANGLE, LT SIDE, STA 14911, STR 11. INSTALLED DOUBLER REPAIR PER US AIRWAYS EA NR 47506. (X)Aug 6, 1997 · N869US · Fokker F28MK0100 · Fuselage Miscellaneous StructureSDR USAA970256Skin · delaminatedPIT - DURING Q-1 CHECK, FOUND SKIN DELAMINATION 14.50 INCHES BY 3.50 INCHES IN SKIN AT STA 14011 TO STA 14611 STR 22 AND STR 23, RIGHT SIDE. INSTALLED EXTERNAL DOUBLER 20 INCHES BY 10.25 INCHES PER US AIRWAYS EA NR 29764A. (X)Aug 6, 1997 · N869US · Fokker F28MK0100 · Fuselage Main, Plate/SkinSDR USAAF96086Efis · failedGSP-LGA - FLT 926 - DURING CLIMB-OUT OF GSP, NR 1 NAV DISPLAY LOCKED UP. CAPTAIN WAS UNABLE TO SWITCH TO ROSE OF SELECT HEADING. FLIGHT DIVERTED TO CLT. NO EMERGENCY DECLARED AND FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED LEFT EFIS CONTROAug 5, 1996 · N869US · Fokker F28MK0100 · Integrated Flight SystemSDR USAAF96084Squat Sw · failedFLT 1025 - PIT-ABE - AFTER TAKEOFF, PILOT TRIED TO RAISE GEAR. RECEIVED GRD/FTL CONTROLS, TCAS, AND LIFT DUMPER MESSAGES. RETURNED TO FIELD. MAINTENANCE REPLACED LEFT INBOARD GND/FLT SENSOR. CYCLED GEAR SEVERAL TIMES. ALL CHECKS NORMAL. (M)Aug 1, 1996 · N869US · Fokker F28MK0100 · Landing Gear Position and WarningSDR USAAF96063Prsov · failedPIT - FLT 2049 - CLIMBING THROUGH 12,000 FEET, CREW NOTICED A NOISE FROM LEFT PACK, AFTER WHICH THE OUTPUT TEMPERATURE ROSE TO 150 DEGREES. RIGHT PACK TEMPERATURE WAS RUNNING HOT BUT COOLED WHEN ENGINE POWER WAS REDUCED ON DESCENT. CABIN BECAME VERY WARM. FJun 21, 1996 · N869US · Fokker F28MK0100 · Cabin Pressure Control SystemSDR USAAF96051Door Seal · failedPHL - FLT 328 - CREW LOST PRESSURIZATION AT 33,OOO FEET. CREW DESCENDED TO 10,000 FEET. FLIGHT LANDED WITH NO FURTHER INCIDENT. MAINTENANCE FOUND THE FORWARD CARGO DOOR SEAL LEAKING. THE DOOR SEAL WAS REPLACED. AIRCRAFT WAS PRESSURIZED WITH LEAK RATE CHECMay 22, 1996 · N869US · Fokker F28MK0100 · Cargo/Baggage DoorsSDR USAAF96023AHeat Shield · bentFLT NR 1543 - CLT - ON TAKEOFF FROM RDU RWY 23R, CAPTAIN HAD GEAR FAULT MESSAGE, RDU TOWER TOLD HIM IT LOOKED LIKE SOMETHING FELL OFF THE AIRCRAFT. WHILE THE FLIGHT HELD IN THE AIR OVER RDU, THEY FOUND THE NR 2 MAIN WHEEL ASSEMBLY. FLIGHT PROCEEDED TO CLT. Feb 22, 1996 · N869US · Fokker F28MK0100 · Landing Gear Brake SystemSDR USAAF96023Wheel · departedCLT - FLT 1543 - ON TAKEOFF FROM RDU RWY 23R, CAPT HAD GEAR FAULT MESSAGE, RDU TOWER TOLD HIM IT LOOKED LIKE SOMETHING FELL OFF THE AIRCRAFT. WHILE THE FLT HELD IN THE AIR OVER RDU, THEY FOUND THE NR 2 MAIN WHEEL ASSY. FLT PROCEEDED TO CLT. CORRECTIVE ACTIOFeb 22, 1996 · N869US · Fokker F28MK0100 · Wheel/Ski/FloatSDR USAA950445Windshield · crackedPIT - FLIGHT NR 0403 - ON CLIMB-OUT, A CRACK DEVELOPED IN THE CAPTAINS WINDSHIELD. FLIGHT RETURNED TO PIT WITHOUT INCIDENT. (M)May 4, 1995 · N869US · Fokker F28MK0100 · Flight Compartment WindowsSDR USAA950224Unsafe Light · illuminatedBUF - FLT 0873 - AFTER TAKEOFF, THE RIGHT MAIN LANDING GEAR UNSAFE LIGHT ILLUMINATED WHEN THE GEAR WAS RETRACTED. THE GEAR WAS RECYCLED TWICE WITH THE SAME RESULTS. CREW RETURNED TO BUF WITHOUT INCIDENT. MAINTENANCE INSPECTED THE GEAR AND FOUND HEAVY ICE. Feb 24, 1995 · N869US · Fokker F28MK0100 · Landing Gear Position and WarningSDR USAA950039Retract Mech · iced upPIT - FLT 977 - ON TAKEOFF, THE CREW GOT A RT MAIN LANDING GEAR WARNING ON THE MFDU. GEAR WAS RECYCLED BUT THE WARNING REMAINED. ACFT RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED A LARGE AMOUNT OF ICE AND SAND FROM THE MLG. OPERATION Jan 23, 1995 · N869US · Fokker F28MK0100 · Landing Gear Retraction/Extension System
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