N881US, cancelled Jun 3, 2003

Service difficulty reports · 18

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 = 'N881US' AND deregistration_id = 'N881US-2003-06-03'
  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 USAAF01076Actuator · failedPIT-RDU - FLT 280 - AFTER TAKEOFF, THE LEFT MAIN LANDING GEAR WOULD NOT RETRACT. WHEN TRYING TO EXTEND THE LANDING GEAR, THE NOSE GEAR EXTENDED BUT NOT THE MAIN GEAR. THE ALTERNATE GEAR EXTENSION WAS USED TO EXTEND THE GEAR. THE AIRCRAFT RETURNED TO THE FIEOct 7, 2001 · N881US · Fokker F28MK0100 · Landing Gear ActuatorSDR USAAF01034Windshield · crackedCLT-MEM - FLT 865 - THE RIGHT FORWARD WINDSHIELD INNER PANE SHATTERED, AND HAD A LARGE BUBBLE ON THE OUTER PANE DURING FLIGHT. THE FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE FIRST OFFICERS WINDSHIELD. OPERATIONALLY CHECKED OK. (M)Jun 23, 2001 · N881US · Fokker F28MK0100 · Window/Windshield SystemSDR USAAF00084Battery Pack · dischargedRDU - THE CABIN EMERGENCY EXIT LIGHTING FLOOR STRIP WAS INOPERATIVE JUST FORWARD OF THE EMERGENCY EXIT ROW. MAINTENANCE REPLACED THE BATTERY PACK. OPERATIONALLY CHECKED OK. (M)Nov 27, 2000 · N881US · Fokker F28MK0100 · Emergency LightingSDR USAAF00023Sequence Valve · malfunctionedCLT-CMH - FLT 912 - AFTER TAKEOFF, THE NOSE GEAR RETRACTED BUT THE MAIN LANDING GEAR DID NOT. FLIGHT RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE MLG SEQUENCE VALVES. OPS AND LEAK CHECK OK. (M)Mar 9, 2000 · N881US · Fokker F28MK0100 · Landing Gear Retraction/Extension SystemSDR USAAF00022Selector Valve · malfunctionedCLT-CHS - FLT 553 - ON FINAL APPROACH, SELECTED GEAR DOWN AND ONLY RECEIVED NOSE GEAR DOWN INDICATION. A FLYBY OF THE TOWER CONFIRMED THAT ONLY THE NOSE GEAR WAS DOWN AND MLG DOORS WERE OPEN. AFTER A MISSED APPROACH TO DOWNWIND, BOTH MAINS FINALLY EXTENDED. Mar 7, 2000 · N881US · Fokker F28MK0100 · Landing Gear SelectorSDR USAAF00020Light · inoperativeCLE - THE GALLEY SERVICE DOOR EMERGENCY EXIT LIGHT WAS INOPERATIVE. MAINTENANCE REPAIRED A BROKEN WIRE AT THE GALLEY SERVICE DOOR EMERGENCY EXIT LIGHT. (M)Feb 28, 2000 · N881US · Fokker F28MK0100 · Emergency LightingSDR USAAF99060Selector Valve · failedCLT/ROA - FLT 2122 - DURING CLIMB OUT FROM CLT, LANDING GEAR WOULD NOT RETRACT. ACCOMPLISHED CHECKLIST PROCEDURES. RETURNED TO FIELD FOR A NORMAL LANDING. MAINTENANCE REPLACED THE LANDING GEAR SELECTOR VALVE. LEAKS AND OPS CHECKED GOOD. ALL GEAR RETRACT. Dec 31, 1999 · N881US · Fokker F28MK0100 · Landing Gear SelectorSDR USAAF00001Selector Valve · failedRDU/CLT - FLT 2327 - DURING CLIMB-OUT FROM CLT, LANDING GEAR WOULD NOT RETRACT. RECYCLED GEAR AFTER 2-3 MINUTES, GEAR RETRACTED. ON APPROACH, GEAR SELECTED DOWN, BUT MAINS DID NOT EXTEND. FOUR MINUTES LATER, RECEIVED THREE GREEN INDICATIONS. MADE SAFE LANDJan 2, 1999 · N881US · Fokker F28MK0100 · Landing Gear SelectorSDR USAA980576Skin · chafedPIT - DURING C-1 CHECK, FOUND TWO 1 INCH HOLES CHAFFED IN SKIN BETWEEN STATION 27526 AND OBLIQUE FRAME NR 16-2. INSTALLED DOUBLER PER EA 50951. (M)Nov 11, 1998 · N881US · Fokker F28MK0100 · Fuselage Main, Plate/SkinSDR USAA980575Longeron · chafedPIT - DURING C-1 CHECK, FOUND LONGERON CHAFED THROUGH .125 INCH BY .25 INCH AT LONGERON NR 50 CHAFED THROUGH AT STATION 27526. LONGERON DAMAGE CUT OUT, NEW PIECE SPLICED IN PER SRM 51-70-06 PAGE 206. (M)Nov 11, 1998 · N881US · Fokker F28MK0100 · Fuselage Main, Longeron/StringerSDR USAAF98045Rt Unit · failedPIT - FLT 0669 - AFTER TAKEOFF FROM PIT, RA FLAG ON PFD ILLUMINATED ALONG WITH THE FOLLOWING FAULT MESSAGES: GPWS, ALAND, STAB TRIM 1. THE NR 1 AUTOPILOT DISENGAGED. FLIGHT RETURNED TO PIT WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE NR 1 RADIO ALTIMEMay 24, 1998 · N881US · Fokker F28MK0100 · Ground Proximity SystemSDR USAAF98033Lights · inoperativePIT - DURING OVERNIGHT MAINTENANCE VISIT, FOUND LOW LEVEL LIGHTING IN AFT CABIN INOPERATIVE. MAINTENANCE REPAIRED WIRING IN AFT LOW LEVEL LIGHTING CIRCUIT. (M)Mar 17, 1998 · N881US · Fokker F28MK0100 · Emergency LightingSDR USAAF97019Flow Contl Valve · failedILM/GRR - FLT 1612 - EN ROUTE TO GRR, BOTH AUTOMATIC PRESSURIZATION SYSTEMS WENT OFF LINE. MANUAL SYSTEM WORKED OK. FLIGHT DIVERTED TO PIT TO ACCOMMODATE MAINTENANCE. FLIGHT LANDED IN PIT WITHOUT FURTHER INCIDENT. MAINTENANCE ADJUSTED LEFT AND RIGHT PRESSUFeb 14, 1997 · N881US · Fokker F28MK0100 · Cabin Cooling SystemSDR USAAF96111Battery Pack · dischargedDURING OVERNIGHT MAINTENANCE CHECK, MECHANIC FOUND FIRST CLASS FLOOR LEVEL EMERGENCY LIGHTING INOP. MAINTENANCE REPLACED BATTERY PACK. OPERATIONAL CHECK GOOD. (M)Oct 26, 1996 · N881US · Fokker F28MK0100 · Emergency LightingSDR USAAF96055Inverter · inoperativeFIRST CLASS FLOOR EMERGENCY LIGHTS INOPERATIVE. REPLACED INVERTER. (M)Jun 7, 1996 · N881US · Fokker F28MK0100 · Emergency LightingSDR USAAF96038Adc · malfunctionedSTL - FL 2129 - AT FL 350, CREW NOTICED THE THRUST WAS BEING REDUCED BY THE AUTOPILOT, THE CAPT'S AIRSPEED WAS DEGRADING DOWNWARD WHILE THE F/O'S WAS GOING TO REDLINE. THE CAPT TOOK CONTROL OF THE A/C, FLYING MANUALLY, AND STARTED A DESCENT. AT FL 300 THE A/Apr 28, 1996 · N881US · Fokker F28MK0100 · Air Data ComputerSDR USAAF96031Tube · crackedCLT - FLT 242 - AFTER TAKEOFF, CREW RECEIVED A NR 2 BLEED FAULT MESSAGE AND THEN A NR 2 DUCT LEAK MESSAGE. FLIGHT RETURNED TO CLT AND LANDED WITH NO FURTHER INCIDENT. MAINTENANCE FOUND A CRACKED LINE IN THE NR 2 ENGINE SUB WING TEST BLOCK AREA. A TEMPORARY Mar 25, 1996 · N881US · Fokker F28MK0100 · Compressor Bleed ControlSDR USAA950008Shut Off Valve · failedPIT - FLT 508 - 'THE WING ANTI-ICE CAPACITY' MESSAGE CAME ON WITH THE WING AN TAIL ANTI-ICE TURNED ON. ACFT RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE RT HPSOV NOT OPENING COMPLETELY WHEN AIR IS ON. REPLACED THE RT HPSOV. OPERATIOJan 6, 1995 · N881US · Fokker F28MK0100 · Airfoil Anti/De-ice System
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