N319UP

Service difficulty reports · 170

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 = 'N319UP' AND registry_match = 'registration'
  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 IPXA09655137Wedge · delaminatedINSPECTION TYPE:C LT WING O/B TRAILING EDGE FLAP LOWER T/E MID AREA THE EXISTING REPAIR (REF SURVEY SEQ 319-W3-02) DELAMINATION. COMPOSITE HOT BOND REPAIR CARRIED OUT AS PER SRM 51-70-07 PARA 5A (1) FIG 9 REV 43.Mar 16, 2009 · N319UP · Boeing 76734AF · Trailing Edge FlapsSDR IPXA09655122Floor Panel · puncturedINSPECTION TYPE:C FLOOR PANEL DAMAGED POS 2, FWD RIGHT CORNER OF RIGHT O/B PANEL AT STN 412 (PUNCTURE ABOUT .75 INCH). FLOOR PANEL REPAIRED AS PER SRM 53-00-50-2R REV 43.Mar 14, 2009 · N319UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA09655121Floor Panel · puncturedINSPECTION TYPE:C FLOOR PANEL DAMAGED POS 2 SECOND FLOORBOARD FROM RIGHT STATION 412 .5 INCH PUNCTURE. FLOOR PANEL REPAIRED AS PER SRM 53-00-50-2R REV 43.Mar 14, 2009 · N319UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA09654836Floor Panel · damagedPOSITION 10 L HAS A HOLE 1 INCH IN DIA IN THE FWD O/B CORNER (DEFERRAL 390713). TRANSFERRED TO NRC 353656. VERIFIED FABRICATION OF NEW PANEL PER EO B767-5320-9693-E, APPX B, STEPS 3-6. OK TO INSTALL FLOORBOARD. INSTALLED PANEL ON L/P 012206 THIS CLEARS D390Feb 24, 2009 · N319UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA09654816Floorboard · damagedINSPECTION TYPE:N/A FLOORBOARD DAMAGED. REPLACED FLOORBOARD IAW EO B767-5320-9693-E.Feb 23, 2009 · N319UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA09654814Floorboard · damagedINSPECTION TYPE:N/A FLOORBOARD DAMAGE. FABRICATED NEW PANEL IAW EO B767-5320-9693-E.Feb 23, 2009 · N319UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA09654812Floor Panel · damagedINSPECTION TYPE:N/A MAIN CARGO DECK FLOOR PANEL POSITION 8R HAS 1 INCH DIA HOLE I/B AFT CORNER 2 HOLES 1 INCH DIA. REPAIR PER EO B767-5320-32410-A.Feb 23, 2009 · N319UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA09654811Floor Panel · damagedINSPECTION TYPE:N/A MAIN CARGO DECK FLOOR PANEL POSITION 2R HAS DAMAGE. EXISTING REPAIR DAMAGED 1" X 2" UPPER SKIN AND CORE DAMAGED IN THE AFT POSITION OF AN EXISTING REPAIR LOCATED 2 INCHES FROM AFT EDGE. EXISTING REPAIR IS 4" X 4". REPAIR PER EO B767-5320Feb 23, 2009 · N319UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA09654810Floor Panel · damagedINSPECTION TYPE:N/A MAIN DECK FLOOR PANEL POS 2R HAS 1 INCH HOLE, 2 INCHES AFT OF THE CENTER LOCK, 1 INCH HOLE 2 INCHES AFT OF FWD EDGE OF PANEL 6 INCHES FROM RT EDGE, .75 INCH HOLE AFT OF FWD EDGE OF PANEL 3 .5 INCH FROM EDGE. REPAIR PER EO B767-5320-32412-AFeb 23, 2009 · N319UP · Boeing 76734AF · Fuselage Floor PanelSDR UPS08652348Thermal Switch · inoperativeINSPECTION TYPE:ETOP ATB - DUCT LEAK LIGHT ILLUM. EICAS MSG: LEFT BLEED DUCT LEAK DISPLAYED. FUEL DUMPED. REPLACED M691 CONTROL CARD PER MM 26-10-01-4. REPLACED S236 THERMAL SWITCH PER MM 26-18-01-4. REMOVED AND REPLACED S237 THERMAL SWITCH PER MM 26-18-May 25, 2008 · N319UP · Boeing 76734AF · Overheat DetectionSDR UPS08652308Cap · crackedINSPECTION TYPE:N/A ATB - AFTER TAKEOFF RECEIVED CTR HYD QTY LIGHT FOLLOWED BY LOSS OF CENTER HYD PRESSURE. QTY INDICATED .08 IN CENTER SYSTEM. FOUND NR 3 SPOILER ACT LEAKING FROM FILTER CAP. REPLACED NR 3 SPOILER PCA FILTER CAP AND PACKING.May 21, 2008 · N319UP · Boeing 76734AF · Drag Control ActuatorSDR UPS07650326Transmitter · inoperativeINSPECTION TYPE:ETOP CLEARING THE RUNWAY FLAP ASSY MESSAGE DISPLAYED FOR 3-4 SECONDS THEN CLEARED. REMOVED AND REPLACED NR 1 T/E FLAP POSITION TRANSMITTER IAW MM 27-51-45-2. OPS CHECK GOOD.Jul 20, 2007 · N319UP · Boeing 76734AF · Trailing Flap Position Indicating SystemSDR UPS07650332Connector · corrodedINSPECTION TYPE:ETOP BLOCK TURN BACK DUE TO EICAS MSG FLAP/SLAT ELEC DISPLAYED. BITE CHECK FSEU-FAULT-1 LT O/B TRANSMITTER. FOUND CORROSION IN CONNECTOR. CLEANED. OPS CHECK PER MM 27-58-00-5. CHECKED OK.Jul 14, 2007 · N319UP · Boeing 76734AF · Flight Control System WiringSDR UPS03640444Pump · leakingINSPECTION TYPE:ETOP LEFT ENGINE OIL QTY DECREASE IN FLIGHT, DIVERSION TO CTS EMERGENCY DECLARED. FOUND OIL LEAKING FROM LT ENGINE SCAV OIL PUMP OUTLET PORT TO THE OIL PRESS TRANSMITTER, R/R LUB AND SCAV OIL PUMP ASSY AND REDUCER-TUBE AND OIL LEAK CHECK OK WApr 20, 2003 · N319UP · Boeing 767300 · Engine Oil Distribution (Airframe Furnished)SDR UPS03640419Light · inoperativeEXTERIOR EMERGENCY LIGHT INOP. RELAMPED AND TESTED PER MM 33-51-16-2, CHECKED OK.Apr 6, 2003 · N319UP · Boeing 76734AF · Emergency LightingSDR UPS01634905Shunt · failedINSPECTION TYPE:IN PILOT REPORT - RT ENG EGT FLUCTUATES. INSPECTED CONNECTIONS ON THERMOCOUPLES AND CONNECTIONS ON JUNCTION BOX. RAN RT ENG ALL INDICATIONS NORMAL AT THIS TIME. REMOVED AND REPLACED EGT SHUNT.Feb 6, 2001 · N319UP · Boeing 76734AF · Engine EGT/TIT Indicating SystemSDR UPS99630005Outflow Valve · inoperativeINSPECTION TYPE:ETOP PILOT REPORT PRESSURIZATION AUTO 1 DID NOT INITIATE AT FL 370 DESCENDING INTO ONT. MANUAL PRESSURIZATION INITIATED AT FL 200. PRESSURIZATION AUTO 2 ON DEFFERAL. REMOVED AND REPLACED OUTFLOW VALVE, VALVE CHECKS GOOD.Jul 2, 1999 · N319UP · Boeing 76734AF · Pressure Regulator/Outflow ValveSDR UPS98627046Engine · malfunctionedINSPECTION TYPE:ETOP LT ENGINE POWER FLUX AT A CONSTANT THRUST SETTING. BOTH CLB 2 AND CLB PWR SETTING. NOTICEABLE YAW IN ADDITION TO ALL ENG INDICATION FLUX. REPEAT WRITE UP SEE CONTROL NR 9827042 FOR PREVIOUS WRITE UP. REPLACED N1 SENSOR PERFORMED ENG RUJun 24, 1998 · N319UP · Boeing 76734AF · Engine (Turbine/Turboprop)SDR UPS98627042Engine · malfunctionedINSPECTION TYPE:ETOP LEFT ENGINE POWER FLUCTATES AT A CONSTANT SETTING (THRUST). CONDITION WAS INTERMITTENT ON CLIMB-OUT IN BOTH CLB 2 AND CLB PWR. N1,EGT,N2, AND FUEL FLOW ALL FLUXED WITH NO POWER SETTING CHANGE. PERFORMED BITE CHECK PER FIM 73-21-00 COMBJun 19, 1998 · N319UP · Boeing 76734AF · Engine (Turbine/Turboprop)SDR UPS97624448Switch · failedVOR FREQ DISPLAY DOES NOT RESPOND PROPERLY TO SELECTOR OPERATION. WHEN TOGGLING THE AUTO/MAN SELECTOR SWITCH, SWITCH OPERATION FROZE AN ELECTRICAL BURNING SMELL WAS NOTICED BY ALL CREW MEMBERS. AUTO/MAN SWITCH FROZE. REMOVED AND REPLACED CAPT'S VOR CONTROL Sep 17, 1997 · N319UP · Boeing 76734AF · Localizer/VOR System
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