N328UP

Service difficulty reports · 119

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 = 'N328UP' 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 IPXA09656961Hinge Fitting · crackedINSPECTION TYPE:C RT WING I/B AFT FLAP HINGE FITTING FOUND CRACK. CRACK LENGTH I/B FLANGE 1.2 INCH, O/B FLANGE 1.5 INCH. RT WING I/B AFT FLAP HINGE FITTING REPAIRED AS PER SRM 57-53-02-2R1 FIG 201 REV 44. THIS REPAIR IS CLASSIFIED AS MAJOR REPAIR WITH MATERAug 3, 2009 · N328UP · Boeing 76734AF · Trailing Edge FlapsSDR IPXA09657021Stiffener · crackedINSPECTION TYPE:C MAIN EQUIPMENT CTR STA 246 FLOORBEAM STIFFENER AT LBL 25 FOUND CRACKED. CRACK LENGTH 0.5 INCH. MAIN EQUIPMENT CTR STA 246 FLOORBEAM STIFFENER AT LBL 25 REPLACED AND INSTALLED AS PER SRM 51-10-02 AND 51-40-02 REV 44.Aug 1, 2009 · N328UP · Boeing 76734AF · Fuselage Main, Floor BeamSDR IPXA09657020Stiffener · crackedINSPECTION TYPE:C MAIN EQUIPMENT CENTER STA 246 FLOORBEAM STIFFENER AT RBL 25 FOUND CRACK. CRACK LENGTH 0.75 INCH. MAIN EQUIPMENT CENTER STA 246 FLOORBEAM STIFFENER AT RBL 25 REPLACED AND INSTALLED AS PER SRM 51-10-02 AND 51-40-02 REV 44.Aug 1, 2009 · N328UP · Boeing 76734AF · Fuselage Main, Floor BeamSDR IPXA09656964Stiffener · crackedINSPECTION TYPE:C MAIN EQUIPMENT CENTER STA 246 FLOOR BEAM STIFFENER AT LBL 50 FOUND CRACKED. CRACK LENGTH 0.75. MAIN EQUIPMENT CENTER STA 246 FLOORBEAM STIFFENER AT LBL 50 REPLACED AS PER SRM 51-10-02 AND INSTALLED AS PER SRM 51-40-02 REV 44.Aug 1, 2009 · N328UP · Boeing 76734AF · Fuselage Main, Floor BeamSDR IPXA09656958Stiffener · crackedINSPECTION TYPE:C MAIN EQUIPMENT CENTER STA 246 FLOORBEAM STIFFENER AT RBL 10 FOUND CRACK. CRACK LENGTH 2 INCHES. MAIN EQUIPMENT CENTER STA 246 FLOORBEAM STIFFENER AT RBL 10 REPLACED AS PER SRM 51-10-02 AND INSTALLED AS PER SRM 51-40-02 REV 44.Aug 1, 2009 · N328UP · Boeing 76734AF · Fuselage Main, Floor BeamSDR IPXA09656985Floor Panel · damagedINSPECTION TYPE:C MCD FLOOR PANEL FOUND DAMAGED AT STA 975 TO 1114, LBL 11 TO RBL 11. FLOOR PANEL FABRICATED PER EO B767-5320-9693-F & INSTALLED AS PER MM 53-01-01.Jul 31, 2009 · N328UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA09656984Floor Panel · damagedINSPECTION TYPE:C MCD FLOOR PANEL FOUND DAMAGED AT STA 1197+22 TO 1207 RBL 55 TO RBL 77. FLOOR PANEL FABRICATED PER EO B767-5320-9693-F & INSTALLED AS PER MM 53-01-01.Jul 31, 2009 · N328UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA09656967Floor Panel · damagedINSPECTION TYPE:C MCD FLOOR PANEL FOUND DAMAGED AT STA 654+22 TO 690, LBL 11 TO RBL 11. FLOOR PANEL FABRICATED PER EO B767-5320-9693-F & INSTALLED AS PER MM 53- 01-01.Jul 31, 2009 · N328UP · Boeing 76734AF · Fuselage Floor PanelSDR UPS08651966Regulator · leakingUPON BLOCKING IN, CREW O2 ON EICAS READS 250PSI AND FALLING. FOUND UPPER O2 REGULATOR LEAKING. REPLACED BOTH O2 REGULATORS AS PRECAUTIONARY.Apr 3, 2008 · N328UP · Boeing 76734AF · Crew Oxygen SystemSDR UPS07650849Seat Track · corrodedINSPECTION TYPE:C1 FUSELAGE UPPER LOBE, CORROSION ON I/B FLANGE OF SEAT TRACK AT NUT PLATE HOLE, BS 527, LBL 55, WL 200. BLENDED CORROSION, FABRICATED & INSTALLED REPAIR PARTS PER ER 07-3583.Sep 23, 2007 · N328UP · Boeing 76734AF · Fuselage, Seat/Cargo Attach FittingsSDR UPS07650847Frame · puncturedINSPECTION TYPE:C1 FRAME BENT AND PUNCTURED STA 654+66 STR 7L. CUT OUT DAMAGED, FABRICATED & INSTALLED REPAIR PARTS PER ER 07-3560.Sep 20, 2007 · N328UP · Boeing 76734AF · Fuselage Main, FrameSDR UPS07650846Support Angle · corrodedINSPECTION TYPE:C1 LOWER FUSELAGE, KEEL BEAM PANEL SUPPORT ANGLE HAS SURFACE CORROSION COMMON TO NUT PLATE LOCATIONS, BS 827, BS 877, BLENDED CORROSION. FABRICATED & INSTALLED REPAIR PARTS PER SRM 51-40-02.Sep 20, 2007 · N328UP · Boeing 76734AF · Fuselage Main, KeelSDR UPS07650845Plate · corrodedINSPECTION TYPE:C1 CORROSION ON NUT PLATE HOLE. BLENDED CORROSION, FABRICATED AND INSTALLED REPAIR PER SRM 53-00-51.Sep 20, 2007 · N328UP · Boeing 76734AF · Fuselage Miscellaneous StructureSDR UPS07650781Stringer Clip · bentINSPECTION TYPE:C1 BENT STRINGER CLIP. REMOVED, FABRICATED, INSTALLED PER SRM 51-40-02 AND DRAWING 143T1126.Sep 20, 2007 · N328UP · Boeing 76734AF · Fuselage Main, Attach FittingsSDR UPS07650779Stringer Clip · bentINSPECTION TYPE:C1 BENT STRINGER CLIP. REMOVED, FABRICATED, AND INSTALLED PER SRM 51-40-02 AND DRAWING 143T1126.Sep 20, 2007 · N328UP · Boeing 76734AF · Fuselage Main, Attach FittingsSDR UPS07650778Stringer Clip · bentINSPECTION TYPE:C1 BENT STRINGER CLIP. REMOVED, FABRICATED, INSTALLED PER SRM 51-40-02 AND DRAWING 143T1126.Sep 20, 2007 · N328UP · Boeing 76734AF · Fuselage Main, Attach FittingsSDR UPS05644141Smoke Goggles · crackedINSPECTION TYPE:N/A F/O'S SMOKE GOGGLES HAS A CRACK IN LENS AT NOSE PIECE .375 INCH LONG. REPLACED BROKEN GOGGLES WITH SERVICEABLE GOGGLES.Mar 19, 2005 · N328UP · Boeing 76734AF · Emergency EquipmentSDR UPS03641622Hmu · malfunctionedRT ENGINE ROLLED BACK TO IDLE AND WOULD NOT RESPOND TO THRUST LEVER MOVEMENT. DIVERSION TO STL REPLACED HMU, EEC, AND CONTROL ALT. OPS , LEAK , POWER TESTS NORMAL.Dec 2, 2003 · N328UP · Boeing 767300 · Fuel Controlling SystemSDR UPS00633814Latch · failedINSPECTION TYPE:N/A, F/O''S EXTERIOR EMERGENCY EXIT HANDLE UNLOCKED ON EXTERIOR WAS LOCKED PRIOR TO FLIGHT. *S/D* REMOVED COTTER PIN FROM SHAFT TO LINK BOLT, LOOSENED NUT, REMOVED AND REPLACED EMERGENCY DOOR GEARBOX ASSY IAW MM 56-11-04 PG 425-426. ALL CHECSep 30, 2000 · N328UP · Boeing 76734AF · Emergency Exits
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