N325UP

Service difficulty reports · 117

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 = 'N325UP' 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 IPXA09657626Floorbeam · crackedMEC COMPT STA 246 FLOORBEAM STIFFENER FOUND CRACK AT RBL 10 INCHES. MEC COMPT STA 246 FLOORBEAM RBL 10 INCHES STIFFENER REPLACED AND INSTALLED AS PER SRM 51-10-2 AND 51-40-02 REV 45.Oct 13, 2009 · N325UP · Boeing 76734AF · Fuselage Main, Floor BeamSDR IPXA09657686Support · crackedINSPECTION TYPE:6C RT WING L/E LES 675 FIXED FAIRING SUPPORT WEB UPPER AFT MOUNT SPAR CLIP FOUND CRACK. RHW L/E LES 675 FIXED FAIRING SUPPORT WEB UPPER AFT FRONT SPAR CLIP REPLACE AND INSTALLED AS PER SRM 51-10-02 AND 51-40-02 REV 45.Oct 6, 2009 · N325UP · Boeing 76734AF · Wing Miscellaneous StructureSDR IPXA09657679Rib · crackedRHW - L/E LES 252 FIXED FAIRING LWR SUPPORT RIB FW AREA FOUND CRACKED CRACK LENGTH 0.75 INCH. RHW L/E LES252 FIX FAIRING LWR SUPPORT RIB FWD AREA REPAIRED AS PER HX RS R57-00-36458 AND EO B767-5710-35230-A ORG MAT'L 7050-T7451 BARE ALUMINUM PLATE PER AMS4050 Oct 6, 2009 · N325UP · Boeing 76734AF · Wing, Rib/BulkheadSDR IPXA09657680Panel · delaminatedINSPECTION TYPE:C RT WING NR 7 SLAT LOWER CLOSURE PANEL THE EXISTING REPAIR DELAMINATION. COMPOSITE HOT BOND REPAIR CARRIED OUT AS PER SRM 51-70-07 PAR 5H FIG 15 REV 45.Oct 5, 2009 · N325UP · Boeing 76734AF · Leading Edge DevicesSDR IPXA09657668Skin · crackedNR 9 SLAT INBD NOSE SKIN RIVET HOLE FOUND CRACKED JUST AT OSS 572.77 CRACK LENGTH 0.125 INCH. RHW NR 9 SLAT AT OSS572.77 INBD NOSE SKIN REPAIRED AS PER SRM 57-43-01-2R2 FIG 201 REV45 ORG MATERIAL CLAD 7075T6-0.063 IN ORG CRACK LENGTH .125 INCH DAMAGED SKIN CUOct 5, 2009 · N325UP · Boeing 76734AF · Leading Edge DevicesSDR IPXA09657667Skin · crackedNR 9 SLAT OTBD NOSE SKIN RIVET HOLE FOUND CRACKED JUST AT OSS641.62 CRACK LENGTH 0.125 INCH. RHW NR 9 SLAT AT OSS641.62 OTBD NOSE SKIN REPAIRED AS PER SRM 57-43 -01-2R2 FIG 201 REV45. ORG MATERIAL CLAD 7075T6-0.063 IN ORG, CRACK LENGTH .125 INCH DAMAGED SKIN Oct 5, 2009 · N325UP · Boeing 76734AF · Leading Edge DevicesSDR IPXA09657614Stiffener · crackedINSPECTION TYPE:C AFT CARGO STA 1087 RBL 25 STIFFENER FOUND CRACK, CRACK .375 INCH LENGTH. AFT CARGO STA 1087 RBL 25 STIFFENER REPLACED AND INSTALLED AS PER SRM 51-10-02 AND 51-40-02 REV 45.Oct 5, 2009 · N325UP · Boeing 76734AF · Fuselage Miscellaneous StructureSDR IPXA09657613Stiffener · crackedINSPECTION TYPE:C MEC COMPT STA 246 FLOORBEAM STIFFENER FOUND CRACK AT LBL 50, CRACK .375 INCH LENGTH. MEC COMPT STA 246 FLOORBEAM AT LBL 50 STIFFENER REPLACED AND INSTALLED AS PER SRM 51-10-02 AND 51-40-02 REV 45.Oct 5, 2009 · N325UP · Boeing 76734AF · Fuselage Main, Floor BeamSDR IPXA09657612Stiffener · crackedINSPECTION TYPE:C AFT CARGO STA 1087 LBL 25 STIFFENER FOUND CRACK, CRACK .25 INCH LENGTH. AFT CARGO STA 1087 LBL 25 STIFFENER REPLACED AND INSTALLED AS PER SRM 51-10-02 AND 51-40-02 REV 45.Oct 5, 2009 · N325UP · Boeing 76734AF · Fuselage Miscellaneous StructureSDR IPXA09657611Stiffener · crackedINSPECTION TYPE:C MEC COMPT STA 246 FLOORBEAM STIFFENER FOUND CRACK AT LBL 25, CRACK .5 INCH LENGTH. MEC COMPT STA 246 FLOORBEAM AT LBL 25 STIFFENER REPLACED AND INSTALLED AS PER SRM 51-10-02 AND 51-40-02 REV 45.Oct 5, 2009 · N325UP · Boeing 76734AF · Fuselage Main, Floor BeamSDR IPXA09656911Floor Panel · damagedINSPECTION TYPE:N/A FLOOR PANEL 9C DAMAGED. FABRICATED NEW FLOOR PANEL.Aug 2, 2009 · N325UP · Boeing 76734AF · Fuselage Floor PanelSDR UPS08654212Circuit Card · faultyINSPECTION TYPE:ETOP L DUCT LIGHT ILLUMINATED. L BLEED DUCT LEAK DISPLAYED. LIGHT EXTINGUISHED AFTER ENGINE BLEED AIR SUPPLY AND ISOLATION VALVE CLOSED. T/S IAW FIM 26-18-00 FIG 104. WING AND BODY DUCT LEAK BITE CHK FOUND OK. REMOVED WING ACCESS PANELS. Dec 16, 2008 · N325UP · Boeing 76734AF · Pneumatic Indicating SystemSDR UPS08652605Bracket · crackedINSPECTION TYPE:AD NOSE LANDING GEAR WHEEL WELL RT SENSOR BRACKET CRACK. CRACK LENGTH .375 INCH. NOSE LANDING GEAR WHEEL WELL RT SENSOR SUPPORT BRACKET REPLACED AND INSTALLED AS PER SRM 51-10-02 AND 51-40-02.Jun 23, 2008 · N325UP · Boeing 76734AF · Landing Gear Position and WarningSDR UPS07649940Floor Panel · crackedINSPECTION TYPE:N/A FOUND DENT WITH CRACK ON FLOOR PANEL IN BULK CARGO COMPARTMENT. POS STA 1497 LEFT BBL 16. TWO INCHES DIA DENT AND 1 INCH CRACK AT CENTER OF DENT - DEPTH .25 INCHES. INTERIM REPAIRED PER EO B767-2550-8036-D APPX A (2).Jun 11, 2007 · N325UP · Boeing 76734AF · Fuselage Floor PanelSDR UPS07649554Engine · unknownINSPECTION TYPE:ETOP ENGINE OIL FUMES ENTERED CABIN. FUMES STOPPED WITH LEFT ENGINE BLEED CLOSED. ALL PARAMETERS NORMAL (STRONG ODOR) TET = 23832, TEC = 7538. LEFT ENG REQ BORESCOPE PER FIM 79-21-00. BORESCOPED PER 72-30-00. FOUND STAINS ON BLADES & IGVS.Mar 27, 2007 · N325UP · Boeing 76734AF · Engine (Turbine/Turboprop)SDR UPS06646658Actuator · crackedFOUND THE NLG RETRACT ACTUATOR CRACKED AROUND THE END OF THE ROD INTO THE CHROME. RECEIVED RETRACT ACTUATOR PER M/M 32-34-01-4 FUNCTIONAL TEST AND LEAK CHECK OKApr 7, 2006 · N325UP · Boeing 767300 · Landing Gear ActuatorSDR UPS05644142Smoke Goggles · crackedSMOKE GOGGLES IN CENTER JUMP SEAT HAS CRACKED LENS. REMOVED AND REPLACED SMOKE GOGGLES IN CENTER JUMP SEAT AS REQ'D REF AM 25-64-00.Mar 19, 2005 · N325UP · Boeing 76734AF · Emergency Equipment
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