N325US

Service difficulty reports · 226

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 = 'N325US' 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 DALA2019111806759Shear Pin · shearedR2 DOOR, DAMPER AND EMER OPENING CYLINDER, SHEAR PIN SHEARED AT ARMING LEVER, REPLACED SHEAR PIN REF. A320 AMM 52-11-14.Nov 18, 2019 · N325US · Airbus A320211 · Service DoorsSDR DALA2019111806758Shear Pin · shearedL2 DOOR, DAMPER AND EMER OPENING CYLINDER, SHEAR PIN SHEARED AT ARMING LEVER, REPLACED SHEAR PIN REF. A320 AMM 52-11-14Nov 18, 2019 · N325US · Airbus A320211 · Passenger/Crew DoorsSDR DALA2019012300609Light · malfunctionedALL CABIN EMERGENCY LIGHTS CAME ON DURING DESCENT. WENT OUT WHEN LANDING GEAR WAS EXTENDED. RAN CIDS TEST AND RESET. NO FAULTS FOUND.Jan 22, 2019 · N325US · Airbus A320211 · Emergency LightingSDR DALA2018101106002Apu · leakingCREW REPORTS SMELL IN FLIGHT DECK AT TAKE-OFF FOR 5 MINUTES. (NOTE: OIL SVC'D IN BOS. OIL PUDDLE UNDER ENGINES). BOROSCOPED NR 1 ENGINE HPC STAGE 1 AND 2. NO OIL WETTING NOTED. REPLACED OIL TANK CAP. FOUND APU COMPARTMENT OIL SOAKED. REMOVED AND REPLACED APU, Oct 7, 2018 · N325US · Airbus A320211 · APU Core EngineSDR DALA2018092705782Pump · not reported(LP# 3858576) STRONG ODOR IN COCKPIT. SMELLS LIKE DIRTY SOCKS. EXTERNAL AIR CONNECTED, APU OFF. DISCONNECTED GROUND AIR, STARTED APU AND APPLIED AIR. NO CHANGE IN SMELL. REMOVED AND REPLACED APU OIL PUMP AND COMPLIED WITH TASK CARDS 4916-2001, 2100-2002, 2100-Sep 27, 2018 · N325US · Airbus A320211 · APU Oil SystemSDR DALA2018062204161Light · inoperativeBOTH AFT LEFT AND RIGHT OVERWING EMERGENCY EXIT HANDLE LIGHTS INOPERATIVE. RELAMPED. OPERATION CHECKS GOOD.Jun 19, 2018 · N325US · Airbus A320211 · Emergency LightingSDR DALA2018060903917Bushing · not seatedDOOR R2 ARMS WITH THE PIN IN PLACE. RESEATED BUSHING IN LOCK PIN RETAINER. OPERATION CHECKS GOOD.Jun 8, 2018 · N325US · Airbus A320211 · Emergency ExitsSDR DALA2018041202560Connector · looseROW 28 OVERHEAD EMERGENCY LIGHT INOPERATIVE. MAINTENANCE FOUND CONNECTOR LOOSE. SECURED. OPS CHECKED NORMAL.Apr 10, 2018 · N325US · Airbus A320211 · Light System WiringSDR DALA2016080905920Battery Pack · no testDURING EMERGENCY LIGHT TEST, BATTERY PACK FAILED. REMOVED & REPLACED THE BATTERY PACK IAW AMM 33-51. CHECKED GOOD.Aug 8, 2016 · N325US · Airbus A320211 · Emergency LightingSDR DALA2016053004253Receptacle · missingBOTH RT OVERWING EXIT DOOR HANDLE EMERGENCY LIGHT RECEPTICLES MISSING, UNDER COVER, BOTH LT OVERWING EXIT DOOR HANDLE EMERGENCY LIGHTS INOPERATIVE. RELAMPED LT OVERWING EXIT DOOR HANDLE LIGHTS. REPLACED RT FWD OVERWING EXIT DOOR HANDLE LIGHT.May 27, 2016 · N325US · Airbus A320211 · Emergency LightingSDR DALA2016042003047Skin · gougedGOUGE FOUND ON AFT CARGO COMPARTMENT DOOR OUTER SKIN BETWEEN FRAME 54 AND FRAME 54A AND AT BEAM 4. PERFORMED PERMANENT RAPAIR ON EXTERNAL SKIN ON DOOR 826 LOCATED 33" AFT EDGE IN AFT CARGO COMPARTMENT IAW ER/A NR 54-0586-14, REV 0, MEASURE OF DAMAGE IS L:0.3Nov 7, 2015 · N325US · Airbus A320211 · Cargo/Baggage DoorsSDR DALA2015110706866Skin · dentedDENT ON EXTERNAL SKIN PASSENGER CREW DOOR 831, LOCATED AFT LOWER EDGE AT FWD GALLEY AREA. PERFORMED PERMANENT REPAIR ON EXTERNAL SKIN PASSENGER CREW DOOR 831 LOCATED AFT LOWER EDGE IAW SRM 52-10-00, PARA 5 C, FIGURE 203.Nov 6, 2015 · N325US · Airbus A320211 · Passenger/Crew DoorsSDR DALA2015110606776Strap · corrodedCORROSION ON INTERNAL STRUCTURE STRAP, LOCATED STR 43R TO STR 44 AND FRAME 64 MEASURES ARE: L=2.810", W=1.300" APPROXIMATELY. REPLACED STRAP LOCATED INTERNAL STRUCTURE STR 43R TO STR 44 AND FRAME 64 IN AFT CARGO COMPARTMENT IAW SRM 51-72-11 AND DWG D534-7034Nov 5, 2015 · N325US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA2016112509235Boss · corrodedCORROSION FOUND ON FWD WEB BOSS OF MLG RIB GEAR SUPPORT AT RIB 5 AREA OF THE RH WING. PERFORMED TIME LIMITED REPAIR IAW ERA.Nov 4, 2015 · N325US · Airbus A320211 · Wing, Landing Gear Attach FittingsSDR DALA2015110606777Stringer · corrodedCORROSION STR 27LT INTERNAL STRUCTURE AT LEVEL FRAME 67 AT LOWER FUSELAGE, REPLACED SECTION CONNECTION ON STRINGER 27LT AT LEVEL FRAME 67 IAW PRI 540587-14, REV 0 AND ER/A 540587-14, REV ORIGINAL.Nov 3, 2015 · N325US · Airbus A320211 · Fuselage Main, Longeron/StringerSDR DALA2016111708957Support · corrodedCORROSION FOUND ON FWD WEB BOSS OF MLG RIB GEAR SUPPORT AT RIB 5 AREA OF THE LT WING. PERFORMED TIME LIMITED REPAIR ON FALSE SPAR BOX OUTBOARD FACE OF THE OUTER GEAR-SUPPORT RIB#5 AS PER PRELIMINARY REPAIR INSTRUCTION ERA 570607-14.Nov 2, 2015 · N325US · Airbus A320211 · Wing, Landing Gear Attach FittingsSDR DALA2015110206724Floor Panel · delaminatedDELAMINATED FLOOR PANEL 261FF AT AFT GALLEY AREA, REPLACED FLOOR PANEL 261FF AT AFT GALLEY AREA.Oct 31, 2015 · N325US · Airbus A320211 · Fuselage Floor PanelSDR DALA2015102606525Stringer · corrodedCORROSION ON STRINGER 30L, FRAME 67. REPLACED THE STRINGER IAW SRM 51-72-11 AND DWG D53480019.Oct 25, 2015 · N325US · Airbus A320211 · Fuselage Main, Longeron/StringerSDR DALA2015102606524Fitting · corrodedCORROSION FITTINGS ON EMERGENCY EXIT DOOR. REPLACED THE FITTING IAW SRM 51-72-11 AND DWG D522-79040.Oct 25, 2015 · N325US · Airbus A320211 · Emergency ExitsSDR DALA2015102606523Support · corrodedCORROSION ON LOWER SUPPORT BETWEEN FRAMES 66 TO 68 AND STRINGER 23R AT A FT GALLEY AREA. REPLACED LOWER SUPPORT IAW SRM 51-72-11 AND DWG D53480019, E53474250.Oct 25, 2015 · N325US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA2015102606522Fitting · corrodedCORROSION ON CORNER FITTING FRAME 66, RT MEASURE OF CORROSION ARE AT AFT GALLEY AREA. REPLACED CORNER FITTING FRAME 66 RT AT AFT GALLEY AREA IAW SRM 51-72-11 AND DWG D53480019.Oct 25, 2015 · N325US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA2015102606521Floor Support · corrodedCORROSION ON FLOOR SUPPORT -Y254, FRAMES 12 TO 24. REPAIRED THE FLOOR SUPPORT IAW SRM 53-00-14, PARA 4.F, FIG 206.Oct 25, 2015 · N325US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA2015102606430Fitting · corrodedCORROSION FITTING ON EMERGENCY EXIT DOOR 834 IN PASSENGER CABIN. REPLACED FITTING ON EMERGENCY EXIT DOOR 834 IAW SRM 51-72-11 AND DWG D522-79040, JOB COMPLETE.Oct 25, 2015 · N325US · Airbus A320211 · Fuselage Main, Attach FittingsSDR DALA2015102606429Floor Support · corrodedCORROSION ON FLOOR SUPPORT -Y765, FRAMES 12 TO 24. REPLACED THE FLOOR SUPPORT IAW SRM 51-72-11, DWS D53112812, D53110984, AND D53110920.Oct 25, 2015 · N325US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA2015102606428Fitting · corrodedCORROSION FITTING ON EMERGENCY EXIT DOOR 844 IN PASSENGER CABIN. REPLACED FITTING ON EMERGENCY EXIT DOOR 844 IAW SRM 51-72-11 AND DWG D522-79040.Oct 25, 2015 · N325US · Airbus A320211 · Fuselage Main, Attach FittingsSDR DALA2015102606427Stringer · corrodedCORROSION ON SECTION CONNECTION ON STR 28 LT INTERNAL STRUCTURE LEVEL FRAME 67 AT LOWER FUSELAGE. REPLACED SECTION CONNECTION AND FASTENERS ON STR 28 LT INTERNAL STRUCTURE LEVEL FR 67 AT LOWER FUSELAGE IAW SRM 51-72-11 AND DWG D53480019.Oct 25, 2015 · N325US · Airbus A320212 · Fuselage Main, Longeron/StringerSDR DALA2015102606426Floorbeam · crackedCRACK ON FLOORBEAM, -Y254 LOCATED AT LEVEL FRAME 32 IN PASSENGER CABIN. PERFORMED PERMANENT REPAIR ON FLOORBEAM -Y254 AT LEVEL FR 32 IN PASSENGER CABIN IAW 53-21-14 PARA 5.A FIG 201.Oct 25, 2015 · N325US · Airbus A320212 · Fuselage Main, Floor BeamSDR DALA2015102606431Web · corrodedCORROSION ON WEB AT STR 38L, FRAMES 33 - 34 . REPLACED THE WEB IAW SRM 51-72-11 AND DWG D53230340.Oct 24, 2015 · N325US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA2016111808972Dummy Rail · corrodedCORROSION ON DUMMY RAIL BETWEEN FRAMES 12 TO 16. REPLACED THE DUMMY RAIL IAW SRM.Oct 23, 2015 · N325US · Airbus A320211 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2015102406413Stringer · corrodedCORROSION ON SECTION CONNECTION ON STR 29LT INTERNAL STRUCTURE LEVEL FRAME 67 AT LOWER FUSELAGE. REPLACED SECTION CONNECTION AND FASTENERS ON STR 29LT INTERNAL STRUCTURE LEVEL FRAME 67 AT LOWER FUSELAGE IAW SRM 51-72-11 AND DWG D53480019.Oct 23, 2015 · N325US · Airbus A320211 · Fuselage Main, Longeron/StringerSDR DALA2015102406412Seat Track · corrodedOUT OF LIMITS, SEAT TRACK +Y1292 ON CENTER WING BOX BETWEEN FRAME 41 TO FRAME 47. MEASURE OF REWORK ARE L: 2.722", W: 0.374", D: 0.096", REPLACED SEAT TRACK +Y1292 ON CENTER WING BOX BETWEEN FRAME 41 TO FRAME 47 IAW SRM 51-72-11 AND DWG D53370500 AND D533710Oct 23, 2015 · N325US · Airbus A320211 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2015102306407Floor Support · corrodedCORROSION ON FLOORBEAM -Y1292 LOCATED FRAME 12 TO FRAME 24 MEASURE ARE L=0, 250" W=0.125", D=O.010", APPROXIMATELY SSI 531189 AT FWD GALLEY AREA. REPLACED FLOORBEAM Y1292 LOCATED FRAME 12 TO FRAME 24 IAW SRM 51-72-11 AND DWG D53112812.Oct 22, 2015 · N325US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA2015101906244Floor Support · corrodedCORROSION ON FLOOR SUPPORT -Y1162 BETWEEN FRAMES 67+15 - 69. REPLACED THE FLOOR SUPPORT IAW SRM 51-72-11 AND DWG D5347200.Oct 18, 2015 · N325US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA2015101906243Floor Support · corrodedCORROSION ON FLOOR SUPPORT +Y1162 BETWEEN FRAMES 67+15 - 69. REPLACED THE FLOOR SUPPORT IAW SRM 51-72-11 AND DWG D53472000.Oct 18, 2015 · N325US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA2015101906242Floor Support · corrodedCORROSION ON FLOOR SUPPORT +Y1225 BETWEEN FRAMES 66+5 - 67+15. REPLACED THE FLOOR SUPPORT IAW SRM 51-72-11 AND DWG D53472000.Oct 18, 2015 · N325US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA2015101906241Floor Support · corrodedCORROSION ON FLOOR SUPPORT -Y1225 BETWEEN FRAMES 66+5 - 67+15. REPLACED THE FLOOR SUPPORT IAW SRM 51-72-11 AND DWG D53472000.Oct 18, 2015 · N325US · Airbus A320212 · Fuselage Miscellaneous StructureSDR DALA2015101606218Fitting · corrodedCORROSION ON CORNER FITTING FRAME 68 AT LEVEL STR 23L AT AFT GALLEY AREA. REPLACED CORNER FITTING LOCATED FRAME 68 AT LEVEL STR 23L AFT GALLEY AREA IAW SRM 51-72-11 AND DWG D53480020.Oct 15, 2015 · N325US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA2016112209103Stringer · corrodedSTRINGER 43L HAS CORROSION BETWEEN FRAMES 56 & 57. REMOVED AND REPLACED THE STRINGER IAW SRM.Apr 21, 2015 · N325US · Airbus A320211 · Fuselage Main, Longeron/StringerSDR DALA2015042202880Skin · corrodedDURING INSPECTION, FOUND CORROSION FOUND ON STRINGERS 42L AND 43L BETWEEN FRAMES 56 & 57 ALSO ON SKIN BETWEEN 42L AND 43L AND FRAMES 56 & 57. INSTALLED DOUBLER 165942. C/W ERA 535278-14 AD AND PRI 535278-14, REV O AND REV 1.Apr 21, 2015 · N325US · Airbus A320212 · Fuselage Main, Plate/SkinSDR DALA2015042202878Stringer · corrodedDURING INSPECTION, FOUND STRINGER 42L HAS CORROSION ON IT BETWEEN FRAMES 56-57. REPLACED STRINGER 42L IAW SRM 53-00-13.Apr 21, 2015 · N325US · Airbus A320212 · Fuselage Main, Longeron/StringerSDR DALA2014081204422Battery Pack · no testDURING NON ROUTINE CHECK, FOUND EMERGENCY LIGHTS TEST FAULTED BATTERY AFT LT OF CABIN. MAINTENANCE REPLACED AFT LT BATTERY PACK AND FUNCTIONAL CHECK WAS NORMAL.Aug 11, 2014 · N325US · Airbus A320211 · Emergency LightingSDR DALA12014783225Battery Pack · failedDURING SERVICE CHECK, EMERGENCY LIGHT TEST FAILED BATTERY LT AFT. MX REPLACED BATTERY PACK AND FUNCTIONAL CHECK WAS NORMAL.Dec 2, 2012 · N325US · Airbus A320211 · Emergency LightingSDR DALA1155113225Skin · gougedFUSELAGE SKIN GOUGE 23.5 INCHES AFT OF 2L DOOR CUTOUT. APPROX STA 3320 STR 17L. REMOVED DAMAGE BY BLENDING PER A320SRM 51-73-00. THE BLENDED AREA IS OUT OF LIMITS INSTALL TEMP REPAIR INSTALLED DOUBLER PER A320 SRM 53-41-11. INSTALL RII COMPLETE. OK TO PAISep 22, 2011 · N325US · Airbus A320211 · Fuselage Main, Plate/SkinSDR DALA1017883225Wire · inoperativeDURING A NON ROUTINE CHECK, FOUND THE EMERGENCY LIGHT AT ROW 11ABC INOPERATIVE. MX REPLACED BUTT SPLICE AND FUNCTIONAL CHECK WAS NORMAL. ACFT RETURNED TO SERVICE.Jul 31, 2010 · N325US · Airbus A320211 · Light System WiringSDR DALA103913225Skin · damagedDURING "H" CHECK AND AFT AIRPHONE ANTENNA MOD FOUND DRILL STARTS IN SKIN NEXT TO FWD HOLE 3LT & 4LT. REPAIRED IAW ERA NR 13-478992-14.Feb 20, 2010 · N325US · Airbus A320211 · Fuselage Main, Plate/SkinSDR DALA103903225Sill · corrodedDURING "H" CHECK FOUND CORROSION ON LT AFT UTILITY DOOR SILL THRESHOLD BETWEEN FR67 & FR68 UNDER GIRT BAR. REPAIRED IAW SRM 51-42-11.Feb 19, 2010 · N325US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA103893225Floor Panel · corrodedDURING H-CHECK FOUND CORROSION ON CARGO FLOOR PANEL 132DF. REPLACED CARGO FLOOR PANEL PER SRM 51-72-11.Feb 19, 2010 · N325US · Airbus A320211 · Fuselage Floor PanelSDR DALA103853225Floorbeam · corrodedDURING "H" CHECK FOUND CORROSION ON FLOORBEAM AT -Y465 FR66. REPAIRED IAW SRM 51-42-11 & 51-23-11.Feb 18, 2010 · N325US · Airbus A320211 · Fuselage Main, Floor BeamSDR DALA103763225Floor Support · corrodedDURING "H" CHECK FOUND CORROSION ON FLOOR SUPPORT BEAM AT +Y1292 BETWEEN FR67-FR68. REPAIRED IAW SRM 51-42-11.Feb 16, 2010 · N325US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA103753225Seat Track · corrodedDURING "H" CHECK FOUND SEAT TRACK CORRODED AT -Y1292 BETWEEN FR66 AND FR 68. REPAIRED IAW SRM 51-42-11.Feb 16, 2010 · N325US · Airbus A320211 · Fuselage, Seat/Cargo Attach Fittings
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