N103US

Service difficulty reports · 298

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 = 'N103US' 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 USAA2010102592390Floorbeam · corrodedSAL - S5 - MAJOR REPAIR - LEVEL 2 GALVANIC CORROSION ON FLOORBEAM BETWEEN FR68 TO FR70, -Y254. REPLACED FLOORBEAM BETWEEN FR68 TO FR70, -Y254 IAW A320 SRM 51-72-11.Oct 9, 2010 · N103US · Airbus A320214 · Fuselage Main, Floor BeamSDR USAA2010102592389Floorbeam · corrodedSAL - S5 - MAJOR REPAIR - LEVEL 2 GALVANIC CORROSION ON FLOORBEAM BETWEEN FR66 + 5 INCHES TO FR70, -Y765. REPLACED FLOORBEAM BETWEEN FR66 + 5 INCHES TO FR70, -Y765 IAW A320 SRM 51-72-11 & AIRBUS DRAWING D53472000.Oct 9, 2010 · N103US · Airbus A320214 · Fuselage Main, Floor BeamSDR USAA2010102592388Floorbeam · corrodedSAL - S5 - MAJOR REPAIR - LEVEL 2 GALVANIC CORROSION ON FLOORBEAM BETWEEN FR65 TO FR66, Y512.5. REPLACED FLOORBEAM BETWEEN FR65 TO FR66, Y512.5 IAW A320 SRM 51-72-11.Oct 9, 2010 · N103US · Airbus A320214 · Fuselage Main, Floor BeamSDR USAA2010102592387Floorbeam · corrodedSAL - S5 - MAJOR REPAIR - LEVEL 2 GALVANIC CORROSION ON FLOORBEAM BETWEEN FR64 TO FR66 + 5 INCHES, -Y765. REPLACED FLOORBEAM BETWEEN FR64 TO FR66 + 5 INCHES, -Y765 IAW A320 SRM 51-72-11 & AIRBUS DRAWING D5347219020300.Oct 9, 2010 · N103US · Airbus A320214 · Fuselage Main, Floor BeamSDR USAA2010102592386Floorbeam · corrodedSAL - S5 - MAJOR REPAIR - LEVEL 2 EXFOLIATION CORROSION ON FLOORBEAM BETWEEN FR66 + 5 INCHES TO FR70, Y765. REPLACED FLOORBEAM BETWEEN FR66 + 5 INCHES TO FR70, Y765 IAW A320 SRM 51-72-11 & AIRBUS DRAWING D53472000.Oct 9, 2010 · N103US · Airbus A320214 · Fuselage Main, Floor BeamSDR USAA2010110592523Support · corrodedSAL - S-5 - MAJOR REPAIR - LEVEL 2 GALVANIC CORROSION ON SUPPORT STRUCTURE BETWEEN FR28 TO FR29 & BETWEEN S43L TO S43R. REPLACED STAMPING SUPPORT BETWEEN FR28 TO FR29 & BETWEEN S43L TO S43R IAW A320 SRM 51-72-11 & AIRBUS DRAWING D53230861.Oct 7, 2010 · N103US · Airbus A320214 · Fuselage Miscellaneous StructureSDR USAA2010110392478Seat Track · corrodedSAL - S5 - MAJOR REPAIR - CORROSION ON SEAT TRACK BETWEEN FR37 TO FR39, -Y765. REPLACED SEAT TRACK BETWEEN FR37 TO FR39, -Y765 IAW A320 SRM 51-72-11.Oct 7, 2010 · N103US · Airbus A320214 · Fuselage, Seat/Cargo Attach FittingsSDR USAA2010102892429Seat Track · corrodedSAL - S5 - MAJOR REPAIR - LEVEL 2 GALVANIC CORROSION ON SEAT TRACK BETWEEN FR24 TO FR35, -Y1292. REPLACED SEAT TRACK BETWEEN FR24 TO FR35, -Y1292 IAW A320 SRM 51-72-11.Oct 7, 2010 · N103US · Airbus A320214 · Fuselage, Seat/Cargo Attach FittingsSDR USAA2010102892428Seat Track · corrodedSAL - S5 - MAJOR REPAIR - NR 6284552 - LEVEL 2 GALVANIC CORROSION ON SEAT TRACK BETWEEN FR36 TO FR41, -Y1292. REPLACED SEAT TRACK BETWEEN FR36 TO FR41, -Y1292 IAW A320 SRM 51-72-11 & AIRBUS DRAWING D53370500.Oct 7, 2010 · N103US · Airbus A320214 · Fuselage, Seat/Cargo Attach FittingsSDR USAA2010102592396Support Fitting · wornSAL - S5 - MAJOR REPAIR - WEAR ON SUPPORT FITTING ASSEMBLY AT R-2 DOOR. REPLACED SUPPORT FITTING ASSEMBLY AT R-2 DOOR IAW A320 CMM 52-13-15.Oct 7, 2010 · N103US · Airbus A320214 · Passenger/Crew DoorsSDR USAA2010102592394Seat Track · corrodedSAL - S5 - MAJOR REPAIR - CORROSION ON SEAT TRACK BETWEEN FR12 TO FR24, -Y765. REPLACED SEAT TRACK BETWEEN FR12 TO FR24, -Y765 IAW A320 SRM 51-72-11 & AIRBUS DRAWING D53112812.Oct 7, 2010 · N103US · Airbus A320214 · Fuselage, Seat/Cargo Attach FittingsSDR USAA2010102592393Seat Track · corrodedSAL - S5 - MAJOR REPAIR - CORROSION ON SEAT TRACK BETWEEN FR12 TO FR24, Y1292. REPLACED SEAT TRACK BETWEEN FR12 TO FR24, Y1292 IAW A320 SRM 51-72-11 & AIRBUS DRAWING D53112812.Oct 7, 2010 · N103US · Airbus A320214 · Fuselage, Seat/Cargo Attach FittingsSDR USAA2010110492512Skin · saturatedSAL - S5 - MAJOR REPAIR - TRAPPED WATER FOUND IN LEFT ELEVATOR UPPER SKIN HONEYCOMB STRUCTURE BETWEEN STAB STA 527 TO STAB STA 601, 37 INCHES INBOARD FROM HORIZ STAB RIB 8 TO RIB 10 & 7 INCHES FROM LEADING EDGE. REPAIRED LEFT ELEVATOR UPPER SKIN HONEYCOMB STROct 4, 2010 · N103US · Airbus A320214 · Elevator, Plate/SkinSDR USAA2010110492511Skin · saturatedSAL - S5 - MAJOR REPAIR - TRAPPED WATER FOUND IN LEFT ELEVATOR UPPER SKIN HONEYCOMB STRUCTURE BETWEEN STAB STA 466 TO STAB STA 589, 69 INCHES INBOARD FROM HORIZ STAB RIB 8 TO RIB 10 & 6 INCHES FROM LEADING EDGE. REPAIRED LEFT ELEVATOR UPPER SKIN HONEYCOMB STRUOct 4, 2010 · N103US · Airbus A320214 · Elevator, Plate/SkinSDR USAA2010110492510Skin · saturatedSAL - S5 - MAJOR REPAIR - TRAPPED WATER FOUND IN LEFT ELEVATOR UPPER SKIN HONEYCOMB STRUCTURE BETWEEN STAB STA131 TO STAB STA 227, 23 INCHES OUTBOARD FROM HORIZ STAB RIB 1 TO RIB 3 & 6 INCHES FROM LEADING EDGE. REPAIRED LEFT ELEVATOR UPPER SKIN HONEYCOMB STRUOct 4, 2010 · N103US · Airbus A320214 · Elevator, Plate/SkinSDR USAA2010110492509Skin · saturatedSAL - S5 - MAJOR REPAIR - TRAPPED WATER FOUND IN LEFT ELEVATOR UPPER SKIN HONEYCOMB STRUCTURE BETWEEN STAB STA 131 TO STAB STA 227, 13 INCHES OUTBOARD FROM HORIZ STAB RIB 1 TO RIB 3 & 9 INCHES FROM LEADING EDGE. REPAIRED LEFT ELEVATOR UPPER SKIN HONEYCOMB STROct 4, 2010 · N103US · Airbus A320214 · Elevator, Plate/SkinSDR USAA2010110492508Skin · saturatedSAL - S5 - MAJOR REPAIR - NR 6284654 - TRAPPED WATER FOUND IN RIGHT HAND ELEVATOR UPPER SKIN HONEYCOMB STRUCTURE BETWEEN STAB STA181 TO STAB STA271, 32 INCHES OUTBOARD FROM HORIZ STAB RIB 1 TO RIB 3 & 5 INCHES FROM TRAILING EDGE. REPAIRED RIGHT HAND ELEVATOR UOct 4, 2010 · N103US · Airbus A320214 · Elevator, Plate/SkinSDR USAA2010110492507Skin · saturatedSAL - S5 - MAJOR REPAIR - TRAPPED WATER FOUND IN RIGHT ELEVATOR UPPER SKIN HONEYCOMB STRUCTURE BETWEEN STAB STA 446 TO STAB STA 601, 32 INCHES INBOARD FROM HORIZ STAB RIB 9 TO RIB 10 & 5 INCHES FROM LEADING EDGE. REPAIRED RIGHT ELEVATOR UPPER SKIN HONEYCOMB SOct 4, 2010 · N103US · Airbus A320214 · Elevator, Plate/SkinSDR USAA2010110492506Skin · saturatedSAL - S5 - MAJOR REPAIR - TRAPPED WATER FOUND IN RIGHT ELEVATOR UPPER SKIN HONEYCOMB STRUCTURE BETWEEN STAB STA 271 TO STAB STA 404, 42 INCHES OUTBOARD FROM HORIZ STAB RIB 5 TO RIB 8 & 5 INCHES FROM LEADING EDGE. REPAIRED RIGHT ELEVATOR UPPER SKIN HONEYCOMB SOct 4, 2010 · N103US · Airbus A320214 · Elevator, Plate/SkinSDR USAA2010110492505Skin · saturatedSAL - S5 - MAJOR REPAIR - TRAPPED WATER FOUND IN RIGHT ELEVATOR UPPER SKIN HONEYCOMB STRUCTURE BETWEEN STAB STA 271 TO STAB STA 404, 56 INCHES OUTBOARD FROM HORIZ STAB RIB 5 TO RIB 8 & 10 INCHES FROM LEADING EDGE. REPAIRED RIGHT ELEVATOR UPPER SKIN HONEYCOMB Oct 4, 2010 · N103US · Airbus A320214 · Elevator, Plate/SkinSDR USAA2009111993168Lens · missingFLT 727 - DEN - EEL - R2 DOOR EMERGENCY LIGHT LENS MISSING. MAINTENANCE INSTALLED LENS AS REQUIRED.Nov 18, 2009 · N103US · Airbus A320214 · Emergency LightingSDR USAA2009052791293Light · odorLOG PAGE 8599434 - FLT 1781-OKC - BURNING ODOR AROUND ROW 20 RT - NO VISIBLE SMOKE. MAINTENANCE FOUND NO OBVIOUS DEFECTS TO CAUSE BURNING ODOR. MAINTENANCE RELAMPED THE READING LIGHT AT 20D. NO SUBSEQUENT EVENTS.May 26, 2009 · N103US · Airbus A320214 · Passenger Compartment LightingSDR USAA2009022390401Power Supply · malfunctionedFLT 1195 - PHL - EEL - FORWARD CEILING EMERGENCY LIGHT WILL NOT ILLUMINATE. MAINTENANCE RESET THE POWER SUPPLY UNIT - OPERATIONAL CHECK GOOD.Feb 20, 2009 · N103US · Airbus A320214 · Emergency LightingSDR USAA2008120992196Unknown · fumesFLT 873 LAS-SAN - FUMES - PASSENGERS SEATED AFT OF THE WING COMPLAINED OF FUMES IN THE CABIN, EYE IRRITATION AND SNEEZING. MAINTENANCE INSPECTED THE APU FOR LEAKS - NONE NOTED. RAN THE APU AND BOTH ENGINES INDEPENDENTLY WITH NO ODORS NOTED. AIRCRAFT IS OK FDec 8, 2008 · N103US · Airbus A320214 · Air Distribution SystemSDR USAA920080921Hose · rupturedFLT NR 1910 CLT-LGA - DIV - CREW REPORTED GREEN HYDRAULIC LOW LEVEL LIGHT DURING CRUISE. THE CREW DECLARED AN EMERGENCY AND DIVERTED TO PHL. AIRCRAFT WAS TOWED TO GATE DUE TO LOSS OF NOSE WHEEL STEERING. MAINTENANCE REPLACED RUPTURED HYDRAULIC SENSE LINE, AApr 25, 2008 · N103US · Airbus A320214 · Hydraulic System, MainSDR SA06090Epsu · faultedCLT - RECEIVED -EMER L- MESSAGE DURING THE EMERGENCY LIGHTS TEST. MAINTENANCE REPLACED THE MID-CABIN, LEFT EMERGENCY POWER SUPPLY UNIT. OPERATIONALLY CHECKS OK.Dec 2, 2006 · N103US · Airbus A320214 · Emergency LightingSDR SA06078Control Unit · faultyRDU - FLT 873 ON TAKEOFF, RDU TO PHL, DURING TAKEOFF ROLL, THE AIRCRAFT RIGHT BRAKE LOCKED UP. THE FLIGHT REJECTED TAKEOFF AT ABOUT 50-60 KNOTS. AFTERWARDS, THE TOWER REPORTED TO THE CREW THAT THE NR 3 MAIN GEAR WHEEL ASSEMBLY APPEARED TO HAVE SMOKE COMING FOct 3, 2006 · N103US · Airbus A320214 · BrakeSDR USAA040969Sill · corrodedPIT - S1 - SILL, 1 INCH X 1 INCH X .07 INCH DEEP; CORROSION; LEVEL 2; TASK NR JA-260-53500-006; CABIN FLOOR, R-2 DOOR SEAL ASSY ON CROSSBEAM C66 AND AFT ENDI OF FRAME - Y1732. REPLACED DOOR SEAL IAW SRM 51-74-00, 53-41-14, 51-42-11.Nov 3, 2004 · N103US · Airbus A320214 · Fuselage Miscellaneous StructureSDR USAA040955Floor Support · corrodedBFM - S1 - FLOOR SUPPORT, 2 INCH X 3 INCH X 0.075 INCH AREA; CORROSION; LEVEL 2; TASK NR JA-220-53500; MAIN CABIN FLOOR - Y254 BET FR 16 AND 20. FABRICATED PARTS IAW SRM 53-00-14 FIG 206 PR SRM 53-11-14, 51-74-00, 53-14-00, 51-42-11.Nov 3, 2004 · N103US · Airbus A320214 · Fuselage Miscellaneous StructureSDR USAA040958Track · corrodedBFM - S1 - TRACK ASSEMBLY, 2 INCH X 2 INCH X 0.50 INCH AREA, CORROSION LEVEL 2; TASK NR JA-220-53500, MAIN CABIN FLOOR- Y254 BET FR16 AND 23. REMOVED AND REPLACED IAW SRM.Nov 2, 2004 · N103US · Airbus A320214 · Fuselage Miscellaneous StructureSDR USAA040957Web · corrodedBFM - S1 - FLOOR WEB, 1.5 INCH X 2 INCHES X 0.50 INCH AREA, CORROSION; LEVEL 2; TASK NR JA-220-53500, MAIN CABIN FLOOR; Y1584, BET FR14 AND 16. REMOVED AND REPLACED IAW SRM.Nov 2, 2004 · N103US · Airbus A320214 · Fuselage Miscellaneous StructureSDR USAA040959Support · corrodedBFM - S1 - SUPPORT, 2 INCH X 5 INCHES X .025 INCH AREA; CORROSION; LEVEL 2; TASK NR JA-220-53500, MAIN CABIN FL -Y189, FR 20. REMOVED AND REPLACED IAW SRM.Nov 1, 2004 · N103US · Airbus A320214 · Fuselage Miscellaneous StructureSDR USAA040966Dummy Rail · corrodedBFM - S1 - DUMMY RAIL, 2 INCHES X 1 INCH X .050 INCH AREA; CORROSION; LEVEL 2; TASK NR JA-220-53500. MAIN CABIN FLOOR @ FR 16, LB -Y81. REPLACED DUMMY RAIL IAW SRM.Oct 31, 2004 · N103US · Airbus A320214 · Fuselage, Seat/Cargo Attach FittingsSDR USAA040962Floor Support · corrodedBFM - S1 - FLOOR SUPPORT, 1.5 INCH X 2 INCHES X .040 INCH AREA; CORROSION; LEVEL 2; TASK NR JA-200-53500, BTW FR 16 AND 20, Y1292, FLOOR SUPPORT. REPLACED FLOOR SUPPORT IAW SRM 51-74-00, 53-11-14, 51-42-11.Oct 31, 2004 · N103US · Airbus A320214 · Fuselage Miscellaneous StructureSDR USAA040956Floor Support · corrodedBFM - S1 - FLOOR SUPPORT, 2 INCHES X 12 INCHES X 0.020 INCH AREA, CORROSION; LEVEL 2; TASK NR JA-220-53500, MAIN CABIN FLOOR BET FR 16, 20, BL-Y1292. REPLACED FLOOR SUPPORT IAW SRM 51-74-00, 53-11-14, 51-42-11.Oct 31, 2004 · N103US · Airbus A320214 · Fuselage Miscellaneous StructureSDR USAA040954Support · corrodedBFM - S1- SEAL SUPPORT, .5 INCH X .5 INCH AREA; CORROSION; LEVEL 2; TASK NR JA-220-53500-015, MAIN CABIN FLOORBOARD SEAL SUPPORT AT Y1584 BETWEEN 14 AND 16. REMOVED AND REPLACED FLOORBOARD SEAL SUPPORT IAW SRM 51-74-00, SRM 53-11-14, SRM 51-42-11.Oct 31, 2004 · N103US · Airbus A320214 · Fuselage Miscellaneous StructureSDR USAA040965Floorbeam · corrodedBFM - S1 - FLOORBEAM- 2 INCHES X 1.5 INCHES X .04 INCH AREA; CORROSION; LEVEL 2; TASK NR JA-260-53500-012, Y1292, BTW C68 AND C69 MAIN CABIN FLOOR. REMOVED AND REPLACED FLOOR BEAM IAW SRM 53-00-14, SRM 51-42-11.Oct 30, 2004 · N103US · Airbus A320214 · Fuselage Main, Floor BeamSDR USAA040963Dummy Rail · corrodedPIT - S1 - DUMMY RAIL, 2.5 INCHES X 2 INCHES X .075 INCH AREA; CORROSION; LEVEL 2; TASK NR JA-220-53500; MAIN CABIN FLOOR FR 16, Y503.2. REPLACED DUMMY RAIL (BEAM) ALT PN INSTALLED IAW SRM 51-74-00, 53-11-14, 51-42-11.Oct 30, 2004 · N103US · Airbus A320214 · Fuselage, Seat/Cargo Attach FittingsSDR USAA040960Floorbeam · corrodedBFM - S1 - BEAM, 18 INCHES X 2 INCHES X .03 INCH AREA, CORROSION; LEVEL 2; TSK NR JA 260-53500-004, MAINT CABIN FLOOR Y1292 BET C66 AND C68. REMOVED AND REPLACED FLOORBEAM IAW SRM.Oct 30, 2004 · N103US · Airbus A320214 · Fuselage Main, Floor BeamSDR USAA040964Shear Plate · corrodedBFM - S2 - SHEAR PLATE, 1 INCH X 1 INCH X .030 INCH AREA, CORROSION; LEVEL 2; TASK NR JA-260-53500, MAIN CABIN FLOOR BTW 69 AND 70, BL - Y1292. REMOVED AND REPLACED SHEAR PLATE (WEB) IAW SRM.Oct 29, 2004 · N103US · Airbus A320214 · Fuselage Miscellaneous StructureSDR USAA040961Floorbeam · corrodedBFM - S1 - BEAM, 3 INCHES X 2 INCHES X .030 INCH AREA, CORROSION; LEVEL 2; TASK NR JA-260-53500; MAIN DECK FLOOR RAIL, FRAME 68, -Y765. REMOVED AND REPLACED FLOORBEAM IAW SRM 53-00-14, 51-42-11.Oct 28, 2004 · N103US · Airbus A320214 · Fuselage Main, Floor BeamSDR SA04092Slide · separatedTHE SLIDE SHOP FOUND THAT THE BRIDGING ON UPPER TUBE AT RUNWAY END HAD A SEAM SEPARATION. THE REPAIR SHOP SENT THE SLIDE BACK TO THE VENDOR FOR REPAIR.Sep 29, 2004 · N103US · Airbus A320214 · Escape SlideSDR USAASA03039Battery · inoperativeDURING EMERGENCY LIGHTS TEST, RECEIVED 'EPSU INT LOAD EMER R' FAULT. MAINTENANCE REPLACED EMERGENCY POWER SUPPLY UNIT BATTERY PACK AT THE RIGHT EMERGENCY EXIT. OPERATIONALLY CHECKS OK. (M)May 13, 2003 · N103US · Airbus A320214 · Emergency LightingSDR USAASA02007Relay · failedLGA - THE EMERGENCY EXIT LIGHTS DO NOT ILLUMINATE WHEN PED SWITCH IS TURNED ON. MAINTENANCE REPLACED RELAY. OPERATIONALLY CHECKS OK. (M)Jan 11, 2002 · N103US · Airbus A320214 · Emergency LightingSDR USAASA01068Cam · brokenBOS - L1 DOOR ARMING CAM BROKE. MAINTENANCE REPLACED THE CAM. SMELL PIECE FELL FROM MAIN ENTRY DOOR. REPLACED DOOR HOOK. OPS OK. (M)Dec 21, 2001 · N103US · Airbus A320214 · Passenger/Crew DoorsSDR USAASA00016Electronic Unit · odorDCA-LGA - FLT 6360 - PASSENGER REPORTED ELECTRICAL FUMES AT ROW 20. MAINTENANCE REPLACED SEB AT ROW 20. SYSTEM TEST OK. (M)Apr 20, 2000 · N103US · Airbus A320214 · Electrical Power SystemSDR USAASA00013Slide · malfunctionedBOS - FOUND FORWARD LEFT ESCAPE SLIDE FAILED EMERGENCY LIGHT CHECK. CIDS DISPLAYED EPSU EXT LOAD FWD LT. MAINTENANCE REPLACED THE FORWARD LEFT ESCAPE SLIDE. OPERATIONAL CHECK OK. (M)Apr 2, 2000 · N103US · Airbus A320214 · Escape SlideSDR USAA991004Skin · disbondedDURING A-2 CHECK VISUAL INSPECTION, FOUND A 12 INCH BY 36 INCH DISBONDED AREA AT SLIDE DOOR COVERING OUTER SKIN AND LEFT A/C RT OFF WING SLIDE DOOR. REMOVED AND REPLACED SLIDE. (X)Sep 14, 1999 · N103US · Airbus A320214 · Emergency Exits
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