N122US

Service difficulty reports · 347

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 = 'N122US' 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 USAA2012121800017Floor Panel · delaminated2S CHECK - DELAMINATION ON FLOOR PANEL 252EF BETWEEN FR47 TO FR51 & BETWEEN -Y1732 TO -Y1292. REPLACED FLOOR PANEL 252EF IAW A320 SRM 53-02-00 FIG 209 & IRM 9701 REV G.Dec 4, 2012 · N122US · Airbus A320214 · Fuselage Floor PanelSDR USAA2012121800015Floor Panel · delaminated2S CHECK - DELAMINATION ON FLOOR PANEL 251GF BETWEEN FR51 TO FR54 & BETWEEN Y254 TO Y765. REPLACED FLOOR PANEL 251GF IAW A320 SRM 53-02-00 FIG 209 & IRM 9701 REV G.Dec 4, 2012 · N122US · Airbus A320214 · Fuselage Floor PanelSDR USAA2013011400055Web · cracked2S CHECK - CRACK ON WEB AT FLIGHT COMPARTMENT FLOOR STRUCTURE AREA BETWEEN FR8 TO FR11, Y765. REPLACED FLIGHT COMPARTMENT FLOOR STRUCTURE WEB BETWEEN FR8 TO FR11, Y765 IAW A320 SRM 51-72-11 & AIRBUS DRAWING D53110285.Dec 3, 2012 · N122US · Airbus A320214 · Fuselage Miscellaneous StructureSDR USAA2013011000023Skin · worn2S CHECK - WORN AREA INTERNAL LOWER SKIN OF SLAT TRACK NR 5 AT SLAT NR 2 BETWEEN WS 486 TO WS 670 OF RIGHT WING. REPAIRED RIGHT WING LOWER SKIN OF SLAT TRACK NR 5 AT SLAT NR 2 BETWEEN WS 486 TO WS 670 IAW A320 EA 503633.Dec 3, 2012 · N122US · Airbus A320214 · Leading Edge DevicesSDR USAA2013011000008Flap · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION AT 2 POINTS ON INTERNAL AREA BETWEEN INNER RIB & OUTBOARD RIB 14 ON LEFT WING OUTBOARD FLAP BETWEEN WS 486 TO WS 11664 & BETWEEN RIB 9 TO RIB 22. REPLACED LEFT WING OUTBOARD FLAP IAW A320 AMM 27-54-62.Dec 3, 2012 · N122US · Airbus A320214 · Trailing Edge FlapsSDR USAA2013011000007Rib · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION AT 6 POINTS ON INTERNAL AREA OF OUTBOARD FACE OF RIB 15 ON LEFT WING OUTBOARD FLAP BETWEEN WS 486 TO WS 11664 & BETWEEN RIB 9 TO RIB 22. REPLACED LEFT WING OUTBOARD FLAP IAW A320 AMM 27-54-62.Dec 3, 2012 · N122US · Airbus A320214 · Trailing Edge FlapsSDR USAA2012122000016Fitting · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON CORNER FITTING AT AFT PASSENGER/CREW DOORWAY AT FR68, S23R. REPLACED CORNER FITTING AT AFT PASSENGER/CREW DOORWAY AT FR68, S23R IAW A320 SRM 51-72-11 & AIRBUS DRAWING D53480505.Dec 3, 2012 · N122US · Airbus A320214 · Fuselage Miscellaneous StructureSDR USAA2012122000014Sill · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON SHAPE SILL (CENTER FITTING) AT AFT PASSENGER/CREW DOORWAY BETWEEN FR66 TO FR68, S23R. REPLACED SHAPE SILL AT AFT PASSENGER/CREW DOORWAY BETWEEN FR66 TO FR68, S23R IAW A320 SRM 51-72-11 & AIRBUS DRAWING D53480505.Dec 3, 2012 · N122US · Airbus A320214 · Fuselage Miscellaneous StructureSDR USAA2012121800014Web · cracked2S CHECK - CRACK IN WEB OF FLIGHT COMPARTMENT FLOOR STRUCTURE BETWEEN FR8 TO FR11, S23R, -Y765. REPLACED WEB BETWEEN FR8 TO FR11, S23R, -Y765 IAW A320 SRM 51-72-11 & AIRBUS DRAWING D53113322.Dec 3, 2012 · N122US · Airbus A320214 · Fuselage Miscellaneous StructureSDR USAA2012121800022Floor Panel · delaminated2S CHECK - DELAMINATION ON FLOOR PANEL 221DF BETWEEN FR16 TO FR21 & BETWEEN -Y254 TO Y254. REPLACED FLOOR PANEL 221DF IAW A320 SRM 53-12-00 FIG 206 & IRM 9701 REV G.Dec 2, 2012 · N122US · Airbus A320214 · Fuselage Floor PanelSDR USAA2013010200023Floor Panel · delaminated2S CHECK - DELAMINATION ON FLOOR PANEL 262BG BETWEEN FR64 TO FR66 & BETWEEN -Y254 TO -Y1732. REPLACED FLOOR PANEL 262BG IAW A320 SRM 53-02-00 F209, EA 503642/504555A & MCGILL IRM 9701 REV G.Dec 2, 2012 · N122US · Airbus A320214 · Fuselage Floor PanelSDR USAA2013010200021Fitting · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON L1 DOOR CENTER FITTING BETWEEN FR16 TO FR20, S23R. REPLACED L1 DOOR CENTER FITTING BETWEEN FR16 TO FR20, S23R IAW A320 SRM 51-72-11 & AIRBUS DRAWING D53112109.Dec 2, 2012 · N122US · Airbus A320214 · Fuselage Miscellaneous StructureSDR USAA2012122100020Floor Panel · delaminated2S CHECK - DELAMINATION ON FLOOR PANEL 261BG BETWEEN FR64 TO FR66 & BETWEEN Y254 TO Y1732. REPLACED FLOOR PANEL 261BG IAW A320 SRM 53-02-00 FIG 209, EA 503641 & IRM 9701, REV G.Dec 2, 2012 · N122US · Airbus A320214 · Fuselage Floor PanelSDR USAA2012122000015Fitting · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON CENTER FITTING AT FORWARD PASSENGER/CREW DOORWAY BETWEEN FR16 TO FR20, S23L. REPLACED CENTER FITTING AT FORWARD PASSENGER/CREW DOORWAY BETWEEN FR16 TO FR20, S23L IAW A320 SRM 51-72-11 & AIRBUS DRAWING D53112109.Dec 2, 2012 · N122US · Airbus A320214 · Fuselage Miscellaneous StructureSDR USAA2012121800021Floor Panel · delaminated2S CHECK - DELAMINATION ON FLOOR PANEL 221PF BETWEEN FR12 TO FR16 & BETWEEN Y254 TO Y1732. REPLACED FLOOR PANEL 221PF IAW A320 SRM 53-12-00 FIG 206 & IRM 9701 REV G.Dec 2, 2012 · N122US · Airbus A320214 · Fuselage Floor PanelSDR USAA2012121800018Floor Panel · delaminated2S CHECK - DELAMINATION ON FLOOR PANEL 242LF BETWEEN FR42 TO FR47 & BETWEEN -Y1292 TO -Y765. REPLACED FLOOR PANEL 242LF IAW A320 SRM 53-02-00 FIG 209 & IRM 9701 REV G.Dec 2, 2012 · N122US · Airbus A320214 · Fuselage Floor PanelSDR USAA2012121800016Floor Panel · delaminated2S CHECK - DELAMINATION ON FLOOR PANEL 231FF BETWEEN FR20 TO FR24 & BETWEEN Y1732 TO Y1292. REPLACED FLOOR PANEL 231FF IAW A320 SRM 53-12-00 FIG 206 & IRM 9701 REV G.Dec 2, 2012 · N122US · Airbus A320214 · Fuselage Floor PanelSDR USAA2013011000024Fitting · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION CORNER FITTING AT FORWARD CARGO DOORWAY AT FR28, S38R. REPLACED CORNER FITTING AT FORWARD CARGO DOORWAY AT FR28, S38R IAW A320 SRM 51-72-11 & EA 503689.Dec 1, 2012 · N122US · Airbus A320214 · Fuselage Miscellaneous StructureSDR USAA2013011000005Web · corroded2S CHECK - LEVEL 2 FILFORM CORROSION ON FLOOR STRUCTURE WEB BETWEEN FR12 TO FR16, Y1732. REPLACED FLOOR STRUCTURE WEB BETWEEN FR12 TO FR16, Y1732 IAW A320 SRM 51-72-11 EA 503659 & AIRBUS DRAWING D53114392.Dec 1, 2012 · N122US · Airbus A320214 · Fuselage Miscellaneous StructureSDR USAA2013010900015Seat Track · corroded2S CHECK - 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 & AIRBUS DRAWING D53231730.Dec 1, 2012 · N122US · Airbus A320214 · Fuselage, Seat/Cargo Attach FittingsSDR USAA2013010900014Seat Track · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON SEAT TRACK BETWEEN FR47 TO FR64, -Y1292. REPLACED SEAT TRACK BETWEEN FR47 TO FR64, -Y1292 IAW A320 SRM 51-72-11 & AIRBUS DRAWING D53472770.Dec 1, 2012 · N122US · Airbus A320214 · Fuselage, Seat/Cargo Attach FittingsSDR USAA2013010900011Coupling · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON COUPLING AT FR64, -Y1292. REPLACED COUPLING AT FR64, -Y1292 IAW A320 SRM 51-72-11 & AIRBUS DRAWING D53472831.Dec 1, 2012 · N122US · Airbus A320214 · Fuselage Miscellaneous StructureSDR USAA2013010900008Coupling · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON COUPLING AT FR64, -Y1292. REPLACED COUPLING AT FR64, -Y1292 IAW A320 SRM 51-72-11 & AIRBUS DRAWING D53472831.Dec 1, 2012 · N122US · Airbus A320214 · Fuselage Miscellaneous StructureSDR USAA2013010200022Seat Track · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON SEAT TRACK BETWEEN FR12 TO FR24, Y1292. REPLACED SEAT TRACK BETWEEN FR12 TO FR24, Y1292 IAW A320 SRM 53-72-11 & AIRBUS DRAWING D53110920 & D53112812.Dec 1, 2012 · N122US · Airbus A320214 · Fuselage, Seat/Cargo Attach FittingsSDR USAA2012122400012Seat Track · corroded2S CHECK - LEVEL 2 GALVANIC 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 & D53110920.Dec 1, 2012 · N122US · Airbus A320214 · Fuselage, Seat/Cargo Attach FittingsSDR USAA2012122100021Floor Panel · delaminated2S CHECK - DELAMINATION ON FLOOR PANEL 151GF BETWEEN FR52 TO FR56 & BETWEEN Y765 TO -Y765. REPLACED FLOOR PANEL 151GF IAW A320 SRM 53-02-00 FIG 209, IRM 9701, REV G.Dec 1, 2012 · N122US · Airbus A320214 · Fuselage Floor PanelSDR USAA2012122100019Floor Panel · delaminated2S CHECK - DELAMINATION ON FLOOR PANEL 151DF BETWEEN FR49 TO FR53 & BETWEEN Y765 TO -Y765. REPLACED FLOOR PANEL 151DF IAW A320 SRM 53-02-00 FIG 209 & IRM 9701, REV G.Dec 1, 2012 · N122US · Airbus A320214 · Fuselage Floor PanelSDR USAA2012122000020Seat Track · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON SEAT TRACK BETWEEN FR36 TO FR41, Y765. REPLACED SEAT TRACK BETWEEN FR36 TO FR41, Y765 IAW A320 SRM 51-42-11 & AIRBUS DRAWING D53370500.Dec 1, 2012 · N122US · Airbus A320214 · Fuselage, Seat/Cargo Attach FittingsSDR USAA2012122000019Seat Track · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON SEAT TRACK BETWEEN FR47 TO FR64, Y1292. REPLACED SEAT TRACK BETWEEN FR47 TO FR64, Y1292 IAW A320 SRM 51-72-11, 53-41-15, AIRBUS DRAWING D53472176 & D53472831.Dec 1, 2012 · N122US · Airbus A320214 · Fuselage, Seat/Cargo Attach FittingsSDR USAA2012122000018Seat Track · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON SEAT RAIL BETWEEN FR47 TO FR64, -Y765. REPLACED SEAT RAIL BETWEEN FR47 TO FR64, -Y765 IAW A320 SRM 51-72-11 & AIRBUS DRAWING D53472770.Dec 1, 2012 · N122US · Airbus A320214 · Fuselage, Seat/Cargo Attach FittingsSDR USAA2012122000017Seat Track · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON SEAT RAIL BETWEEN FR47 TO FR64, Y765. REPLACED SEAT RAIL BETWEEN FR47 TO FR64, Y765 IAW A320 SRM 51-72-11.Dec 1, 2012 · N122US · Airbus A320214 · Fuselage, Seat/Cargo Attach FittingsSDR USAA2012121000024Cleat · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON CLEAT AT FR26 BETWEEN S41L TO S42L. REPLACED CLEAT AT FR26 BETWEEN S41L TO S42L IAW A320 SRM 51-72-11 & AIRBUS DRAWING D53230829.Dec 1, 2012 · N122US · Airbus A320214 · Fuselage Miscellaneous StructureSDR USAA2013010700025Hinge Fitting · excess play2S CHECK - EXCESSIVE PLAY ON RUDDER HINGE ARM END FITTING NR 7 AT FORK END AT VERTICAL STABILIZER STA 561, RIB 11. REPLACED RUDDER HINGE ARM END FITTING NR 7 IAW A320 SRM 51-72-11.Nov 30, 2012 · N122US · Airbus A320214 · Rudder StructureSDR USAA2013010300004Sill · corroded2S CHECK - CORROSION ON R2 DOOR SILL BETWEEN FR66 TO FR68, S23R, -Y1732. REPAIRED R2 DOOR SILL BETWEEN FR66 TO FR68, S23R, -Y1732 IAW A320 SRM 51-72-11, AIRBUS DRAWING D53480505, D53480076 & EA 503612.Nov 28, 2012 · N122US · Airbus A320214 · Fuselage Miscellaneous StructureSDR USAA2013010200020Fitting · corroded2S CHECK - CORROSION ON R1 DOOR LOWER SILL FITTING BETWEEN FR16 TO FR20, -Y1732. REPLACED R1 DOOR LOWER SILL FITTING BETWEEN FR16 TO FR20, -Y1732 IAW A320 SRM 51-72-11 & AIRBUS DRAWING D53110339.Nov 28, 2012 · N122US · Airbus A320214 · Fuselage Miscellaneous StructureSDR USAA2012072300026Bottle · low pressureL2 DOOR ASSIST BOTTLE PRESSURE BELOW 1300 PSI. SERVICED L2 DOOR ASSIST BOTTLE TO 1850 PSI.Jul 21, 2012 · N122US · Airbus A320214 · Passenger/Crew DoorsSDR USAA2012062500019Lens · missingR2 DOOR LOWER EMERGENCY LIGHT LENS MISSING. REPLACED EMERGENCY LIGHT LENS ON R-2 DOOR.Jun 22, 2012 · N122US · Airbus A320214 · Emergency LightingSDR USAA2012031900023Battery · dischargedEMERGENCY FLASHLIGHT BATTERY DEAD ON REAR RT FLIGHT ATTENDANT SEAT AND REAR SWING F/A SEAT. REMOVED AND REPLACED BATTERIES IN EMERGENCY FLASHLIGHTS.Mar 17, 2012 · N122US · Airbus A320214 · Emergency EquipmentSDR USAA2012031200009Floorbeam · corrodedC11 CHECK - LEVEL 2 EXFOLIATION CORROSION ON FLOORBEAM BETWEEN FR66 TO FR70, Z-500, -Y765. REPLACED FLOORBEAM BETWEEN FR66 TO FR70, Z-500, -Y765 IAW A320 SRM 51-72-11.Mar 9, 2012 · N122US · Airbus A320214 · Fuselage Main, Floor BeamSDR USAA2012030900010Floor Panel · delaminatedC11 CHECK - DELAMINATION ON FLOOR PANEL # 232DF BETWEEN FR12 TO FR16, Z-500, -Y510. REPLACED FLOOR PANEL # 232DF IAW JOB CARD # 26C22053014 & IRM 9701.Mar 9, 2012 · N122US · Airbus A320214 · Fuselage Floor PanelSDR USAA2012031200007Shear Plate · crackedC11 CHECK - CRACK ON SHEAR PLATE BETWEEN FR68 TO FR69.6, Z-500, -Y1292. REPLACED SHEAR PLATE BETWEEN FR68 TO FR69.6, Z-500, -Y1292 IAW A320 SRM 51-72-11 & TYPICAL REPAIR # TR320-2528-10-0011C.Mar 8, 2012 · N122US · Airbus A320214 · Fuselage Miscellaneous StructureSDR USAA2012031200005Shear Plate · crackedC11 CHECK - SHEAR PLATE CRACKED BETWEEN FR68 TO FR69, Z-500, -Y1162.5. REPLACED SHEAR PLATE BETWEEN FR68 TO FR69, Z-500, -Y1162.5 IAW A320 SRM 53-41-14, 51-21-11, 51-23-11 & 51-72-11.Mar 8, 2012 · N122US · Airbus A320214 · Fuselage Miscellaneous StructureSDR USAA2012030900007Floorbeam · corrodedC11 CHECK - LEVEL 2 GALVANIC CORROSION ON FLOORBEAM BETWEEN FR16 TO FR21, Z-500, Y254. REPLACED FLOORBEAM BETWEEN FR16 TO FR21, Z-500, Y254 IAW A320 SRM 51-72-11.Mar 8, 2012 · N122US · Airbus A320214 · Fuselage Main, Floor BeamSDR USAA2012030800022Floorbeam · corrodedC11 CHECK - LEVEL 2 EXFOLIATION CORROSION ON FLOORBEAM AT FR20, -Y1292. REPLACED FLOORBEAM AT FR20, -Y1292 IAW A320 SRM 51-42-11.Mar 8, 2012 · N122US · Airbus A320214 · Fuselage Main, Floor BeamSDR USAA2012030700001Floor Panel · delaminatedC11 CHECK - DELAMINATION ON FLOOR PANEL # 221DF BETWEEN FR16 TO FR20, Z-500, Y=0. REPLACED FLOOR PANEL # 221DF IAW IRM 9701 REV G.Mar 6, 2012 · N122US · Airbus A320214 · Fuselage Floor PanelSDR USAA2012031200014Seat Track · corrodedC11 CHECK - LEVEL 2 EXFOLIATION CORROSION ON SEAT TRACK FLOORBEAM AT FR64, Z-500, -Y765. REPLACED SEAT TRACK FLOORBEAM AT FR64, Z-500, -Y765 IAW A320 SRM 51-72-11 & EA # 201988.Mar 3, 2012 · N122US · Airbus A320214 · Fuselage, Seat/Cargo Attach FittingsSDR USAA2012030900008Floorbeam · corrodedC11 CHECK - LEVEL 2 EXFOLIATION CORROSION ON FLOORBEAM BETWEEN FR16 TO FR21, Z-500, -Y254. REPLACED FLOORBEAM BETWEEN FR16 TO FR21, Z-500, -Y254 IAW A320 SRM 51-72-11.Mar 3, 2012 · N122US · Airbus A320214 · Fuselage Main, Floor BeamSDR USAA2012030900005Support · corrodedC11 CHECK - LEVEL 2 GALVANIC CORROSION ON SHEAR TIE SUPPORT BETWEEN FR69 TO FR70, Z-500 & BETWEEN -Y1162.5 TO -Y1292. REPLACED SHEAR TIE SUPPORT BETWEEN FR69 TO FR70, Z-500 & BETWEEN -Y1162.5 TO -Y1292 IAW A320 SRM 51-72-11.Mar 3, 2012 · N122US · Airbus A320214 · Fuselage Miscellaneous StructureSDR USAA2012030800003Floorbeam · corrodedC11 CHECK - LEVEL 2 EXFOLIATION CORROSION ON FLOORBEAM AT FR20, Z-500, -Y765. REPLACED FLOORBEAM AT FR20, Z-500, -Y765 IAW A320 SRM 51-72-11 & AIRBUS DRAWING # D53112807.Mar 3, 2012 · N122US · Airbus A320214 · Fuselage Main, Floor BeamSDR USAA2012031600005Cover · corrodedC11/SY6 CHECK - LEVEL 2 EXFOLIATION CORROSION ON JOINT COVER BETWEEN FR12 TO FR14, -Y81, -Z500. REPLACED JOINT COVER BETWEEN FR12 TO FR14, -Y81, -Z500 IAW A320 SRM 51-42-11.Mar 2, 2012 · N122US · Airbus A320214 · Fuselage Miscellaneous Structure
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