N742PS

Service difficulty reports · 263

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 = 'N742PS' 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 USAA2011120900018Floor Panel · delaminated2S CHECK - DELAMIANTION ON FLOOR PANEL 251RF BETWEEN FR58 TO FR62 & BETWEEN Y254 TO Y765. REPLACED FLOOR PANEL 251RF IAW A319 SRM 53-12-00 & IRM 9701 REV G.Dec 4, 2011 · N742PS · Airbus A319112 · Fuselage Floor PanelSDR USAA2011120900017Floor Panel · delaminated2S CHECK - DELAMINATION ON FLOOR PANEL 222EF BETWEEN FR20 TO FR24 & BETWEEN -Y254 TO -Y765. REPLACED FLOOR PANEL 222EF IAW A319 SRM 53-12-00 & IRM 9701 REV G.Dec 4, 2011 · N742PS · Airbus A319112 · Fuselage Floor PanelSDR USAA2011120900012Floor Panel · delaminated2S CHECK - DELAMINATION ON FLOOR PANEL 251HF BETWEEN FR51 TO FR54, BETWEEN Y765 TO Y1292. REPLACED FLOOR PANEL 251HF IAW A319 SRM 53-02-00 AND IRM 9701 REV G.Dec 4, 2011 · N742PS · Airbus A319112 · Fuselage Floor PanelSDR USAA2011122100012Seat Track · corrodedDURING 2S CHECK, CORROSION ON SEAT TRACK BETWEEN FR43 TO FR46, Y1292. REPLACED SEAT TRACK IAW 51-72-11 & DRAWING D53370500.Dec 3, 2011 · N742PS · Airbus A319112 · Fuselage, Seat/Cargo Attach FittingsSDR USAA2011121400012Seat Track · corrodedON 2S CHECK, CORROSION ON SEAT TRACK BETWEEN FR36 TO FR41, -Y1292. REPLACED SEAT TRACK IAW SRM 51-72-11 & DRAWING D57130147.Dec 3, 2011 · N742PS · Airbus A319112 · Fuselage, Seat/Cargo Attach FittingsSDR USAA2011122700004Seat Track · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON SEAT RAIL BETWEEN FR58 +10 INCHES TO FR64, -Y1292. REPAIRED SEAT RAIL BETWEEN FR58 +10 INCHES TO FR64, -Y1292 IAW A319 SRM 53-41-15.Dec 3, 2011 · N742PS · Airbus A319112 · Fuselage, Seat/Cargo Attach FittingsSDR USAA2011122200004Seat Track · corroded2S CHECK - CORROSION ON SEAT TRACK BETWEEN FR 36 AND FR 41AT -Y765. REPLACED SEAT TRACK BETWEEN FR 36 AND FR 41AT -Y765 IAW A319 SRM 51-72-11 & 51-42-11.Dec 3, 2011 · N742PS · Airbus A319112 · Fuselage, Seat/Cargo Attach FittingsSDR USAA2011120100006Light · inoperativeDOOR L2 EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED DOOR L2 EMERGENCY LIGHT.Nov 29, 2011 · N742PS · Airbus A319112 · Emergency LightingSDR USAA2011092000014Battery · dischargedFORWARD FLIGHT ATTENDANT BREAKAWAY FLASHLIGHT WON'T TEST. REMOVED AND REPLACED BATTERY FORWARD FLIGHT ATTENDANT FLASHLIGHT. OPS CHECK GOOD.Sep 19, 2011 · N742PS · Airbus A319112 · Emergency LightingSDR USAA2011090100010Lens · broken2L DOOR EXIT LIGHT LENS (AFT MID DOOR FRAME LEVEL) FELL OFF, LENS CLIP EARS BROKEN. REMOVED AND REPLACED LENS. OPS CHECKED GOOD.Aug 31, 2011 · N742PS · Airbus A319112 · Emergency LightingSDR USAA2011062300017Slide · low pressureSAL - C11 - GAUGE NEEDLE IS NOT ON GREEN GO BAND ON FWD SLIDE LT. REPLACED SLIDE PACK ASSEMBLY AT DOOR 831 IAW AMM 25-62-44-400-006 AND EA 133590.Jun 22, 2011 · N742PS · Airbus A319112 · Escape SlideSDR USAA2011062200008Connector · inoperativeSAL - C11 - EMERGENCY LIGHT INOP ON CEILING PANEL 4. INSTALLED ELECTRICAL CONNECTOR ON EMERGENCY LIGHT (201WL) IAW AMM 33-51-00, OPS TEST GOOD.Jun 22, 2011 · N742PS · Airbus A319112 · Light System WiringSDR USAA2011062100016Mechanism · out of adjustSAL - C11 - NR 6427963 - OUT OF TOLERANCE DIM "A" OF THE DOOR DAMPER MECHANISM AND EMERGENCY OPERATION CYLINDER AT PASS/CREW DOOR 841. PERFORMED ADJUSTMENT DIM "A"(J2) BETWEEN PERCUSSION BELL CRANK FINGER OF THE DOOR DAMPER AND EMERGENCY OPERATION CYLINDER ATJun 14, 2011 · N742PS · Airbus A319112 · Passenger/Crew DoorsSDR USAA2011062100015Mechanism · out of adjustSAL - C11 - OUT OF TOLERANCES DIM "A" OF THE DOOR DAMPER MECHANISM AND EMERGENCY OPERATION CYLINDER AT PASS/CREW DOOR 842. PERFORMED ADJUSTMENT DIM "A"(J2) BETWEEN PERCUSSION BELL CRANK FINGER OF THE DOOR DAMPER AND EMERGENCY OPERATION CYLINDER AT PASS/CREW DJun 14, 2011 · N742PS · Airbus A319112 · Passenger/Crew DoorsSDR USAA2011062100014Mechanism · out of adjustSAL - C11 - OUT OF TOLERANCE DIM "A" OF THE DOOR DAMPER MECHANISM AND EMERGENCY OPERATION CYLINDER AT PASS/CREW DOOR 832. PERFORMED ADJUSTMENT DIM "A" (J2) BETWEEN PERCUSSION BELL CRANK FINGER OF THE DOOR DAMPER AND EMERGENCY OPERATION CYLINDER AT PASS/CREW DJun 14, 2011 · N742PS · Airbus A319112 · Passenger/Crew DoorsSDR USAA2011062100018Damper · low pressureSAL - C11 - LOW PRESS IN DAMPER CYLINDER AT PASS/CREW DOOR 832. CHARGED DAMPER & EMERGENCY OPERATION CYLINDER AT PASS/CREW DOOR 832 IAW A319 AMM 52-10-00-614-001.Jun 14, 2011 · N742PS · Airbus A319112 · Passenger/Crew DoorsSDR USAA2011062100017Damper · low pressureSAL - C11 - LOW PRESSURE IN DAMPER CYLINDER AT PASS/CREW DOOR 842. CHARGED DAMPER & EMERGENCY OPERATION CYLINDER AT PASS/CREW DOOR 842 IAW A319 AMM 52-10-00-614-001.Jun 14, 2011 · N742PS · Airbus A319112 · Passenger/Crew DoorsSDR USAA2011062100013Damper · out of adjustSAL - C11 - OUT OF TOLERANCE DIM "A" OF THE DOOR DAMPER MECHANISM & EMERGENCY OPERATION CYLINDER AT PASS/CREW DOOR 831. PERFORMED ADJUSTMENT DIM. "A" (J2) OF THE DOOR DAMPER MECHANISM & EMERGENCY OPERATION CYLINDER AT PASS/CREW DOOR 831 IAW AMM 52-11-14-820-0Jun 11, 2011 · N742PS · Airbus A319112 · Passenger/Crew DoorsSDR USAA2011061700017Coupling · corrodedSAL - C11 - CORROSION ON COUPLING AT FR. 67+10 INCHES, Y1162. REPLACED COUPLING AT FR. 67+10 INCHES, Y1162 IAW A319 SRM 51-72-11.Jun 10, 2011 · N742PS · Airbus A319112 · Fuselage Miscellaneous StructureSDR USAA2011061700015Coupling · corrodedSAL - C11 - CORROSION ON COUPLING AT FR66, Y1162. REPLACED COUPLING AT FR66, Y1162 IAW A319 SRM 51-72-11.Jun 10, 2011 · N742PS · Airbus A319112 · Fuselage Miscellaneous StructureSDR USAA2011061700009Coupling · corrodedSAL - C11 - LEVEL 2 GALVANIC CORROSION ON COUPLING AT FR 67+10 INCHES, Y1162. REPLACED COUPLING AT FR 67+10 INCHES, Y1162 IAW A319 SRM 51-72-11.Jun 10, 2011 · N742PS · Airbus A319112 · Fuselage Miscellaneous StructureSDR USAA2011062100011Seat Track · corrodedSAL - C11 - LEVEL 2 GALVANIC CORROSION ON SEAT TRACK BETWEEN FR24 TO FR25, -Y765. REPAIRED SEAT TRACK BETWEEN FR24 TO FR25, -Y765 IAW A319 SRM 53-21-15.Jun 9, 2011 · N742PS · Airbus A319112 · Fuselage, Seat/Cargo Attach FittingsSDR USAA2011062100005Seat Track · corrodedSAL - C11 - LEVEL 2 GALVANIC CORROSION ON SEAT TRACK BETWEEN FR24 TO FR25, -Y1292. REPAIRED SEAT TRACK BETWEEN FR24 TO FR25, -Y1292 IAW A319 SRM 53-21-15 & AIRBUS DRAWING D53110920 & D53233450.Jun 9, 2011 · N742PS · Airbus A319112 · Fuselage, Seat/Cargo Attach FittingsSDR USAA2011062200007Sill · corrodedSAL C11 - LEVEL 2 GALVANIC CORROSION ON LOWER SILL AT FR67 + 16 INCHES, S23R. REPAIRED LOWER SILL AT FR67 + 16 INCHES, S23R IAW EA 133611.Jun 8, 2011 · N742PS · Airbus A319112 · Fuselage Miscellaneous StructureSDR USAA2011062200006Sill · corrodedSAL C11 - LEVEL 2 GALVANIC CORROSION ON LOWER SILL AT FR68, S23L. REPAIRED LOWER SILL AT FR68, S23L IAW EA 133604.Jun 8, 2011 · N742PS · Airbus A319112 · Fuselage Miscellaneous StructureSDR USAA2011062200005Seat Track · corrodedSAL C11 - LEVEL 2 GALVANIC CORROSION ON SEAT TRACK BETWEEN FR20 TO FR24, -Y189. REPLACED SEAT TRACK BETWEEN FR20 TO FR24, -Y189 IAW EA 133608, A319 SRM 51-72-11 & AIRBUS DRAWING D53111406.Jun 8, 2011 · N742PS · Airbus A319112 · Fuselage, Seat/Cargo Attach FittingsSDR USAA2011062200004Sill · corrodedSAL C11 - LEVEL 2 GALVANIC CORROSION ON LOWER SILL AT FR66, S23R. REPAIRED LOWER SILL AT FR66, S23R IAW EA 133611.Jun 8, 2011 · N742PS · Airbus A319112 · Fuselage Miscellaneous StructureSDR USAA2011062100019Cover · corrodedSAL - C11 - LEVEL 2 GALVANIC CORROSION ON JOINT COVER BETWEEN FR12 TO FR16, -Y81. REPLACED JOINT COVER BETWEEN FR12 TO FR16, -Y81 IAW A319 SRM 51-72-11 & AIRBUS DRAWING D53112829.Jun 8, 2011 · N742PS · Airbus A319112 · Fuselage Miscellaneous StructureSDR USAA2011062100012Seat Track · corrodedSAL - C11 - LEVEL 2 GALVANIC CORROSION ON SEAT BEAM RAIL BETWEEN FR64 TO FR66 + 5 INCHES, -Y765. REPLACED SEAT BEAM RAIL BETWEEN FR64 TO FR66 + 5 INCHES, -Y765 IAW A319 SRM 51-72-11.Jun 8, 2011 · N742PS · Airbus A319112 · Fuselage, Seat/Cargo Attach FittingsSDR USAA2011062100010Shear Plate · corrodedSAL - C11 - LEVEL 2 GALVANIC CORROSION ON SHEAR PLATE BETWEEN FR69 TO FR70, S23R. REPLACED SHEAR PLATE BETWEEN FR69 TO FR70, S23R IAW A319 SRM 51-72-11 & DRAWING D53474180.Jun 8, 2011 · N742PS · Airbus A319112 · Fuselage Miscellaneous StructureSDR USAA2011062100009Floor Support · corrodedSAL - C11 - LEVEL 2 GALVANIC CORROSION ON FLOOR SUPPORT BETWEEN FR12 TO FR24, Y254. REPLACED FLOOR SUPPORT BETWEEN FR12 TO FR24, Y254 IAW A319 SRM 51-72-11 & AIRBUS DRAWING D53110920 & D53112816.Jun 8, 2011 · N742PS · Airbus A319112 · Fuselage Miscellaneous StructureSDR USAA2011062100008Seat Track · corrodedSAL - C11 - LEVEL 2 GALVANIC CORROSION ON SEAT TRACK BETWEEN FR12 TO FR24, Y1292. REPLACED SEAT TRACK BETWEEN FR12 TO FR24, Y1292 IAW A319 SRM 51-72-11 & AIRBUS DRAWING D53112812.Jun 8, 2011 · N742PS · Airbus A319112 · Fuselage, Seat/Cargo Attach FittingsSDR USAA2011062100007Seat Track · corrodedSAL - C11 - LEVEL 2 GALVANIC CORROSION ON SEAT TRACK BETWEEN FR12 TO FR24, S23R, -Y765. REPLACED SEAT TRACK BETWEEN FR12 TO FR24, S23R, -Y765 IAW A319 SRM 51-72-11 & AIRBUS DRAWING D53112812.Jun 8, 2011 · N742PS · Airbus A319112 · Fuselage, Seat/Cargo Attach FittingsSDR USAA2011062100006Seat Track · corrodedSAL - C11 - LEVEL 2 GALVANIC CORROSION ON SEAT TRACK BETWEEN FR12 TO FR24, -Y1292. REPLACED SEAT TRACK BETWEEN FR12 TO FR24, -Y1292 IAW A319 SRM 51-72-11 & AIRBUS DRAWING D53112812 & D53110920.Jun 8, 2011 · N742PS · Airbus A319112 · Fuselage, Seat/Cargo Attach FittingsSDR USAA2011062100004Hinge Fitting · excess playSAL - C11 - EXCESSIVE PLAY ON LEFT NR 1 ELEVATOR HINGE FITTING. REPLACED LEFT NR 1 ELEVATOR HINGE FITTING IAW A319 AMM 55-16-42.Jun 8, 2011 · N742PS · Airbus A319112 · Elevator StructureSDR USAA2011062100003Fitting · corrodedSAL - C11 - LEVEL 2 GALVANIC CORROSION ON LOWER AFT CORNER FITTING AT FR68, S23L. REPLACED LOWER AFT CORNER FITTING AT FR68, S23L IAW A319 SRM 51-72-11 & AIRBUS DRAWING D53480505.Jun 8, 2011 · N742PS · Airbus A319112 · Fuselage Miscellaneous StructureSDR USAA2011062100002Floor Support · corrodedSAL - C11 - LEVEL 2 GALVANIC CORROSION ON FLOOR SUPPORT TRACK BETWEEN FR12 TO FR24, -Y254. REPAIRED FLOOR SUPPORT TRACK BETWEEN FR12 TO FR24, -Y254 IAW A319 SRM 51-72-11 & AIRBUS DRAWING D53111461 & D53110920.Jun 8, 2011 · N742PS · Airbus A319112 · Fuselage Miscellaneous StructureSDR USAA2011062100001Sill · corrodedSAL - C11 - LEVEL 2 GALVANIC CORROSION ON CENTER SHAPE SILL BETWEEN FR66 + 5 INCHES TO FR67 + 16INCHES, S23L. REPLACED CENTER SHAPE SILL BETWEEN FR66 + 5 INCHES TO FR67 + 16INCHES, S23L IAW A319 SRM 51-72-11 & AIRBUS DRAWING D53480505 & D53480048.Jun 8, 2011 · N742PS · Airbus A319112 · Fuselage Miscellaneous StructureSDR USAA2011061700019Sill · corrodedSAL - C11 - LEVEL 2 GALVANIC CORROSION ON EXISTING REPAIR ON LOWER SILL AT FR66, S23L. REPAIRED EXISTING REPAIR ON LOWER SILL AT FR66, S23L IAW A319 SRM 51-72-11 & 53-41-14.Jun 8, 2011 · N742PS · Airbus A319112 · Fuselage Miscellaneous StructureSDR USAA2011061700018Floorbeam · corrodedSAL - C11 - LEVEL 2 GALVANIC CORROSION ON FLOORBEAM AT FR 65+21 INCHES, Y1292. REPLACED FLOORBEAM AT FR 65+21 INCHES, Y1292 IAW A319 SRM 51-72-11 & AIRBUS DRAWING D53472780.Jun 8, 2011 · N742PS · Airbus A319112 · Fuselage Main, Floor BeamSDR USAA2011061700016Floorbeam · corrodedSAL - C11 - CORROSION ON FLOORBEAM BETWEEN FR66+5 INCHES TO FR70, Y765. REPLACED FLOORBEAM BETWEEN FR66+5 INCHES TO FR70, Y765 IAW A319 SRM 51-72-11 & AIRBUS DRAWING D53472780.Jun 8, 2011 · N742PS · Airbus A319112 · Fuselage Main, Floor BeamSDR USAA2011061700014Dummy Rail · corrodedSAL - C11 - LEVEL 2 GALVANIC CORROSION ON RAIL DUMMY AT FR 14+8 INCHES, -Y81. REPLACED RAIL DUMMY AT FR 14+8 INCHES, -Y81 IAW A319 SRM 51-72-11.Jun 8, 2011 · N742PS · Airbus A319112 · Fuselage Miscellaneous StructureSDR USAA2011061700013Dummy Rail · corrodedSAL - C11 - LEVEL 2 GALVANIC CORROSION ON RAIL DUMMY BETWEEN FR12 TO FR16, Y503.2. REPLACED RAIL DUMMY BETWEEN FR12 TO FR16, Y503.2 IAW A319 SRM 51-72-11 & AIRBUS DRAWING D53112825 & D53110984.Jun 8, 2011 · N742PS · Airbus A319112 · Fuselage Miscellaneous StructureSDR USAA2011061700012Floorbeam · corrodedSAL - C11 - LEVEL 2 GALVANIC CORROSION ON FLOORBEAM BETWEEN FR 66+5 INCHES TO FR70 INCHES, -Y765. REPLACED FLOORBEAM BETWEEN FR 66+5 INCHES TO FR70 INCHES, -Y765 IAW A319 SRM 51-72-11 & AIRBUS DRAWING D53472780.Jun 8, 2011 · N742PS · Airbus A319112 · Fuselage Main, Floor BeamSDR USAA2011061700011Floorbeam · corrodedSAL - C11 - LEVEL 2 GALVANIC CORROSION ON FLOORBEAM AT FR FR 67+18 INCHES, Y1162. REPLACED FLOORBEAM AT FR FR 67+18 INCHES, Y1162 IAW A319 SRM 51-72-11 & AIRBUS DRAWING D53472780.Jun 8, 2011 · N742PS · Airbus A319112 · Fuselage Main, Floor BeamSDR USAA2011061700010Shear Plate · corrodedSAL - C11 - LEVEL 2 GALVANIC CORROSION ON SHEAR PLATE BETWEEN FR69 TO FR70, S23L. REPLACED SHEAR PLATE BETWEEN FR69 TO FR70, S23L IAW A319 SRM 51-72-11 & AIRBUS DRAWING D53474180.Jun 8, 2011 · N742PS · Airbus A319112 · Fuselage Miscellaneous StructureSDR USAA2011061700007Floorbeam · corrodedSAL - C11 - LEVEL 2 GALVANIC CORROSION ON FLOORBEAM AT FR 67+11INCHES, -Y1162. REPLACED FLOORBEAM AT FR 67+11 INCHES, -Y1162 IAW A319 SRM 51-72-11 & AIRBUS DRAWING D53472780.Jun 8, 2011 · N742PS · Airbus A319112 · Fuselage Main, Floor BeamSDR USAA2011061700006Floorbeam · corrodedSAL - C11 - LEVEL 2 GALVANIC ON CORROSION FLOORBEAM BETWEEN FR68 TO FR69, -Y1162. REPLACED FLOORBEAM BETWEEN FR68 TO FR69, -Y1162 IAW A319 SRM 51-72-11 & AIRBUS DRAWING D53472780.Jun 8, 2011 · N742PS · Airbus A319112 · Fuselage Main, Floor BeamSDR USAA2011061700005Floorbeam · corrodedSAL - C11 - LEVEL 2 GALVANIC CORROSION ON FLOOR BEAM AT FR 66+16 INCHES, Y1162. REPLACED FLOORBEAM AT FR 66+16 INCHES, Y1162 IAW A319 SRM 51-72-11 & AIRBUS DRAWING D53472780.Jun 8, 2011 · N742PS · Airbus A319112 · Fuselage Main, Floor BeamSDR USAA2011061700004Seat Track · corrodedSAL - C11 - LEVEL 2 GALVANIC CORROSION ON SEAT BEAM RAIL AT FR 66+3 INCHES, -Y1292. REPLACED SEAT BEAM RAIL AT FR 66+3 INCHES, -Y1292 IAW A319 SRM 51-72-11 & AIRBUS DRAWING D53472815.Jun 8, 2011 · N742PS · Airbus A319112 · Fuselage, Seat/Cargo Attach Fittings
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