N730US
Service difficulty reports · 285
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 = 'N730US' 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.
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 = 'N730US' AND registry_match = 'registration' ORDER BY difficulty_date DESC
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR USAA2012030800006Web · cracked2S CHECK - CRACK ON WEB AT FR11, Y765. REPLACED WEB AT FR11, Y765 IAW A319 SRM 51-72-11, AIRBUS DRAWING # D53113219 & D53913033.SDR USAA2012032300004Bolt · worn2S CHECK - WEAR ON NR 2 SPOILER FITTING MODIFIED BOLT REQUIRED PER SRM 57-70-00 PAR 5C (2) REPAIR BETWEEN WS 7792 & WS 8278, ALSO BETWEEN RIB 11 & RIB 12 LEFT WING. REPLACED NR 2 SPOILER CENTER HINGE FITTING IAW A319 SRM 57-70-00 PAR 5C (2) FIGURE 201.SDR USAA2012032300003Bolt · worn2S CHECK - WEAR ON NR 2 SPOILER FITTING MODIFIED BOLT REQUIRED PER SRM 57-70-00 PAR 5C (2) REPAIR BETWEEN WS 7792 & WS 8278 ALSO BETWEEN RIB 11 & RIB 12 LEFT WING. REPLACED NR 2 SPOILER CENTER HINGE FITTING MODIFIED BOLT IAW A319 SRM 57-70-00 PAR. 5C (2) FIGSDR USAA2012032200003Hinge Fitting · worn2S CHECK - WEAR ON NR 3 SPOILER FITTING MODIFIED BOLT REQUIRED PER SRM 57-70-00 PAR 5C (2) REPAIR BETWEEN WS 7792 & WS 8278 ALSO BETWEEN RIB 14 & RIB 15 LEFT WING. REPAIRED NR 3 SPOILER CENTER HINGE FITTING IAW A319 SRM 57-70-00 PAR 5C (2) FIGURE 201.SDR USAA2012032200001Attach Bolt · worn2S CHECK - WEAR ON NR 3 SPOILER FITTING MODIFIED BOLT REQUIRED PER SRM 57-70-00 PAR 5C (2) REPAIR BETWEEN WS 7792 & WS 8278, ALSO BETWEEN RIB 14 & RIB 15 LEFT WING. REPLACED NR 3 SPOILER FITTING MODIFIED BOLT IAW A319 SRM 57-70-00 PAR 5 C (2) FIGURE 201.SDR USAA2012031400004Fitting · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON CORNER FITTING AT FR68, S23L. REPLACED CORNER FITTING AT FR68, S23L IAW A319 SRM 51-72-11 & AIRBUS DRAWING D53480505.SDR USAA2012032600002Flap · corroded2S CHECK - LEFT OUTBOARD FLAP INTERNAL AREA CORRODED BETWEEN WS 486 TO WS 1166 & BETWEEN RIB 9 TO RIB 22. REPLACED LEFT OUTBOARD FLAP IAW A319 AMM 27-54-62.SDR USAA2012031400007Splice · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON CONNECTING SECTION AT FR64, S43L. REPLACED CONNECTING SECTION AT FR64, S43L IAW A319 SRM 51-72-11 & AIRBUS DRAWING D53476160.SDR USAA2012030600019Floor Panel · delaminated2S CHECK - DELAMINATION ON FLOOR PANEL # 261PF BETWEEN FR68 TO FR70 & BETWEEN -Y1292 TO Y1292. REPLACED FLOOR PANEL # 261PF IAW A319 SRM 53-02-00 TABLE 103 & IRM 9701 REV G.SDR USAA2012030600016Floor Panel · delaminated2S CHECK - DELAMINATION ON FLOOR PANEL 261BF BETWEEN FR64 TO FR66 & BETWEEN Y765 TO Y1732. REPLACED FLOOR PANEL 261BF IAW A319 SRM 53-02-00 FIG 209 & IRM 9701 REV G.SDR USAA2012030600013Floor Panel · delaminated2S CHECK - DELAMINATION ON FLOOR PANEL 252SF BETWEEN FR58 TO FR62 & BETWEEN -Y254 TO Y254. REPLACED FLOOR PANEL 252SF IAW A319 SRM 53-02-00 FIG 209 & IRM 9701 REV G.SDR USAA2012032600005Plate · worn2S CHECK - ELONGATED HOLE ON RIGHT WING LOWER SURFACE MOUNTING PLATE BETWEEN WS376 TO WS 407 & BETWEEN RIB 7 & RIB 8. REPLACED RIGHT WING LOWER SURFACE MOUNTING PLATE IAW A319 SRM 51-72-11.SDR USAA2012032600004Spar · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON RIGHT OUTBOARD FLAP FRONT SPAR AT RIB 15 & ATTACHMENT AREA AT TRACK NR 4. REPLACED RIGHT OUTBOARD FLAP IAW A319 AMM 27-54-62-400-001.SDR USAA2012032000010Seat Track · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON SEAT TRACK BETWEEN FR24 TO FR35, S23R, -Y1292. REPLACED WEB BETWEEN FR34 TO FR36, S30R IAW A319 SRM 51-72-11 & AIRBUS DRAWING D53310175.SDR USAA2012032000007Seat Track · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON SEAT TRACK BETWEEN FR24 TO FR35, Y1292. REPLACED SEAT TRACK BETWEEN FR24 TO FR35, Y1292 IAW A319 SRM 51-72-11 & DRAWING D53110920.SDR USAA2012031400006Seat Track · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON SEAT TRACK BETWEEN FR42 TO FR47, Y1292. REPLACED SEAT TRACK BETWEEN FR42 TO FR47, Y1292 IAW A319 SRM 51-72-11 & AIRBUS DRAWING D53370500.SDR USAA2012031400005Seat Track · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON SEAT TRACK AT FR43+13", Y765. REPLACED SEAT TRACK AT FR43+13", Y765 IAW A319 SRM 51-72-11 & AIRBUS DRAWING D53370500.SDR USAA2012031400003Sill · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON SHAPE SILL BETWEEN FR66+5 INCHES TO FR67+16 INCHES, S23L. REPLACED SHAPE SILL BETWEEN FR66+5 INCHES TO FR67+16 INCHES, S23L IAW A319 SRM 51-72-11 & AIRBUS DRAWING D53480505.SDR USAA2012030600018Floor Panel · delaminated2S CHECK - DELAMINATION ON FLOOR PANEL # 231EF BETWEEN FR20 TO FR24 & BETWEEN Y765 TO Y1292. REPLACED FLOOR PANEL # 231EF IAW A319 SRM 53-12-00 FIG 101& IRM 9701 REV G.SDR USAA2012030600017Floor Panel · delaminated2S CHECK - DELAMINATION ON FLOOR PANEL 232FF BETWEEN FR20 TO FR24 & BETWEEN -Y1732 TO -Y1292. REPLACED FLOOR PANEL 232FF IAW A319 SRM 53-12-00 FIG 101& IRM 9701 REV G.SDR USAA2012030600015Floor Panel · delaminated2S CHECK - DELAMINATION ON FLOOR PANEL 221LF BETWEEN FR12 TO FR16 & BETWEEN -Y254 TO Y254. REPLACED FLOOR PANEL 221LF IAW A319 SRM 53-12-00 FIG 101 & IRM 9701 REV G.SDR USAA2012030600014Floor Panel · delaminated2S CHECK - DELAMINATION ON FLOOR PANEL 221PF BETWEEN FR12 TO FR16 & BETWEEN Y254 TO Y1292. REPLACED FLOOR PANEL 221PF IAW A319 SRM 53-12-00 FIG 101 & IRM 9701 REV G.SDR USAA2012032000006Hinge Fitting · excess play2S CHECK - EXCESSIVE PLAY AT RUDDER HINGE NR 3. REPLACED RUDDER HINGE ARM FITTING NR 3 IAW A319 AMM 55-36-41.SDR USAA2012031300005Floor Panel · delaminated2S CHECK - DELAMINATION ON FLOOR PANEL # 151ZG BETWEEN FR46 TO FR59 & BETWEEN, Y765 TO -Y7659. REPLACED FLOOR PANEL # 151ZG IAW A319 SRM 53-02-00 TABLE 104 & IRM 9701 REV G.SDR USAA2012030900016Floor Panel · delaminated2S CHECK - DELAMINATION ON FLOOR PANEL # 151VG BETWEEN FR53 TO FR55 & BETWEEN -Y765 TO Y765. REPLACED FLOOR PANEL # 151VG IAW A319 SRM 53-02-00 & IRM 9701 REV G.SDR USAA2012030600012Floor Panel · delaminated2S CHECK - DELAMINATION ON FLOOR PANEL 232PF BETWEEN FR24 TO FR28 & BETWEEN -Y1732 TO -Y1242. REPLACED FLOOR PANEL 232PF IAW A319 SRM 53-02-00 FIG 209 & IRM 9701 REV G.SDR USAA2011080300003Shear Tie · corrodedC11 CHECK - LEVEL 2 EXFOLIATION CORROSION ON RIGHT SHEAR TIE AT FR20, -Y1762. REPLACED RIGHT SHEAR TIE AT FR20, -Y1762 IAW A319 SRM 51-72-11.SDR USAA2011080300002Floorbeam · corrodedC11 CHECK - LEVEL 2 INTERGRANULAR CORROSION IN 4 AREAS ON UPPER SURFACE OF FLOORBEAM BETWEEN FR20 TO FR23, Y254. REPLACED FLOORBEAM BETWEEN FR20 TO FR23, Y254 IAW A319 SRM 51-72 & AIRBUS DRAWING D53110920.SDR USAA2011080100013Clevis Pin · bentC11 CHECK - FOUND BENT CLEVIS PIN WHERE YELLOW LOCK ARM PIVITS ON LEFT EMERGENCY EXIT HATCH INTERIOR HANDLE. REPLACED CLEVIS PIN IAW A319 AMM 52-21-11-400-002.SDR USAA2011080100012Skin · saturatedC11 CHECK - INDICATION OF TRAPPED WATER ON LEFT ELEVATOR UPPER SURFACE IN 2 AREAS APPROX. 150.5 INCHES FROM INBOARD EDGE & 14.4 INCHES FROM TRAILING EDGE. ALSO AT 169.5 INCHES FROM INBOARD EDGE & 12 INCHES FROM TRAILING EDGE. REPAIRED LEFT ELEVATOR UPPER SURSDR USAA2011080100011Skin · saturatedC11 CHECK - INDICATION OF TRAPPED WATER ON LEFT ELEVATOR UPPER SURFACE APPROX 141.5 INCHES FROM INBOARD EDGE & 14 INCHES FROM TRAILING EDGE. REPAIRED LEFT ELEVATOR UPPER SURFACE IAW EA 200451.SDR USAA2011080100010Skin · saturatedC11 CHECK - INDICATION OF TRAPPED WATER ON LEFT ELEVATOR UPPER SURFACE APPROX 141.5 INCHES FROM INBOARD EDGE & 14 INCHES FROM TRAILING EDGE. REPAIRED LEFT ELEVATOR UPPER SURFACE IAW EA 200451.SDR USAA2011080100009Skin · saturatedC11 CHECK - INDICATION OF TRAPPED WATER ON LEFT ELEVATOR UPPER SURFACE APPROX 100 INCHES FROM INBOARD EDGE & 5 INCHES FROM TRAILING EDGE. REPAIRED LEFT ELEVATOR UPPER SURFACE IAW A319 SRM 55-21-11 FIGURE 205.SDR USAA2011080100007Skin · saturatedC11 CHECK - INDICATION OF TRAPPED WATER ON LEFT ELEVATOR UPPER SURFACE APPROX 72 INCHES FROM INBOARD EDGE & 4.5 INCHES FROM TRAILING EDGE. REPAIRED LEFT ELEVATOR UPPER SURFACE IAW A319 SRM 55-21-11 FIGURE 205.SDR USAA2011080100006Skin · saturatedC11 CHECK - INDICATION OF TRAPPED WATER ON LEFT ELEVATOR UPPER SURFACE APPROX 45.5 INCHES FROM INBOARD EDGE & 15.5 INCHES FROM TRAILING EDGE. REPAIRED LEFT ELEVATOR UPPER SURFACE IAW A319 SRM 55-21-11 FIGURE 205.SDR USAA2011080100005Skin · saturatedC11 CHECK - INDICATION OF TRAPPED WATER ON LEFT ELEVATOR UPPER SURFACE APPROX. 21.5 INCHES FROM INBOARD EDGE & 14 INCHES FROM TRAILING EDGE. REPAIRED LEFT ELEVATOR UPPER SURFACE IAW A319 SRM 55-21-11 FIGURE 205.SDR USAA2011080100004Skin · saturatedC11 CHECK - INDICATION OF TRAPPED WATER ON LEFT ELEVATOR UPPER SURFACE APPROX. 173 INCHES FROM INBOARD EDGE & 7 INCHES FROM TRAILING EDGE. REPAIRED LEFT ELEVATOR UPPER SURFACE IAW EA 200451.SDR USAA2011080100015Damper · lack of lubeC11 CHECK - R2 DOOR DAMPER GAUGE & PLUG WAS OUT OF DAMPING FLUID. REPLACED R2 DOOR DAMPER IAW A319 AMM 52-13-14.SDR USAA2011072600024Skin · saturatedC11 CHECK - WATER DAMAGE IN HONEY COMB STRUCTURE OF RIGHT ELEVATOR UPPER SURFACE APPROX 75 INCHES FROM INBOARD END & 4.5 INCHES FROM TRAILING EDGE. REPAIRED RIGHT ELEVATOR UPPER SURFACE IAW A319 SRM 55-21-11 REPAIR E.SDR USAA2011072600023Skin · saturatedC11 CHECK - WATER DAMAGE IN HONEY COMB STRUCTURE OF RIGHT ELEVATOR UPPER SURFACE APPROX 22.5 INCHES FROM INBOARD END & 23 INCHES FROM TRAILING EDGE. REPAIRED RIGHT ELEVATOR UPPER SURFACE IAW EA 200452.SDR USAA2011072600022Skin · saturatedC11 CHECK - WATER DAMAGE IN HONEY COMB STRUCTURE OF RIGHT ELEVATOR UPPER SURFACE APPROX 19.5 INCHES FROM INBOARD END & 15.25 INCHES FROM TRAILING EDGE. REPAIRED RIGHT ELEVATOR UPPER SURFACE IAW EA 200452.SDR USAA2011072600021Skin · saturatedC11 CHECK - WATER DAMAGE IN HONEY COMB STRUCTURE OF RIGHT ELEVATOR UPPER SURFACE APPROX 166 INCHES FROM INBOARD END & 12 INCHES FROM TRAILING EDGE. REPAIRED RIGHT ELEVATOR UPPER SURFACE IAW A319 SRM 55-21-11 REPAIR E.SDR USAA2011072600010Floorbeam · corrodedC11 CHECK - LEVEL 2 INTERGRANULAR CORROSION ON FLOORBEAM BETWEEN FR20 TO FR22, -Y765. REPLACED FLOORBEAM BETWEEN FR20 TO FR22, -Y765 IAW A319 SRM 51-72-11.SDR USAA2011072600012Floorbeam · corrodedC11 CHECK - LEVEL 2 INTERGRANULAR CORROSION ON FLOORBEAM BETWEEN FR16 TO FR24, -Y1292. REPLACED FLOORBEAM BETWEEN FR16 TO FR24, -Y1292 IAW A319 SRM 51-72-11 AIRBUS DRAWING D53112812.SDR USAA2011072600020Floor Panel · damagedC11 CHECK - MINOR SURFACE DAMAGE ON FLOOR PANEL 241JF BETWEEN FR62 TO FR64, Y=0. REPLACED FLOOR PANEL 241JF IAW MCGILL IRM 9701 REV G.SDR USAA2011072600013Floorbeam · corrodedC11 CHECK - LEVEL 2 INTERGRANULAR CORROSION ON FLOORBEAM BETWEEN FR20 TO FR22, -Y189. REPLACED FLOORBEAM BETWEEN FR20 TO FR22, -Y189 IAW TYPICAL REPAIR 320-2528-10-011A & AIRBUS DRAWING D53111406.SDR USAA2011072600014Floorbeam · corrodedC11 CHECK - LEVEL 2 INTERGRANULAR CORROSION ON FLOORBEAM BETWEEN FR66 TO FR66 - 6 INCHES, -Y465. REPLACED FLOORBEAM BETWEEN FR66 TO FR66 - 6 INCHES, -Y465 IAW A319 SRM 51-72-11.SDR USAA2011072600019Floorbeam · corrodedC11 CHECK - LEVEL 2 INTERGRANULAR CORROSION ON FLOORBEAM BETWEEN FR16 TO FR20, -Y254. REPLACED FLOORBEAM BETWEEN FR16 TO FR20, -Y254 IAW A319 SRM 51-72-11.SDR USAA2011072600018Floorbeam · corrodedC11 CHECK - LEVEL 2 INTERGRANULAR CORROSION ON FLOORBEAM BETWEEN FR16 TO FR20, Y1292. REPLACED FLOORBEAM BETWEEN FR16 TO FR20, Y1292 IAW A319 SRM 51-72-11.SDR USAA2011072600017Floorbeam · corrodedC11 CHECK - LEVEL 2 INTERGRANULAR CORROSION ON FLOORBEAM AT FR12, -Y50. REPLACED FLOORBEAM AT FR12, -Y50 IAW A319 SRM 51-42-00.
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