N737US
Service difficulty reports · 312
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 = 'N737US' 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 = 'N737US' 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 USAA2014061300014Slide Raft · unserviceableTHE AFT RT SLIDE RAFT COVER TOUCHING FUSELAGE WHEN DOOR IS OPEN. REPLACED R2 SLIDE RAFT ASSEMBLY DUE TO BULGING & NO SLOTS IN FRAME FOR COVER IAW JOB CARD 26L00025011.SDR USAA2014051200010Cover · missingCREW REPORTED SEAT 3C EXIT PATH LIGHTING COVER MISSING. REPLACED MISSING COVER.SDR USAA2014040300002Cover · brokenCREW REPORTED THE COVER AT LOWER LEVEL EMERGENCY LIGHT 3C BROKEN. REPLACED COVER LENS AS REQUIRED IAW MPPM 54-01-10, OPERATIONS OK.SDR USAA2014033100003Computer · faultyCREW REPORTED A F/CTL FLAPS FAULT ECAM INFLIGHT. DIVERTED TO IAD FOR LONGER RUNWAY & NO FLAPS LANDING, EMERGENCY WAS DECLARED. ACCOMPLISHED TSM 27-51-00-810-810-A. R & R NR 1 1 SFCC IAW AMM 27-51-34. OPERATIONS CHECKED GOOD AT THIS TIME, OK FOR FURTHER FLISDR USAA2013121200002Unknown · odorCOCKPIT ODOR DURING FLIGHT. TROUBLESHOOT CABIN AIR QUALITY JOB CARD 26L00021001. NO ODOR DETECTED.SDR USAA2013100700013Megaphone · inoperativeMX REPORTED THE MEGAPHONE INOPERATIVE ON MX CHECK. MX R & R MEGAPHONE IAW 25-60-00.SDR USAA2013071500007Sign · wrong partCREW REPORTED THE EXIT SIGN IN AFT GALLEY HAS NO ARROWS (SHOULD) AND EXIT SIGN 2R DOOR HAS ARROWS (SHOULD NOT). MX SWAPPED SIGNS.SDR USAA2013010400003Unknown · malfunctionedON APPROACH, CREW REPORTED THEY WERE UNABLE TO EXTEND FLAPS FOR LANDING. SLATS OPERATED NORMALLY. CREW DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED FLAP SYSTEM PER AIRBUS TSM 27-51-00-810-810A. NO DISCREPANCIES NOTED AT THIS TIMSDR USAA2012042300002Housing · broken2S CHECK - BROKEN LENS HOUSING OF EMERGENCY LIGHT AT FORWARD LEFT CLOSET. REPLACED LENS HOUSING OF EMERGENCY LIGHT AT FORWARD LEFT CLOSET IAW A319 AMM 33-51-18.SDR USAA2012042400012Strut · corroded2S CHECK - CORROSION ON LEFT WING INTERCONNECTING STRUT BETWEEN WS 4067 TO WS 4862, RIB 1 OUTB/FLAP. REPLACED LEFT WING INTERCONNECTING STRUT IAW A319 AMM 27-51-44-400-001-A.SDR USAA2012041900011Strut · corroded2S CHECK - DURING DISASSEMBLY OF THE RIGHT WING INTERCONNECTING STRUT CORROSION WAS FOUND IN IMMER HOUSING BETWEEN WS 4067 TO WS 4862, RIB 1 O/B FLAP. REPLACED RIGHT WING INTERCONNECTING STRUT IAW A318 AMM 27-51-44-400-001.SDR USAA2012042400003Door Frame · cracked2S CHECK - CRACK ON RIGHT AFT EMERGENCY EXIT DOOR FRAME SEGMENT 844 BETWEEN FR38 TO FR39 & BETWEEN BEAM 1 TO 4. REPLACED FRAME SEGMENT AT RIGHT AFT EMERGENCY EXIT DOOR 844 IAW EO 5210Y228.SDR USAA2012042400013Fitting · cracked2S CHECK - CRACK ON FITTING ON LEFT PYLON AT XM9528, RIB 1. REPLACED FITTING AT LEFT PYLON AT XM9528, RIB 1 IAW A319 SRM 54-55-12; PARAGRAPH 5B; FIGURE 202.SDR USAA2012041900012Fitting · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON LEFT PYLON SPIGOT FITTING RECEPTICAL BETWEEN PYLON RIB 4 & RIB 5. REPLACED LEFT PYLON SPIGOT FITTING IAW A319 SRM 54-51-12.SDR USAA2012041900014Fitting · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON CENTER FITTING OF R1 DOOR ENTRANCE BETWEEN FR16 TO FR20, S23R. REPLACED R1 DOOR OPENING CENTER FITTING IAW A319 51-72-11 & AIRBUS DRAWING D53112109.SDR USAA2012041900013Fitting · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON CENTER FITTING OF L1 DOOR ENTRANCE BETWEEN FR16 TO FR20, S23L. REPLACED L1 DOOR OPENING CENTER FITTING IAW A319 51-72-11 & AIRBUS DRAWING D53112109.SDR USAA2012042400014Floor Panel · delaminated2S CHECK - DELAMINATION ON FLOOR PANEL 261DF BETWEEN FR66 TO FR68 & BETWEEN Y1292 TO -Y1292. REPLACED FLOOR PANEL 261DF IAW A319 SRM 53-02-00, IRM 9701 REV G & EA # 500608.SDR USAA2012042300015Fitting · corroded2S CHECK - LEVEL 2 CORROSION ON LOWER DOOR SILL FITTING AT FR19+5 INCHES, S23R. REPLACED LOWER DOOR SILL FITTING AT FR19+5 INCHES, S23R IAW A319 SRM 51-72-11 & AIRBUS DRAWING D53110339.SDR USAA2012041900019Cleat · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON CLEAT AT FR28 BETWEEN S43L TO S43R. REPLACED CLEAT AT FR28 BETWEEN S43L TO S43R IAW A319 SRM 51-72-11 & AIRBUS DRAWING D53233523 & D53231616.SDR USAA2012041900018Fitting · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON LOWER SILL FITTING AT R1 DOOR OPENING FR16+4 INCHES, S23R. REPLACED LOWER SILL FITTING AT R1 DOOR OPENING BETWEEN FR16+4 INCHES & FR20, S23R IAW A319 SRM 51-72-11 & AIRBUS DRAWING D53110339.SDR USAA2012041900017Fitting · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON LOWER SILL FITTING AT L1 DOOR OPENING FR16+4 INCHES, S23L. REPLACED LOWER SILL FITTING AT L1 DOOR OPENING BETWEEN FR16+4 INCHES & FR20, S23L IAW A319 SRM 51-72-11 & AIRBUS DRAWING D53110339.SDR USAA2012041900015Fitting · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON FITTING OF L1 DOOR ENTRANCE BETWEEN FR16 TO FR20, S23L. REPLACED L1 DOOR OPENING FITTING IAW A319 51-72-11 & AIRBUS DRAWING D53110339.SDR USAA2012041000016Floor Panel · delaminated2S CHECK, DELAMINATION ON FLOOR PANEL 261QF BETWEEN FR64 TO FR66 & BETWEEN Y765 TO -Y765. REPLACED FLOOR PANEL IAW SRM 53-02-00 & IRM 9701 REV G.SDR USAA2012040900019Floor Panel · delaminated2S CHECK - DELAMINATION ON FLOOR PANEL 252GF BETWEEN FR51 TO FR54, BETWEEN -Y765 TO -Y254. REPLACED FLOOR PANEL 252GF IAW SRM 53-02-00 AND IRM 9701 REV G.SDR USAA2012040900014Floor Panel · delaminated2S CHECK - DELAMINATION ON FLOOR PANEL 251FF BETWEEN FR51 TO FR54, BETWEEN Y254 TO -Y254. REPLACED FLOOR PANEL 251FF IAW A319 SRM 53-02-00 AND IRM 9701 REV G.SDR USAA2012042400024Seat 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 & AIRBUS DRAWING D53233450.SDR USAA2012042300017Seat Track · corroded2S CHECK - LEVEL 2 CORROSION ON SEAT RAIL AT FR47/51 TO FR 64, -Y1292. REPLACED SEAT RAIL AT FR 47/51 TO FR 64, -Y1292 IAW A319 SRM 51-72-11 & AIRBUS DRAWING D53476977.SDR USAA2012042300016Coupling · damaged2S CHECK - CORROSION & ELONGATED HOLE ON SEAT RAIL COUPLING AT FR64, -Y1292. REPLACED SEAT RAIL COUPLING AT FR64, -Y1292 IAW A319 SRM 51-72-11 & AIRBUS DRAWING D53472832.SDR USAA2012041900023Splice · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON SEAT TRACK BRACKET SPLICE AT FR47/51, -Y765. REPLACED SEAT TRACK BRACKET SPLICE AT FR47/51, -Y765 IAW A319 SRM 51-72-11 & AIRBUS DRAWING D53470080.SDR USAA2012041900022Seat Track · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON SEAT TRACK AT FR46+15 INCHES, Y1292. REPLACED SEAT TRACK AT FR46+15 INCHES, Y1292 IAW A319 SRM 51-72-11 & AIRBUS DRAWING D53476977.SDR USAA2012041900021Seat Track · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON RAIL SEAT BETWEEN FR47/51 TO FR64, -Y765. REPLACED RAIL SEAT BETWEEN FR47/51 TO FR64, -Y765 IAW A319 SRM 51-72-11 & AIRBUS DRAWING D53476977.SDR USAA2012041900020Seat Track · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON RAIL SEAT AT FR53+11 INCHES, Y765. REPLACED RAIL SEAT AT FR53+11 INCHES, Y765 IAW A319 SRM 51-72-11 & AIRBUS DRAWING D53476977, D53478313 & D53470080.SDR USAA2012041200013Seat Track · corroded2S CHECK, LEVEL 2 GALVANIC CORROSION ON SEAT TRACK BETWEEN FR24 TO FR34, -Y765. REPLACED SEAT TRACK BETWEEN FR24 TO FR34, -Y765 IAW SRM 51-72-11 & DRAWING D531-10920.SDR USAA2012041200005Seat Track · corroded2S CHECK, LEVEL 2 GALVANIC CORROSION ON SEAT TRACK AT FR40+12 INCHES, Y765. REPLACED SEAT TRACK AT FR40+12 INCHES, Y765 IAW SRM 51-72-11 & DRAWING D53370500.SDR USAA2012041200004Seat Track · corroded2S CHECK, LEVEL 2 GALVANIC CORROSION ON SEAT TRACK BETWEEN FR41 TO FR47/51, -Y1292. REPLACED SEAT TRACK BETWEEN FR41 TO FR47/51, -Y1292 IAW SRM 51-72-11 & DRAWING D53370500.SDR USAA2012042000011Hinge Fitting · excess play2S CHECK - EXCESSIVE PLAY ON RUDDER HINGE POINT NR 7 AT VERTICAL STABILIZER STATION RIB 11. REPLACED NR 7 RUDDER HINGE FITTING ASSY - FORK END AT RIB 11 IAW A319 AMM 55-36-41-0401 & SRM 51-72-11.SDR USAA2012041000018Floor Panel · delaminated2S CHECK, DELAMINATION ON FLOOR PANEL 151VG BETWEEN FR53 TO FR55A & BETWEEN Y765 TO -Y765. REPLACED FLOOR PANEL IAW SRM 53-02-00 & IRM 9701 REV G.SDR USAA2012041000017Floor Panel · delaminated2S CHECK, DELAMINATION ON FLOOR PANEL 151ZG BETWEEN FR46 TO FR59 & BETWEEN Y765 TO -Y765. REPLACED FLOOR PANEL IAW SRM 53-02-00 & IRM 9701 REV G.SDR USAA2012041900016Attach Fitting · corroded2S CHECK - CORROSION ON RIGHT MAIN LANDING GEAR ATTACHMENT FITTING AT KEEL BEAM AT FR24, S42R. REPLACED RIGHT MAIN LANDING GEAR ATTACHMENT FITTING IAW SRM A319 51-72-11 & AIRBUS DRAWING D53370600.SDR USAA2011091300010Slide Raft · out of adjustC11 CHECK - SLIDE RAFT AFT LEFT HIT'S ON THE FUSELAGE. REPACKED SLIDE RAFT IAW CMM 25-61-20 REV 16 DATE 25-FEB-2011 PAGE 309 SEC. DISASSEMBLY AND FOLDING PROCEDURE P-11915 REV. AC DATE 03-SEP-2010, PERFORMED FINAL TEST AND TEST OK.SDR USAA2011091300009Slide Raft · out of adjustC11 CHECK - SLIDE RAFT AFT RIGHT HIT'S ON THE FUSELAGE. REPACKED SLIDE RAFT IAW CMM 25-61-20 REV 16 DATE 25-FEB-2011 PAGE 309 SEC. DISASSEMBLY AND FOLDING PROCEDURE P-11915 REV. AC DATE 03-SEP-2010, PERFORMED FINAL TEST AND TEST OK.SDR USAA2011091300008Damper · low pressureC11 CHECK - LOW PRESS ON DOOR DAMPER AND EMERGENCY OPERATION CYLINDER AT DOOR 841. PERFORMED CHARGING OF THE DOOR DAMPER AND EMERGENCY OPERATION CYLINDER AT DOOR 841 AS PER AMM 52-10-00-614-001.SDR USAA2011091300007Damper · low pressureC11 CHECK - LOW PRESS ON DOOR DAMPER AND EMERGENCY OPERATION CYLINDER AT DOOR 831. PERFORMED CHARGING OF THE DOOR DAMPER AND EMERGENCY OPERATION CYLINDER AT DOOR 831 AS PER AMM 52-10-00-614-001.SDR USAA2011091400022Coupling · corrodedC11 CHECK - LEVEL 2 GALVANIC CORROSION ON COUPLING AT FR66, S23L. REPLACED COUPLING AT FR66, S23L IAW A319 SRM 51-72-11.SDR USAA2011091100006Floor Panel · delaminatedC11/SY6 CHECK - DELAMINATION ON FLOOR PANEL 262BF BETWEEN FR 64 - FR 66 AND -Y254 TO -Y1732. REPLACED FLOOR PANEL 262BF BETWEEN FR 64 - FR 66 AND -Y254 TO -Y1732 IAW A319 SRM 53-02-00 AND EA 133771.SDR USAA2011091100005Floor Panel · corrodedC11/SY6 CHECK - CORROSION ON FLOOR PANEL 262FF BETWEEN FR 66 AND FR 68, S23R. REPLACED FLOOR PANEL 262FF BETWEEN FR 66 AND FR 68, S23R IAW A319 SRM 51-72-11.SDR USAA2011091100004Floor Panel · corrodedC11/SY6 CHECK - CORROSION ON FLOOR PANEL 261FF BETWEEN FR 66 AND FR 68, S23L. REPLACED FLOOR PANEL 261FF BETWEEN FR 66 AND FR 68, S23L IAW A319 SRM 51-72-11.SDR USAA2011091100003Floor Panel · corrodedC11/SY6 CHECK - CORROSION ON FLOOR PANEL 221FF BETWEEN FR 20 AND FR 24, S23L. REPLACED FLOOR PANEL 221FF BETWEEN FR 20 AND FR 24, S23L IAW A319 SRM 53-12-12.SDR USAA2011091100002Floor Panel · corrodedC11/SY6 CHECK - CORROSION ON FLOOR PANEL 222FF BETWEEN FR 20 AND FR 24, S23R. REPLACED FLOOR PANEL 222FF BETWEEN FR 20 AND FR 24, S23R IAW A319 AMM 53-12-12.SDR USAA2011091100001Floor Panel · delaminatedC11/SY6 CHECK - DELAMINATION ON FLOOR PANEL 261BF BETWEEN FR 64 - FR 66 AND Y765 - Y1732. REPLACED FLOOR PANEL 261BF BETWEEN FR 64 - FR 66 AND Y765 - Y1732 IAW A319 SRM 53-02-00.
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