N766US
Service difficulty reports · 250
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 = 'N766US' 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 = 'N766US' 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 USAA2013062400040Floor Panel · delaminated2S CHECK - DELAMINATION ON FLOOR PANEL 261PF BETWEEN FR68 TO FR70 & BETWEEN Y1292 TO -Y1292. REPLACED FLOOR PANEL 261PF IAW SRM 53-02-00, FIG 209 & IRM 9701, REV G.SDR USAA2013062400038Floor Panel · delaminated2S CHECK - DELAMINATION ON FLOOR PANEL 221DF BETWEEN FR16 TO FR22 & BETWEEN -Y254 TO Y254. REPLACED FLOOR PANEL 221DF IAW SRM 53-12-00, FIG 206 & IRM 9701, REV G.SDR USAA2013062400037Floor Panel · delaminated2S CHECK - DELAMINATION ON FLOOR PANEL 222EF BETWEEN FR16 TO FR20 & BETWEEN -Y1292 TO -Y254. REPLACED FLOOR PANEL 222EF IAW SRM 53-12-00, FIG 102 & IRM 9701, REV G.SDR USAA2013070100028Frame · cracked2S CHECK -CRACK ON FRAME SEGMENT 1 OF EMERGENCY EXIT HATCH DOOR 834 BETWEEN FR40 TO FR41 & BETWEEN BEAM 1 TO BEAM 3. REPLACED FRAME SEGMENT 1 OF EMERGENCY EXIT HATCH DOOR NR 834 IAW EO 5210Y228.SDR USAA2013070100027Frame · cracked2S CHECK -CRACK ON FRAME SEGMENT 1 OF EMERGENCY EXIT HATCH DOOR NR 844 BETWEEN FR40 TO FR41 & BETWEEN BEAM 1 TO BEAM 3. REPLACED FRAME SEGMENT 1 OF EMERGENCY EXIT HATCH DOOR NR 844 IAW EO 5210Y228.SDR USAA2013070100026Hinge Fitting · excess play2S CHECK - EXCESSIVE PLAY ON VERTICAL STABABILIZER HINGE ARM FITTING NR 7 AT STAB STA 569, RIB 11. REPLACED VERTICAL STABABILIZER HINGE ARM FITTING NR 7 IAW AMM 55-36-41-0401.SDR USAA2013070100025Hinge Fitting · excess play2S CHECK - EXCESSIVE PLAY ON VERTICAL STABABILIZER HINGE ARM FITTING NR 5 AT STAB STA 249 BETWEEN RIB 5 TO RIB 6. REPLACED VERTICAL STABABILIZER HINGE ARM FITTING NR 5 IAW AMM 55-36-41-400-001-A.SDR USAA2013070100024Hinge Fitting · excess play2S CHECK - EXCESSIVE PLAY ON VERTICAL STABABILIZER HINGE ARM FITTING NR 2 AT STAB, STA 120 BETWEEN RIB 2 TO RIB 3. REPLACED VERTICAL STABABILIZER HINGE ARM FITTING NR 2 IAW AMM 55-36-41-400-001-A.SDR USAA2013062700013Hinge Fitting · excess play2S CHECK - EXCESSIVE PLAY ON VERTICAL STABILIZER NR 1 HINGE ARM FITTING AT VERTICAL STAB. STA. AMM 55-36-41-400-001-A.SDR USAA2013062700012Hinge Fitting · excess play2S CHECK - EXCESSIVE PLAY ON VERTICAL STABILIZER NR 4 HINGE ARM FITTING AT VERT STAB STA 206 & BETWEEN RIB 4 TO RIB 5. REPLACED VERTICAL STABILIZER NR 4 HINGE ARM FITTING IAW AMM 55-36-41-400-001-A.SDR USAA2012102200031Shock Absorber · faultyAFTER TAKEOFF THE LANDING GEAR HANDLE WOULD NOT MOVE UP FOR ABOUT 5 SECONDS IN ADDITION AN ECAM: L/G SHOCK ABSORBER FAULT. REMOVED AND REPLACED NOSE LANDING GEAR SHOCK ABSORBER ASSEMBLY. OPS CHECKED GOOD.SDR USAA2012092100016None · contaminatedSTRONG DIRTY SOCK SMELL IN THE LAST 15 MINUTES OF FLIGHT. A REPEAT EVENT OCCURRED THE FOLLOWING DAY (19 SEPT) DIVERTED TO PHL AND DECLARED EMERGENCY. NO SOURCE OF ODOR FOUND AT THIS TIME. FOUND EXCESS ZIP CHEM IN FORWARD CARGO BELLY. CLEANED AS REQUIRED. SDR USAA2012091300003Damper · out of adjustC11/SY6 CHECK - OUT OF ADJUSTMENT DIM "A" (J2) BETWEEN FINGER AND STRIKER LEVER OF DAMPER MECHANISM AND EMERGENCY OPERATION CYLINDER ON DOOR 841. PERFORMED ADJUSTMENT DIM "A" (J2) BETWEEN FINGER AND STRIKE / LEVER OF DAMPER MECHANISM AND EMERGENCY OPERATION CSDR USAA2012091400037Crossbeam · damagedC11 CHECK - ELONGATED HOLE IN CROSSBEAM AT FR 67, S23R & -Y1292. REMOVED AND REPLACED CROSSBEAM IAW A319 SRM 51-72-11 AND AIRBUS DRAWING D53474250.SDR USAA2012091400039Seat Track · corrodedC11 CHECK - SEAT TRACK CORRODED BETWEEN FR 24 AND FR 28 AT -Y1292. REPAIRED SEAT TRACK IAW A319 SRM 51-21-15 FIG 204.SDR USAA2012091700027Floor Panel · delaminatedC11 CHECK - FLOOR PANEL 262 BG DELAMINATED. REMOVED AND REPLACED PANEL IAW IRM 9701, REV G AND EA 502937.SDR USAA2012091700016Hinge Fitting · damagedC11 CHECK - NOSE LANDING GEAR LEFT AFT DOOR AFT HINGE FITTING HAS ELONGATED HOLE. REMOVED AND REPLACED FITTING IAW A319 SRM 51-72-11.SDR USAA2012091700015Hinge Fitting · damagedC11 CHECK - NOSE LANDING GEAR RIGHT AFT DOOR AFT HINGE FITTING HAS ELONGATED HOLE. REMOVED AND REPLACED HINGE FITTING IAW A319 SRM 51-72-11.SDR USAA2012091700030Floor Panel · delaminatedC11 CHECK - FLOOR PANEL 221 PF DELAMINATED. REMOVED AND REPLACED PANEL IAW IRM 9701 REV G AND EA 502941.SDR USAA2012091700028Floor Panel · delaminatedC11 CHECK - FLOOR PANEL 261DF DELAMINATED. REMOVED AND REPLACED PANEL IAW A319 SRM 53-02-00-201, IRM 9701 REV G AND EA 502933.SDR USAA2012091700025Fitting · corrodedC11 CHECK - L2 DOOR SILL CENTER FITTING CORRODED BETWEEN FR 66 AND FR 68 AT S23L. REMOVED AND REPLACED FITTING IAW A319 SRM 51-72-11 AND AIRBUS DRAWING D53480505.SDR USAA2012091700024Fitting · corrodedC11 CHECK - R2 DOOR SILL AFT FITTING IS CORRODED AT FR 68 AND S23R. REMOVED AND REPLACED FITTING IAW A319 SRM 51-72-11AND AIRBUS DRAWING D53480505.SDR USAA2012091700023Shear Plate · corrodedC11 CHECK - FLOORBEAM SHEAR PLATE CORRODED BETWEEN FR 69 AND FR 70 AT S23R. REMOVED AND REPLACED SHEAR PLATE IAW A319 SRM 51-72-11 AND AIRBUS DRAWING D53474180.SDR USAA2012091700022Shear Plate · corrodedC11 CHECK - FLOORBEAM SHEAR PLATE CORRODED BETWEEN FR 69 AND FR 70 AT S23L. REMOVED AND REPLACED SHEAR PLATE IAW A319 SRM 51-72-11 AND AIRBUS DRAWING D53474180.SDR USAA2012091400063Coupling · corrodedC11 CHECK - R2 DOOR SILL COUPLING CORRODED BETWEEN FR 65 AND FR 68 AT S23R. REMOVED AND REPLACED COUPLING IAW A319 SRM 51-72-11, AIRBUS DRAWING D53480505 AND EA 502945.SDR USAA2012091400062Coupling · damagedC11 CHECK - FLOORBEAM COUPLING HAS AN ELONGATED HOLE BETWEEN FR 65 AND FR 66 AT S23R. REMOVED AND REPLACED COUPLING IAW A319 SRM 51-72-11 AND AIRBUS DRAWING D53474230.SDR USAA2012091400061Fitting · wornC11 CHECK - R2 DOOR SILL CORNER FITTING WORN AT FR 66 AND S23R. REMOVED AND REPLACED FITTING IAW A319 SRM 51-72-11.SDR USAA2012091400060Sill · corrodedC11 CHECK. R2 DOOR SILL CORRODED BETWEEN FR 66 AND FR 68 AT S23R. REMOVED AND REPLACED SILL IAW A319 SRM 51-72-11, AIRBUS DRAWING D53480505 AND EA 502945.SDR USAA2012091400059Coupling · damagedC11 CHECK - FLOORBEAM LOWER SIDE COUPLING HAS ELONGATED HOLE AT FR 66 AND S23L. REMOVED AND REPLACED COUPLING IAW A319 SRM 51-72-11, AIRBUS DRAWINGS D53480505 & D53474250 AND EA 502944.SDR USAA2012091400058Coupling · damagedC11 CHECK - FLOORBEAM UPPER SIDE COUPLING HAS ELONGATED HOLE AT FR 66 AND S23L. REMOVED AND REPLACED COUPLING IAW A319 SRM 51-72-11, AIRBUS DRAWINGS D53480505 & D53474250 AND EA #502944.SDR USAA2012091400057Coupling · damagedC11 CHECK - FLOORBEAM COUPLING HAS ELONGATED HOLE AT FR 66 AND S23L. REMOVED AND REPLACED COUPLING IAW A319 SRM 51-72-11, AIRBUS DRAWINGS D53480505 & D53474250 AND EA 502944.SDR USAA2012091400056Coupling · damagedC11 CHECK - FLOORBEAM COUPLING HAS ELONGATED HOLE AT FR 66 AND S23L. REMOVED AND REPLACED COUPLING IAW A319 SRM 51-72-11, AIRBUS DRAWINGS D53480505 & D53474250 AND EA 502944.SDR USAA2012091400055Sill · corrodedC11 CHECK - L2 DOOR SILL CORRODED BETWEEN FR 66 AND FR 68 AT S23L. REMOVED AND REPLACED SILL IAW A319 SRM 51-72-11, AIRBUS DRAWINGS D53474250 & D53480505 AND EA 502944.SDR USAA2012091400054Floorbeam · corrodedC11 CHECK - FLOORBEAM CORRODED BETWEEN FR 67 AND FR 70 AT Y1162. REMOVED AND REPLACED FLOORBEAM IAW A319 SRM 51-72-11 AND AIRBUS DRAWING D53472780.SDR USAA2012091400053Floorbeam · damagedC11 CHECK - ELONGATED HOLE IN FLOORBEAM BETWEEN FR 67 AND FR 68 AT Y1162. REMOVED AND REPLACED FLOORBEAM IAW A319 SRM 51-72-11 AND AIRBUS DRAWING D53472780.SDR USAA2012091400052Floorbeam · damagedC11 CHECK - ELONGATED HOLE IN FLOORBEAM BETWEEN FR 67 AND FR 68 AT Y1162. REMOVED AND REPLACED FLOORBEAM IAW A319 SRM 51-72-11 AND AIRBUS DRAWING D53472780.SDR USAA2012091400051Floorbeam · corrodedC11 CHECK - FLOORBEAM CORRODED BETWEEN FR 66 & FR 67 AT Y1292. REMOVED AND REPLACED FLOORBEAM IAW A319 SRM 51-72-11 AND AIRBUS DRAWING D53472815.SDR USAA2012091400050Floorbeam · corrodedC11 CHECK - FLOORBEAM CORRODED BETWEEN FR 66 & FR 68 FROM Y1292 TO Y1162. REMOVED AND REPLACED FLOORBEAM IAW A319 SRM 51-72-11 AND AIRBUS DRAWING D53472815.SDR USAA2012091400049Floorbeam · corrodedC11 CHECK - FLOORBEAM CORRODED BETWEEN FR 64 & FR 67 AT Y1292. REMOVED AND REPLACED FLOORBEAM IAW A319 SRM 51-72-11 AND AIRBUS DRAWING D53472831.SDR USAA2012091400048Floorbeam · corrodedC11 CHECK - FLOORBEAM CORRODED BETWEEN FR 66 & FR 70 AT -Y765. REMOVED AND REPLACED FOORBEAM IAW A319 SRM 51-72-11 AND AIRBUS DRAWING D53472780.SDR USAA2012091400047Seat Track · corrodedC11 CHECK - SEAT RAIL COUPLING HAS ELONGATED FASTENER HOLE AT FR 66 & FR 67 AT -Y765. REMOVED AND REPLACED RAIL IAW A319 SRM 51-72-11 AND AIRBUS DRAWING D53472816.SDR USAA2012091400046Coupling · corrodedC11 CHECK - FLOORBEAM RAIL COULPLING CORRODED BETWEEN FR 66 & FR 67 AT -765. REMOVED AND REPLACED COUPLING IAW A319 SRM 51-72-11 AND AIRBUS DRAWING D53472816.SDR USAA2012091400045Floorbeam · corrodedC11 CHECK - FLOORBEAM CORRODED BETWEEN FR 67 & FR 70 AT -Y1162. REMOVED AND REPLACED FLOORBEAM IAW A319 SRM 51-72-11 DRAWING D53472780.SDR USAA2012091400044Coupling · corrodedC11 CHECK - R2 DOOR SILL COUPLING CORRODED BETWEEN FR 67 & FR 68 AT -Y1162. REMOVED AND REPLACED COUPLING IAW A319 SRM 51-72-11 DRAWING 53472780.SDR USAA2012091400043Coupling · corrodedC11 CHECK - R2 DOOR SILL COUPLING HAS ELONGATED HOLE BETWEEN FR 67 & FR 68 AT -Y1162. REMOVED AND REPLACED COUPLING IAW A319 SRM 51-72-11 AND AIRBUS DRAWING D53472780.SDR USAA2012091400042Floorbeam · corrodedC11 CHECK - FLOORBEAM CORRODED BETWEEN FR 66 & FR 68 FROM -Y1292 TO -Y1162. REMOVED AND REPLACED FLOORBEAM IAW A319 SRM 51-72-11 AND DRAWING D53472816.SDR USAA2012091400041Coupling · corrodedC11 CHECK - R2 DOOR SILL COUPLING CORRODED BETWEEN FR 66 AND FR 67 AT -Y1292. REMOVED AND REPLACED COUPLING IAW A319 SRM 51-72-11 AND AIRBUS DRAWING D53472816.SDR USAA2012091400040Seat Track · corrodedC11 CHECK - SEAT RAIL CORRODED BETWEEN FR 64 & FR67 AT -Y1292. REMOVED AND REPLACED SEAT RAIL IAW A319 SRM 51-72-11 AND AIRBUS DRAWING D53472816.SDR USAA2012091400038Floorbeam · corrodedC11 CHECK - FLOORBEAM CORRODED BETWEEN FR 65 & FR 66 AT -Y1500. REMOVED AND REPLACED FLOORBEAM IAW A319 SRM 51-72-11 AND AIRBUS DRAWING D53472750 & D53474250.SDR USAA2012091200024Support Frame · corrodedC11 CHECK - LEVEL 2 GALVANIC CORROSION ON SUPPORT FRAME BETWEEN FR69 TO FR70, S23R. REPLACED SUPPORT FRAME BETWEEN FR69 TO FR70, S23R IAW A319 SRM 51-72-11, AIRBUS DRAWINGS D53474180.
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