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.

SDR USAA2012091200023Dummy Rail · corrodedC11 CHECK - LEVEL 2 GALVANIC CORROSION ON DUMMY RAIL AT FR16, Y503.2. REPLACED DUMMY RAIL AT FR16, Y503.2 IAW A319 SRM 51-72-11, AIRBUS DRAWINGS D53112825 & D53110984.Sep 2, 2012 · N766US · Airbus A319112 · Fuselage, Seat/Cargo Attach FittingsSDR USAA2012091200022Seat Track · corrodedC11 CHECK - LEVEL 2 GALVANIC CORROSION ON SEAT TRACK AT FR23+2 INCHES, Y1292. REPLACED SEAT TRACK AT FR23+2 INCHES, Y1292 IAW A319 SRM 51-72-11 & AIRBUS DRAWING D53112812.Sep 2, 2012 · N766US · Airbus A319112 · Fuselage, Seat/Cargo Attach FittingsSDR USAA2012091200021Seat Track · corrodedC11 CHECK - LEVEL 2 GALVANIC CORROSION ON SEAT TRACK AT FR20, -Y765. REPLACED SEAT TRACK AT FR20, -Y765 IAW A319 SRM 51-72-11 & AIRBUS DRAWINGS D53110984, D53112812.Sep 2, 2012 · N766US · Airbus A319112 · Fuselage, Seat/Cargo Attach FittingsSDR USAA2012091200020Seat Track · corrodedC11 CHECK - LEVEL 2 GALVANIC CORROSION ON SEAT TRACK AT FR18, -Y1292. REPLACED SEAT TRACK AT FR18, -Y1292 IAW A319 SRM 51-72-11 & AIRBUS DRAWING D53112812.Sep 2, 2012 · N766US · Airbus A319112 · Fuselage, Seat/Cargo Attach FittingsSDR USAA2012091200019Fitting · corrodedC11 CHECK - LEVEL 2 GALVANIC CORROSION ON LOWER CORNER FITTING AT FR68, S23L AT LEFT AFT ENTRY DOOR CUTOUT. REPLACED LOWER CORNER FITTING AT FR68, S23L AT LEFT AFT ENTRY DOOR CUTOUT IAW A319 SRM 51-72-11 & AIRBUS DRAWING D53480505.Sep 2, 2012 · N766US · Airbus A319112 · Fuselage Miscellaneous StructureSDR USAA2012091200018Fitting · corrodedC11 CHECK - LEVEL 2 GALVANIC CORROSION ON LOWER CORNER FITTING AT FR66, S23L AT LEFT AFT ENTRY DOORWAY. REPLACED LOWER CORNER FITTING AT FR66, S23L AT LEFT AFT ENTRY DOORWAY IAW A319 SRM 51-72-11 & AIRBUS DRAWING D53480505.Sep 2, 2012 · N766US · Airbus A319112 · Fuselage Miscellaneous StructureSDR USAA2012091200017Floorbeam · corrodedC11 CHECK - LEVEL 2 GALVANIC CORROSION ON FLOORBEAM BETWEEN FR12 TO FR24, -Y254. REPLACED FLOORBEAM BETWEEN FR12 TO FR24, -Y254 IAW A319 SRM 51-72-11 & AIRBUS DRAWING D53111462.Sep 2, 2012 · N766US · Airbus A319112 · Fuselage Main, Floor BeamSDR USAA2012091200016Floorbeam · corrodedC11 CHECK - LEVEL 2 GALVANIC CORROSION ON FLOORBEAM BETWEEN FR12 TO FR24, Y765. REPLACED FLOORBEAM BETWEEN FR12 TO FR24, Y765 IAW A319 SRM 51-72-11 & AIRBUS DRAWING D53112812.Sep 2, 2012 · N766US · Airbus A319112 · Fuselage Main, Floor BeamSDR USAA2012091200015Floorbeam · corrodedC11 CHECK - LEVEL 2 GALVANIC CORROSION ON FLOORBEAM BETWEEN FR65 TO FR67, -Y318. REPLACED FLOORBEAM BETWEEN FR65 TO FR67, -Y318 IAW A319 SRM 51-72-11 & AIRBUS DRAWING D53472814.Sep 2, 2012 · N766US · Airbus A319112 · Fuselage Main, Floor BeamSDR USAA2012091200014Floorbeam · corrodedC11 CHECK - LEVEL 2 GALVANIC CORROSION ON FLOORBEAM BETWEEN FR64 TO FR66+5 INCHES, -Y765. REPLACED FLOORBEAM BETWEEN FR64 TO FR66+5 INCHES, -Y765 IAW A319 SRM 51-72-11 & AIRBUS DRAWING D53472816.Sep 2, 2012 · N766US · Airbus A319112 · Fuselage Main, Floor BeamSDR USAA2012091200013Floorbeam · corrodedC11 CHECK - LEVEL 2 GALVANIC CORROSION ON FLOORBEAM BETWEEN FR64 TO FR67+10 INCHES, -Y465. REPLACED FLOORBEAM BETWEEN FR64 TO FR67+10 INCHES, -Y465 IAW A319 SRM 51-72-11 & AIRBUS DRAWING D53472816.Sep 2, 2012 · N766US · Airbus A319112 · Fuselage Main, Floor BeamSDR USAA2012091300010Seat Track · corrodedC11/SY6 CHECK - GALVANIC CORROSION ON SEAT TRACK BETWEEN FR20 TO FR24, S23R, -Y189. REPLACED SEAT TRACK BETWEEN FR20 TO FR24, S23R, -Y189 IAW A319 SRM 51-72-11 AND AIRBUS DRAWING D53111406.Sep 2, 2012 · N766US · Airbus A319112 · Fuselage, Seat/Cargo Attach FittingsSDR USAA2012091300009Web · corrodedC11/SY6 CHECK - GALVANIC CORROSION ON WEB BETWEEN FR20 TO FR24, S23R, -Y1732. REPLACED WEB BETWEEN FR20 TO FR24, S23R, -Y1732 IAW A319 SRM 51-72-11 AND AIRBUS DRAWING D53114392.Sep 2, 2012 · N766US · Airbus A319112 · Fuselage Miscellaneous StructureSDR USAA2012091300008Floorbeam · corrodedC11/SY6 CHECK - GALVANIC CORROSION ON FLOORBEAM BETWEEN FR64 TO FR66 PLUS 5 INCHES. REPLACED FLOORBEAM BETWEEN FR64 TO FR66 PLUS 5 INCHES IAW A319 SRM 51-72-11 AND AIRBUS DRAWING D53472815.Sep 2, 2012 · N766US · Airbus A319112 · Fuselage Main, Floor BeamSDR USAA2012091300007Floor Support · corrodedC11/SY6 CHECK - GALVANIC CORROSION ON FLOOR SUPPORT BETWEEN FR12 TO FR24, S23L, Y254. REPLACED FLOOR SUPPORT BETWEEN FR12 TO FR24, S23L, Y254 IAW A319 SRM 51-72-11 AND AIRBUS DRAWINGS D53110984, D53110920.Sep 2, 2012 · N766US · Airbus A319112 · Fuselage Miscellaneous StructureSDR USAA2012091300006Floorbeam · corrodedC11/SY6 CHECK - GALVANIC CORROSION ON FLOORBEAM BETWEEN FR66 PLUS 5 INCHES TO FR70, Y765. REPLACED FLOORBEAM BETWEEN FR66 PLUS 5 INCHES TO FR70, Y765 IAW A319 SRM 51-72-11 AND AIRBUS DRAWING D53472780.Sep 2, 2012 · N766US · Airbus A319112 · Fuselage Main, Floor BeamSDR USAA2012091300005Dummy Rail · corrodedC11/SY6 CHECK - GALVANIC CORROSION ON DUMMY RAIL AT FR16, -Y81. REPLACED DUMMY RAIL AT FR16, -Y81 IAW A319 SRM 51-72-11, AND AIRBUS DRAWINGS D53112828, D53110984, D53112758.Sep 2, 2012 · N766US · Airbus A319112 · Fuselage, Seat/Cargo Attach FittingsSDR USAA2012091300004Dummy Rail · damagedC11/SY6 CHECK - ELONGATED FASTENER HOLE ON DUMMY RAIL AT FR12, -Y81. REPLACED FASTENER AT FR12, -Y81 IAW A319 SRM 51-72-11 DRAWING D53112758.Sep 2, 2012 · N766US · Airbus A319112 · Fuselage, Seat/Cargo Attach FittingsSDR USAA2012091700020Skin · saturatedC11 CHECK - LEFT ELEVATOR UPPER SKIN HAS TRAPPED WATER INDICATION AT STA 5274, 4 INCHES FORWARD OF TRAILING EDGE. REPAIRED SKIN IAW A319 SRM 55-21-11 PARAGRAPH 5.E.Sep 1, 2012 · N766US · Airbus A319112 · Elevator, Plate/SkinSDR USAA2012091700029Skin · saturatedC11 CHECK - RIGHT ELEVATOR UPPER SKIN HAS TRAPPED WATER INDICATION AT STATION 4655, 9.25 INCHES FORWARD OF TRAILING EDGE. REPAIRED SKIN IAW A319 SRM 55-21-11 PARAGRAPH 5.E.Sep 1, 2012 · N766US · Airbus A319112 · Elevator, Plate/SkinSDR USAA2012091700026Skin · saturatedC11 CHECK - RIGHT ELEVATOR UPPER SKIN HAS TRAPPED WATER INDICATION BETWEEN STATION 1809 AND STATION 2265, 15.5 INCHED AFT OF LEADING EDGE. REPAIRED SKIN IAW A319 SRM 55-21-11 PARAGRAPH 5.E.Sep 1, 2012 · N766US · Airbus A319112 · Elevator, Plate/SkinSDR USAA2012091700021Skin · saturatedC11 CHECK - LEFT ELEVATOR UPPER SKIN HAS TRAPPED WATER INDICATION AT STATION 4655, 4 INCHES FORWARD OF TRAILING EDGE. REPAIRED SKIN IAW A319 SRM 55-21-11 PAR 5.E.Sep 1, 2012 · N766US · Airbus A319112 · Elevator, Plate/SkinSDR USAA2012091700019Skin · saturatedC11 CHECK - LEFT ELEVATOR UPPER SKIN HAS TRAPPED WATER INDICATION AT STATION 2707, 4 INCHES FORWARD OF TRAILING EDGE. REPAIRED SKIN IAW A319 SRM 55-21-11 PARAGRAPH 5.E.Sep 1, 2012 · N766US · Airbus A319112 · Elevator, Plate/SkinSDR USAA2012091700018Skin · saturatedC11 CHECK - RIGHT ELEVATOR UPPER SKIN HAS TRAPPED WATER INDICATION AT STATION 3416, 11.5 INCHES FORWARD OF TRAILING EDGE. REPAIR SKIN IAW A319 SRM 55-21-11 PARAGRAPH 5.E.Sep 1, 2012 · N766US · Airbus A319112 · Elevator, Plate/SkinSDR USAA2012091700017Skin · saturatedC11 CHECK - RIGHT ELEVATOR UPPER SKIN HAS TRAPPED WATER INDICATION BETWEEN STATION 2265 AND STATION 2707, 6.25 INCHES FORWARD OF TRAILING EDGE. REPAIRED SKIN IAW A319 SRM 55-21-11 PARAGRAPH 5.E.Sep 1, 2012 · N766US · Airbus A319112 · Elevator, Plate/SkinSDR USAA2012091700014Skin · saturatedC11 CHECK - LEFT ELEVATOR UPPER SKIN HAS TRAPPED WATER INDICATION BETWEEN STATION 5894 & STATION 6009, 4 INCHES FORWARD OF TRAILING EDGE. REPAIR SKIN IAW A319 SRM 55-21-11 PARAGRAPH 5E.Sep 1, 2012 · N766US · Airbus A319112 · Elevator, Plate/SkinSDR USAA2012020200011Cylinder · low pressureL2 DOOR DAMPER AND OPERATION CYLINDER HAS LOW PRESSURE. SERVICED CYLINDER PER AMM 52-10-00-614-001.Feb 1, 2012 · N766US · Airbus A319112 · Passenger/Crew DoorsSDR USAA2011112100020Battery · dischargedRETAINING STRAP FOR EMERGENCY FLASHLIGHT AT FORWARD FLIGHT ATTENDENT POSITION BROKEN. REMOVED AND REPLACED OUTBOARD FLASHLIGHT BATTERY & REPLACED BOTH BROKEN STRAPS, OPS CHECKED GOOD.Nov 20, 2011 · N766US · Airbus A319112 · Emergency EquipmentSDR USAA2011092000015Lens · missingEXIT SIGN FLOOR LEVEL AT 1R DOOR NEEDS TO RE-INSTALLED. REMOVED AND REPLACED R1 DOOR EXIT SIGN COVER.Sep 16, 2011 · N766US · Airbus A319112 · Emergency LightingSDR USAA2011033191285Lens · missingFLT 2044 - DCA-BOS - EMERGENCY LIGHTS - RIGHT OVERWING EMERGENCY EXIT LIGHT LENS MISSING. INSTALLED RIGHT OVERWING EMERGENCY LIGHT COVER. OPERATIONAL CHECK WAS GOOD.Mar 28, 2011 · N766US · Airbus A319112 · Emergency LightingSDR USAA2010032990653Smoke Detector · malfunctionedFLT 1047 - DCA-CLT - BURNING SMELL - STRONG BURNING SMELL IN CABIN, NO ECAM, NO SMOKE NOTED. STRONGEST SMELL IN FORWARD GALLEY, AIRCRAFT LEFT. FOUND CIDS FAULT WITH LAV A SMOKE DETECTOR UNIT EMITTING ACRID SMELL. REMOVED AND REPLACED LAV A SMOKE DETECTOR UMar 28, 2010 · N766US · Airbus A319112 · Smoke DetectionSDR USAA2010030890519Megaphone · inoperativeFLT 1704 - CLT-BDL - EMERGENCY EQUIPMENT - AFT MEGAPHONE INOPERATIVE. REMOVED AND REPLACED AFT MEGAPHONE.Mar 6, 2010 · N766US · Airbus A319112 · Emergency EquipmentSDR USAA920081898Reservoir · lowLOG PAGE 8107178 FLT NR 1817. DCA-CLT EMERGENCY EQUIPMENT CIDS FAULT. RT EMERGENCY SLIDE PRESSURE LOW. R&R RT OFF WING ESCAPE SLIDE RESERVOIR PER MM 25-62-46.Oct 15, 2008 · N766US · Airbus A319112 · Escape SlideSDR USAA920081583Pump · inoperativeLOGPAGE 7907967 FLT 1045 DTW CLT AIR TURN BACK GREEN HYDRAULIC LOW LEVEL AND OVERHEAT. TOTAL LOSS OF GREEN SYSTEM WAS EXPERIENCED DURING CRUISE. THE FLIGHT DECLARED AN EMERGENCY AND RETURNED TO CLT. R&R NR 1 ENGINE HYDRAULIC PUMP. FLUSHED LINES AND REPLACAug 26, 2008 · N766US · Airbus A319112 · Hydraulic Pump (Electric/Engine), MainSDR USAA920081448Yaw Damper · leakingFLT 1740 BUF-PHL - EMERGENCY LANDING - ON APPROACH FROM BUF TO PHL, CREW STATED LOSS OF GREEN HYDRAULIC SYSTEM. ACFT LANDED SAFELY AND TAXIED TO THE GATE UNDER ITS OWN POWER. MAINTENANCE REMOVED AND REPLACED THE LT YAW DAMPER ACTUATOR. OPERATIONAL AND LEAK Jul 29, 2008 · N766US · Airbus A319112 · Autopilot SystemSDR SA08037Slide · low pressureCLT - FLIGHT 1684, CLT-PHL, CAUTION LIGHT ILLUMINATED ON CIDS PANEL. MAINTENANCE REPORTED THE SLIDE EMER R PRESSURE LOW, SERVICED TO GREEN BAND. CIDS CAUTION OUT, OK FOR FLIGHT.May 23, 2008 · N766US · Airbus A319112 · Escape SlideSDR USAA061232Floorbeam · corrodedBETWEEN C67 & C68 AT -Y1160 CORROSION. REPLACED FLOORBEAM PER SRM 51-72-11; CORR TASK JA-260-53500; LEVEL 1.Oct 16, 2006 · N766US · Airbus A319112 · Fuselage Main, Floor BeamSDR USAA061231Floorbeam · corrodedC68 AT -Y1160 CORROSION. REPLACED FLOORBEAM PER SRM 51-72-11; CORR TASK JA-260-53500; LEVEL 1, DEFECT SIZE: 1.5 X 2.5 INCHES AND 1 X 2 INCHES.Oct 16, 2006 · N766US · Airbus A319112 · Fuselage Main, Floor BeamSDR USAA061230Floorbeam · corrodedBETWEEN C66-C67, -Y1292 FLOORBEAM CORROSION. REMOVED AND REPLACED FLOORBEAM PER SRM 51-72-11; CORR TASK JA-260-53500; LEVEL 1, DEFECT SIZE: 1 SQ INCH.Oct 16, 2006 · N766US · Airbus A319112 · Fuselage Main, Floor BeamSDR USAA061229Floorbeam · corrodedC68, Y1160 FLOORBEAM CORROSION. REMOVED AND REPLACED FLOORBEAM PER SRM 51-72-11; CORR TASK JA-260-53500; LEVEL 1, DEFECT SIZE: 1 SQ INCH.Oct 16, 2006 · N766US · Airbus A319112 · Fuselage Main, Floor BeamSDR USAA061228Floorbeam · corrodedC66, Y1292 FLOORBEAM CORROSION. REMOVED & REPLACED FLOORBEAM PER SRM 51-72-11; CORR TASK JA-260-53500; LEVEL 1, DEFECT SIZE: 1 SQ INCH.Oct 16, 2006 · N766US · Airbus A319112 · Fuselage Main, Floor BeamSDR USAA061227Shear Web · corrodedRT SHEAR WEB BETWEEN C69 & C70 UPPER & LOWER SURFACES CORROSION. REMOVED & REPLACED SHEAR WEB PER SRM 51-42-11, 51-72-11; CORR TASK JA-260-53500; LEVEL 1, DEFECT SIZE: 2 INCHES AT 4 PLACES.Oct 16, 2006 · N766US · Airbus A319112 · Fuselage Miscellaneous StructureSDR USAA061226Floorbeam · corrodedBEAM Y765 CORROSION. DEFECTIVE PART REPLACED WITH IDENT PART PER SRM 51-74-00, DEFECT SIZE: 2 X 3 INCHES.Oct 16, 2006 · N766US · Airbus A319112 · Fuselage Main, Floor BeamSDR USAA061225Floorbeam · corrodedFLOORBEAM Y17.32 AT C66, LEFT SIDE CORROSION. CUT OUT CORROSION & INSTALLED REPAIR ANGLES PER SRM 53-41-14; CORR TASK JA-260-53500, LEVEL, DEFECT SIZE: 0.75 X 0.75 INCH.Oct 16, 2006 · N766US · Airbus A319112 · Fuselage Main, Floor BeamSDR USAA061224Floor Support · corrodedFLOOR SUPPORT -Y254 AND CROSSBEAM C-20 CORROSION. CUT OUT DAMAGE, INSTALLED FILLER & DOUBLER PER SRM 53-00-14; FIG 204, DEFECT SIZE: 1 X 1 INCH SPOT.Oct 16, 2006 · N766US · Airbus A319112 · Fuselage Miscellaneous StructureSDR USAA061233Floorbeam · corrodedSTA C17 10 INCHES RT OF CENTER CORROSION. INSTALLED NEW FLOOR SUPPORT BEAM PER SRM 51-72-11; CORR TASK JA-220-53500, LEVEL 1, DEFECT SIZE: 2" X 2" X .075".Oct 16, 2006 · N766US · Airbus A319112 · Fuselage Main, Floor BeamSDR USA2004F00011Battery · dischargedTHE EMERGENCY LIGHTS TEST FAULTS THE AFT EPSU BATTERY. MAINTNANCE REPLACED THE AFT EPSU BATTERY. OPERATIONALLY CHECKS OK.Mar 7, 2004 · N766US · Airbus A319112 · Emergency LightingSDR USAASA03102Light · failedCLT - THE LEFT MAIN ENTRANCE DOOR SLIDE EMERGENCY LIGHTS FAILED DURING TEST. MAINTENANCE REPLACED THE LEFT FORWARD DOOR SLIDE. EMERGENCY LIGHTS PASSED TEST. OK FOR SERVICE. THE REPAIR SHOP FOUND NO FAULTS WITH THE SLIDE LIGHTS. SLIDE RETURNED TO SERVICE. Aug 30, 2003 · N766US · Airbus A319112 · Emergency LightingSDR USAASA03074Battery · inoperativeDURING THE EMERGENCY LIGHTS TEST, RECEIVED 'L AFT EPSU' MESSAGE. MAINTENANCE REPLACED THE AFT LEFT EMERGENCY POWER SUPPLY UNIT BATTERIES. OPERATIONALLY CHECKS OK. (M)Jul 1, 2003 · N766US · Airbus A319112 · Emergency LightingSDR USAA020466Skin · damagedTPA - FOUND SKIN WITH 1 INCH HOLE, BELOW FORWARD CARGO DOOR CUTOUT, FRAME 26.5 AT STRINGER 4R. INSTALLED .063 INCH FILLER WITH .090 INCH DOUBLER PER SRM 53-00-11 PAGE 241/242. (M)Nov 21, 2002 · N766US · Airbus A319112 · Fuselage Main, Plate/Skin
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