N664AW

Service difficulty reports · 234

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 = 'N664AW' 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 USAA2013120400003Coupling · damaged2S CHECK ELONGATED HOLE ON SEAT RAIL COUPLING AT FR 64, Y 1292. REPLACED SEAT RAIL COUPLING AT FR 64, Y 1292 IAW A320 SRM 51-72-11 & DRAWING D53472770.Nov 12, 2013 · N664AW · Airbus A320232 · Fuselage, Seat/Cargo Attach FittingsSDR USAA2013112600007Seat Track · corroded2S CHECK LEVEL 2 GALVANIC CORROSION ON SEAT RAIL AT FR 51+4 INCHES, Y765. REPLACED SEAT RAIL AT FR 51+4 INCHES, Y765 IAW A320 SRM 51-72-11 & DRAWING D53472770 & D53472831.Nov 12, 2013 · N664AW · Airbus A320232 · Fuselage, Seat/Cargo Attach FittingsSDR USAA2013112600006Seat Track · corroded2S CHECK LEVEL 2 GALVANIC CORROSION ON SEAT RAIL AT FR 61+13 INCHES, Y765. REPLACED SEAT RAIL AT FR 61+13 INCHES, Y765 IAW A320 SRM 51-72-11 & DRAWING D53472770.Nov 12, 2013 · N664AW · Airbus A320232 · Fuselage, Seat/Cargo Attach FittingsSDR USAA2013112600002Seat Track · corroded2S CHECK LEVEL 2 GALVANIC CORROSION ON SEAT TRACK BETWEEN FR 24 TO FR 35, Y1292. REPLACED SEAT TRACK BETWEEN FR 24 TO FR 35, Y1292 IAW A320 SRM 51-72-11 & DRAWING D53231730.Nov 12, 2013 · N664AW · Airbus A320232 · Fuselage, Seat/Cargo Attach FittingsSDR USAA2013112500020Seat Track · corroded2S CHECK LEVEL 2 GALVANIC CORROSION ON SEAT RAIL BETWEEN FR 46+15 INCHES TO FR 64, Y 1292. REPLACED SEAT RAIL BETWEEN FR 46+15 INCHES TO FR 64, Y 1292 IAW A320 SRM 51-72-11, DRAWING D53472770 & D53472550.Nov 12, 2013 · N664AW · Airbus A320232 · Fuselage, Seat/Cargo Attach FittingsSDR USAA2013112000001Pin · corroded2S CHECK CORROSION ON PIN OF RT AILERON OTBD ACTUATOR AT WS 12870, RIB 24. REPLACED RT AILERON OTBD ACTUATOR PIN IAW A320 AMM 27-14-41-400-001.Nov 12, 2013 · N664AW · Airbus A320232 · Aileron Control SystemSDR USAA2013120900018Web · corroded2S CHECK, LEVEL 2 GALVANIC CORROSION ON WEB IN BULK CARGO COMPARTMENT BETWEEN FR 62 TO FR 63, STRINGER 38R. REPLACED WEB IN BULK CARGO COMPARTMENT BETWEEN FR 62 TO FR 63, STRINGER 38R IAW A320 SRM 51-72-11 & DRAWING D53475750.Nov 10, 2013 · N664AW · Airbus A320232 · Fuselage Miscellaneous StructureSDR USAA2013112700010Sill · corroded2S CHECK LEVEL 2 GALVANIC CORROSION ON LOWER SILL BETWEEN FR 66 TO FR 68, STRINGER 23L. REPLACED LOWER SILL BETWEEN FR 66 TO FR 68, STRINGER 23L IAW A320 SRM 51-72-11, DRAWING D53480505 & EA 504417.Nov 10, 2013 · N664AW · Airbus A320232 · Fuselage Miscellaneous StructureSDR USAA2013112700009Coupling · corroded2S CHECK LEVEL 2 GALVANIC CORROSION ON COUPLING LOWER SILL AT FR 66, STRINGER 23L. REPLACED COUPLING LOWER SILL AT FR 66, STRINGER 23L IAW A320 SRM 51-72-11 & DRAWING D53474250.Nov 10, 2013 · N664AW · Airbus A320232 · Fuselage Miscellaneous StructureSDR USAA2013112700008Doubler · corroded2S CHECK LEVEL 2 GALVANIC CORROSION ON REPAIR DOUBLER IN BULK CARGO AT FR 60+3 INCHES, STRINGER 30R. REPLACED REPAIR DOUBLER IN BULK CARGO AT FR 60+3 INCHES, STRINGER 30R IAW A320 SRM 53-41-49-201, PARAGRAPH 5C, FIG 203.Nov 10, 2013 · N664AW · Airbus A320232 · Fuselage Miscellaneous StructureSDR USAA2013112000003Coupling · damaged2S CHECK ELONGATED HOLE ON FLOOR BEAM COUPLING AT FRAME 66+5 INCHES, Y1292. REPLACED FLOOR BEAM COUPLING AT FRAME 66+5 INCHES, Y1292 IAW A320 51-72-11 & DRAWING D53472815.Nov 10, 2013 · N664AW · Airbus A320232 · Fuselage Main, Floor BeamSDR USAA2013111900007Seat Track · corroded2S CHECK CABIN SEAT TRACK CORRODED BETWEEN FRAME 64 & FRAME 67 AT Y 765. R & R SEAT TRACK IAW A320 SRM 51-72-11.Nov 10, 2013 · N664AW · Airbus A320232 · Fuselage, Seat/Cargo Attach FittingsSDR USAA2013111900006Seat Track · corroded2S CHECK CABIN SEAT TRACK CORRODED BETWEEN FRAME 64 & FRAME 65 AT Y 765. R & R SEAT TRACK IAW A320 SRM A320 51-72-11.Nov 10, 2013 · N664AW · Airbus A320232 · Fuselage, Seat/Cargo Attach FittingsSDR USAA2013111900005Seat Track · corroded2S CHECK CABIN SEAT TRACK CORRODED BETWEEN FRAME 64 & FRAME 65 AT Y 1292. R & R SEAT TRACK IAW A320 SRM A320 51-72-11 & DRAWING D53472815.Nov 10, 2013 · N664AW · Airbus A320232 · Fuselage, Seat/Cargo Attach FittingsSDR USAA2013120400007Fitting · corroded2S CHECK LEVEL 2 GALVANIC CORROSION ON LOWER SILL FITTING BETWEEN FR 16 TO FR 20, STRINGER 23R. REPLACED LOWER SILL FITTING BETWEEN FR 16 TO FR 20, STRINGER 23R IAW A320 SRM 51-72-11 & DRAWING D53110339.Nov 9, 2013 · N664AW · Airbus A320232 · Fuselage Miscellaneous StructureSDR USAA2013112900006Seat Track · corroded2S CHECK LEVEL 2 GALVANIC CORROSION ON SEAT TRACK BETWEEN FR 12 TO FR 24, Y 1292. REPLACED SEAT TRACK BETWEEN FR 12 TO FR 24, Y 1292 IAW A320 SRM 51-72-11, PAGE 1 - 2, DRAWING D53112812 & D53110920.Nov 9, 2013 · N664AW · Airbus A320232 · Fuselage, Seat/Cargo Attach FittingsSDR USAA2013112600008Floor Panel · delaminated2S CHECK DELAMINATION ON FLOOR PANEL 151QF BETWEEN FR 58 TO FR 59 & BETWEEN Y765 TO Y970.8. REPLACED FLOOR PANEL 151QF IAW A320 SRM 53-02-00, PAR 8H, FIGURE 209 & IRM 9701, REVISION G.Nov 6, 2013 · N664AW · Airbus A320232 · Fuselage Floor PanelSDR USAA2013111900008Floor Panel · delaminated2S CHECK CARGO BIN FLOOR PANEL 152BF DELAMINATED. R & R FLOOR PANEL IAW A320 SRM 53-02-00 PAR 8H F 209 & IRM 9701 REV G.Nov 6, 2013 · N664AW · Airbus A320232 · Fuselage Floor PanelSDR USAA2013090300018Bulb · inoperativeOVERHEAD EMERGENCY EXIT LIGHT BULBS NOT WORKING. REPLACED AFT GALLEY BULL NOSE OVERHEAD EMERGENCY EXIT LIGHT ASSY.Aug 30, 2013 · N664AW · Airbus A320232 · Emergency LightingSDR USAA2013082700007Release Mech · out of adjustREAR ENTRY R2 DOOR, ARMED SLIDE INDICATION INTERMITTENT. FOUND ESCAPE SLIDE GIRT BAR ENGAGEMENT RESTRICTING ARMING LEVER TRAVEL. ACCOMPLISHED ESCAPE SLIDE RELEASE MECHANISM ADJUSTMENT IAW AMM TASK 52-13-22-820-001-A.Aug 26, 2013 · N664AW · Airbus A320232 · Escape SlideSDR USAA2013082600006Slide · inoperativeR2 DOOR SLIDE INDICATION INTERMITTANTLY SHOWS DISARMED INFLIGHT, F/A'S REPORT ARMING HANDLE NOT FLUSH WHEN DOOR ARMED. REPLACED AFT RT ESCAPE SLIDE.Aug 24, 2013 · N664AW · Airbus A320232 · Escape SlideSDR USAA2013071500009Proximity Switch · faultyCREW REPORTED THE 2R DOOR SLIDE DOES NOT SHOW ARMED ON DOOR/IND PAGE. MX R & R PROX SWITCH FOR 2R DOOR.Jul 11, 2013 · N664AW · Airbus A320232 · Door Warning SystemSDR USAA2013071500008Girt Bar · not seatedCREW REPORTED THE AFT RT DOOR ARMING HANDLE RISES UP DURING CRUISE -WILL NOT STAY DOWN AND ARMED. MX RESEATED GIRT BAR INTO FLOOR TRACKS. SYS OPS CHECKS GOOD WITH NO SPONGYNESS IN HANDLE MECHANISM.Jul 11, 2013 · N664AW · Airbus A320232 · Emergency EquipmentSDR USAA2013070500005Battery · dischargedCREW REPORTED THE F/A AFT FLASHLIGHT IS NOT BLINKING. MX R & R AFT F/A FLASHLIGHT BATTERY. OPS CHECK GOOD.Jul 4, 2013 · N664AW · Airbus A320232 · Emergency EquipmentSDR USAA2013070800025Shear Plate · corrodedLEVEL 2 EXFOLIATION CORROSION ON LT SHEAR PLATE BETWEEN FR69 TO FR70, Y1732. REPLACED LT SHEAR PLATE BETWEEN FR69 TO FR70, Y1732 IAW TYPICAL REPAIR TR320-2528-10-0011G.Jul 3, 2013 · N664AW · Airbus A320232 · Fuselage Miscellaneous StructureSDR USAA2013070300012Seal · leakingSY6 CHECK - L2 DOOR DAMPER DOES NOT HOLD PRESSURE. REPLACED DIAPHRAM SEAL OF DAMPER IAW AMM 52-10-00-610-001.Jul 3, 2013 · N664AW · Airbus A320232 · Passenger/Crew DoorsSDR USAA2013070500021Floorbeam · corrodedSY6 CHECK. CABIN FLOORBEAM CORRODED AT FR 66 AND Y -1292. R & R BEAM IAW SRM 51-42-11.Jul 3, 2013 · N664AW · Airbus A320232 · Fuselage Main, Floor BeamSDR USAA2013070500020Shear Plate · corrodedSY6 CHECK. CABIN FLOOR SHEAR PLATE CORRODED BETWEEN FR 69 & FR 70 AT Y 1732. R & R SHEAR PLATE IAW TR 320-2528-10-001163.Jul 3, 2013 · N664AW · Airbus A320232 · Fuselage Miscellaneous StructureSDR USAA2013070500019Web · corrodedSY6 CHECK. CABIN FLOOR WEB CORRODED FR 20 AND Y 62. R & R WEB IAW SRM 51-42-11.Jul 3, 2013 · N664AW · Airbus A320232 · Fuselage Miscellaneous StructureSDR USAA2013070500018Floorbeam · corrodedSY6 CHECK. CABIN FLOORBEAM CORRODED AT FR 68 AND Y 1732. R & R BEAM IAW SRM 51-42-11, SRM 51-42-211/2.Jul 3, 2013 · N664AW · Airbus A320232 · Fuselage Main, Floor BeamSDR USAA2013070500017Floorbeam · corrodedSY6 CHECK. CABIN FLOORBEAM CORRODED BETWEEN FR 68 AND FR 69 AT Y -1292. R & R BEAM IAW SRM 51-72-11.Jul 3, 2013 · N664AW · Airbus A320232 · Fuselage Main, Floor BeamSDR USAA2013070500016Shear Plate · corrodedSY6 CHECK. CABIN FLOOR SHEAR PLATE CORRODED BETWEEN FR 69 & FR 70 AT Y -1732. R & R SHEAR PLATE IAW TR320-2528-10-0011G.Jul 3, 2013 · N664AW · Airbus A320232 · Fuselage Miscellaneous StructureSDR USAA2013070500015Floor Support · corrodedSY6 CHECK. CABIN FLOOR SUPPORT CORRODED AT FR 16 AND Y 254. REPAIRED SUPPORT IAW SRM 53-00-14, FIG 206 AND SRM 51-42-11.Jul 3, 2013 · N664AW · Airbus A320232 · Fuselage Miscellaneous StructureSDR USAA2013070500014Floorbeam · corrodedSY6 CHECK. CABIN FLOORBEAM CORRODED BETWEEN FR 66 AND FR 68 AT Y -1162.5. R & R BEAM IAW SRM 51-72-11.Jul 3, 2013 · N664AW · Airbus A320232 · Fuselage Main, Floor BeamSDR USAA2013070500013Shear Plate · corrodedSY6 CHECK. CABIN FLOOR SHEAR PLATED CORRODED BETWEEN FR 69 AND FR 70 AT Y -1732. R & R SHEAR PLATE IAW TR320-2528-10-0011G.Jul 3, 2013 · N664AW · Airbus A320232 · Fuselage Miscellaneous StructureSDR USAA2013070500011Diaphragm · leakingMX REPORTED THE L2 DOOR DAMPER DOES NOT HOLD PRESSURE. MX R & R DIAPHRAGM SEAL OF L2 DOOR DAMPER PERCUSSION MECHANISM AND SERVICED WITH NITROGEN (BOTTLE HELD PRESSURE) IAW AMM 52-10-00-610-001.Jul 3, 2013 · N664AW · Airbus A320232 · Passenger/Crew DoorsSDR USAA2013053100004Floor Panel · corrodedDEBONDED & CORRODED FLOOR PANEL NR 162GF BETWEEN FR59 TO FR60. REPLACED FLOOR PANEL IAW SRM 53-42-04-40D.May 29, 2013 · N664AW · Airbus A320232 · Fuselage Floor PanelSDR USAA2013052800013Stringer · corrodedA5 VISIT, CORROSION ON STRINGER S33L BETWEEN FR56 TO FR58. REPAIRED STRINGER S33L BETWEEN FR56 TO FR58 IAW SRM 53-00-13, FIG 201.May 22, 2013 · N664AW · Airbus A320232 · Fuselage Main, Longeron/StringerSDR USAA2013040300004Lens · missingROW 10 AIRCRAFT LEFT EMERGENCY LIGHT LENS MISSING. REPLACED LENS AS REQUIRED.Apr 2, 2013 · N664AW · Airbus A320232 · Emergency LightingSDR USAA2013020800035Lens · missingTHE DOOR PROXIMITY LIGHT COVER ON DOOR 2R IS MISSING. INSTALLED NEW EMERGENCY LIGHT COVER ON DOOR 2R.Feb 7, 2013 · N664AW · Airbus A320232 · Emergency LightingSDR USAA2012021700004Servo Valve · leakingAFTER ENGINE START, PILOT REPORTED NR 2 ENGINE FAILED. AIRCRAFT RETURNED TO GATE. MAINTENANCE REMOVED AND REPLACED THE NR 2 ENGINE LOW/HIGH PRESSURE FUEL PUMP AND FUEL METERING UNIT IAW MM 73-12-41 AND 73-22-52. FUEL METERING UNIT WAS A CONFIRMED FAILURE - Feb 16, 2012 · N664AW · Airbus A320232 · Fuel Controlling SystemSDR USAA2012013000017Cylinder · brokenL1 DOOR EMERGENCY OPEN ASSIST BOTTLE PRESSURE GAUGE BROKEN. REMOVED AND REPLACED L1 DOOR ASSIST BOTTLE IAW AIRBUS MAINTENANCE MANUAL 52-11-14.Jan 29, 2012 · N664AW · Airbus A320232 · Passenger/Crew DoorsSDR USAA2012010900014Container · defectiveROW 5B OXYGEN MASKS FELL OUT. MAINTENANCE REMOVED AND REPLACED ROW 5 LEFT EMERGENCY OXYGEN CONTAINER IAW AIRBUS MAINTENANCE MANUAL 35-21-41.Jan 5, 2012 · N664AW · Airbus A320232 · Passenger Oxygen SystemSDR USAA2011122200009Lens · missingFORWARD LT WINDSCREEN EMERGENCY EXIT PATH LIGHT LENS MISSING. INSTALLED LENS ON LT WINDSCREEN EMERGENCY EXIT PATH LIGHT.Dec 21, 2011 · N664AW · Airbus A320232 · Emergency LightingSDR USAA2011121500021Lens · detachedRED EMERGENCY LIGHT LENS COVER ON FORWARD CABIN BULKHEAD POPPED OFF. MAINTENANCE REINSTALLED LENS AS REQUIRED.Dec 13, 2011 · N664AW · Airbus A320232 · Emergency LightingSDR USAA2011120800015Light · looseRED EMERGENCY FLOOR LIGHT ON FORWARD BULKHEAD IS HANGING LOOSE. RE-ATTACHED BULKHEAD LIGHT ASSEMBLY.Dec 6, 2011 · N664AW · Airbus A320232 · Emergency LightingSDR USAA2011092700016Actuator · failedAIRCRAFT YAWED LEFT SUDDENLY AND RUDDER TRIM 1 FAULTED. ON DESCENT, MULTIPLE FAULT APPEARED - YAW DAMPER 1, RUDDER TRIM FAULT, RUDDER TRAVEL LIMITER STUCK 2 DEGREES YAW, AUTO BRAKE FAULT, STATUS PAGE NORMAL BRAKE INOPERATIVE, ECAM SHOWED ALTERNATE BRAKE. DECSep 20, 2011 · N664AW · Airbus A320232 · Rudder ActuatorSDR USAA2011092700015Limiter · failedAIRCRAFT YAWED LEFT SUDDENLY AND RUDDER TRIM 1 FAULTED. ON DESCENT, MULTIPLE FAULT APPEARED - YAW DAMPER 1, RUDDER TRIM FAULT, RUDDER TRAVEL LIMITER STUCK 2 DEGREES YAW, AUTO BRAKE FAULT, STATUS PAGE NORMAL BRAKE INOPERATIVE, ECAM SHOWED ALTERNATE BRAKE. DECSep 20, 2011 · N664AW · Airbus A320232 · Rudder ActuatorSDR USAA2011090900028Apu · leakingCREW REPORTED OILY, DIRTY SOCK ODOR THROUGHOUT ENTIRE AIRCRAFT AT TOP OF DESCENT UNTIL LANDING. MAINTENANCE FOUND EVIDENCE OF APU LEAK. REMOVED AND REPLACED THE APU.Sep 6, 2011 · N664AW · Airbus A320232 · APU Oil SystemSDR USAA2011012590326Lens · missingFLT 73 - SEA - EEL - RED EMERGENCY FLOOR PROXIMITY LIGHT AT FORWARD LT WINDSCREEN IS MISSING LENS & BULB. MAINTENANCE INSTALLED BULB & LENS FOR EMERGENCY PROXIMITY LIGHT AT FORWARD LT WINDSCREEN.Jan 24, 2011 · N664AW · Airbus A320232 · Emergency Lighting
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