N649AW

Service difficulty reports · 290

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 = 'N649AW' 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 AALA201511029011Beam · crackedLEFT SIDE BOX BEAM, FLANGE CRACKED AT FRAME 43 & +Y1650. REPAIRED IAW EO 5315Y066.Oct 5, 2015 · N649AW · Airbus A320232 · Fuselage Main, StructureSDR AALA201511029010Beam · cracked3S CHECK, RT BOX BEAM, FLANGE CRACKED AT FRAME 43 & -Y1650. REPAIRED IAW EO 5315Y066.Oct 5, 2015 · N649AW · Airbus A320232 · Fuselage Main, StructureSDR AALA201510239005Pressure Panel · cracked3S CHECK, PRESS PLATE PANEL CRACKED AT FRAME 43 & STRINGER 23R. REPLACED PRESS PLATE PANEL IAW SRM 51-72-11 & DWG D53370569.Oct 5, 2015 · N649AW · Airbus A320232 · Fuselage Main, BulkheadSDR AALA201510239006Skin · saturated3S CHECK, LT ELEVATOR UPPER SURFACE SKIN HAS INDICATION OF TRAPPED WATER, BETWEEN STATION 404 & 527, RIB 10 - 12. REPAIRED ELEVATOR UPPER SURFACE SKIN IAW SRM 55-21-11-201-1 & 51-77-13-001.Oct 2, 2015 · N649AW · Airbus A320232 · Elevator, Plate/SkinSDR AALA201511039010Pressure Deck · cracked3S CHECK, FWD CARGO COMPARTMENT PRESS DECK PANEL HAS CRACKED FASTENER HOLE AT FRAME 36 & -Y1495. REPAIRED IAW EA 25051.Oct 1, 2015 · N649AW · Airbus A320232 · Fuselage Main, BulkheadSDR AALA201511039009Pressure Deck · cracked3S CHECK, FWD CARGO COMPARTMENT PRESS DECK PANEL HAS CRACKED FASTENER HOLE AT FRAME 36 & -Y1419. REPAIRED IAW EA 255051.Oct 1, 2015 · N649AW · Airbus A320232 · Fuselage Main, BulkheadSDR AALA201511039008Pressure Deck · cracked3S CHECK, FWD CARGO COMPARTMENT PRESS DECK PANEL HAS CRACKED FASTENER HOLE AT FRAME 36 & +Y1342. REPAIRED IAW EA 255050.Oct 1, 2015 · N649AW · Airbus A320232 · Fuselage Main, BulkheadSDR AALA201511039007Pressure Deck · cracked3S CHECK, FWD CARGO COMPARTMENT PRESS DECK PANEL HAS CRACKED FASTENER HOLE AT FRAME 36 & +Y1393. REPAIRED IAW EA 255050.Oct 1, 2015 · N649AW · Airbus A320232 · Fuselage Main, BulkheadSDR AALA201511039006Fitting · cracked3S CHECK, FWD CARGO COMPARTMENT FITTING HAS CRACKED FASTENER HOLE AT FRAME 36, Y1495. REPLACED FITTING IAW DWG D53370500 & SRM 51-72-11.Oct 1, 2015 · N649AW · Airbus A320232 · Fuselage Miscellaneous StructureSDR AALA201510239004Floor Panel · delaminated3S CHECK, FWD CARGO COMPARTMENT, FLOOR PANEL 131GF DELAMINATED. REPLACED FLOOR PANEL IAW IRM 9701 REV G & SRM 53-02-00-201.Oct 1, 2015 · N649AW · Airbus A320232 · Fuselage Floor PanelSDR AALA201510239003Floor Panel · delaminated3S CHECK, AFT CARGO COMPARTMENT FLOOR PANEL 152QF DELAMINATED. REPLACED FLOOR PANEL IAW IRM 9701 REV G & SRM 53-02-00.Oct 1, 2015 · N649AW · Airbus A320232 · Fuselage Floor PanelSDR AALA201510239002Floor Panel · delaminated3S CHECK, AFT CARGO COMPARTMENT FLOOR PANEL 151RF DELAMINATED. REPLACED FLOOR PANEL IAW IRM 9701 REV G & SRM 53-02-00-201.Oct 1, 2015 · N649AW · Airbus A320232 · Fuselage Floor PanelSDR AALA201510239001Floor Panel · delaminated3S CHECK, AFT CARGO COMPARTMENT FLOOR PANEL 151JF HAS DELAMINATION. REPLACED FLOOR PANEL IAW IRM 9701 REV G & SRM 53-02-00-201.Oct 1, 2015 · N649AW · Airbus A320232 · Fuselage Floor PanelSDR AALA201509129013Check Valve · leakingEMERGENCY LANDING, AS FLIGHT 507 WAS EN-ROUTE,, THE CREW NOTED LOW PRESS ON THE GREEN HYD SYS. AN PHONE PATCH WAS ESTABLISHED WITH DISPATCH & TECH OPS. IT WAS DEEMED PRUDENT TO CONTINUE ON, DUE TO LONG RNWYS, RESCUE EQUIPMENT & MX FACILITIES. THE FLIGHT CRESep 9, 2015 · N649AW · Airbus A320232 · Hydraulic System, MainSDR AALA201508059006Lens · missingEMERGENCY EXIT LIGHT LENS COVER MISSING AT 11 LT. REPLACED LENS.Aug 4, 2015 · N649AW · Airbus A320232 · Emergency LightingSDR AALA201507139001Mount · corrodedC7 CHECK, NR 1 ENG, AFT ENG MOUNT INBD PIN BOSS HAS SIGNS OF PITTING CORROSION. REMOVED & INSTALLED A SERVICEABLE AFT ENG MOUNT ON LT ENG IAW AMM 71-22-11-400.Jul 11, 2015 · N649AW · Airbus A320232 · Engine Mount SectionSDR AALA201506309007Wedge · delaminatedLEFT WING OTBD TE FLAP REAR WEDGE DELAMINATED. REPLACED IAW EA 252411.Jun 26, 2015 · N649AW · Airbus A320232 · Trailing Edge FlapsSDR AALA201504089004Fmu · inoperativeAFTER TAKEOFF, THE CREW RECEIVED A NR 2 FUEL CONTROL FAULT. DEFERRING TO THE QRH, WHICH TOLD THEM TO PULL ENG BACK TO IDLE. PROCEDURE WAS FOLLOWED, BUT THE SAME ISSUE WAS ACTIVE. THE FLIGHT WAS DIVERTED, AN EMERGNECY WAS DECLARED. RECEIVED AN NR 2 ENG ADApr 7, 2015 · N649AW · Airbus A320232 · Fuel Controlling SystemSDR USAA2015010500005Lens · missingAISLE EMER EXIT LIGHT LENS MISSING ON SEAT 13 LT. REPLACED MISSING EMER EXIT LIGHT LENS ON SEAT 13 LT.Jan 2, 2015 · N649AW · Airbus A320232 · Emergency LightingSDR USAA2014121700007Battery · dischargedSY6 CHECK AFT LT EMER POWER SUPPLY UNIT FAILED EMER LIGHT TEST. REPLACED AFT LT EMER POWER SUPPLY UNIT 13WL BATTERY IAW AMM 33-51-38-400-001-A.Dec 16, 2014 · N649AW · Airbus A320232 · Emergency LightingSDR USAA2014121500019Floor Panel · delaminatedSYS 6 CHECK, DELAMINATION ON FLOOR PANEL 261HG BETWEEN FRAME 64 TO 66, Z-500 & BETWEEN Y1589 TO Y512.5. REPLACED FLOOR PANEL 261HG IAW IRM 9701 REV G.Dec 12, 2014 · N649AW · Airbus A320232 · Fuselage Floor PanelSDR USAA2014121500018Floor Panel · delaminatedSYS 6 CHECK, DELAMINATION ON FLOOR PANEL 262GF BETWEEN FRAME 68 TO 70, Z-500 & BETWEEN Y1162.5 TO -Y1162.5. REPLACED FLOOR PANEL 262GF IAW IRM 9701 REV G.Dec 12, 2014 · N649AW · Airbus A320232 · Fuselage Floor PanelSDR USAA2014121200012Floor Panel · delaminatedSY6 CHECK, DELAMINATION ON FLOOR PANEL 221DF BETWEEN FRAME 16 TO 21, Z-500, Y0, REPLACED FLOOR PANEL 221DF IAW IRM 9701 REV G.Dec 11, 2014 · N649AW · Airbus A320232 · Fuselage Floor PanelSDR USAA2014121200021Floorbeam · corrodedSYS 6 CHECK, LEVEL 2 EXFOLIATION CORROSION ON FLOORBEAM FRAME 68, Z-500, -Y1292. REPLACED FLOORBEAM IAW SRM 51-72-11.Dec 5, 2014 · N649AW · Airbus A320232 · Fuselage Main, Floor BeamSDR USAA2014121200020Floorbeam · corrodedSYS 6 CHECK, LEVEL 2 EXFOLIATION CORROSION ON FLOORBEAM 8 INCHES FWD OF FRAME 70, STRINGER 23R, Z-500. REPLACED FLOORBEAM IAW SRM 51-42-11 & EA 209101.Dec 5, 2014 · N649AW · Airbus A320232 · Fuselage Main, Floor BeamSDR USAA2014121200019Shear Tie · corrodedSYS 6 CHECK, LEVEL 2 EXFOLIATION CORROSION ON SHEAR TIE BETWEEN FRAME 68 TO 69, STRINGER 23L, Z-500. REPLACED SHEAR TIE IAW SRM 51-42-11 & DWG D53471124.Dec 5, 2014 · N649AW · Airbus A320232 · Fuselage Internal Mounting StructureSDR USAA2014121200018Shear Plate · corrodedSYS 6 CHECK, LEVEL 2 EXFOLIATION CORROSION ON SHEAR PLATE BETWEEN FRAME 69 TO 70, STRINGER 23R, Z-500. REPLACED SHEAR PLATE IAW SRM 51-72-11.Dec 5, 2014 · N649AW · Airbus A320232 · Fuselage Miscellaneous StructureSDR USAA2014121200016Floorbeam · corrodedSYS 6 CHECK, LEVEL 2 EXFOLIATION CORROSION ON FLOORBEAM BETWEEN FRAME 69 TO 70, Z-500 & BETWEEN -Y765 TO -Y465. REPLACED FLOORBEAM BETWEEN FRAME 69 TO 70, Z-500 & BETWEEN Y765 TO -Y465 IAW SRM 51-71-11 & 51-21-11.Dec 5, 2014 · N649AW · Airbus A320232 · Fuselage Main, Floor BeamSDR USAA2014121200015Floorbeam · corrodedSYS 6 CHECK, LEVEL 2 EXFOLIATION CORROSION ON FLOORBEAM AT FRAME 66, Z-500, -Y1732. REPLACED FLOORBEAM AT FRAME 66, Z-500, -Y1732 IAW SRM 51-71-11 & 51-21-11.Dec 5, 2014 · N649AW · Airbus A320232 · Fuselage Main, Floor BeamSDR USAA2014121200014Door Sill · corrodedSYS6 CHECK, LEVEL 2 EXFOLIATION CORROSION ON AFT END OF L2 DOOR SILL BETWEEN FRAME 66 TO 68, Z-500, -Y1500. REPLACED L2 DOOR SILL IAW SRM 51-42-11 & 51-72-11.Dec 5, 2014 · N649AW · Airbus A320232 · Fuselage Miscellaneous StructureSDR USAA2014121200013Door Sill · corrodedSY6 CHECK, LEVEL 2 EXFOLIATION CORROSION ON FWD END OF R2 DOOR SILL BOX BETWEEN FRAME 66 TO 68, Z-500, -Y1500. REPLACED R2 DOOR SILL IAW SRM 51-40-00.Dec 5, 2014 · N649AW · Airbus A320232 · Fuselage Miscellaneous StructureSDR USAA2014120900008Floorbeam · corrodedSYS6 CHECK, LEVEL 2 EXFOLIATION ON FLOORBEAM AT FRAME 68, Z-500, Y765. REPLACED FLOORBEAM IAW SRM 51-72-11 & DWG D53472800.Dec 5, 2014 · N649AW · Airbus A320232 · Fuselage Main, Floor BeamSDR USAA2014120900007Floorbeam · corrodedSYS 6 CHECK, LEVEL 2 EXFOLIATION IN 4 AREAS ON FLOORBEAM BETWEEN FRAME 16 TO 20, Z-500, Y254. REPLACED FLOORBEAM IAW SRM 51-23-12.Dec 5, 2014 · N649AW · Airbus A320232 · Fuselage Main, Floor BeamSDR USAA2014101600014Battery · dischargedAFT RT FLASHLIGHT INOPERATIVE. REPLACED BATTERY.Oct 15, 2014 · N649AW · Airbus A320232 · Emergency EquipmentSDR USAA2014020300027Coffeemaker · faultyACRID ELEC ODOR EMANATING FROM FWD GALLEY. REPLACED FWD COFFEE MAKER, FOUND COFFEE MAKER SMOKING DURING BREW CYCLE.Feb 1, 2014 · N649AW · Airbus A320232 · Buffet/GalleysSDR USAA2013121600015Actuator · inoperativeNR 1 ENGINE FAILURE AND SHUTDOWN ON DESCENT INTO IAH. RELIGHT ATTEMPTED, UNSUCESSFUL AND ENGINE SECURED FOR LANDING. PERFORMED IAW A320 TSM 71-00-00-810-808-A. REPLACED E1 VSV ACTUATOR, REPLACED 10TH STAGE SOLENOID VALVE.Dec 13, 2013 · N649AW · Airbus A320232 · Compressor Bleed ControlSDR USAA2013112700005Lens · missingEMERGENCY EXIT LIGHT AFT IS MISSING. REPLACED LENS AS REQUIRED.Nov 26, 2013 · N649AW · Airbus A320232 · Emergency LightingSDR USAA2013112500005Packing · leakingFLIGHT ATTENDANTS REPORTED A DIRTY SOCK SMELL IN REAR OF AIRCRAFT SHORTLY AFTER DESCENT OUT OF FL250, NO SMELL IN COCKPIT. MX COMPLIED WITH JOB CARDS 26L00021001, 26L00021002 & 26L00021004. FOUND OIL LEAK FROM APU STARTER CLUTCH COVER & ACCESSORY GEARBOX. RNov 23, 2013 · N649AW · Airbus A320232 · APU Oil SystemSDR USAA2013112500010Wire · brokenMAINTENANCE REPORTED ROW 13ABC EMERGENCY LIGHT HAS A BROKEN WIRE. MX FIXED BROKEN WIRE AT ROW 13ABC. OPERATIONS CHECKED GOOD, IAW ESPM 20-43-11 & AMM 33-51-00-710-007-A.Nov 22, 2013 · N649AW · Airbus A320232 · Light System WiringSDR USAA2013091800001Battery · inoperativeFORWARD EMERGENCY FLASHLIGHT INOPERATIVE. REPLACED BATTERIES.Sep 17, 2013 · N649AW · Airbus A320232 · Emergency EquipmentSDR USAA2013071000001Director · faultyLAV E SMOKE DETECTOR ACTIVATED, NO FIRE/SMOKE DETECTED. R & R CIDS 1 DIRECTOR, GROUND SCAN GOOD, LAV E SMOKE MESSAGE CEASED.Jul 9, 2013 · N649AW · Airbus A320232 · Detection SystemSDR USAA2013070800018Smoke Detector · false activationLAV E SMOKE DETECTOR ACTIVATED SEVERAL TIMES WITH NO EVIDENCE OF SMOKE OR FIRE. OPS CHECKED LAV E SMOKE DETECTOR IAW TROUBLESHOOTING MANUAL 26-17-00-001-A. CHECKS NORMAL AT THIS TIME.Jul 6, 2013 · N649AW · Airbus A320232 · Smoke DetectionSDR USAA2013070800017Smoke Detector · false activationLAV E SMOKE DETECTOR ACTIVATED TWICE IN FLIGHT WATER WAS POURED IN TRASH RECEPTICAL WITH NO EVIDENCE OF SMOKE. PERFORMED OPS CHECK OF LAV E SMOKE DETECTION SYS REF TROUBLESHOOTING MANUAL 26-17-00-710-001-A. OK FOR SERVICE AT THIS TIME.Jul 5, 2013 · N649AW · Airbus A320232 · Smoke DetectionSDR USAA2013060300004Lens · missingEMERGENCY LIGHT LENS COVER MISSING 12 LT. INSTALLED LENS COVER AS REQUIRED.May 31, 2013 · N649AW · Airbus A320232 · Emergency LightingSDR USAA2013050300001Lens · brokenLENS COVER FOR EMERGENCY EXIT PATH LIGHTING AT 1C BROKEN. REPLACED LENS COVER.May 2, 2013 · N649AW · Airbus A320232 · Emergency LightingSDR USAA2013032800009Spring · weakFORWARD LAVATORY TRASH RECEPTACLE DOOR WAS NOT CLOSED. REPLACED SPRINGS ON FORWARD LAVATORY TRASH RECEPTACLE FLAP BESIDE SINK REFERENCE MAINTENANCE MANUAL CHAPTER 20.Mar 27, 2013 · N649AW · Airbus A320232 · LavatoriesSDR USAA2012081600011Lens · brokenAIRCRAFT RIGHT EMERGENCY EXIT LIGHT BROKEN (COVER) AT 2R DOOR. REPLACED LENS COVER ON EMERGENCY EXIT LIGHT AT 2R DOOR.Aug 14, 2012 · N649AW · Airbus A320232 · Emergency LightingSDR USAA2012080600059Lens · detachedEMERGENCY EXIT LIGHT COVER DOOR R1 DETACHED. REPLACED LENS AT R1 DOOR.Aug 5, 2012 · N649AW · Airbus A320232 · Emergency LightingSDR USAA2012062500007Strap · crackedC11 CHECK - LEFT AFT EMERGENCY EXIT DOOR LATCH STRAP CRACKED. REPLACED LEFT AFT EMERGENCY EXIT DOOR LATCH STRAP (GUIDE PLATE).Jun 22, 2012 · N649AW · Airbus A320232 · Emergency ExitsSDR USAA2012062700015Skin · saturatedC11 CHECK - WATER INGRESS ON RIGHT ELEVATOR UPPER SURFACE BETWEEN 18 INCHES TO 206 INCHES FROM INBOARD END. REPAIRED RIGHT ELEVATOR UPPER SURFACE BETWEEN 18 INCHES TO 206 INCHES FROM INBOARD END IAW A320 SRM 55-27-11 FIGURE 205.Jun 13, 2012 · N649AW · Airbus A320232 · Elevator Tab, Attach Fittings
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