N602AW, cancelled Apr 21, 2016

Service difficulty reports · 192

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 = 'N602AW' AND deregistration_id = 'N602AW-2016-04-21'
  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 AWXA200700120Hinge Pin · corrodedSAL - CORROSION ON RIGHT WING NR 2 SPOILER INBOARD HINGE PIN, WS 6132 - WS 6699. REPLACED RIGHT WING NR 2 SPOILER INBOARD HINGE PIN, WS 6132 - WS 6699 IAW A320 AMM 27-64-42.Jan 16, 2007 · N602AW · Airbus A320232 · SpoilersSDR AWXA200700101Fitting · corrodedSAL - MAJOR REPAIR - CORROSION ON THE R1 DOOR CUT OUT LOWER SILL CENTER FITTING, FR 16+6", S23R. REPLACED THE R1 DOOR CUT OUT LOWER SILL CENTER FITTING, FR 16+6", S23R IAW A320 SRM 51-72-11.Jan 15, 2007 · N602AW · Airbus A320232 · Fuselage Miscellaneous StructureSDR AWXA200700100Sill · corrodedSAL - MAJOR REPAIR - CORROSION ON L2 DOOR CUT OUT CENTER FITTING (SHAPE SILL), FR 68 -14", S23L. REPLACED L2 DOOR CUT OUT CENTER FITTING (SHAPE SILL), FS 68 -14", S23L IAW A320 SRM 51-72-11.Jan 14, 2007 · N602AW · Airbus A320232 · Fuselage Miscellaneous StructureSDR AWXA200601743Switch · failedORD - PHX - IN CRUISE FLIGHT, ECAM Y RSVR LO LVL MESSAGE, PERFORMED ECAM PTU OFF AND ENG PUMP OFF, SYSTEM RESET. THE CREW DECLARED A PRECAUTIONARY EMERGENCY. AS A PRECAUTIONARY MEASURE MAINTENANCE REPLACED THE LOW LEVEL SWITCH ASSEMBLY FOR THE YELLOW HYDRAULOct 12, 2006 · N602AW · Airbus A320232 · Hydraulic Quantity SensorSDR AWXA200601524Slide · unwanted deployBOS - EE - LOG - 7401419 - WHILE ON BOARD THE AIRCRAFT, THE CLEANING CREW DEPLOYED THE R1 DOOR SLIDE. MAINTENANCE REPLACED THE R1 DOOR SLIDE IAW R1C25305.Aug 19, 2006 · N602AW · Airbus A320232 · Escape SlideSDR AWXA200600193Profile · corrodedSAL - MAJOR REPAIR - DURING C7 CHECK DISCOVERED CORROSION ON ANGLE FLOOR PROFILE ASSY AT Y465 AND FS 66. NO ALLOWABLE DAMAGE LIMITS WERE FOUND IN THE AIRBUS SRM. MAINTENANCE REMOVED AND INSTALLED NEW ANGLE AT Y465 BETWEEN FS 64 AND FS 66 IAW AIRBUS SRM 320 5Jan 13, 2006 · N602AW · Airbus A320232 · Fuselage Miscellaneous StructureSDR AWXA200600191Plate · crackedSAL - MAJOR REPAIR - DURING C7 CHECK DISCOVERED 4 INCH CRACK ON PLATE/TRAY LOCATED AT Y1306 AND BETWEEN FR 68 AND FR 68+12". NO ALLOWABLE DAMAGE LIMITS WERE FOUND IN THE AIRBUS SRM. MAINTENANCE REMOVED AND INSTALLED NEW PLATE/TRAY AT Y1306 AND BETWEEN FS 68 Jan 13, 2006 · N602AW · Airbus A320232 · Fuselage Miscellaneous StructureSDR AWXA200600190Floorbeam · corrodedSAL - MAJOR REPAIR - DURING C7 CHECK DISCOVERED LEVEL 2 CORROSION ON AT LOWER SILL LOCATED FROM FS 67+19" AT Y-1292. RE-WORK WAS FOUND OUT OF LIMITS IAW AIRBUS 320 SRM 53-41-14. MAINTENANCE CUT OUT DAMAGED SECTION ON LOWER SILL IAW AIRBUS 320 SRM 53-41-14. Jan 13, 2006 · N602AW · Airbus A320232 · Fuselage Main, Floor BeamSDR AWXA200600189Sill · corrodedSAL - MAJOR REPAIR - DURING C7 CHECK DISCOVERED LEVEL 2 CORROSION ON AT LOWER SILL LOCATED FROM FS 65 TO FS 68 AT Y1250. RE-WORK WAS FOUND OUT OF LIMITS IAW AIRBUS 320 SRM 53-41-14. MAINTENANCE CUT OUT DAMAGED SECTION ON LOWER SILL IAW AIRBUS 320 SRM 53-41-1Jan 13, 2006 · N602AW · Airbus A320232 · Fuselage Miscellaneous StructureSDR AWXA200600185Shear Plate · corrodedSAL - MAJOR REPAIR - DURING C07 CHECK DISCOVERED LEVEL 2 CORROSION ON SHEAR PLATE LOCATED AT Y1305, FROM FS 69 TO FS 70. NO ALLOWABLE DAMAGE LIMITS WERE FOUND IN THE AIRBUS SRM. MAINTENANCE REMOVED AND INSTALLED A NEW SHEAR PLATE LOCATED AT Y1305 FROM FS 69 Jan 13, 2006 · N602AW · Airbus A320232 · Fuselage Main, StructureSDR AWXA200600184Plate · corrodedSAL - MAJOR REPAIR - DURING C07 CHECK DISCOVERED CORROSION ON PLATE SUPPORT FLOOR STRUCTURE LOCATED AT Y-1732, FROM FS 69 TO FS 70. NO ALLOWABLE DAMAGE LIMITS WERE FOUND IN THE AIRBUS SRM. MAINTENANCE REMOVED AND INSTALLED A NEW PLATE SUPPORT ON FLOOR STRUCTJan 13, 2006 · N602AW · Airbus A320232 · Fuselage Miscellaneous StructureSDR AWXA200600181Floorbeam · corrodedSAL - MAJOR REPAIR - DURING C7 CHECK DISCOVERED CORROSION ON FLOORBEAM LOCATED AT Y1165, BETWEEN FS 67+16" AND FS 69+4". MAINTENANCE FOUND RE-WORK TO BE OUT OF LIMITS IAW AIRBUS 320 SRM 53-00-1A FIG 102. REMOVED AND INSTALLED NEW FLOORBEAM FROM FS 67+16" TO Jan 13, 2006 · N602AW · Airbus A320232 · Fuselage Main, Floor BeamSDR AWXA200600176Floorbeam · corrodedSAL - MAJOR REPAIR - DURING C7 CHECK DISCOVERED CORROSION ON FLOORBEAM LOCATED AT Y510 AND AT FS 66+5". MAINTENANCE FOUND RE-WORK TO BE OUT OF LIMITS IAW AIRBUS 320 SRM 53-00-1A FIG 102. REMOVED AND INSTALLED NEW FLOORBEAM FROM FS 64 TO FS 70 AND AT Y510 IAWJan 13, 2006 · N602AW · Airbus A320232 · Fuselage Main, Floor BeamSDR AWXA200600175Floorbeam · corrodedSAL - MAJOR REPAIR - DURING C7 CHECK DISCOVERED CORROSION ON FLOORBEAM LOCATED AT Y765 AND AT FS 68. MAINTENANCE FOUND RE-WORK TO BE OUT OF LIMITS IAW AIRBUS 320 SRM 53-00-1A FIG 102. REMOVED AND INSTALLED NEW FLOORBEAM FROM FS 66 TO FS 68 AND AT Y765 IAW AIJan 13, 2006 · N602AW · Airbus A320232 · Fuselage Main, Floor BeamSDR AWXA200600171Fitting · corrodedSAL - MAJOR REPAIR - DURING C07 CHECK DISCOVERED CORROSION ON CORNER FITTING LOWER SILL, FRAME 20 AT BL Y1975L. NO ALLOWABLE LIMITS WERE FOUND IN THE AIRBUS SRM. MAINTENANCE REMOVED AND INSTALLED A NEW FITTING AT FRAME 20 AND Y1975L IAW AIRBUS 320 SRM 51-72-Jan 13, 2006 · N602AW · Airbus A320232 · Fuselage Main, Attach FittingsSDR AWXA200600168Fitting · corrodedSAL- MAJOR REPAIR - DURING C-07 CHECK CORROSION WAS FOUND ON RIVET AND CORNER SILL PLATE. CORNER SILL FRAME 20R REPLACED IAW A320 SRM 51-72-11 PAGE 1-2.Jan 13, 2006 · N602AW · Airbus A320232 · Fuselage Main, Attach FittingsSDR AWXA200600199Seat Track · corrodedSAL - MAJOR REPAIR - DURING C7 CHECK DISCOVERED CORROSION ON SUPPORT FLOOR TRACK AT Y-189 AND FROM FR 20 TO FR 24. MAINTENANCE REMOVED CORROSION AND FOUND RE-WORK TO BE OUT OF LIMITS IAW AIRBUS SRM 320 53-11-14. REMOVED AND INSTALLED NEW SUPPORT FLOOR TRACK Jan 12, 2006 · N602AW · Airbus A320232 · Fuselage, Seat/Cargo Attach FittingsSDR AWXA200600192Floor Support · corrodedSAL - MAJOR REPAIR - DURING C7 CHECK DISCOVERED LEVEL 2 CORROSION ON FLOOR SUPPORT, UPPER SURFACE, BETWEEN FS 15 AND FS 21, LOCATED AT Y254. RE-WORK ON FLOOR SUPPORT WAS OUT OF LIMITS IAW AIRBUS 320 SRM 53-11-14. MAINTENANCE REMOVED AND INSTALLED NEW FLOOR SJan 12, 2006 · N602AW · Airbus A320232 · Fuselage Miscellaneous StructureSDR AWXA200600188Seat Track · corrodedSAL - MAJOR REPAIR - DURING C7 CHECK DISCOVERED CORROSION ON DUMMY RAIL, UPPER SURFACE BETWEEN FS 15 AND FS 20 LOCATED AT Y-254. RE-WORK WAS FOUND TO BE OUT OF LIMITS IAW AIRBUS 320 53-11-14. MAINTENANCE REMOVED AND INSTALLED NEW DUMMY RAIL FROM FS 12 TO FS Jan 12, 2006 · N602AW · Airbus A320232 · Fuselage, Seat/Cargo Attach FittingsSDR AWXA200600186Seat Track · corrodedSAL - MAJOR REPAIR - DURING C7 CHECK DISCOVERED LEVEL 2 CORROSION ON DUMMY RAIL, UPPER SURFACE BETWEEN FS 12 AND FS 16 LOCATED AT Y503.2. RE-WORK WAS FOUND TO BE OUT OF LIMITS IAW AIRBUS 320 53-11-14. MAINTENANCE REMOVED AND INSTALLED NEW DUMMY RAIL FROM FR Jan 12, 2006 · N602AW · Airbus A320232 · Fuselage, Seat/Cargo Attach FittingsSDR AWXA200600183Floorbeam · corrodedSAL - MAJOR REPAIR - DURING C7 CHECK DISCOVERED CORROSION ON FLOORBEAM LOCATED AT Y919, FROM FS 66 TO FS 66+6". MAINTENANCE FOUND RE-WORK TO BE OUT OF LIMITS IAW AIRBUS 320 SRM 53-00-1A FIG 102. REMOVED AND INSTALLED NEW FLOORBEAM FROM FS 65 TO FS 67 AND AT Jan 12, 2006 · N602AW · Airbus A320232 · Fuselage Main, Floor BeamSDR AWXA200600182Floorbeam · corrodedSAL - MAJOR REPAIR - DURING C7 CHECK DISCOVERED CORROSION ON FLOORBEAM LOCATED AT Y1165 AND FS 66. MAINTENANCE FOUND RE-WORK TO BE OUT OF LIMITS IAW AIRBUS 320 SRM 53-00-1A FIG 102. REMOVED AND INSTALLED NEW FLOORBEAM FROM FS 64 TO FS 66 AND AT Y1292 IAW AIRJan 12, 2006 · N602AW · Airbus A320232 · Fuselage Main, Floor BeamSDR AWXA200600180Floorbeam · corrodedSAL - MAJOR REPAIR - DURING C7 CHECK DISCOVERED CORROSION ON FLOORBEAM LOCATED AT Y-1292 AND AT FS 67+7". MAINTENANCE FOUND RE-WORK TO BE OUT OF LIMITS IAW AIRBUS 320 SRM 53-00-1A FIG 102. REMOVED AND INSTALLED NEW FLOORBEAM FROM FS 66 TO FS 68 AND AT Y-1292Jan 12, 2006 · N602AW · Airbus A320232 · Fuselage Main, Floor BeamSDR AWXA200600179Floorbeam · corrodedSAL - MAJOR REPAIR - DURING C7 CHECK DISCOVERED CORROSION ON FLOORBEAM LOCATED AT Y-1292 AND AT FS 65+21". MAINTENANCE FOUND RE-WORK TO BE OUT OF LIMITS IAW AIRBUS 320 SRM 53-00-1A FIG 102. REMOVED AND INSTALLED NEW FLOORBEAM FROM FS 64 TO FS 66 AND AT Y-129Jan 12, 2006 · N602AW · Airbus A320232 · Fuselage Main, Floor BeamSDR AWXA200600178Floorbeam · corrodedSAL - MAJOR REPAIR - DURING C7 CHECK DISCOVERED CORROSION ON FLOORBEAM LOCATED AT Y765 AND AT FS 64+10". MAINTENANCE FOUND RE-WORK TO BE OUT OF LIMITS IAW AIRBUS 320 SRM 53-00-1A FIG 102. REMOVED AND INSTALLED NEW FLOORBEAM FROM FS 66 TO FS 66 AND AT Y765 IAJan 12, 2006 · N602AW · Airbus A320232 · Fuselage Main, Floor BeamSDR AWXA200600177Floorbeam · corrodedSAL - MAJOR REPAIR - DURING C7 CHECK DISCOVERED CORROSION ON FLOORBEAM LOCATED AT Y-765 AND AT FS 67+16". MAINTENANCE FOUND RE-WORK TO BE OUT OF LIMITS IAW AIRBUS 320 SRM 53-00-1A FIG 102. REMOVED AND INSTALLED NEW FLOORBEAM FROM FS 66 TO FS 70 AND AT Y-765 Jan 12, 2006 · N602AW · Airbus A320232 · Fuselage Main, Floor BeamSDR AWXA200600174Floorbeam · corrodedSAL - MAJOR REPAIR - DURING C7 CHECK DISCOVERED CORROSION ON FLOORBEAM LOCATED AT Y1165 AND AT FR 67+16". MAINTENANCE FOUND RE-WORK TO BE OUT OF LIMITS IAW AIRBUS 320 SRM 53-00-1A FIG 102. REMOVED AND INSTALLED NEW FLOORBEAM FROM FS 66 TO FS 68 AND AT Y1165 Jan 12, 2006 · N602AW · Airbus A320232 · Fuselage Main, Floor BeamSDR AWXA200600173Floorbeam · corrodedSAL - MAJOR REPAIR - DURING C7 CHECK DISCOVERED LEVEL 2 CORROSION ON FLOORBEAM LOCATED AT Y-1292 AND AT FS 68+8". MAINTENANCE FOUND RE-WORK TO BE OUT OF LIMITS IAW AIRBUS 320 SRM 53-00-1A FIG 102. REMOVED AND INSTALLED NEW FLOORBEAM FROM FS 68 TO FS 69 AND AJan 12, 2006 · N602AW · Airbus A320232 · Fuselage Main, Floor BeamSDR AWXA200600172Floorbeam · corrodedSAL - MAJOR REPAIR - DURING C7 CHECK DISCOVERED CORROSION ON FLOORBEAM LOCATED AT Y 1582 AND BETWEEN FS 65 TO FS 66. MAINTENANCE FOUND RE-WORK TO BE OUT OF LIMITS IAW AIRBUS 320 SRM 53-00-1A FIG 102. REMOVED AND INSTALLED NEW FLOORBEAM FROM FS 65 TO FS 66 ANJan 12, 2006 · N602AW · Airbus A320232 · Fuselage Main, Floor BeamSDR AWXA200600170Fitting · corrodedSAL - MAJOR REPAIR - DURING C07 CHECK DISCOVERED LEVEL 2 CORROSION ON LOWER SILL BRACKET FROM FORWARD PASSENGER LT DOOR. NO ALLOWABLE DAMAGE LIMITS WERE FOUND IN THE AIRBUS SRM. MAINTENANCE REMOVED AND INSTALLED A NEW FITTING ON THE FORWARD LT PASSENGER DOORJan 12, 2006 · N602AW · Airbus A320232 · Fuselage Main, Attach FittingsSDR AWXA200600167Seat Track · corrodedCORROSION ON SEAT TRACK Y 765 BETWEEN FRAME 15 AND FRAME 17. REPLACED IAW SRM A320 51-72-11 PAGE1-2. FASTENERS REMOVED AND INSTALLED IAW SRM A320 51-42-11 PARA. 7.Jan 12, 2006 · N602AW · Airbus A320232 · Fuselage, Seat/Cargo Attach FittingsSDR AWXA200600187Seat Track · corrodedSAL - MAJOR REPAIR - DURING C7 CHECK DISCOVERED CORROSION ON DUMMY RAIL AT FS 16 AND Y-81. RE-WORK WAS FOUND TO BE OUT OF LIMITS IAW AIRBUS 320 53-11-14. MAINTENANCE REMOVED AND INSTALLED NEW DUMMY RAIL FROM FS 12 TO FS 16 AT Y-81 IAW AIRBUS 320 SRM 51-42-11Jan 11, 2006 · N602AW · Airbus A320232 · Fuselage, Seat/Cargo Attach FittingsSDR AWXA200600157Seat Track · corrodedMCN - AT "C" CHECK DISCOVERED CORROSION ON SEAT TRACK Y-765 BETWEEN FRAME 20 AND FRAME 21. NO ALLOWABLE DAMAGE LIMITS WERE FOUND. SEAT TRACK WAS REMOVED AND REPLACED FROM FROM FRAME 12 TO FRAME 24 IAW AIRBUS SRM A320 51-42 -11, PAGE 1-22. CPCP PROTECTION WDec 1, 2005 · N602AW · Airbus A320232 · Fuselage, Seat/Cargo Attach FittingsSDR AWXA200501095Control Unit · malfunctionedDEPARTING PHX, EN ROUTE TO SAN, CREW REPORTED DURING LEVEL OFF GOING THROUGH 330 KTS IAS AT 220K FT MSL AIRPLANE SHOOK ON LONG AXIS AT ABOUT 4-10 CYCLES PER SECOND SHAKING STOPPED BELOW 300KTS IAS. AIRCRAFT DECLARED EMERGENCY AND LANDED IN SAN WITHOUT FURTHERSep 22, 2005 · N602AW · Airbus A320232 · Elevator Control SystemSDR AWXA200500739Battery · dischargedFOUND EMERGENCY LIGHTS AT PASSENGER SEATS 9L AND 11L ARE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED RT MID CABIN EMERGENCY LIGHT BATTERY IAW AMERICA WEST AIRLINES T/C A1C33302. OPERATIONAL CHECKS WERE GOOD.Jun 22, 2005 · N602AW · Airbus A320232 · Emergency LightingSDR AWXA200500683Power Supply · inoperativeDURING 4 DAY CHECK BOTH EMERGENCY EXIT LIGHTS IN THE FORWARD GALLEY WERE NOT ILLUMINATING. MAINTENANCE REMOVED AND REPLACED THE FORWARD POWER SUPPLY IAW TC R1433303 AND TC A1C33302. OPERATIONAL CHECK NORMAL.Jun 9, 2005 · N602AW · Airbus A320232 · Emergency LightingSDR AWXA200500211Proximity Sensor · faultyPHX - LANDING GEAR - AFTER DEPARTING PHX EN ROUTE TO LAS ECAM INDICATED THE LANDING GEAR WAS NOT UP AND LOCKED, FLIGHT CREW CONFIRMED THAT NLG GEAR WAS DOWN BY NOISE LEVEL AND INDICATIONS, RECYCLED THE LANDING GEAR PER ECAM INSTRUCTIONS AND GEAR RETRACTED, PROFeb 14, 2005 · N602AW · Airbus A320232 · Landing Gear Position and WarningSDR AWXA200600163Seat Track · corrodedSAL - MAJOR REPAIR - DURING C-07 CHECK, CORROSION ON SEAT TRACK WAS FOUND AT Y 1292, BETWEEN FRAMES 15-AND 20 IN THREE PLACES. SEAT TRACK WAS REPLACED IAW AIRBUS SRM 51-72-11.Jan 12, 2005 · N602AW · Airbus A320232 · Fuselage, Seat/Cargo Attach FittingsSDR AWXA200600159Seat Track · corrodedSAL - DURING C-07 CHECK, CORROSION FOUND ON SEAT TRACK Y-1292 BETWEEN FRAME 15 AND FRAME 22 IN 5 PLACES. SEAT TRACK WAS REPLACED IAW A320 51-72-11 PAGE 1-2.Jan 12, 2005 · N602AW · Airbus A320232 · Fuselage, Seat/Cargo Attach FittingsSDR AWXA200401417Battery · dischargedPHX - EEL - DURING 4-DAY CHECK THE LT FORWARD EMERGENCY POWER SUPPLY UNIT BATTERY PACK FAILED TEST. MAINTENANCE REMOVED AND REPLACED BATTERY AT LEFT FORWARD EMERGENCY POWER SUPPLY UNIT (10WL), OPERATIONAL CHECK WAS GOOD.Dec 20, 2004 · N602AW · Airbus A320232 · Emergency LightingSDR AWXA200401331Windshield · crackedEN ROUTE, AT FL 370 THE FO`S WINDSHIELD CRACKED WHEN HEATING ELEMENT BURNED THROUGH, DIVERTED INTO ABQ & LANDED WITHOUT FURTHER EVENT. MAINTENANCE REMOVED AND REPLACED THE FIRST OFFICERS WINDSHIELD IAW AMM, & WINDOW HEAT COMPUTER, OPERATIONAL TEST GOOD. FAILNov 21, 2004 · N602AW · Airbus A320232 · Flight Compartment WindowsSDR AWXA200400993Proximity Sensor · faultyAIR TURN BACK, ON CLIMB OUT, EN ROUTE, RECEIVED ECAM WARNING FOR FORWARD CARGO DOOR WARNING INDICATION, TURNED BACK AND LANDED WITHOUT FURTHER EVENT. MAINTENANCE INSPECTED FORWARD CARGO DOOR AND FOUND IT SECURE, ISSUED MEL 52-70-01, COND. 1 (FWD CARGO DOOR INDSep 9, 2004 · N602AW · Airbus A320232 · Door Warning System
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