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 USAA2012062900013Angle · corroded3S CHECK - CORROSION ON T-SECTION ANGLE OF FORWARD LOWER VERTICAL FRAME OF LEFT AFT EMERGENCY EXIT HATCH (834) BETWEEN FR40 TO FR41 & BETWEEN BEAM 4 & EDGE CURVE AREA. REPLACED T-SECTION ANGLE IAW A320 SRM 51-72-11 & AIRBUS DRAWING D52279040.May 31, 2012 · N602AW · Airbus A320232 · Emergency ExitsSDR USAA2012062900012Angle · corroded3S CHECK - CORROSION ON T-SECTION ANGLE OF FORWARD LOWER VERTICAL FRAME OF RIGHT AFT EMERGENCY EXIT HATCH (844) BETWEEN FR40 TO FR41 & BETWEEN BEAM 4 & EDGE CURVE AREA. REPLACED T-SECTION ANGLE IAW A320 SRM 51-72-11 & AIRBUS DRAWING D52279040.May 31, 2012 · N602AW · Airbus A320232 · Emergency ExitsSDR USAA2012062900011Angle · corroded3S CHECK - CORROSION ON T-SECTION ANGLE OF AFT LOWER VERTICAL FRAME OF RIGHT AFT EMERGENCY EXIT HATCH (844) BETWEEN FR40 TO FR41 & BETWEEN BEAM 4 & EDGE CURVE AREA. REPLACED T-SECTION ANGLE IAW A320 SRM 51-72-11 & AIRBUS DRAWING D52279040.May 31, 2012 · N602AW · Airbus A320232 · Emergency ExitsSDR USAA2012062800017Door Frame · cracked3S CHECK - CRACK IN INNER FRAME SEGMENT OF EMERGENCY EXIT DOOR 843 BETWEEN FR38 TO FR39 & BETWEEN BEAM 1 TO BEAM 3. REPLACED INNER FRAME SEGMENT OF EMERGENCY EXIT DOOR 843 IAW EO 5210Y228.May 31, 2012 · N602AW · Airbus A320232 · Emergency ExitsSDR USAA2012062800016Door Frame · cracked3S CHECK - CRACK IN INNER FRAME SEGMENT OF EMERGENCY EXIT DOOR 844 BETWEEN FR40 TO FR41 & BETWEEN BEAM 1 TO BEAM 3. REPLACED INNER FRAME SEGMENT OF EMERGENCY EXIT DOOR 844 IAW EO 5210Y228.May 31, 2012 · N602AW · Airbus A320232 · Emergency ExitsSDR USAA2012062600010Door Frame · corroded3S CHECK - CORROSION ON CURVED EDGE OF LEFT FORWARD EMERGENCY EXIT HATCH (833) AT FR39, BEAM 4. REPLACED CURVED EDGE OF LEFT FORWARD EMERGENCY EXIT HATCH (833) AT FR39, BEAM 4 IAW A320 SRM 51-72-11 DRAWING D52279010.May 31, 2012 · N602AW · Airbus A320232 · Emergency ExitsSDR USAA2012062600009Shear Tie · corroded3S CHECK - LEVEL 2 GALVANIC CORROSION ON SHEAR TIE AT FR34, S43R. REPLACED SHEAR TIE AT FR34, S43R IAW A320 SRM 51-72-11.May 31, 2012 · N602AW · Airbus A320232 · Fuselage Internal Mounting StructureSDR USAA2012062600008Shear Tie · corroded3S CHECK - LEVEL 2 GALVANIC CORROSION ON SHEAR TIE AT FR25, S41L. REPLACED SHEAR TIE AT FR25, S41L IAW A320 SRM 51-72-11.May 31, 2012 · N602AW · Airbus A320232 · Fuselage Internal Mounting StructureSDR USAA2012062600007Spar · corroded3S CHECK - LEVEL 2 GALVANIC CORROSION ON LEFT WING FRONT SPAR OF OUTBOUND FLAP LEADING EDGE BETWEEN WS 7792 TO WS 8268, RIB 14 TO RIB 15. REPLACED LEFT WING FRONT SPAR OF OUTBOUND FLAP LEADING EDGE BETWEEN WS 7792 TO WS 8268, RIB 14 TO RIB 15 IAW A320 SRM 51-May 31, 2012 · N602AW · Airbus A320232 · Trailing Edge FlapsSDR USAA2012061300005Structure · cracked3S CHECK - CRACK ON SECTION CONNECTING AT FR68, S24L. REPLACED SECTION CONNECTING AT FR68, S24L IAW A320 SRM 51-72-11 AND DRAWING D53474250.May 31, 2012 · N602AW · Airbus A320232 · Fuselage Miscellaneous StructureSDR USAA2012061200007Coupling · corroded3S CHECK - CORROSION ON OUTBOARD LOWER COUPLING AT FR66, S23L, Y1450. REPLACED OUTBOARD LOWER COUPLING AT FR66, S23L, Y1450 IAW A320 SRM 51-42-11 AND DRAWING D53474250.May 31, 2012 · N602AW · Airbus A320232 · Fuselage Main, FrameSDR USAA2012061200005Coupling · corroded3S CHECK - CORROSION ON INBOARD LOWER COUPLING AT FR66, S23L, Y1450. REPLACED INBOARD LOWER COUPLING AT FR66, S23L, Y1450 IAW A320 SRM 51-42-11 AND DRAWING D53474250.May 31, 2012 · N602AW · Airbus A320232 · Fuselage Main, FrameSDR USAA2012061200004Coupling · corroded3S CHECK - CORROSION ON OUTBOARD UPPER COUPLING AT FR66, S23L, Y1450. REPLACED OUTBOARD UPPER COUPLING AT FR66, S23L, Y1450 IAW A320 SRM 51-42-11 AND DRAWING D53474250.May 31, 2012 · N602AW · Airbus A320232 · Fuselage Main, FrameSDR USAA2012061200003Coupling · corroded3S CHECK - CORROSION ON INBOARD UPPER COUPLING AT FR66, S23L, Y1450. REPLACED INBOARD UPPER COUPLING AT FR66, S23L, Y1450 IAW A320 A320 51-42-11 AND DRAWING D53474250.May 31, 2012 · N602AW · Airbus A320232 · Fuselage Main, FrameSDR USAA2012061900020Seat Track · corroded3S CHECK - CORROSION ON SEAT TRACK BETWEEN FR56+9 INCHES TO FR59+3 INCHES, Y765. REPAIRED SEAT TRACK BETWEEN FR56+8 INCHES TO FR64, Y765 IAW A320 SRM 53-41-15 FIGURE 102 PAGES 215/216.May 30, 2012 · N602AW · Airbus A320232 · Fuselage, Seat/Cargo Attach FittingsSDR USAA2012061100005Sill · cracked3S CHECK - CRACK ON SHAPE SILL BETWEEN FR66+5 INCHES TO FR67+17 INCHES, S23L. REPLACED SHAPE SILL BETWEEN FR66+5 INCHES TO FR67+17 INCHES, S23L IAW A320 SRM 51-72-11AND DRAWING D53480505.May 30, 2012 · N602AW · Airbus A320232 · Fuselage Miscellaneous StructureSDR USAA2012070300008Fitting · corroded3S CHECK - LEVEL 2 GALVANIC CORROSION ON LOWER SILL FITTING BETWEEN FR16 TO FR20, S23R. REPLACED LOWER SILL FITTING BETWEEN FR16 TO FR20, S23R IAW A320 SRM 51-72-11 & AIRBUS DRAWING D53112320, D53112805 & EA 501956.May 29, 2012 · N602AW · Airbus A320232 · Fuselage Miscellaneous StructureSDR USAA2012062900017Sill · corroded3S CHECK - LEVEL 2 GALVANIC CORROSION ON LOWER SILL BETWEEN FR66 TO FR 66+6", -Y1732. REPLACED LOWER SILL BETWEEN FR66 TO FR 66+6", -Y1732 IAW A320 SRM 51-72-11 & AIRBUS DRAWINGS D53480505 & EA 500738.May 29, 2012 · N602AW · Airbus A320232 · Fuselage Miscellaneous StructureSDR USAA2012062900016Sill · corroded3S CHECK - LEVEL 2 GALVANIC CORROSION ON LOWER SILL BETWEEN FR66 TO FR68, S23R. REPLACED LOWER SILL BETWEEN FR66 TO FR68, S23R IAW A320 SRM 51-72-11 & AIRBUS DRAWINGS D53480505 & D53480076.May 29, 2012 · N602AW · Airbus A320232 · Fuselage Miscellaneous StructureSDR USAA2012062200005Hinge Fitting · excess play2S CHECK - EXCESSIVE PLAY AT RUDDER HINGE FITTING NR 2 AT VERTICAL STABILIZER STA 1926 RIB 4. REPLACED RUDDER HINGE FITTING NR 2 IAW A320 SRM 51-72-11 & AMM 55-36-41-400-001-A.May 28, 2012 · N602AW · Airbus A320232 · Rudder StructureSDR USAA2012061400013Floor Panel · debonded3S CHECK - DISBONDED FLOOR PANEL 151GF BETWEEN FR53 TO FR55, Y765 TO -Y765. REPLACED FLOOR PANEL 151GF IAW A320 SRM 53-02-00 AND IRM 9701 REV G.May 27, 2012 · N602AW · Airbus A320232 · Fuselage Floor PanelSDR USAA2012061400012Floor Panel · debonded3S CHECK - DISBONDED FLOOR PANEL 151LF BETWEEN FR56 TO FR58, Y765 TO -Y765. REPLACED FLOOR PANEL 151LF IAW A320 SRM 53-02-00 AND IRM 9701 REV G.May 27, 2012 · N602AW · Airbus A320232 · Fuselage Floor PanelSDR USAA2012060500014Floor Panel · delaminated3S CHECK - DELAMINATION ON FLOOR PANEL 152MF BETWEEN FR56 TO FR58 & BETWEEN -Y765 TO -Y970.8. REPLACED FLOOR PANEL 152MF IAW A320 SRM 53-02-00 & IRM 9701 REV G.May 27, 2012 · N602AW · Airbus A320232 · Fuselage Floor PanelSDR USAA2012060500006Floor Panel · delaminated3S CHECK - DELAMINATION ON FLOOR PANEL 131AF BETWEEN FR24 TO FR28 & BETWEEN Y765 TO -Y765. REPLACED FLOOR PANEL 131AF IAW A320 SRM 53-02-00 & IRM 9701 REV G.May 27, 2012 · N602AW · Airbus A320232 · Fuselage Floor PanelSDR USAA2012052100028Light · inoperativeEMERGENCY EXIT FLOOR PATH LIGHT SEAT 1C INOPERATIVE. REPAIRED EMERGENCY LIGHT ASSEMBLY AT SEAT 1C. OPERATIONAL CHECK GOOD.May 20, 2012 · N602AW · Airbus A320232 · Emergency LightingSDR USAA2012050700011Cylinder · low pressureR2 DOOR ASSIST PRESSURE LOW. SERVICED R2 DOOR TO PROPER PRESSURE IAW AIRBUS MAINTENANCE MANUAL 52-10-00-614-001.May 6, 2012 · N602AW · Airbus A320232 · Service DoorsSDR USAA2012032600044Wire · brokenROW 22 ABC EMERGENCY EXIT LIGHT INOP. RETERMINATED BROKEN WIRE TERMINAL AT SEAT LIGHT IAW ELECTRICAL STANDARD PRACTICES MANUAL 20-25-22.Mar 23, 2012 · N602AW · Airbus A320232 · Light System WiringSDR USAA2012031900028Smoke Detector · false activationLAV E SMOKE DETECTION AURAL AND LIGHT ACTIVATED IN FLIGHT. NO SMOKE WAS FOUND. RESET AFT PANEL - AURAL AND LIGHT INDICATIONS EXTINGUISHED. CIDS PANEL LAV SMOKE ILLUMINATED. MAINTENANCE PERFORMED OPERATIONAL TEST OF THE LAV SMOKE DETECTION SYSTEM IAW AIRBUSMar 17, 2012 · N602AW · Airbus A320232 · Smoke DetectionSDR USAA2012022300002Megaphone · no testFLIGHT ATTENDANT REPORTED AFT MEGAPHONE FAILED PREFLIGHT TEST. MAINTENANCE REPLACED FORWARD MEGAPHONE.Feb 22, 2012 · N602AW · Airbus A320232 · Emergency EquipmentSDR USAA2012020300003Megaphone · brokenFORWARD MEGAPHONE HANDLE BROKEN. REPLACED FORWARD MEGAPHONE AS REQUIRED.Jan 31, 2012 · N602AW · Airbus A320232 · Emergency EquipmentSDR USAA2012020200015Cylinder · low pressureR2 DOOR BOTTLE ASSIST PRESSURE LOW. SERVICED R2 DOOR ASSIST BOTTLE IAW AMM 52-10-00.Jan 31, 2012 · N602AW · Airbus A320232 · Service DoorsSDR USAA2012011800017Warning System · malfunctionedON TAKEOFF ROLL AT 65 KNOTS, ECAM CHIME WITH ENGINE 2 COMPRESSOR FAULT ON UPPER ECAM. MAINTENANCE PERFORMED TROUBLESHOOTING PER TROUBLESHOOTING MANUAL 75-30-00-810-84601 AND POWER ASSURANCE TEST PER AIRBUS MAINTENANCE MANUAL 71-00-00-710-013. NO FAULTS FOUNDJan 13, 2012 · N602AW · Airbus A320232 · Engine Indicating SystemSDR USAA2011122700028Lens · missingDOOR 2L EMERGENCY EXIT LIGHT PLASTIC COVER MISSING. REPLACED EMERGENCY EXIT LIGHT PLASTIC LENS COVER AT 2L DOOR.Dec 23, 2011 · N602AW · Airbus A320232 · Emergency LightingSDR USAA2011100300014Oven · defectiveFLIGHT ATTENDANT REPORTED A BURNING PLASTIC ODOR EMANATING FROM FORWARD GALLEY. TURNED BOTH OVEN SWITCHES AND BUN WARMERS TO OFF - ODOR STILL PRESENT AT TIMES. NO SMOKE OR OTHER INDICATIONS ASSOCIATED WITH SMELL. MAINTENANCE REMOVED AND REPLACED NR 1 OVEN ISep 28, 2011 · N602AW · Airbus A320232 · Buffet/GalleysSDR USAA2011071800013Bottle · low pressureR-2 DOOR ASSIST BOTTLE PSI LOW. SERVICED R-2 DOOR ASSIST BOTTLE.Jul 15, 2011 · N602AW · Airbus A320232 · Service DoorsSDR USAA2011050291723Light · inoperativeFLT 231 - PHX - EEL - AIRCRAFT LEFT OVERWING RED EMERGENCY EXIT LIGHT INOP. MAINTENANCE REPLACED LENS AND RELAMPED.Apr 30, 2011 · N602AW · Airbus A320232 · Emergency LightingSDR USAA2011032991266Fan · faultyFLT 658 SFO-PHL - BURNING SMELL - AT CRUISE (340), CREW REPORTED STRONG SMELL OF INSULATION OR BURNING PLASTIC COMING FROM GASPER VENTS IN FLIGHT DECK. FLIGHT ATTENDANT REPORTED SMELL STRONGEST OVERWING. WHEN PACK 1 WAS TURNED OFF, SMELL INCREASED; PACK 2 OFMar 27, 2011 · N602AW · Airbus A320232 · Air Distribution FanSDR USAA2011022890913Wire · damagedFLT 191 - PHX - EEL - EMERGENCY EXIT AISLE LIGHTS SEAT ROW 22 INOPERATIVE. MAINTENANCE REPAIRED WIRING AT SEAT ROW 22 LEFT EMERGENCY LIGHT.Feb 26, 2011 · N602AW · Airbus A320232 · Light System WiringSDR USAA2011021790766Power Supply · failedFLT 187 - PHX - EEL - CIDS PANEL EMERGENCY LIGHT DOES NOT TEST. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY POWER SUPPLY AT LEFT CENTER CABIN POSITION IAW AIRBUS MAINTENANCE MANUAL 33-51-39.Feb 16, 2011 · N602AW · Airbus A320232 · Emergency LightingSDR USAA2010121593074Hinge Fitting · wornPIT - C3 - MAJOR REPAIR - DEEP WEAR ON LEFT MAIN LANDING GEAR FORWARD HINGE ATTACH FITTING LUG AT FR42, Y230. REPAIRED LEFT MAIN LANDING GEAR FORWARD HINGE ATTACH FITTING LUG AT FR42, Y230 IAW EA 116645.Dec 13, 2010 · N602AW · Airbus A320232 · Fuselage, Door HingeSDR USAA2010121593073Hinge Fitting · wornPIT - C3 - MAJOR REPAIR - DEEP WEAR ON RIGHT MAIN LANDING GEAR FORWARD HINGE ATTACH FITTING LUG AT FR42, -Y230. REPAIRED RIGHT MAIN LANDING GEAR FORWARD HINGE ATTACH FITTING LUG AT FR42, -Y230 IAW EA 116646.Dec 13, 2010 · N602AW · Airbus A320232 · Fuselage, Door HingeSDR USAA2010121593072Floor Panel · debondedPIT - C3 - MAJOR REPAIR - DISBOND ON FLOOR PANEL 251RF AT FORWARD OUTBOARD CORNER. REPLACED FLOOR PANEL 251RF IAW IAW MCGILL IRM 9701 REV G.Dec 8, 2010 · N602AW · Airbus A320232 · Fuselage Floor PanelSDR USAA2010121593070Flap · delaminatedPIT - C3 - MAJOR REPAIR - DISBOND ON LEFT OUTBOARD FLAP TRAILING EDGE. REPAIRED LEFT OUTBOARD FLAP TRAILING EDGE IAW A320 SRM 57-53-00.Dec 7, 2010 · N602AW · Airbus A320232 · Trailing Edge FlapsSDR USAA2010121593069Floor Panel · delaminatedPIT - C3 - MAJOR REPAIR - DELAMINATION ON FLOOR PANEL 221DF AT FR13, Y=0. REPLACED FLOOR PANEL 221DF IAW MCGILL IRM 9701 REV G.Dec 5, 2010 · N602AW · Airbus A320232 · Fuselage Floor PanelSDR USAA2010121593071Aileron · corrodedPIT - C3 - MAJOR REPAIR - CORROSION ON UPPER TRAILING EDGE OF LEFT AILERON. REPAIRED UPPER TRAILING EDGE OF LEFT AILERON IAW A320 SRM 57-61-21 REPAIR A FIGURE 212.Dec 1, 2010 · N602AW · Airbus A320232 · AileronsSDR USAA2010121593068Floor Panel · delaminatedPIT - C3 - MAJOR REPAIR - DELAMINATION ON FLOOR PANEL 222EF. REPLACED FLOOR PANEL 222EF IAW MCGILL IRM 9701 REV G.Dec 1, 2010 · N602AW · Airbus A320232 · Fuselage Floor PanelSDR USAA2010121593067Floor Panel · peelingPIT - C3 - MAJOR REPAIR - UPPER SURFACE OF FLOOR PANEL 261QF PEELING AT FR13, Y=0 1 INCH FROM INBOARD EDGE & 1 INCH FROM AFT EDGE. REPLACED FLOOR PANEL 261QF IAW MCGILL IRM 9701 REV G.Dec 1, 2010 · N602AW · Airbus A320232 · Fuselage Floor PanelSDR USAA10121393030AChannel · corrodedPIT - C3 - MAJOR REPAIR - LEVEL 2 EXFOLIATION CORROSION ON CHANNEL AT FR12, S12R. REPLACED CHANNEL AT FR12, S12R IAW A320 SRM 51-42-00 & 51-76-11.Nov 23, 2010 · N602AW · Airbus A320232 · Fuselage Miscellaneous StructureSDR USAA2010120192744Floorbeam · corrodedPIT - MAJOR REPAIR - C3 CHECK - LEVEL 2 EXFOLIATION CORROSION ON FLOORBEAM AT FR 20, -Y254. REPAIRED FLOORBEAM AT FR 20, -Y254 IAW A320 SRM 53-53-00-14 FIG 204.Nov 23, 2010 · N602AW · Airbus A320232 · Fuselage Main, Floor BeamSDR USAA2010101892309Cylinder · low pressureFLT 307 - LAS - EES - R2 DOOR ASSIST PRESSURE LOW. MAINTENANCE SERVICED R2 DOOR IAW AIRBUS MAINTENANCE MANUAL 52-22-00-614.Oct 16, 2010 · N602AW · Airbus A320232 · Service Doors
Back to N602AW, cancelled Apr 21, 2016