N658AW

Service difficulty reports · 223

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 = 'N658AW' 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 AWXA200501443Battery · inoperativeLAS - EEL - DURING OVERNIGHT INSPECTION, FOUND EMERGENCY ESCAPE PATH LIGHTING IN SEVERAL ROWS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE MID CABIN RT AND LT EMERGENCY PATH LIGHTING BATTERIES. OPERATIONAL CHECKS WERE GOOD.Nov 25, 2005 · N658AW · Airbus A320232 · Emergency LightingSDR AWXA200600047Window · failedCREW REPORTED THAT DURING CRUISE, EN ROUTE TO BOS, THE F/O'S WINDOW MIDDLE PANE SHATTERED AND WAS ARCING. PER QRH CREW WAS TO DESCEND. DECLARED EMERGENCY TO EXPEDITE DESCENT. ONCE AT LOWER ALTITUDE CANCELLED EMERGENCY AND CONTINUED TO BOS, LANDING WITHOUT FNov 23, 2005 · N658AW · Airbus A320232 · Flight Compartment WindowsSDR AWXA200501293Power Supply · inoperativeORD - EEL - DURING 4 DAY CHECK DISCOVERED EVERY OTHER EMERGENCY EXIT LIGHT ILLUMINATED IN FWD CABIN DURING EMERGENCY LIGHTS TEST. MAINTENANCE REMOVED AND REPLACED THE LT OVERWING EMERGENCY POWER SUPPLY UNIT (11WL). OPERATIONAL TESTS WERE GOOD.Oct 31, 2005 · N658AW · Airbus A320232 · Emergency LightingSDR AWXA200600251Rib · damagedPHX - DURING ROUTINE MAINTENANCE THE LT PYLON NUMBER 5-RIB, LINE ATTACHMENT CLEATS (PN'S D463072820000 & D54610270200) WERE FOUND WORN AND ELONGATED AT SEVERAL LINE ATTACHMENT POINTS. MAINTENANCE REMOVED DISCREPANT PARTS FROM THE LT PYLON. WELDED DISCREPANT Oct 18, 2005 · N658AW · Airbus A320232 · Nacelle/Pylon, Frame/Spar/RibSDR AWXA200401130Floorbeam · corrodedDURING BC-4 CHECK GALVANIC CORROSION WAS FOUND ON LONGITUDINAL FLOORBEAM Y1292, UNDER LT AFT LAVATORY AT FR 66. MAINTENANCE REMOVED FLOORBEAM Y1292 LT AT FR 66; FABRICATED A NEW REPLACEMENT BEAM; INSTALLED REPAIR PART IAW A320 SRM 51-71-11.Sep 25, 2004 · N658AW · Airbus A320232 · Fuselage Main, Floor BeamSDR AWXA200401108Floor Panel · delaminatedDURING BC-4 CHECK, AFT CARGO COMPARTMENT FLOOR PANEL 151GF WAS FOUND DELAMINATED AT FS 53. MAINTENANCE REMOVED FLOOR PANEL 151GF; CUTOUT DELAMINATED AREA; PERFORMED EDGE FILLING PROCEDURE (DOUBLER) IAW A320 SRM 53-02-00, FIG 209.Sep 25, 2004 · N658AW · Airbus A320232 · Fuselage Floor PanelSDR AWXA200401107Floor Panel · crackedDURING BC-4 CHECK, A 4 INCH CRACK WAS FOUND IN FORWARD CARGO COMPARTMENT FLOOR PANEL 131DF BETWEEN FS 24 AND FS 28. MAINTENANCE REMOVED FLOOR PANEL 131DF; CUTOUT DAMAGED AREA; PERFORMED EDGE FILLING PROCEDURE (DOUBLER) IAW A320 SRM 53-02-00, FIG 209.Sep 25, 2004 · N658AW · Airbus A320232 · Fuselage Floor PanelSDR AWXA200401106Floor Panel · crackedDURING BC-4 CHECK, FORWARD CARGO COMPARTMENT FLOOR PANEL 131EF WAS FOUND DELAMINATED AND CRACKED BETWEEN FS 28 AND FS 30. MAINTENANCE REMOVED FLOOR PANEL 131EF; CUTOUT DELAMINATED AND CRACKED AREA; PERFORMED EDGE FILLING PROCEDURE (DOUBLER) IAW A320 SRM 53-02Sep 25, 2004 · N658AW · Airbus A320232 · Fuselage Floor PanelSDR AWXA200401105Floor Panel · delaminatedDURING BC-4 CHECK, AFT CARGO COMPARTMENT FLOOR PANEL 151DF WAS FOUND DELAMINATED BETWEEN FS 49 AND FS 53. MAINTENANCE REMOVED FLOOR PANEL 151DF; CUTOUT DELAMINATED AREA; PERFORMED EDGE FILLING PROCEDURE (DOUBLER) IAW A320 SRM 53-02-00, FIG 209.Sep 25, 2004 · N658AW · Airbus A320232 · Fuselage Floor PanelSDR AWXA200401104Floor Panel · delaminatedDURING BC-4 CHECK, AFT CARGO COMPARTMENT FLOOR PANEL 151LF WAS FOUND DISBONDED BETWEEN FS 56 AND FS 58. MAINTENANCE REMOVED FLOOR PANEL 151LF; CUTOUT DISBOND AREA; PERFORMED EDGE FILLING PROCEDURE (DOUBLER) IAW A320 SRM 53-02-00, FIG 209.Sep 25, 2004 · N658AW · Airbus A320232 · Fuselage Floor PanelSDR AWXA200401099Floor Support · corrodedDURING BC-4 CHECK GALVANIC CORROSION WAS FOUND ON LONGITUDINAL FLOORBEAM Y1292 LT BETWEEN FR 66 AND FR 67, LT AFT GALLEY AREA. MAINTENANCE REMOVED CORRODED FLOORBEAM Y1292 LT FROM FS 66 TO FS 67; INSTALLED NEW REPLACEMENT FLOORBEAM IAW A320 SRM 51-72-11.Sep 25, 2004 · N658AW · Airbus A320232 · Fuselage Miscellaneous StructureSDR AWXA200401098Floor Support · corrodedDURING BC-4 CHECK, GALVANIC CORROSION WAS FOUND ON FLOOR SUPPORT Y254 LT AT FR 16. MAINTENANCE REMOVED CORRODED FLOOR SUPPORT Y254 LT AT FS 16; FABRICATED A NEW REPLACEMENT FLOOR SUPPORT PER DWG D53112816; INSTALLED REPAIR PART IAW A320 SRM 51-42-11.Sep 25, 2004 · N658AW · Airbus A320232 · Fuselage Miscellaneous StructureSDR AWXA200401100Fitting · crackedDURING BC-4 CHECK, A 2 INCH CRACK WAS FOUND ON SUPPORT FITTING AT AFT FACE OF PRESSURE BULKHEAD STR 32 LT, FS 35. MAINTENANCE REMOVED CRACKED SUPPORT FITTING AT AFT FACE OF PRESSURE BULKHEAD STR 32 LEFT, FS 35; FABRICATED A NEW REPLACEMENT FITTING PER DWG D53Sep 24, 2004 · N658AW · Airbus A320232 · Fuselage Main, BulkheadSDR AWXA200300872Thermostat · defectiveAFTER TAKEOFF RECEIVED NR 1 & NR 2 ENGINE BLEED CLASS MESSAGES. BOTH BLEED VALVES CLOSED & TEMP AT 320 C, CYCLED SWITCHES WITH NO SUCCESS. TURNED APU BLEED ON & BOTH ENG BLEEDS RETURNED TO NORMAL. RETURNED BOTH ENG BLEEDS TO SERVICE & 2 MIN LATER BOTH ENG BLAug 3, 2003 · N658AW · Airbus A320232 · Bleed Air Indicating SystemSDR AWXA200300801Selector Valve · bypassingEN ROUTE, CREW OBSERVED A GREEN HYD SYS OVERHEAT MESSAGE ON ECAM & PROCEEDED WITH ECAM ACTIONS. FLT RETURNED TO PHX WHERE MX PERFORMED A GREEN HYD SYS INTERNAL LEAKAGE TEST IAW TSM 29-00-00-280-001. MAINT DISCOVERED MLG SELECTOR VALVE BYPASSING HEAVILY & PROCJul 13, 2003 · N658AW · Airbus A320232 · Hydraulic Indicating SystemSDR AWXA200300777Pump · faultyPHX - EMERGENCY LANDING - FLT 0614 - AFTER TAKEOFF PHX EN ROUTE FOR ATL, PILOT REPORTED THAT A GREEN RESERVOIR OVERHEAT ECAM MESSAGE APPEARED. PILOT FOLLOWED ECAM DIRECTIONS, HOWEVER WAS UNABLE TO RESTORE GREEN SYSTEM PRESSURE. MAINTENANCE REMOVED AND REPLACEDJul 5, 2003 · N658AW · Airbus A320232 · Hydraulic Pump (Electric/Engine), MainSDR AWXA200300272Power Supply · dischargedCMH - EEL - DURING COCKPIT/CABIN GENERAL CHECK THE EMERGENCY LIGHTS FAILED TEST. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY POWER SUPPLY UNIT (11WL) AT L/H OVER WING EXIT LOWER SIDEWALL IAW AMM 33-51-38, OPERATIONAL CHECK WAS GOOD.Mar 16, 2003 · N658AW · Airbus A320232 · Emergency LightingSDR AWXA0001693O-Ring · damagedSJC - EMERGENCY LANDING - 4/27/01 - FLT 285 - EN ROUTE FROM PHX TO SJC THE CREW REC''D AN ECAM MSG HYD Y RSVR LO LVL FOLLOWED BY HYD Y ENG 2 PUMP LO PR. PERFORMED ECAM ACTIONS AND CONTINUED TO LANDING IN SJC. IN SJC MAINTENANCE FOUND THE CENTER FITTING ON AUMay 3, 2001 · N658AW · Airbus A319132 · Hydraulic System, MainSDR AWXA0000868Skin · lightning strikeLIGHTNING STRIKE LT SIDE OF FUSELAGE FRAME NR 3, 10 BELOW LAP LINE. REPAIRED AS PER AWA ER 26-5331-00317-DL1.Nov 14, 2000 · N658AW · Airbus A319132 · Fuselage Main, Plate/SkinSDR AWXA0000867Skin · lightning strikeLIGHTNING STRIKE LT SIDE FRAME NR 2 AT LAP SEAM. REPAIRED AS PER AWA ER NR 26-5331-00317-DL1.Nov 14, 2000 · N658AW · Airbus A319132 · Fuselage Main, Plate/SkinSDR AWXA0000866Skin · lightning strikeLIGHTENING STRIKE DAMAGE B/T FRAMES NR 2 AND NR 3. REPAIRED AS PER AWA ER 26-5331-00317.Nov 14, 2000 · N658AW · Airbus A319132 · Fuselage Main, Plate/SkinSDR AWXA0000014Transducer · malfunctionedAIR TURNBACK FLIGHT CONTROL FAULTS, REF LP 7584603, NR 2 ELAC PITCH FAULT WHILE CLIMBING THROUGH 18,000 FT. REMOVED AND REPLACED COMMAND AND MONITOR UNIT TRANSDUCERS. ALSO, EXTENSIVELY TROUBLESHOT WIRING PER TECH SUPPORT ALERT. AIRCRAFT HAS REPETITVE ELAC 2Jan 18, 2000 · N658AW · Airbus A319132 · Autopilot SystemSDR AWXA9900434Transducer · failedAMBER FLT CONT ELAC 2 PITCH FAULT MSG ON UPPER ECAM. REPLACED TRIMMABLE HORIZONTAL STABILIZER TRANSDUCER, OPS CK GOOD. CURRENT HISTORY: 27 NOV A/C WAS WRITTEN FOR PITCH FAULT WITH NO FAULT FOUND. REPLACED ELAC2, TEST GOOD. RECOMMENDATION: REMAIN OPEN PENov 28, 1999 · N658AW · Airbus A319132 · Autopilot System
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