N801AW

Service difficulty reports · 297

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 = 'N801AW' 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 AWXA200601548Floor Panel · corrodedSAL - CORROSION ON FLOORBOARD NR 222 FF, ON R1 THRESHOLD AREA BETWEEN FR 76 TO FR 20. REPLACED FLOORBOARD 222 FF BETWEEN FS 16 TO FS 20, AND -Y1292 TO -Y1354.Aug 25, 2006 · N801AW · Airbus A319132 · Fuselage Floor PanelSDR AWXA200601547Floor Panel · corrodedSAL - CORROSION ON FLOOR BOARD AT THRESHOLD OF R2 DOORWAY BETWEEN FS 66 TO FS 68. REPLACED FLOOR PANEL AT R2 THRESHOLD BETWEEN FS 66 TO FS 68 AND -Y1164 TO -Y1192.Aug 25, 2006 · N801AW · Airbus A319132 · Fuselage Floor PanelSDR AWXA200601565Sill · corrodedSAL - FOUND CORROSION ON SILL OF L2 DOOR AT FS 67 + 19". CORROSION ON SILL OF L2 DOOR AT FS 67 + 19", WAS REPAIRED PER SRM A319 53-41-14, PAGES 211-212, FIG 201, SHEET 3.Aug 23, 2006 · N801AW · Airbus A319132 · Fuselage Miscellaneous StructureSDR AWXA200601551Fitting · corrodedSAL - FOUND CORROSION ON CENTRAL FITTING OF SILL L2 DOOR BETWEEN FS 66 + 5" TO FS 68 - 4". FITTING OF SILL L2 DOOR BETWEEN FS 66 + 5" TO FS 68 - 4" WAS REPLACED IAW A319 SRM 51-72-11, PAGE 1 - 2 AND DWG D53480048.Aug 23, 2006 · N801AW · Airbus A319132 · Fuselage Miscellaneous StructureSDR AWXA200601549Floorbeam · corrodedSAL - FOUND CORROSION ON LONGITUDINAL BEAM -Y1162, AND FS 68 - 1". REPLACED LONGITUDINAL BEAM LOCATED FROM FS 68 - 3" TO FS 69 + 2", -Y1162 IAW SRM 51-72-11, AND PER A319 SRM 51-42-11, PARA 6-7, PAGE 10 TO 28.Aug 23, 2006 · N801AW · Airbus A319132 · Fuselage Main, Floor BeamSDR AWXA200601546Sill · corrodedSAL - FOUND CORROSION ON AFT CARGO FLOOR STRUCTURE AT FS 58 + 4", +Y28. RELACED PLATE DOORSILL ON AFT CARGO FLOOR STRUCTURE AT FS 58 TO FS 59, +Y28 IAW A319 SRM 51-72-11, PAGE 1-2.Aug 23, 2006 · N801AW · Airbus A319132 · Fuselage Miscellaneous StructureSDR AWXA200601545Seat Track · corrodedSAL - FOUND CORROSION ON LONGITUDINAL BEAM -Y1292, AT FS 20. REPAIRED SEAT TRACK LOCATED BETWEEN FS 19 TO FS 24, -Y1292 IAW A319 SRM 53-11-15, PAGE 206, 211/212, FIG 16.Aug 23, 2006 · N801AW · Airbus A319132 · Fuselage, Seat/Cargo Attach FittingsSDR AWXA200601566Sill · corrodedSAL - FOUND CORROSION ON SILL OF R2 DOORWAY AT FS 67 + 19". CORROSION ON SILL OF R2 DOORWAY AT FS 67 + 19" WAS REWORKED, IAW A319 SRM 51-74-00, AND FOUND OUT OF LIMITS IAW A319 SRM 53-41-14. REPAIRED AREA IAW A319 SRM 53-41-14, REPAIR IS FROM 67 + 12" TO FS Aug 22, 2006 · N801AW · Airbus A319132 · Fuselage Miscellaneous StructureSDR AWXA200601553Floorbeam · corrodedSAL - FOUND CORROSION ON LONGITUDINAL BEAM, +Y1292 ALONG FS 66 TO FS 68. REPLACED LONGITUDINAL BEAM LOCATED FROM FS 66 TO FS 68, +Y1292 IAW A319 SRM 51-72-11, PAGE 1 - 2, AND A319 SRM 51-42-11, PAR 6 AND 7.Aug 22, 2006 · N801AW · Airbus A319132 · Fuselage Main, Floor BeamSDR AWXA200601552Fitting · corrodedSAL - FOUND CORROSION AROUND HOLES OF CENTRAL FITTING OF SILL L1 DOOR, BETWEEN FS 16 + 5" TO FS 20 - 4". CENTRAL FITTING ON SILL L1 DOOR BETWEEN FS 16 + 5" TO FS 20 - 4" WAS REPLACED IAW A319 SRM 51-42-11.Aug 21, 2006 · N801AW · Airbus A319132 · Fuselage Miscellaneous StructureSDR AWXA200601550Seat Track · corrodedSAL - CORROSION ON SEAT TRACK LOCATED AT FS 47/51 + 6", FS 52 + 15", FS 57 + 4", +Y765, LT INBD PASSENGER CABIN (3 POINTS). PERFORMED PERMANENT REPAIR ON SEAT TRACK LOCATED AT FS 47/51 + 6", +Y765, LT INBD PASSENGER CABIN IAW A319 SRM 53-00-15, PAGE 207 TO PAAug 21, 2006 · N801AW · Airbus A319132 · Fuselage, Seat/Cargo Attach FittingsSDR AWXA200601523Seat Track · corrodedSAL - FOUND CORROSION ON SEAT TRACK LOCATED FROM FS 36 TO FS 41, -Y1292, RT OUTBOARD, PASSENGER CABIN (2 POINTS). REPLACED SEAT TRACK LOCATED FROM FS 36 TO FS 41, -Y1292, RT OUTBOARD, PASSENGER CABIN, IAW A319 SRM 51-72-11, PAGE 1.Jul 18, 2006 · N801AW · Airbus A319132 · Fuselage, Seat/Cargo Attach FittingsSDR AWXA200600889Windshield · bird strikeSIT - UNSCHEDULED LANDING - FLT 142 - LG 7271483 - AT FL350, GOOSE IMPACTED CAPTAIN'S WINDSHEILD SHATTERING OUTER PANE. FLIGHT DESCENDED TO 9000 FT AND DIVERTED TO SIT. MAINTENANCE REMOVED AND REPLACED THE CAPTAIN'S WINDSHIELD PER AMM 56-11-11, AND AS A PRECJun 2, 2006 · N801AW · Airbus A319132 · Flight Compartment WindowsSDR AWXA200600253Skin · damagedPHX - DISCOVERED THE RT OUTBOARD FLAP ASSEMBLY, TRAILING EDGE SEPARATING. DAMAGED COMPOSITE HONEYCOMB 7" BY 9". MAINTENANCE REMOVED TOP SKIN AND CORE. ADDITIONAL CORROSION WAS FOUND UNDER UPPER SKIN. REMOVED CORRODED CORE, FINAL DIMENSION OF REMOVED SECTIOSep 27, 2005 · N801AW · Airbus A319132 · Trailing Edge FlapsSDR AWXA200400843Adiru · faultyAIR TURN BACK, ON CLIMB OUT, EN ROUTE FOR YYZ AT APPROXIMATELY 4000 FT THE FO`S PRIMARY FLIGHT DISPLAY (PFD) SPEED TAPE INDICATED OVER SPEED. REDUCED SPEED TO 235 KTS AND WARNING EXTINGUISHED, AUTOPILOT DISCONNECTED, CAPTAINS PFD WAS NORMAL, TURNED BACK AND LAAug 2, 2004 · N801AW · Airbus A319132 · Inertial Guidance SystemSDR AWXA200400342Scavenge Pump · leakingBUR - TAILPIPE FIRE - FLT 0476 - NR 1 ENGINE HAD TAILPIPE FIRE AT ENGINE SHUTDOWN AFTER 5 MIN COOL DOWN. MAINTENANCE REMOVED AND REPLACED NR 1 ENGINE OIL SCAVENGE PUMP IAW T/C R5M79301. RAN ENGINE AT IDLE, NO TAILPIPE FIRE AT SHUTDOWN, LEAK CHECK OF PUMP WASApr 2, 2004 · N801AW · Airbus A319132 · Turbine Engine Oil SystemSDR AWXA200400298Servo · failedON CLIMBOUT, RT WING NR 4 SPOILER WAS FLOATING CAUSING A/C TO ROLL LT AND BETA TARGET TO BE OUT TO RT. TURNED BACK AND LANDED WITHOUT FURTHER EVENT. MX PLACED NR 4 SPOILER ON MEL 27-64-01, COND 3, & DEACTIVATED BOTH LT & RT WING NR 4 SPOILERS. R & R RT WINGMar 20, 2004 · N801AW · Airbus A319132 · Drag Control ActuatorSDR AWXA200400178Epsu · dischargedEMERGENCY LIGHT SYSTEM TEST FAILED AT PUSH BUTTON ON FLIGHT ATTENDANT FORWARD PANEL. MAINTENANCE REMOVED AND REPLACED FORWARD EMERGENCY POWER SUPPLY UNIT (11WL), OPERATIONAL CHECK WAS GOOD.Feb 14, 2004 · N801AW · Airbus A319132 · Emergency LightingSDR AWXA200300836Connector · damagedMCN - EEL - DURING C-04 CHECK THE EMERGENCY ESCAPE PATH LIGHT CONNECTOR AT SEAT ROW 12 LT WAS FOUND DAMAGED. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY ESCAPE PATH LIGHT CONNECTOR AT SEAT ROW 12 LT IAW ESPM 20-48-21, PG 12-16, OPERATIONAL CHECK WAS GOOD.Jul 13, 2003 · N801AW · Airbus A319132 · Emergency LightingSDR AWXA200300835Floorbeam · corrodedMCN - MAJOR REPAIR - DURING C-04 CHECK EXFOLIATION CORROSION WAS FOUND ON UPPER SURFACE OF FLOORBEAM Y1292, BETWEEN FR 16-18. MAINTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS; CUT OUT DAMAGED AREA OF FLOORBEAM Y1292, BETWEEN FR 16-17; Jul 9, 2003 · N801AW · Airbus A319132 · Fuselage Main, Floor BeamSDR AWXA200300833Floorbeam · corrodedMCN - MAJOR REPAIR - DURING C-04 CHECK EXFOLIATION CORROSION WAS FOUND ON UPPER SURFACE OF FLOORBEAM (DUMMY RAIL) Y503, FR 16. MAINTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS; REMOVED FLOORBEAM Y503 FROM FR 12 TO FR 16; FABRICATED A NJul 9, 2003 · N801AW · Airbus A319132 · Fuselage Main, Floor BeamSDR AWXA200300832Floorbeam · corrodedMCN - MAJOR REPAIR - DURING C-04 CHECK CORROSION WAS FOUND ON UPPER SURFACE OF FLOORBEAM Y1292, FR 66. MAINTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS; REMOVED FLOOR BEAM Y1292 FROM FR 64 TO FR 66; FABRICATED A NEW REPLACEMENT SECTIONJul 9, 2003 · N801AW · Airbus A319132 · Fuselage Main, Floor BeamSDR AWXA200300831Floorbeam · corrodedMCN - MAJOR REPAIR - DURING C-04 CHECK EXFOLIATION CORROSION WAS FOUND ON UPPER SURFACE OF FLOORBEAM Y1292, FR 68. MAINTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS; REMOVED FLOORBEAM Y1292 FROM FR 68 TO FR 69; FABRICATED A NEW REPLACEJul 9, 2003 · N801AW · Airbus A319132 · Fuselage Main, Floor BeamSDR AWXA200300824Skin · corrodedDURING C-04 CHECK CORROSION WAS FOUND ON AFT LOWER INNER SKIN OF THE NR 1 PYLON AFT FIXED FAIRING. MAINTENANCE CUT OUT DAMAGED AREA OF NR 1 PYLON AFT FIXED FAIRING SKIN BETWEEN RIBS 11-16A; FABRICATED A NEW REPLACEMENT SECTION OF SKIN; INSTALLED REPAIR PART IJul 9, 2003 · N801AW · Airbus A319132 · Nacelle/Pylon, Plate/SkinSDR AWXA200300822Angle · crackedMCN - MINOR REPAIR - DURING C-04 CHECK .5000 INCH CRACK WAS FOUND ON FUSELAGE RT SIDE ANGLE AT BS 1323, FR 34, STR 32 RT. MAINTENANCE REMOVED RT SIDE ANGLE AT BS 1323, FR 34, STR 32 RT; FABRICATED A NEW REPLACEMENT ANGLE; INSTALLED REPAIR PART IAW A319 SRM 5Jul 9, 2003 · N801AW · Airbus A319132 · Fuselage Miscellaneous StructureSDR AWXA200300820Floorbeam · corrodedDURING C-04 CHECK EXFOLIATION CORROSION WAS FOUND ON UPPER SURFACE OF FLOORBEAM Y1292 AT FR 68. MAINTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS; REMOVED DAMAGED SECTION OF FLOORBEAM 1292 AT FR 68; FABRICATED A NEW REPLACEMENT SECTIONJul 9, 2003 · N801AW · Airbus A319132 · Fuselage Main, Floor BeamSDR AWXA200300819Plate · crackedMCN - MINOR REPAIR - DURING C-04 CHECK .25 INCH CRACK WAS FOUND ON CLOSING PLATE AT LT SIDE PANEL BS 1323, FR 34, STR 32 LT. MAINTENANCE REMOVED AND REPLACED CLOSING PLATE AT LT SIDE PANEL BS 1323, FR 34, STR 32 LT IAW A319 SRM 51-42-11, PG 28-32, FIG 12 AND Jul 9, 2003 · N801AW · Airbus A319132 · Fuselage Miscellaneous StructureSDR AWXA200300818Floorbeam · corrodedMCN - MAJOR REPAIR - DURING C-04 CHECK EXFOLIATION CORROSION WAS FOUND ON FLOORBEAM Y254, FR 20. MAINTENANCE BLENDED OUT CORROSION AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS; REMOVED DAMAGED AREA OF FLOORBEAM Y254 AT FR 20; FABRICATED A REPAIR ANGLE AND FIJul 9, 2003 · N801AW · Airbus A319132 · Fuselage Main, Floor BeamSDR AWXA200300817Plate · corrodedMCN - MAJOR REPAIR - DURING C-04 CHECK EXFOLIATION CORROSION WAS FOUND ON SHEAR PLATE Y1292, BETWEEN FR 69-70. MAINTENANCE BLENDED OUT CORROSION AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS; REMOVED DAMAGED SHEAR PLATE Y1292, BETWEEN FR 69-70; FABRICATED A NEWJul 9, 2003 · N801AW · Airbus A319132 · Fuselage Miscellaneous StructureSDR AWXA200300810Plate · corrodedDURING C-04 CHECK EXFOLIATION CORROSION WAS FOUND ON SHEAR PLATE Y-1292, BETWEEN FR 69 AND FR 70. MAINTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS; REMOVED CORRODED SHEAR PLATE Y-1292, BETWEEN FR 69 AND FR 70; FABRICATED A NEW REPLACEJul 9, 2003 · N801AW · Airbus A319132 · Fuselage Miscellaneous StructureSDR AWXA200300809Floorbeam · corrodedDURING C-04 CHECK EXFOLIATION CORROSION WAS FOUND ON FLOORBEAM Y-1292, BETWEEN FR67 AND FR 68. MAINTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS; REMOVED CORRODED FLOORBEAM Y-1292, BETWEEN FR67 AND FR 68; INSTALLED A NEW REPLACEMENT FLJul 9, 2003 · N801AW · Airbus A319132 · Fuselage Main, Floor BeamSDR AWXA200300821Profile · crackedDURING C-04 CHECK .25 INCH CRACK WAS FOUND ON AFT CARGO COMPARTMENT CEILING PANEL FORWARD PROFILE AT FORWARD END OF FR 51, Y1397. MAINTENANCE CUT OUT DAMAGED SECTION OF PROFILE AT FORWARD END OF FR 51, Y1397; FABRICATED A SPLICE REPAIR AND FILLER; INSTALLED RJul 7, 2003 · N801AW · Airbus A319132 · Fuselage Miscellaneous StructureSDR AWXA200300839Profile · corrodedDURING C-04 CHECK CORROSION WAS FOUND ON UPPER SURFACE OF AFT CARGO COMPARTMENT PROFILE BETWEEN FR-52 AND FR 56, LBL 711.2. MAINTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS; REMOVED DAMAGED SECTION OF AFT CARGO COMPARTMENT PROFILE BETJul 6, 2003 · N801AW · Airbus A319132 · Fuselage Miscellaneous StructureSDR AWXA200300834Profile · corrodedMCN - MAJOR REPAIR - DURING C-04 CHECK EXFOLIATION CORROSION WAS FOUND ON UPPER SURFACE OF AFT CARGO COMPARTMENT PROFILE BETWEEN FR 59-62, RBL 711.2. MAINTENANCE REMOVED CORRODED PROFILE BETWEEN FR 59-62, RBL 711.2; FABRICATED A NEW REPLACEMENT SECTION OF PROFJul 6, 2003 · N801AW · Airbus A319132 · Fuselage Miscellaneous StructureSDR AWXA200300823Profile · corrodedDURING C-04 CHECK CORROSION WAS FOUND ON UPPER SURFACE OF AFT CARGO COMPARTMENT PROFILE BETWEEN FR 54 AND FR 55, RBL 711.2. MAINTENANCE CUT OUT DAMAGED SECTION OF PROFILE BETWEEN FR 54 AND FR 55, RBL 711.2; FABRICATED A REPAIR SPLICE AND NEW SECTION OF PROFILJul 6, 2003 · N801AW · Airbus A319132 · Fuselage Miscellaneous StructureSDR AWXA200300337Power Supply · dischargedPHX - EEL - RT EMERGENCY LIGHTS DO NOT ILLUMINATE WHEN ARMED AND POWER INTERRUPTION OCCURS. MAINTENANCE REMOVED AND REPLACED RT MID CABIN EMERGENCY POWER SUPPLY UNIT (12WL) AND EMERGENCY LIGHT BATTERY PACK, OPERATIONAL CHECK WAS GOOD.Apr 6, 2003 · N801AW · Airbus A319132 · Emergency LightingSDR AWXA200300111Computer · failedLAS - ABORTED TAKEOFF - FLT 0532 - ON TAKEOFF ROLL IN LAS EN ROUTE FOR RNO AT 85 TO 90 KTS BOTH NAV DISPLAYS AND FLIGHT MANAGEMENT GUIDANCE COMPUTERS (FMGC) TIMED OUT, SCREEN NOT DISPLAYING MAPS. REJECTED TAKEOFF AND RETURNED TO GATE. MAINTENANCE RESET FMGC CIFeb 8, 2003 · N801AW · Airbus A319132 · Flight ControllerSDR AWXA200200757Connector · brokenCMH - EEL - DURING INSPECTION THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 4 LT WAS FOUND INOPERATIVE. MAINTENANCE REMOVED AND REPLACED CONNECTOR AT SEAT ROW 4 LT, OPERATIONAL CHECK WAS GOOD.Aug 16, 2002 · N801AW · Airbus A319132 · Emergency LightingSDR AWXA200200705Power Supply · dischargedPHX - EEL - DURING INSPECTION THE EMERGENCY EXIT LIGHTS ABOVE THE L1, R1, AND SEAT ROW 1 WERE FOUND INOPERATIVE. MAINTENANCE REMOVED AND REPLACED EMERGENCY POWER SUPPLY UNIT (10WL) IAW AMM 33-51-04, OPERATIONAL CHECK WAS GOOD.Aug 8, 2002 · N801AW · Airbus A319132 · Emergency LightingSDR AWXA200200696Battery · dischargedPHX - FLIGHT CREW REPORTED EMERGENCY FLASHLIGHT UNDER THE FORWARD FLIGHT ATTENDANT SEAT IS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE FORWARD EMERGENCY FLASHLIGHT BATTERIES, OPERATIONAL CHECK WAS GOOD.Aug 6, 2002 · N801AW · Airbus A319132 · Emergency EquipmentSDR AWXA200200690Power Supply · dischargedPHX - THE L1 DOOR, R1 DOOR, AND SEAT ROW 1 LT EMERGENCY LIGHTS WERE FOUND INOPERATIVE DURING EMERGENCY LIGHTING TEST. MAINTENANCE REMOVED AND REPLACED EMERGENCY POWER SUPPLY UNIT (10WL) AND BATTERY IAW AMM 33-51-38-401, OPERATIONAL CHECK WAS GOOD.Aug 4, 2002 · N801AW · Airbus A319132 · Emergency LightingSDR AWXA200200674Power Supply · dischargedLAS - EEL - DURING INSPECTION THE FORWARD EMERGENCY ESCAPE PATH LIGHTS WERE FOUND INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE FORWARD EMERGENCY POWER SUPPLY UNIT (10WL), OPERATIONAL CHECK WAS GOOD.Jul 28, 2002 · N801AW · Airbus A319132 · Emergency LightingSDR AWXA200200615Audio Panel · malfunctionedCRUISE, A LOUD BANG & FLASH OF LIGHT BEHIND F/O SEAT ON ELECTRICAL PANEL, DEBRIS & SMOKE FOLLOWED. NO INDICATIONS OF PROBLEM ON ECAM, STARTED SMOKE REMOVAL PROCEDURES. DISCONNECTED PWR FROM GALLEY, DID NOT DISCONNECT GENERATOR. SMOKE STOPPED 15 MIN. MX IDEJul 14, 2002 · N801AW · Airbus A319132 · Audio Integrating SystemSDR AWXA0001252Gearbox · out of adjDURING POST MAINTENANCE FLIGHT TEST THE LANDING GEAR WAS EXTENDED USING MANUAL EXTENSION AND THE NOSE GEAR FAILED TO EXTEND, LGCIU 1 & 2 FAULTS WERE PRESENT. THE GEAR WAS RESET AND GEAR WAS EXTENDED HYDRAULICALLY AND ALL GEAR EXTENDED NORMALLY. MAINTENANCE TJan 18, 2001 · N801AW · Airbus A319132 · Landing Gear Retraction/Extension SystemSDR AWXA0000145Servo · malfunctionedAFTER TAKEOFF, LT AILERON HAD UPWARD DEFLECTION WITH NEUTRAL STICK, FLT CONT PAGE AND VISUAL CONFIRMED LT AILERON UP, RT AILERON NEUTRAL, MANUALLY FLEW A/C. COMPLIED WITH CRITICAL ALERT FUP. SECURITY, RIG, AND WIRING CHECKS COMPLETED. NO DEFECTS FOUND. REMar 20, 2000 · N801AW · Airbus A319132 · Aileron Control SystemSDR AWXA9900385Valve · failedCONDITION: AIR TURN-BACK ENGINE BLEED FAULT LP 7559931DISCREPANCY: ENG 2 BLEED FAULT AT 1500 FT AGL AFTER TAKE-OFFCORRECTIVE ACTION: R&R'D ENG 2 BLEED PRESSURE VALVE IAW MM 36 36-11-52-401--LEAK AND OPS GOOD TT 0065680CURRENT HISTORY: BLEED FAULT Oct 27, 1999 · N801AW · Airbus A319132 · Pneumatic Distribution SystemSDR AWXA9900379Engine · damagedAIR TURNBACK, AFTER TAKEOFF 5 MIN & 6000 RT ENG CLASS 1 EGT OVERLIMIT WITH LOUD BANG AND ENG SPOOL DOWN. REPLACED NR 2 ENG IAW R5M71302, 4TH STAGE BLADE DAMAGE.Oct 22, 1999 · N801AW · Airbus A319132 · Engine (Turbine/Turboprop)
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