N806AW

Service difficulty reports · 248

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 = 'N806AW' 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 SA08017Indication Sys · malfunctionedPIT - FLT 257 - PHL TO PHX - DURING CRUISE, FLIGHT EXPERIENCED A HIGH, NUMBER TWO ENGINE VIBRATION INDICATION PROBLEM. AIRFRAME VIBRATION WAS NOT DETECTED OR INDICATED. THE CREW REDUCED POWER ON THE NUMBER TWO ENGINE TO IDLE. SINCE AIRSPEED AND ALTITUDE COUMar 22, 2008 · N806AW · Airbus A319132 · Engine Vibration AnalyzerSDR AWXA200700986Control Unit · failedPHX - OTH - LOG NR 4151512 - MX REPORTED SMOKE LAV AND CRG DET FAULT ON ECAM. MX REPLACED THE SMOKE DETECTION UNIT. OPERATIONAL CHECK WAS GOOD.Aug 10, 2007 · N806AW · Airbus A319132 · Smoke DetectionSDR AWXA200700900Spar · corrodedSAL - MAJOR REPAIR - BC-6 CHECK - NR 5964268, 5964269, 5964270, AND 5964344, CORROSION FOUND ON LT WING REAR INNER SPAR, RIB 2 - RIB 5, AREA ON HOLE 52, 53 AND 54 OF MAIN LANDING GEAR ANCHORAGE FITTING. CORROSION REMOVED ON LT WING REAR INNER SPAR, RIB 2 - RIJul 23, 2007 · N806AW · Airbus A319132 · Wing SparSDR AWXA200700899Fitting · corrodedSAL - MAJOR REPAIR- BC-6 CHECK - NR 5964268, 5964269, 5964270 AND 5964344, CORROSION FOUND ON HOLE 52, 53, AND 54 OF LT MAIN LANDING GEAR ANCHORAGE FITTING ON LT WING INNER REAR SPAR BETWEEN RIB 2 TO RIB 5. CORROSION REMOVED FROM HOLE 52, 53, AND 54 OF LT MAJul 23, 2007 · N806AW · Airbus A319132 · Wing, Attach FittingsSDR AWXA200700871Sill · corrodedSAL - MAJOR REPAIR - BC-6 CHECK - NR 5971972, CORROSION ON R2 DOOR CUT OUT LOWER SILL, BS 2838 / FR 67 + 19.5", -Y1265. REPAIRED R2 DOOR CUT OUT LOWER SILL, BS 2838/FR 67 + 19.5", -Y1265 IAW A319 SRM 53-41-14.Jul 19, 2007 · N806AW · Airbus A319132 · Fuselage Miscellaneous StructureSDR AWXA200700875Sill · corrodedSAL - MAJOR REPAIR - BC-6 CHECK - NR 5972146, CORROSION ON AFT CARGO COMPARTMENT DOOR CUT OUT LOWER SILL PLATE, BS 2350/FR 58 + 5", -Y705. REPLACED AFT CARGO COMPARTMENT DOOR CUT OUT LOWER SILL PLATE, BS 2350/FR 58 + 5", -Y705 IAW A319 SRM 51-72-11.Jul 13, 2007 · N806AW · Airbus A319132 · Fuselage Miscellaneous StructureSDR AWXA200700874Seat Track · corrodedSAL - MAJOR REPAIR - BC-6 CHECK - NR 5971953, CORROSION ON CABIN SEAT TRACK, +Y1292, BS 1650/FR 41 TO BS 1976/FR 47. REPLACED CABIN SEAT TRACK, +Y1292, BS 1650/FR 41 TO BS 1976/FR 47 IAW A319 SRM 51-72-11.Jul 13, 2007 · N806AW · Airbus A319132 · Fuselage, Seat/Cargo Attach FittingsSDR AWXA200700873Seat Track · corrodedSAL - MAJOR REPAIR - BC-6 CHECK - NR 5971952, CORROSION ON CABIN SEAT TRACK, +Y1292, BS 1430/FR 36 TO BS 1650/FR 41. REPLACED CABIN SEAT TRACK, +Y1292, BS 1430/FR 36 TO BS 1650/ FR 41 I/A/W A319 SRM 51-72-11.Jul 13, 2007 · N806AW · Airbus A319132 · Fuselage, Seat/Cargo Attach FittingsSDR AWXA200700902Skin · crackedSAL - MAJOR REPAIR - BC - 6 CHECK, NR 5963167, CRACK ON LT ELEVATOR EXTERNAL UPPER SKIN LOCATED BETWEEN HORIZONTAL STABLIZER RIB 4 TO RIB 5, AT 14" FROM UPPER EDGE AND 23" FROM INBOARD EDGE. CRACK WAS REPAIRED AT AT LT ELEVATOR EXTERNAL UPPER SKIN LOCATED BJul 12, 2007 · N806AW · Airbus A319132 · Elevator, Plate/SkinSDR AWXA200700885Hinge Fitting · wornSAL - MAJOR REPAIR - BC-6 CHECK - NR 5964298, NR 5 RUDDER HINGE BEARING HAS EXCESSIVE PLAY, VERTICAL STABILIZER STATION 2985/RIB 7. REPLACED NR 5 RUDDER HINGE FITTING, VERTICAL STABILIZER STATION 2985/RIB 7 IAW A319 AM 55-36-41.Jul 11, 2007 · N806AW · Airbus A319132 · Rudder/Tab, Attach FittingsSDR AWXA200700884Hinge Fitting · wornSAL - MAJOR REPAIR - BC-6 CHECK - NR 5964249, NR 4 RUDDER HINGE BEARING HAS EXCESSIVE PLAY, VERTICLE STABILZER STATION 2632/RIB 6. REPLACED NR 4 RUDDER HINGE FITTING, VERTICLE STABILZER STATION 2632/RIB 6 IAW A319 AMM 55-36-41.Jul 11, 2007 · N806AW · Airbus A319132 · Rudder/Tab, Attach FittingsSDR AWXA200700883Hinge Fitting · wornSAL - MAJOR REPAIR - BC-6 CHECK - NR 5964295, NR 3 RUDDER HINGE BEARING HAS EXCESSIVE PLAY, VERTICLE STABILZER STATION 2279/RIB 5. REPLACED NR 3 RUDDER HINGE FITTING, VERTICLE STABILZER STATION 2279/RIB 5 IAW A319 AMM 55-36-41.Jul 11, 2007 · N806AW · Airbus A319132 · Rudder/Tab, Attach FittingsSDR AWXA200700882Hinge Fitting · wornSAL - MAJOR REPAIR - BC-6 CHECK - NR 5964296, NR 2 RUDDER HINGE BEARING HAS EXCESSIVE PLAY, VERTICLE STABILZER STATION 1926/RIB 4. REPLACED NR 2 RUDDER HINGE FITTING, VERTICLE STABILZER STATION 1926/RIB 4 IAW A319 AMM 55-36-41.Jul 11, 2007 · N806AW · Airbus A319132 · Rudder/Tab, Attach FittingsSDR AWXA200700881Hinge Fitting · wornSAL - MAJOR REPAIR - BC-6 CHECK - NR 5964297, NR 1 RUDDER HINGE BEARING HAS EXCESSIVE PLAY, VERTICLE STABILZER STATION 780/RIB 2. REPLACED NR 1 RUDDER HINGE FITTING, VERTICLE STABILZER STATION 780/RIB 2 IAW A319 AMM 55-36-41.Jul 11, 2007 · N806AW · Airbus A319132 · Rudder/Tab, Attach FittingsSDR AWXA200700834Seat Track · corrodedSAL - MAJOR REPAIR - BC-6 CHECK - NR 5964132, CORROSION ON CABIN SEAT TRACK, -Y765, BS 1323 / FR 34. REPAIRED CABIN SEAT TRACK, -Y765, BS 1323/FR 34 IAW A319 SRM 53-00-15.Jul 11, 2007 · N806AW · Airbus A319132 · Fuselage, Seat/Cargo Attach FittingsSDR AWXA200700833Sill · corrodedSAL - MAJOR REPAIR - BC-6 CHECK - NR 5964045, CORROSION ON L2 DOOR CUT OUT LOWER SILL, +Y1265, FR 67 + 18.5"/ BS 2835. REPAIRED L2 DOOR CUT OUT LOWER SILL, +Y1265, FR. 67 + 18.5"/ BS 2835 IAW A319 SRM 53-41-14.Jul 11, 2007 · N806AW · Airbus A319132 · Fuselage Miscellaneous StructureSDR AWXA200700838Cover · crackedSAL - MAJOR REPAIR - BC-6 CHECK - NR 5962429, CRACKED CABIN FLOOR COVER SHEET, BS 2884 / FR68, +Y1235. REPLACED CABIN FLOOR COVER SHEET, BS 2884 / FR68, +Y1235. I/A/W A319 SRM 51-72-11.Jul 10, 2007 · N806AW · Airbus A319132 · Fuselage Miscellaneous StructureSDR AWXA200700837Floor Panel · corrodedSAL - MAJOR REPAIR - BC-6 CHECK - NR 5963182, CORROSION ON CABIN FLOOR PANEL 261FF, BS 2786 - BS 2884/FR 66 - FR68, +Y1292 TO +Y1732. REPLACED CABIN FLOOR PANEL 261FF, BS 2786 - BS 2884 / FR 66 - FR68, +Y1292 TO +Y1732 IAW A319 SRM 51-72-11.Jul 10, 2007 · N806AW · Airbus A319132 · Fuselage Floor PanelSDR AWXA200700836Floor Panel · corrodedSAL - MAJOR REPAIR - BC-6 CHECK - NR 5963181, CORROSION ON CABIN FLOOR PANEL 262FF, BS 2786 - BS 2884/FR 66 - FR68, -Y1292 TO -Y1732. REPLACED CABIN FLOOR PANEL 262FF, BS 2786 - BS 2884 / FR 66 - FR68, -Y1292 TO -Y1732 IAW A319 SRM 51-72-11.Jul 10, 2007 · N806AW · Airbus A319132 · Fuselage Floor PanelSDR AWXA200700901Wire Harness · damagedSAL - EEL - BC-6 CHECK - NR 5971751, DURING OPERATIONAL TEST OF EMERGENCY LIGHTS THE FOLLOWING MESSAGE WAS FOUND "ESPU EXT LOAD EMER L" "EPSU COMM FWD L"ON PTP PANEL. REPLACED AND OPERATIONAL CHECKED WIRE HARNESS AT SEAT 1A IAW A319 AMM 33-51-19 AND 33-51-00.Jul 7, 2007 · N806AW · Airbus A319132 · Light System WiringSDR AWXA200700878Floor Panel · corrodedSAL - MAJOR REPAIR - BC-6 CHECK - NR 5972035, CORROSION ON FLOOR PANEL 221FF, BS 709/FR 16 - BS 808/FR 20, +Y1292 TO +Y1732. REPLACED FLOOR PANEL 221FF, BS 709/FR 16 - BS 808/FR 20, +Y1292 TO +Y1732 IAW AWA TASK CARD C1C53302.Jul 7, 2007 · N806AW · Airbus A319132 · Fuselage Floor PanelSDR AWXA200700877Floor Panel · corrodedSAL - MAJOR REPAIR - BC-6 CHECK - NR 5972146, CORROSION ON FLOOR PANEL 222FF, BS 709/FR 16 - BS 808/FR 20, -Y1292 TO -Y1732. REPLACED FLOOR PANEL 222FF, BS 709/FR 16 - BS 808/FR 20, -Y1292 TO -Y1732 IAW AWA TASK CARD C1C53302.Jul 7, 2007 · N806AW · Airbus A319132 · Fuselage Floor PanelSDR AWXA200700825Floorbeam · corrodedSAL - MAJOR REPAIR - BC-6 CHECK - CORROSION ON CABIN FLOORBEAM, FR 66/BS 2786 - FR 68 / 2884, -Y1165. REPLACED CABIN FLOORBEAM, FR 66/BS 2786 - FR 68/2884, -Y1165 IAW A319 SRM 51-72-11.Jul 7, 2007 · N806AW · Airbus A319132 · Fuselage Main, Floor BeamSDR AWXA200700824Seat Track · corrodedSAL - MAJOR REPAIR - BC-6 CHECK - NR 5971950, CORROSION ON CABIN SEAT TRACK, FR 36/BS 1430 - FR 41/1650, +Y765. REPLACED CABIN SEAT TRACK, FR 36/BS 1430 - FR 41/1650, +Y765 IAW A319 SRM 51-72-11.Jul 7, 2007 · N806AW · Airbus A319132 · Fuselage, Seat/Cargo Attach FittingsSDR AWXA200700823Sill · corrodedSAL - MAJOR REPAIR - BC-6 CHECK - NR 5971971, CORROSION ON THE L2 DOOR CUT OUT LOWER SILL, FR 67 + 18.5"/BS 2835, +Y1265. REPAIRED THE L2 DOOR CUT OUT LOWER SILL, FR 67 + 18.5"/BS 2835, +Y1265 IAW A319 SRM 53-41-14.Jul 7, 2007 · N806AW · Airbus A319132 · Fuselage Miscellaneous StructureSDR AWXA200700682Hose · leakingLAX - CREW REPORTED LOW GRN HYD PRESS, FOLLOWED BY PTU, LOW LVL. CREW DECLARED AN EMERGENCY DUE TO LOSS OF NOSE WHEEL STEERING. THE LANDING WAS UNEVENTFUL AND THE A/C WAS TOWED TO THE GATE. MX FOUND THE RIGHT GEAR DOOR ACT HOSE ASSY LEAKING. MX REPLACED HOMay 15, 2007 · N806AW · Airbus A319132 · Landing Gear ActuatorSDR AWXA200501329Battery · failedLAX - EEL - DURING OVERNIGHT INSPECTION OPERATIONAL TEST OF EMERGENCY LIGHTS FAILING TEST. MAINTENANCE REMOVED AND REPLACED THE L1 POWER SUPPLY BATTERY PACK. OPERATIONAL TESTS WERE GOOD.Nov 2, 2005 · N806AW · Airbus A319132 · Emergency LightingSDR AWXA200500953Odor · detectedPHX - BURNING SMELL - FLT 0880 - DURING FLIGHT, FLIGHT ATTENDANT REPORTED ODOR COMING FROM THE AFT END OF THE AIRCRAFT THAT SMELLED LIKE NAIL POLISH REMOVER, HER EYES WERE BURNING. CREW TURNED OFF RT PACK AND PLACED PACK FLOW TO HIGH POSITION. SMELL DISSIPATAug 13, 2005 · N806AW · Airbus A319132 · Air Distribution SystemSDR AWXA200400781Beam · corrodedMCN - MAJOR REPAIR - DURING B-04 CHECK EXFOLIATION CORROSION WAS FOUND ON BEAM Y1292 RIGHT BETWEEN FR 66 AND FR 67. MAINTENANCE REMOVED CORRODED BEAM Y1292 RIGHT FROM FR 66 TO FR 67, FABRICATED A NEW REPLACEMENT BEAM PER DWG D534-72172; INSTALLED REPAIR PART Jul 10, 2004 · N806AW · Airbus A319132 · Fuselage Main, StructureSDR AWXA200400780Beam · corrodedMCN - MAJOR REPAIR - DURING B-04 CHECK EXFOLIATION CORROSION WAS FOUND ON BEAM Y1292 RIGHT AT FR 68. MAINTENANCE REMOVED CORRODED BEAM Y1292 RIGHT AT FR 68, INSTALLED NEW REPLACEMENT BEAM IAW A319 SRM 51-42-11 FIG 12 & 18.Jul 10, 2004 · N806AW · Airbus A319132 · Fuselage Main, StructureSDR AWXA200400779Beam · corrodedMCN - MAJOR REPAIR - DURING B-04 CHECK EXFOLIATION CORROSION WAS FOUND ON BEAM Y1292 RIGHT AT FR 66. MAINTENANCE REMOVED CORRODED BEAM Y1292 RT AT FR 66; FABRICATED A NEW REPLACEMENT BEAM; INSTALLED REPAIR PART IAW A319 SRM 51-42-11 PG 1-2.Jul 10, 2004 · N806AW · Airbus A319132 · Fuselage Main, StructureSDR AWXA200400775Shear Plate · corrodedDURING B-04 CHECK EXFOLIATION CORROSION WAS FOUND ON LT AFT SHEAR PLATE AT AFT END OF BEAM Y1292, BETWEEN FR 69 AND FR 70. MAINTENANCE REMOVED CORRODED LT AFT SHEAR PLATE AT AFT END OF BEAM Y1292, FROM FR 69 TO FR 70; FABRICATED A NEW REPLACEMENT SHEAR PLATE;Jul 10, 2004 · N806AW · Airbus A319132 · Fuselage Miscellaneous StructureSDR AWXA200400774Splice Plate · corrodedDURING B-04 CHECK EXFOLIATION CORROSION WAS FOUND ON UPPER IB SPLICE PLATE (COUPLING) BEAM Y1292 LT AT FR 68. MAINTENANCE REMOVED CORRODED UPPER IB SPLICE PLATE ON BEAM Y1292 LT AT FR 68. FABRICATED A NEW REPLACEMENT SPLICE PLATE; INSTALLED REPAIR PART IAW SJul 10, 2004 · N806AW · Airbus A319132 · Fuselage Miscellaneous StructureSDR AWXA200400773Floorbeam · corrodedDURING B-04 CHECK EXFOLIATION CORROSION WAS FOUND ON BEAM Y1292 LT BETWEEN FR 67 AND FR 68. MAINTENANCE REMOVED CORRODED SECTION OF BEAM Y1292 LT FROM FR 67 TO FR 68. FABRICATED A NEW REPLACEMENT SECTION OF BEAM; INSTALLED REPAIR PART IAW SRM 51-72-11, PG. 1-Jul 10, 2004 · N806AW · Airbus A319132 · Fuselage Main, Floor BeamSDR AWXA200400771Seat Track · corrodedDURING B-04 CHECK EXFOLIATION CORROSION WAS FOUND ON SEAT TRACK BEAM Y765, AT FR 66. MAINTENANCE REMOVED CORRODED SECTION OF SEAT TRACK BEAM Y765 FROM FR 64 TO FR 66; FABRICATED A NEW REPLACEMENT SECTION OF BEAM; INSTALLED REPAIR PART IAW SRM 51-72-11, PG. 1-2Jul 10, 2004 · N806AW · Airbus A319132 · Fuselage, Seat/Cargo Attach FittingsSDR AWXA200400770Seat Track · corrodedDURING B-04 CHECK EXFOLIATION CORROSION WAS FOUND ON SEAT TRACK BEAM Y765, AT FR 16. MAINTENANCE CUTOUT DAMAGE ON SEAT TRACK BEAM Y765, AT FR 16; FABRICATED A NEW REPLACEMENT SECTION OF BEAM AND 4 EACH REPAIR ANGLES; INSTALLED REPAIR PARTS IAW A319 SRM 53-11-1Jul 10, 2004 · N806AW · Airbus A319132 · Fuselage, Seat/Cargo Attach FittingsSDR AWXA200400769Shear Plate · corrodedDURING B-04 CHECK EXFOLIATION CORROSION WAS FOUND ON RT AFT SHEAR PLATE AT AFT END OF BEAM Y1292, BETWEEN FR 69 AND FR 70. MAINTENANCE REMOVED CORRODED RT AFT SHEAR PLATE AT AFT END OF BEAM Y1292, FROM FR 69 TO FR 70; FABRICATED A NEW REPLACEMENT SHEAR PLATE;Jul 10, 2004 · N806AW · Airbus A319132 · Fuselage Miscellaneous StructureSDR AWXA200400460Wire · brokenPHX - EEL - DURING INSPECTION FOUND A BROKEN WIRE IN HARNESS FOR EMERGENCY ESCAPE PATH LIGHT AT CONNECTOR 5751VC, SEAT ROW 8 RT. MAINTENANCE REMOVED AND REPLACED EMERGENCY ESCAPE PATH LIGHT WIRE HARNESS AT SEAT ROW 8 RT, OPERATIONAL CHECK WAS GOOD.May 2, 2004 · N806AW · Airbus A319132 · Light System WiringSDR AWXA200300700Warning Horn · activatedON TAKEOFF ROLL AT SNA EN ROUTE FOR LAS AT 70 KTS TAKEOFF CONFIGURATION WARNING SOUNDED, REJECTED TAKEOFF. RECONFIGURED FLAP HANDLE AND TOOK OFF WITHOUT FURTHER EVENT.Jun 15, 2003 · N806AW · Airbus A319132 · Trailing Flap Position Indicating SystemSDR AWXA200300357Wire · brokenDURING INSPECTION MAINTENANCE FOUND THE EMERGENCY ESCAPE PATH LIGHT CONNECTOR BROKEN AT SEAT ROW 18 LT. MAINTENANCE REPAIRED WIRING ON THE EMERGENCY ESCAPE PATH LIGHT CONNECTOR AT SEAT ROW 18 LT.Apr 9, 2003 · N806AW · Airbus A319132 · Light System WiringSDR AWXA200201156Power Supply · dischargedPHX - EEL - DURING EMERGENCY LIGHT TEST THE LT AFT EMERGENCY POWER SUPPLY UNIT FAILED CIDS BITE CHECK. MAINTENANCE REMOVED AND REPLACED THE LT AFT EMERGENCY POWER SUPPLY UNIT (13WL) IAW AMM 33-51-38-401, FUNCTIONAL CHECK WAS GOOD.Dec 1, 2002 · N806AW · Airbus A319132 · Emergency LightingSDR AWXA200200391Apu · leakingPHX - TAILPIPE FIRE - WHEN AUXILIARY POWER UNIT (APU) WAS SHUTDOWN AN APU TAILPIPE FIRE WAS NOTICED FROM THE GROUND. MAINTENANCE REMOVED AND REPLACED THE APU IAW T/C R6D49301, LEAK AND OPERATIONAL CHECK WAS GOOD.May 1, 2002 · N806AW · Airbus A319132 · APU Core EngineSDR AWXA200200128Power Supply · dischargedPHX - EEL - C - DURING INSPECTION OF EMERGENCY LIGHT SYSTEM RT OVERWING EXIT LIGHTS DID NOT ILLUMINATE. MAINTENANCE REPLACED EMERGENCY POWER SUPPLY UNIT 12WL WITH BATTERY PACK IAW AMM 33-51-38-401. OPERATIONAL CHECK WAS GOOD.Feb 13, 2002 · N806AW · Airbus A319132 · Emergency LightingSDR AWXA200200065Connector · defectiveYWG - EEL - "C" - DURING BC-02 CHECK INSPECTION ROWS #4 L/H, #10 L/H & R/H, #14 L/H, #16 L/H EMERGENCY SEAT LIGHTS CONNECTORS WERE FOUND TO REQUIRE REPLACEMENT. MAINTENANCE REPLACED EMERGENCY SEAT LIGHT CONNECTORS AT ROWS #4 L/H, #10 L/H & R/H, #14 L/H, #16 L/Jan 20, 2002 · N806AW · Airbus A319132 · Emergency LightingSDR AWXA0001852Warning Light · illuminatedPHX - AIR TURNBACK - 6/8/01 - FLT 83 - AFTER TAKEOFF THE EQUIPMENT COOLING EXTRACT VALVE LIGHT REMAINED AMBER AND THE AIRCRAFT RETURNED TO PHX. MX PERFORMED A BITE CHECK OF THE AVEC SYSTEM WHICH TESTED OK. CHECKED THE LAST LEG REPORT AND NO FAULTS NOTED. CHJun 12, 2001 · N806AW · Airbus A319132 · Air Distribution SystemSDR AWXA0000716Wire · brokenFLOOR PATH LIGHT AT 10C DOES NOT WORK. RE-TERMINATED E-PATH WIRE AT SEAT DISCONNECT 5751VC, 10 RT.Oct 5, 2000 · N806AW · Airbus A319132 · Light System WiringSDR AWXA0000017Unknown · odorAIR TURNBACK, BURNING ODOR REF LP7621610, AFTER PASSING THROUGH 5,000 FT, FLT ATT ADVISED OF ELECTRICAL BURNING SMELL IN AFT GALLEY. COMPLETED AN EXTENSIVE REGIMEN TO ISOLATE. BORESCOPED NR 2 ENG FOR INTERNAL OIL LEAK, RAN ENGINES TO PERFORM BLEED ISOLATION,Jan 19, 2000 · N806AW · Airbus A319132 · Air Distribution SystemSDR AWXA9900312Air Dist · odorOBNOXIOUS ODOR LIKE WD-40 COMING FROM AC SYSTEM WHEN PACKS 1 AND 2 ARE RUNNING OFF APU AIR. RAN PACKS OFF NR 1 AND NR 2 ENG AND OFF APU BLEED. NO ABNORMAL ODORS IN CABIN.Sep 13, 1999 · N806AW · Airbus A319132 · Air Distribution System
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