N405AW

Service difficulty reports · 198

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 = 'N405AW' 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 A6WA200940582Sill · corrodedPASSENGER ENTRY, LOWER SILL CORRODED. LWR SILL REPLACED IAW SRM 51-42-06 AND REO 601R-52-11-577. (K)Sep 10, 2009 · N405AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200940591Crossbeam · crackedFOUR CLIPS CRACKED ON CROSSBEAM FS 280 AT LBL 9 AND RBL 9. FOUR CLIPS REPLACED ON CROSSBEAM FS 280 AT LBL 9 AT RBL 9 IAW SRM 51-42-21 AND SRM 51-42-06. CLIP AT FS 280, RBL 9 OTBD SIDE REPLACED IAW REO 601R-53-11-171, REV D. (K)Sep 9, 2009 · N405AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200940584Access Panel · corrodedCORROSION AROUND SCREW HOLES ON INTERNAL SIDE OF ACCESS PANEL 650KB ON INTERNAL SIDE OF ACCESS PANEL 650KB, CORROSION AROUND SCREW HOLES REMOVED IAW SRM 51-21-06 WITHIN LIMIT IAW SRM 51-21-00. (K)Sep 9, 2009 · N405AW · Cndair CL6002B19 · Wing, Plate/SkinSDR A6WA200940586Angle · crackedPRESSURE BULKHEAD CAP ANGLE IS CRACKED IN THE RADIUS FS 559.00, LBL18, CRACK LENGTH .350" PRESSURE BULKHEAD CAP ANGLE REPAIRED IAW REO 601R-53-41-260, REV C. (K)Sep 8, 2009 · N405AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200940592Floorbeam · crackedFLOORBEAM LWR FLANGE CRACKED AT FS 280, RBL 9, CRACK LENGTH 1.20". REPAIR PERFORMED IAW REO 601R-53-11-171, REV D. ANGLE FILLER FABRICATED IAW REO 601R-53-11-171, REV D. (K)Sep 8, 2009 · N405AW · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR A6WA200940590Access Panel · corrodedCORROSION AT FUEL ACCESS PANEL HSG 640EB IN NON CRITICAL REGION. CORROSION REMOVED IN NON CRITICAL REGION AT FUEL ACCESS PANEL 640EB IAW EO E06/021/457 REV A AND REO 601R-57-21-030. (K)Sep 4, 2009 · N405AW · Cndair CL6002B19 · Wing, Plate/SkinSDR A6WA200940589Access Panel · corrodedCORROSION AT FUEL ACCESS PANEL HSG 550AB IN NON CRITICAL REGION. CORROSION REMOVED IN NON CRITICAL REGION AT FUEL ACCESS PANEL 550AB IAW EOE06/021/457, REV A AND REO 601R-57-21-030, REV 6. (K)Sep 4, 2009 · N405AW · Cndair CL6002B19 · Wing, Plate/SkinSDR A6WA200940588Structure · crackedREPLACEMENT OF FWD UPPER CORNER COVER (PAX DOOR) DUE TO CRACK FOUND DURING INCORPORATION OF EO E07/027/452, REO 601R-52-11-827 AND REO 601R-52-11-159, REV B. FWD UPPER CORNER COVER OF PAX DOOR REPLACED IAW SRM 51-42-13. (K)Sep 4, 2009 · N405AW · Cndair CL6002B19 · Passenger/Crew DoorsSDR A6WA200940580Plate · corrodedCARGO DOOR NET TIE DOWN STRUCTURE (PLATES) (3X) UPPER SURFACE BTWN FS 621 AND FS 574 FOUND CORRODED. CORROSION REMOVED IAW SRM 51-21-06. (K)Sep 4, 2009 · N405AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200940578Rib · corrodedLT WING L/E RIBS AT WS 139.54, WS 149.58, WS 247.95 AND WS 252.87 FRETTING CORROSION FOUND. CORROSION REMOVED ON LT WING, L/E RIBS IAW SRM 51-21-06. (K)Sep 3, 2009 · N405AW · Cndair CL6002B19 · Wing, Rib/BulkheadSDR A6WA200940579Sill · crackedCARGO DOOR FLOOR SILL LANDING PLATE CRACKED AT FS 589.00 RIVET HOLE. GARGO DOOR FLOOR SILL LANDING PLATE REPAIRED AT FS 589.00 RIVET HOLE IAW REO 601R-53-61-433 REV NC. (K)Sep 2, 2009 · N405AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200940289Wire Harness · out of positionON INITIAL CLIMBOUT APPROX 2000 FT "PAX DOOR OUT HANDLE" CAUTION MESSAGE APPEARED. WHILE COMPLYING WITH QRH PAGE 3, PAX DOOR WOAR MESSAGE APPEARED. QRH FOR PAX DOOR MESSAGE, LANDED AT NEAREST SUITABLE AIRPORT. LANDED OVERWEIGHT APPROX 50K LBS. UNABLE TO DUJun 7, 2009 · N405AW · Cndair CL6002B19 · Door System WiringSDR A6WA200940279Angle · crackedMWC 136500-10- CARGO DOOR CAMTRACK CROSSMEMBER, LOWER ANGLE AT AFT BULKHEAD CRACKED. LOWER ANGLE AT CARGO DOOR CAMTRACK CROSSMEMBER FABRICATED IAW SRM 51-24-36 AND INSTALLED IAW SRM 51-42-21. (K)May 17, 2009 · N405AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200940218Line · damagedIN CRUISE, HYD 1 LOW PRESSURE CAUTION MESSAGE. PERFORMED QRH. DIVERTED, ENGINE DRIVEN PUMP RAN APPROX 1 HOUR AND 5 MIN AT 0 PSI, QUANTITY 0. SWEDGED AND REPAIRED DAMAGED NR 1 HYD PRESSURE LINE FOR EXTERNAL HYD POWER IAW AMM 20-22-00. OPS CHECK GOOD AND LEAApr 19, 2009 · N405AW · Cndair CL6002B19 · Hydraulic System, MainSDR A6WA200940207Check Valve · malfunctionedLT PACK HI TEMP AFTER EXITING RUNWAY ALL TEMP IND NORMAL. BURNING ODOR IN COCKPIT. UPON BOARDING ACFT, OBSERVED NO BURNING ODOR. STARTED APU AND SELECTED RT PACK ON, INSP CB`S INSTRUMENTS AND COCKPIT LIGHTING, VERIFIED WINDOW HEAT AND FANS OP NORMAL. SELECApr 9, 2009 · N405AW · Cndair CL6002B19 · Cabin Cooling SystemSDR A6WA200940204Tire · failed190919 - NR 3 MAIN TIRE BLOW/SHREDDED FWD ON POST FLIGHT, RT INBD FLAP AND BUTE DOOR SHOW DAMAGE FROM TIRE DEBRIS. INSPECTED RT INBD FLAP AND ACFT FLAP DAMAGE FOUND TO BE OUT OF LIMITS REF BUT 2+3+4. REF 190919/1 RT INBD FLAP LOWER SURFACE HAS 4 DENTS NO LOOApr 6, 2009 · N405AW · Cndair CL6002B19 · TireSDR A6WA200840131Psu · detachedPSU AND OXYGEN MASK UNIT DETACHED FROM ROW 8A AND C. RESECURED PSU, COMPLIED WITH OPS CHECK OF PSU ABOVE SEATS 8A AND 8C, OPS CHECK GOOD IAW AMM 25-20. PSU PROPERLY INSTALLED AT THIS TIME. (M)Feb 25, 2008 · N405AW · Cndair CL6002B19 · Passenger Compartment EquipmentSDR A6WA200740542Smoke Detector · malfunctionedRECEIVED SMOKE CARGO WARNING DURING TAXI OUT, MESSAGE LIT FOR 5 SECONDS AND EXTINGUISHED RAMP INSPECTED CARGO BAY AND FOUND NO EVIDENCE OF SMOKE AND FIRE. DEACTIVATED BOTH CARGO SMOKE DETECTORS IAW AMM 26-15-00-040-801. (M)Sep 17, 2007 · N405AW · Cndair CL6002B19 · Smoke DetectionSDR A6W2007F00000Duct · crackedINSPECTED APU AND FOUND UPPER AND LOWER INTAKE DUCTS CRACKED BEYOND LIMITS IAW AMM 49-14-01. REMOVED AND REPLACED UPPER AND LOWER APU INTAKE DUCTS. OPERATIONAL CHECK GOOD IAW 49-52-01. UPPER DUCT, TSN 7728, LOWER DUCT, TSN 11740. (K)Mar 23, 2007 · N405AW · Cndair CL6002B19 · APU Bleed Air SystemSDR A6WA200740081Duct · crackedINSPECTED APU AND FOUND UPPER AND LOWER INTAKE DUCTS CRACKED BEYOND LIMITS IAW AMM 49-14-01. REMOVED AND REPLACED UPPER AND LOWER APU INTAKE DUCTS. OPERATIONAL CHECK GOOD IAW 49-52-01. UPPER DUCT TSN = 7728, LOWER DUCT TSN = 11740.Feb 23, 2007 · N405AW · Cndair CL6002B19 · APU Bleed Air SystemSDR A6WA200640404Cover · dislodgedOXYGEN MASKS COVERS FELL FROM SEATS 4 AND 5 (A) AND (C). RESECURED PSU COVERS AT SEATS 4 AND 5 IAW AMM. (K)Dec 7, 2006 · N405AW · Cndair CL6002B19 · Passenger Oxygen SystemSDR A6WA200640127Idg · underservicedON DEPARTURE IDG NR2 ILLUMINTED AND CLEARED (IDG NR 1 ALREADY ON MEL). SERVICED IDG NR 2 IAW AMM. OPS CHECK GOOD. NO LEAKS NOTED. (K)Apr 3, 2006 · N405AW · Cndair CL6002B19 · Alternator-Generator DriveSDR A6WA200540330Rheostat · faultyWHEN F/O SELECTED FLOOD LIGHTS ON, SMOKE ERUPTED FROM BEHIND SW PANEL FLOOD LABEL DSTLA ON FO`S SIDE PANEL AND CBP3 C1 POPPED AND WAS NOT RESET. INSPECTED AND FOUND FO`S FLOOD LIGHT RHEOSTAT FAULTED. NO OTHER SYS AFFECTED. (K)Nov 22, 2005 · N405AW · Cndair CL6002B19 · Flight Compartment LightingSDR A6WA200540282Vane · wornRIGHT OUTBOARD FLAP VANE, OUTBOARD FLAP VANE FITTING WORN EVEN WITH LEADING EDGE OF VANE .030 INCH IS MINIMUM CLEARANCE ALLOWED PER BOMBARDIER, INC REO 601R-57-53-195. REMOVED OLD VANE FITTING FROM RIGHT OUTBOARD FLAP AS WS 296.073 AND INSTALLED NEW VANE FITTAug 3, 2005 · N405AW · Cndair CL6002B19 · Trailing Edge FlapsSDR A6WA200540276Vane · wornRT OB FLAP VANE, OB FLAP VANE FITTING WORN EVEN WORN LEADING EDGE OF VANE .030 INCH IS MINIMUM CLEARANCE ALLOWED IAW REO. REMOVED OLD VANE FITTING FROM RT OB FLAP AS WS296.073 AND INSTALLED NEW VANE FITTING IAW REO. (K)Aug 3, 2005 · N405AW · Cndair CL6002B19 · Trailing Edge FlapsSDR A6WA200540281Rib · crackedRIGHT MLG WHEEL WELL BATTERY RIB AT WS 48.30, FS 523.8 IS CRACKED AT UPPER RADIUS APPROX 1.25 INCH LONG. REPAIRED IAW REO 601R-57-51-046 REV B. (M)Jul 28, 2005 · N405AW · Cndair CL6002B19 · Wing, Rib/BulkheadSDR A6WA200540271Rib · crackedLT MLG WHEEL WELL BATT RIB AT WS 48.30, FS 523.8 IS CRACKED AT UPPER RADIUS APPROX 1.25 INCH LONG. REPAIRED IAW REO. (K)Jul 28, 2005 · N405AW · Cndair CL6002B19 · Wing, Rib/BulkheadSDR A6WA200540269Angle · crackedLT FS 484, LBL27, ANGLE IS CRACKED APPROX 1.25 INCH L THRU THICKNESS OF MATERIAL AT UPPER END OF RADIUS. REMOVED CRACKED ANGLE, FABED NEW ANGLE FROM ANGLE TO SMPLE AND INSTALLED IAW SRM. (K)Jul 26, 2005 · N405AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200540273Clip · crackedFS 280, RBL 9, OB, CLIP ANGLE IS CRACKED 1 INCH LONG. REMOVED AND REPLACED ANGLE IAW EO AND SRM. (K)Jul 25, 2005 · N405AW · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR A6WA200540263Angle · crackedFS 280, LBL 9, CLIP ANGLE IS CRACKED, 1 INCH LONG. REMOVED AND REPLACED CLIP ANGLE FS 280, LBL 9, OB, IAW SRM. (K)Jul 25, 2005 · N405AW · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR A6WA200540262Clip · crackedFS 280, LBL 9, IB CLIP ANGLE IS CRACKED, 1 INCH LONG. REMOVED AND REPLACED FS 280, LBL 9, IB CLIP IAW SRM. (K)Jul 25, 2005 · N405AW · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR A6WA200540261Clip · crackedFS 280, RBL 9, IB CLIP ANGLE IS CRACKED 1 INCH LONG. REMOVED AND REPLACED FS 280, RBL9, IB CLIP IAW SRM. (K)Jul 25, 2005 · N405AW · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR A6WA200540268Fitting · looseHORIZONTAL STABILIZER FORWARD STEADY FITTING HAS 6 LOOSE MOUNT BOLTS. REMOVED BOLTS, VISUALLY INSPECTED HARDWARE AND HOLES, REINSTALLED BOLTS AND TORQUED IAW AMM. (K)Jul 24, 2005 · N405AW · Cndair CL6002B19 · Horizontal Stabilizer, Attach FittingsSDR A6WA200540265Skin · chafedLT WING IB FLAP, IB END AT FLAP STA 50.498 IB BELOW THE LEADING EDGE IS CHAFED FROM THE STUB FAIRING. CHAFE MEASURES 1.50 INCH LONG X .50 INCH WIDE X .035 INCH DEEP. (K)Jul 24, 2005 · N405AW · Cndair CL6002B19 · Trailing Edge FlapsSDR A6WA200540264Skin · dentedLT WING IB FLAP INNER SKIN IS DENTED BETWEEN FLAP STATION 142 AND 147 AT THE INTERCOSTAL SPAR AREA. DEN MEASURES .850 INCH LT X .800 INCH X .067 INCH DEEP. PERFORMED REPAIR BY CUTTING OUT DAMAGE AND INSTALLING 11.5 INCH X 3 INCH FLUSH REPAIR IAW SRM REPAIR Jul 24, 2005 · N405AW · Cndair CL6002B19 · Trailing Edge FlapsSDR A6WA200540144Potentiometer · failedIN CRUISE FIGHT ED1, ED2, FMS 1 AND 2, RTU 1 AND 2, AND STANDBY RTU DISPLAY ALL WENT BLANK. REMOVED AND REPLACED CENTER PEDESTAL LIGHTING PANEL DISPLAY KNOB POTENTIOMETER. OPS CHECK GOOD IAW AMM 33-12-19. (M)Apr 10, 2005 · N405AW · Cndair CL6002B19 · Flight Compartment LightingSDR A6WA200440224Connector · dirtyENGINE NR 1 READS 0 PERCENT IN FLIGHT, ALL OTHER PARAMETERS NORMAL. CLEANED ALL CONNECTOR PLUGS, NR 1 ALTERNATOR AND SOCKET GROUND RAN TO TAKEOFF POWER, OPS CHECK GOOD. NO DEFECTS NOTED IAW AMM.Dec 19, 2004 · N405AW · Cndair CL6002B19 · Power Indicating SystemSDR A6WA200440188Controller · failedRT AOA, RT TAT, RT STATIC, RT PITOT AFTER TAKEOFF RETURNED IAW DISPATCH. REMOVED AND REPLACED RT AIR DATA SENSOR HEAT CONTROLLER IAW MM 30-31-15, OPS CHECK GOOD.Nov 18, 2004 · N405AW · Cndair CL6002B19 · Pitot/Static Anti-Ice SystemSDR A6WA200340201Skin · corrodedLT WING LOWER SKIN PLANK HAS CORROSION AT PANEL OPENING 540CB, FORWARD AND AFT OF PANEL OPENING. PERFORMED A MAJOR REPAIR BY BLENDING OUT CORROSION AND TREATING METAL IAW REO 601R-57-21-030. (M)Dec 27, 2003 · N405AW · Cndair CL6002B19 · Wing, Plate/SkinSDR A6WA200340195Skin · scratchedLEFT SIDE FUSELAGE SKIN SCRATCHES FS 280 TO FS 295, STRINGER 25L TO STRINGER 26L. PERFORMED A MAJOR REPAIR BY CUTTING OUT DAMAGED SECTION OF SKIN, COMPLYING WITH HFEC TO ENSURE CRACK EXIST AND INSTALLING A NON-FLUSH PATCH IAW CRJ SRM 53-00-31 REPAIR NR 1 REO Dec 21, 2003 · N405AW · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR A6WA200340196Floor Panel · crackedFOUND FLOOR STRUCTURE CRACKED AT FS 621, LT AND RT SIDE ANGLE, P/N 601R35032-239. PERFORMED A MAJOR REPAIR BY CUTTING AWAY DAMAGES PORTION OF ANGLE AND INSTALLING REPAIR ANGLE AND STRAP IAW BOMBARDIE REO 601R-53-61-117 REV C. (M)Dec 20, 2003 · N405AW · Cndair CL6002B19 · Fuselage Floor PanelSDR A6WA200340194Bracket · crackedFOUND CRACKED BRACKETS, QTY 2, AT FS 484 RIGHT FUSELAGE, FLOOR LEVEL. REMOVED AND FABRICATED TWO BRACKETS AS PER SAMPLE MATERAL 6144-13 (2024-T42.050) WVAC PO 27909/1 IAW WVAC EO601R-53-4502 RT SIDE FS 484 RBL 9 AND RBL 27 AND INSTALLED SAME BRACKETS IAW WVACDec 20, 2003 · N405AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200340042Gcu · failedPERFORM ADG DEPLOYMENT TEST FLIGHT. ADG FAILED TO POWER AC ESS BUS TEST FLIGHT UNSATISFACTORY. REPLACED GCU, (S/N OFF: 0212, S/N ON: 0290). COMPLETED TEST FLIGHT REQUIREMENTS. NO DEFECTS NOTED. GCU COMPONENT REPAIR SHOP TEAR-DOWN FINDINGS, NO FAULT FOUND Mar 31, 2003 · N405AW · Cndair CL6002B19 · AC Generation SystemSDR A6WA200340029A/C Pack · leakingF/A REPORTED SMOKE IN CABIN. NOTICED TEMPERATURE RISING. PACK NR 2 SELECTED MANUALLY. REDUCED TEMP PACK, ODOR AND SMOKE SUBSIDED. GROUND RAN A/C NR 1 AND NR 2 PACKS. OPS NORMAL. NR 2 PACK SHOWS EVIDENCE OF OIL LEAKAGE. PLACED PACK ON MEL.Feb 4, 2003 · N405AW · Cndair CL6002B19 · Cabin Cooling SystemSDR A6WA200240029Smoke · detectedSMOKE TOILET CAUTION MESSAGE ON APPROACH INTO DENVER WITH PACKS SWITCHED TO APU. FLIGHT ATTENDANT SAW SMALL AMOUNT OF SMOKE ALONG FLOOR. ALSO, REPORTED OIL SMELL IN/NEAR LAVATORY. OPS CHECK GOOD ON GROUND. COULD NOT DUPLICATE. OK FOR SERVICE AT THIS TIME.Dec 16, 2002 · N405AW · Cndair CL6002B19 · Air Distribution SystemSDR A6WA200240012Window · failedPILOTS SIDE WINDOW SHATTERED IN FLIGHT MAINTENANCE REMOVED AND REPLACED PILOT 'B' SCREEN. OPERATIONAL AND PRESSURIZATION CHECK GOOD. (M)Apr 28, 2002 · N405AW · Cndair CL6002B19 · Flight Compartment WindowsSDR A6WA200240004Torque Link · disconnectedUPON DEPARTING OUT OF DENT, GEAR RETRACTION, GEAR DISAGREE WOW INPUT AND WOW OUTPUT MESSAGE MAINTENANCE FOUND NLG SCISSORS (TORQUE LINKS) DISCONNECTED. UPPER TORQUE LINK DAMAGED. INSPECTED GEAR. REPAIRED DAMAGE TO SCISSOR. PERFORMED GEAR SWINGS. (M)Feb 4, 2002 · N405AW · Cndair CL6002B19 · Nose/Tail Landing Gear Strut/AxleSDR A6WA200100052Transducer · failedZERO OIL PRESSURE ON RT ENGINE DURING FLIGHT. NO ASSOCIATED MESSAGES. ALL OTHER ENGINE INDICATIONS WERE NORMAL. NO LOW OIL PRESSURE LIGHT ILLUMINATED. MAINTENANCE REMOVED AND REPLACED RT ENGINE OIL PRESSURE TRANSDUCER.Aug 16, 2001 · N405AW · Cndair CL6002B19 · Engine Oil Pressure
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