N419AW

Service difficulty reports · 178

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 = 'N419AW' 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 A6WA20134M1128Angle · crackedANGLE CRACKED AT FS 484, RBL 27. REMOVED CRACKED ANGEL AND INSTALLED NEW SERVICEABLE ANGLE IAW SRMS 51-24-21, 51-40-11, 51-21-11, 51-25-06, 51-25-16, 51-42-06, 51-42-21.Jul 28, 2013 · N419AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA201301224006Warning System · activatedON APPROACH INTO MKE AT APPROX 2500 FT AGL, SELECTED FLAPS TO 8 AND RECEIVED A FLAP FAIL CAS MSG. WENT AROUND AND RECEIVED DELAY VECTORS TO RUN THE QRH AND PREPARE FOR A ZERO FLAP LANDING. DECLARED THE EMERGENCY AND MADE AN UNEVENTFUL LANDING.Jan 22, 2013 · N419AW · Cndair CL6002B19 · Trailing Flap Position Indicating SystemSDR A6WA201240806Escape Hatch · unsecureCREW HATCH POPPED OPEN FROM REAR OF HATCH ABOUT 1 INCH. ABORTED TO AT 100 KNOTS. MAX BTMS 5,6,7,6. HES STOP INSP NOT REQUIRED IAW MXCTL.Aug 22, 2012 · N419AW · Cndair CL6002B19 · Emergency ExitsSDR A6WA201240643Sill · corrodedPAX DOOR LOWER SILL FWD AND AFT CLEATS CORRODED. REMOVED FWD CLEAT, REMOVED CORROSION, RESTORED FINISH. REINSTALLED, REMOVED OUT OF LIMITS AFT CLEAT. LOCATED AND INSTALLED NEW CLEAT IAW SRM 51-21-06, 51-21-16, 51-42-13, 51-42-06.Jun 13, 2012 · N419AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA201240526Warning Light · illuminatedAT CLIMB OUT, RT STATIC HEAT, RT PITOT HEAT, RT AOA HEAT AND TAT PROBE HEAT CAUTION MESSAGES. C/W QRH WOULD NOT RESET. PERFORMED FIM RESET PROCEDURE SYS. OPS CHECKED GOOD.May 9, 2012 · N419AW · Cndair CL6002B19 · Central WarningSDR A6WA201240007Actuator · failedGEAR SELECTED UP. NOSE AND RIGHT INDICATED UP. LEFT INDICATED DOWN. MESSAGE CLEARED & LEFT GEAR INDICATED UP AND LOCKED AFTER 30 SECONDS. ALONG GEAR DISSAGREE HAD PARK BRAKE SOV AND OTBD ANTISKID MSGS. THESE CLEARED AS WELL. R & R LT MLG SIDE STAY ACTUATJan 3, 2012 · N419AW · Cndair CL6002B19 · Landing Gear ActuatorSDR A6WA201141144Priority Valve · failedON SELECTING GEAR UP, RECEIVED ANTI-SKID INBD CAUTION FOR 2 SECONDS, THEN MESSAGE EXTINGUISHED. R & R OF MLG PRIORITY VALVE. PERFORMED OPS CK OF ANTI-SKID SYS IAW 32-44-06, OPS CK GOOD.Dec 17, 2011 · N419AW · Cndair CL6002B19 · Brake Anti-Skid SectionSDR A6WA201141134Wire Harness · damagedAFTER TAKEOFF, RECEIVED ANTI-SKID INBD CAUTION MESSAGE. MESSAGE CLEARED WITH GEAR RETRACTION AND DID NOT RETURN WITH GEAR EXTENSION. R & R LT MLG INBD HARNESS IAW AMM 32-61-20. OPS CHECKED GOOD.Dec 9, 2011 · N419AW · Cndair CL6002B19 · Landing Gear System WiringSDR A6WA201140971Connector · disconnectedAFTER GEAR UP SELECTION, RECEIVED ANTI-SKID INBD CAUTION, THEN GEAR DISAGREE DOWN WHICH LASTED ABOUT 5 SECONDS. MESSAGES ALL CLEARED. TROUBLE SHOOTING FOUND A CONNECTOR ON RT INBD GEAR HARNESS DISCONNECTED, RECONNECTED CONNECTOR TO HARNESS. PERFORMED EXT ANNov 11, 2011 · N419AW · Cndair CL6002B19 · Landing Gear System WiringSDR A6WA201140701Skin · dentedLT LWR CORE COWL DENT BETWEEN FWD AND AFT HINGES. REWORKED DENT BY REO 601R-71-12-4066.Jul 8, 2011 · N419AW · Cndair CL6002B19 · Nacelle/Pylon, Plate/SkinSDR A6WA201140694Skin · gougedSERVICE DOOR HANDLE CUT OUT GOUGED. BLENDED OUT DAMAGE TO SMOOTH CONTOUR SERVICE DOOR CUT OUT IAW SRM 51-12-08 AND EXCEEDING MAX REPORTED DEPTH, BLEND OUTS ARE WITH LIMITS IAW REO 601R-52-41-183, REV.Jul 8, 2011 · N419AW · Cndair CL6002B19 · Service DoorsSDR A6WA201140702Angle · crackedREMOVED CRACKED ANGLE, LOCATED ON UPPER FLANGE OF PAX DOOR STAIRS, THEN FABRICATED AND INSTALLED NEW ANGLE IAW REO 601R-52-11-1959.Jul 7, 2011 · N419AW · Cndair CL6002B19 · Passenger/Crew DoorsSDR A6WA201140700Guide · chafedLT OTBD FLAP ROLLER GUIDE FITTING CHAFED C/W IAW REO 601R-57-51-143.Jul 7, 2011 · N419AW · Cndair CL6002B19 · Trailing Edge FlapsSDR A6WA201140703Skin · chafedLT & RT WING CHAFING ON BOTTOM SKIN PLANK NR APPROX WS 45.0. ALSO TO INCLUDE (1) HI-LITE FASTENER HEAD ON RT WING. BLENDED AND SMOOTHED MINOR CHAFING IAW REO 601R-57-21-880. CHANGED OUT DAMAGED FASTENER IAW 601R-57-21-880.Jul 6, 2011 · N419AW · Cndair CL6002B19 · Wing, Plate/SkinSDR A6WA201140692Panel · crackedPAX DOOR AFT STAIR CRACKED NEXT TO AFT HANDRAIL 1 BRACKET AND CORNER OF 3RD STEP. REPAIRED AFT STAIR STRUCTURE NEXT TO AFT HANDRAIL BRACKET AND CORNER OF 3RD STEP. REPAIRED AFT STAIR STRUCTURE NEXT TO AFT HANDRAIL BRACKET AND CORNER OF 3RD STEP IAW REO 601R-Jul 2, 2011 · N419AW · Cndair CL6002B19 · Passenger/Crew DoorsSDR A6WA201140691Panel · crackedPAX DOOR FWD STAIR STRUCTURE IS CRACKED NEXT TO FWD HANDRAIL BRACKET. REPAIRED FWD STAIR STRUCTURE NEXT TO FWD HANDRAIL BRACKET IAW REO 601R-52-11-702 REV C ZONE 2 REPAIR.Jul 2, 2011 · N419AW · Cndair CL6002B19 · Passenger/Crew DoorsSDR A6WA201140693Skin · chafedLT MLG DOOR FWD CORNER CHAFED. REMOVED UNSERVICEABLE 1 FILLER AND INSTALLLED SERVICEABLE 1 FILLER IAW REO 601R-52-82-034.Jul 1, 2011 · N419AW · Cndair CL6002B19 · Landing Gear DoorsSDR A6WA201140696Skin · chafedRT MLG DOOR (INTERIOR) IS CHAFED IN TWO PARTS. BLENDED AND REMOVED PAINT, SCRATCHES-ALODINED, PRIMED AND TOP COATED.Jun 30, 2011 · N419AW · Cndair CL6002B19 · Landing Gear DoorsSDR A6WA201140697Skin · chafedRT MLG DOOR L/E IS CHAFED AT 2 FILLER. REMOVED CHAFED FILLER, FABRICATED NEW FILLER AND INSTALLED.Jun 30, 2011 · N419AW · Cndair CL6002B19 · Landing Gear DoorsSDR A6WA201140695Rib · crackedLT BATTERY RIB CRACKED CUT AWAY DAMAGE, FABRICATED ANGLE DOUBLER & FILLER IAW REO 601R-57-51-046. INSTALLED IAW REO 601R-57-51-046.Jun 29, 2011 · N419AW · Cndair CL6002B19 · Wing, Rib/BulkheadSDR A6WA201140698Skin · chafedRT INBD FLAP VANE L/E CHAFE POINTS 3 PLACES BLENDED, FOUND TO BE WITHIN LIMITS, ALODINED, PRIMED AND TEFLON TOP COATED.Jun 29, 2011 · N419AW · Cndair CL6002B19 · Trailing Edge FlapsSDR A6WA201140699Vane · chafedLT OTBD FLAP VANE L/E CHAFE POINTS 3EA. BLEND AND FINISH IAW REO 601R-57-52-004, REV C. FINISH RESTORATION IAW SRM 51-21-16.Jun 29, 2011 · N419AW · Cndair CL6002B19 · Trailing Edge FlapsSDR A6WA201140511Angle · crackedLT OBLIQUE ANGLE CRACKED. REMOVED UNSERVICEABLE LT OBLIQUE ANGLE AND INSTALLED SERVICEABLE ANGLE IAW SRM 51-42-21 AND REO 601R-53-61-422.Jun 26, 2011 · N419AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA201140510Angle · crackedRT OBLIQUE ANGLE CRACKED. REMOVED UNSERVICEABLE RT OBLIQUE ANGLE AND INSTALLED SERVICEABLE ANGLE IAW SRM 51-42-21 & REO 601R-53-61-422.Jun 26, 2011 · N419AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA201140500Engine · failedIN CLIMB, BETWEEN 8000-8500 FT A/P LT ENG MADE LOUD BANG FOLLOWED BY SHUDDERING AND VIBRATION ITT WELL ABOVE 900 DEGREES. BROUGHT LT ENGINE THRUST TO IDLE VIBRATION DAMPENED. ADVANCED ENGINE THRUST, BROUGHT NO ADDITIONAL THRUST RAN IMMEDIATE ACTION CHECKLISTJun 10, 2011 · N419AW · Cndair CL6002B19 · Turbine Engine Compressor SectionSDR A6WA201140437Brake Assy · leakingLOG AFTER SHUTTING DOWN SMOKE COMING OFF LT GEAR/ BRAKE AREA, FLUID LEAKING CAUSING SMOKE AND POOLING UNDER LT MAIN GEAR. REPLACED NR 2 MLG BRAKE IAW 32-46-26. LEAK OPS CHECK GOOD.May 25, 2011 · N419AW · Cndair CL6002B19 · Landing Gear Brake SystemSDR A6WA201140690Attach Fitting · corrodedLOWER SECTION OF PAX DOOR DRAINAGE RAMP AREA HAS 4 CORRODED CLIPS 2 EA AT FS 320.10 & FS 338.00. REMOVED 4 CORRODED CLIPS 2EA AT FS 320.10 AND FS 338.00. THEN INSTALLED 4 NEW SERVICEABLE CLIPS 2 EA AT FS 320.10 & FS 338.00 IAW SRM 51-42-06, 51-42-21.Apr 27, 2011 · N419AW · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR A6WA201040709Pressure Blkhd · crackedFOUND CRACK INDICATION AT FS 559, LBL9 AND WL 58.70. REPAIRED CRACK AT FS559, LBL 9 & WL 58.70 BY FULL CORPORATION OF REO 601R-53-41-260, REV E 2010/09/24 AND INCLUDING DEVIATION REO 601R-53-41-609 REV B DEVIATION E TO THE FS 559 PRESSURE BULKHEAD, LT & RT SISep 21, 2010 · N419AW · Cndair CL6002B19 · Fuselage Main, BulkheadSDR A6WA201040671Strip · dirtyAS SOON AS FLAPS ARE SELECTED TO 45 DEG, ACFT BECOMES UNSTABLE AROUND A LONGITUDINAL AXIS. ACFT SNAPS TO THE LT AND RT WITHOUT AILERON INPUT, AND WHEN APPLYING AILERON , CORRECTION AILERONS DOS100-0080-01 EFFECTIVE UNTIL SIGNIFICANT. CLEANED AND PAINTED INBDSep 3, 2010 · N419AW · Cndair CL6002B19 · Aileron Control SystemSDR A6WA201040611Unknown · odorAFTER PACKS WERE RUN ON APU 10-15 MINUTES, FUEL SMELL NOTED FROM ROWS 8-13. RAN PACKS ON ENGINE AND APU SMELL DID NOT SUBSIDE. INSPECTED A/C, NO EXTERNAL LEAKS NOTED. INSPECTED APU ENCLOSURE WITH APU RUNNING, NO LEAKS NOTED. RAN PACKS ON APU AND ENGINE BLEAug 16, 2010 · N419AW · Cndair CL6002B19 · Air Distribution SystemSDR A6AW200940397Cargo Track · corrodedCARGO BAGGAGE RAIL BTW FS 574 AND 559+112, LBL 9.00 IS CORRODED. CARGO BAGGAGE RAIL BTW FS 574 AND 559+112, LBL 9.00. REPLACED IAW AMM 53-01-11-400-802. (K)Jul 5, 2009 · N419AW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR A6WA200940398Cargo Track · corrodedCARGO BAGGAGE RAIL BTW FS 574 AND FS 559+112, RBL 9.0 IS CORRODED. CARGO BAGGAGE RAIL BTW FS 574 AND FS 559+112, RBL 9.0 REPLACED IAW AMM 53-01-11-400-802. (K)Jul 5, 2009 · N419AW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR A6WA200940395Cargo Track · corrodedCARGO BAGGAGE RAIL FWD OFFS 621.00, LBL 9.00 IS CORRODED. NEW RAIL INSTALLED IAW SRM 51-41-04. (K)Jul 5, 2009 · N419AW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR A6WA200940399Cargo Track · corrodedCARGO BAGGAGE RAIL BTW FS 559+80 AND FS 559+96, LBL 27.00 IS CORRODED. CARGO BAGGAGE RAIL BTW FS 559+80 AND FS 559+96, LBL 27.00. REPLACED IAW AMM 53-01-11-400-802. (K)Jul 4, 2009 · N419AW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR A6WA200940396Anchor Fitting · corrodedCARGO ANCHOR PLATE FWD OF FS 605.00, LBL 9.00 IS CORRODED. REPLACED ANCHOR IAW SRM 51-41-04. (K)Jul 3, 2009 · N419AW · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR A6WA200940393Pressure Blkhd · crackedFWD PRESSURE BULKHEAD WEB AT 202.75, LBL 23.71, WL 69.79 IS CRACKED. FWD PRESSURE BULKHEAD WEB AT FS 202.75, LBL 23.71, WL 69.79 REPAIRED IAW REO 601R-53-11-563. (K)Jul 2, 2009 · N419AW · Cndair CL6002B19 · Fuselage Main, BulkheadSDR A6WA200940394Floorbeam · crackedUPPER AFT ANGLE ON CROSSBEAM AT FS 280.00, LBL 9.0, WL 72.00 IS CRACKED. CRACK LENGTH IS .350. UPPER AFT ANGLE ON CROSSBEAM AT FS 280.00, LBL 9.00, WL 72.00. REPAIR IAW REO 601R-53-11-136, REV A. (K)Jul 1, 2009 · N419AW · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR A6WA200940400Floorbeam · crackedCROSSBEAM AT FS 280.00, RBL 9.00, WL 71.00 IS CRACKED IN THE LOWER RADIUS. CROSSBEAM AT FS 280.00 RBL 9.00, WL 71.00 REPAIRED IAW REO 601R-53-11-171, REV D. (K)Jul 1, 2009 · N419AW · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR A6WA200940405Seat Track · corrodedSEGMENT TRACK BTWN FS 559+80 AND FS 559+96 CORRODED. SEGMENT TRACK BTWN FS559+80 AND FS 559+96, RBL 9.00 REPLACED IAW SRM 51-41-04. (K)Jun 30, 2009 · N419AW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR A6WA200940403Attach Fitting · crackedCLIP AT FS 484.00, RBL 27.00, WL 72.00 IS CRACKED. CRACKED LENGTH .200 INCH CLIP AT FS 484.00, RBL 27.00, WL 72.00 REPLACED IAW SRM 51-42.06. (K)Jun 30, 2009 · N419AW · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR A6WA200940404Attach Fitting · crackedCLIP AT FS 484.00, LBL 27.00, WL 72.00, IS CRACKED. CRACKED LENGTH .250" CLIP AT FS 484.00, LBL 27.00, WL 72.00, REPLACED IAW SRM 51-42-06. (K)Jun 30, 2009 · N419AW · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR A6WA200940402Intercostal · crackedINTERCOSTAL AT FS 484.00, LBL 36.00, WL 72.00 IS CRACKED. CRACK LENGTH IS .400 ". REPAIRED IAW REO 601R-53-41-059, REV A. (K)Jun 29, 2009 · N419AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200940401Intercostal · crackedINTERCOSTAL AT FS 484.00, RBL 36.00, WL 72 IS CRACKED. CRACK LENGTH IS .600 INCH. REPAIRED IAW REO 601R-53-41-059, REV A. (K)Jun 29, 2009 · N419AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200940014Target · looseLOG 198286/3 - RT MLG DISAGREE LIGHT CAME ON DURING RETRACTION. INSP BOTH NLG AND MLG WITH NO FAULTS FOUND. MX ACTION C/W PLACED ON MEL. LOG 198286/4 FOUND UPLOCK TARGET EXCESSIVELY LOOSE, RESECURED AND OP CHECKS IAW AMM 32-61-05 AND 32-30-00. OPS CHECKS GJan 14, 2009 · N419AW · Cndair CL6002B19 · Landing Gear Position and WarningSDR A6WA200840557O-Ring · missingAT CRUISE SPEED RECEIVED LT ENG OPERATION WARNING MESSAGE AND OIL PRESSURE INDICATED 25-36 PSI. MESSAGE RECURRED AND PRESSURE DROPPED TO 25 PSI SEVERAL TIMES IN FLIGHT. INSPECTED NR 1 ENG AND FOUND OIL LEAKING FROM SCAVENGE FILTER. UPON REMOVING FILTER FOUNAug 4, 2008 · N419AW · Cndair CL6002B19 · Turbine Engine Oil SystemSDR A6WA200740703Idg · inoperativeON T/O ROLL RECEIVED (IDG 2) CAUTION MESSAGE FOLLOWED BY (GEN 2 OFF) CAUTION MESSAGE. ABORTED T/O AT APPROXIMATELY 70 KNOTS, MAX BTMS READINGS = 3,3,2,3. FOUND FAULT MESSAGE CHANGED AFTER IDG WAS PREVIOUSLY CHANGED FROM (NR 2 GEN OFF) MESSAGE TO (IDG 2) MESSADec 16, 2007 · N419AW · Cndair CL6002B19 · AC Generator-AlternatorSDR A6WA200740463Retainer · corrodedCORROSION FOUND ON FORWARD SEAL RETAINER OF THE MAIN AVIONICS COMPARTMENT DOOR. SEAL RETAINER P/N 601R14533-41, CC670-386743 AND CC 670-38663-5 REPLACED IAW SRM 51-42-06. (M)Jul 13, 2007 · N419AW · Cndair CL6002B19 · Electrical/Electronic Compartment DoorsSDR A6WA200740465Skin · corrodedFOUND CORROSION ON AVIONIC DOOR INNER SKIN AT FS 364 BTW STRINGER 25L TO STRINGER 25R. MAINTENANCE PERFORMED REPAIR TO AVIONIC DOOR APERTURE INNER DOUBLER FS 364 TO FS 379 STRINGER 27 TO STRINGER 25R IAW REO 601R-53-21-781. (M)Jul 13, 2007 · N419AW · Cndair CL6002B19 · Electrical/Electronic Compartment DoorsSDR A6WA200740464Skin · corrodedFOUND CORROSION ON SKIN CUT OUT OF MAIN AVIONIC DOOR SURROUND. MAINTENANCE PERFORMED BOMBARDIER MODSUM 601R53210045 TO COMPLY WITH REO 601R-53-21-781. (M)Jul 13, 2007 · N419AW · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR A6WA200740383Door · out of rig110612 MWC NR 53 CREW ESCAPE HATCH FAILED FUNCTIONAL TEST, ADJUSTMENT TO BE CARRIED OUT IAW AMM 52-22-00-820-801. CREW ESCAPE HATCH RIGGED IAW AMM 52-22-00-820-801. CREW ESCAPE HATCH RIGGED IAW AMM 52-22-00-820-002. (K)Jul 9, 2007 · N419AW · Cndair CL6002B19 · Emergency Exits
Back to N419AW