N413AW

Service difficulty reports · 159

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 = 'N413AW' 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 A6WA201140207Lever · wornPAX DOOR FWD PULL IN LEVERS WORN (PN 601R318968-3). REPAIRED IAW REO 601R-52-11-524, REV A.Mar 21, 2011 · N413AW · Cndair CL6002B19 · Passenger/Crew DoorsSDR A6WA201140204Skin · chafedRT AILERON UPPER L/E SKIN CHAFING. REPAIRED IAW REO 601R-57-60-013.Mar 21, 2011 · N413AW · Cndair CL6002B19 · AileronsSDR A6WA201140210Plate · gougedPAX DOOR FWD STRIKER PLATE GOUGED. BLENDED GOUGE FROM FWD STRIKER PLATE OF PAX DOOR IAW REO 601R-52-11-296 AND SRM 51-12-00.Mar 21, 2011 · N413AW · Cndair CL6002B19 · Passenger/Crew DoorsSDR A6WA201140209Plate · gougedPAX DOOR AFT STRIKER PLATE GOUGED BLENDED GOUGE FROM AFT STRICKER PLATE OF PAX DOOR IAW REO 601R-52-11-296 AND SRM 51-12-20.Mar 21, 2011 · N413AW · Cndair CL6002B19 · Passenger/Crew DoorsSDR A6WA201140205Skin · damagedRT OTBD FLAP, FLAP VANE L/E HAS DENT ON OTBD END. UPON EVALUATION OF RT OTBD FLAP VANE L/E ON OTBD END FOUND TO BE WITHIN LIMITS IAW REO 601R-57-53-030.Mar 18, 2011 · N413AW · Cndair CL6002B19 · Trailing Edge FlapsSDR A6WA201140313Seat Track · corrodedLBL 9 & RBL 9 SEAT TRACKS AT FS 559+112 CORRODED. REMOVED UNSERVICEABLE SEAT TRACKS ON LBL 9 & RBL 9 AT FS 559+112 AND INSTALLED SERVICEABLE SEAT TRACKS IAW AMM 53-01-11.Mar 17, 2011 · N413AW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR A6WA201140062Actuator · faultyGEAR DISAGREE WARNING FOR RT MLG TOOK APPROXIMATELY 40 SECONDS FOR RT MLG TO SHOWED STOWED. FAULT VERIFIED, GEAR DISAGREE WARNING TO BE REPORTING FROM BOTH DCU`S. CW INSTALLED RT MLG STAY ACTUATOR MASSY OPS CK GOOD GEAR SWING GOOD LK CHECK GOOD IAW AMM 32-32Jan 23, 2011 · N413AW · Cndair CL6002B19 · Landing Gear ActuatorSDR A6WA201040783Pdu · malfunctioned"LT REV UNLOCKED" CAUTION MSG IN FLIGHT. FOLLOWED QRH PROCEDURES. NO CHANGE TO AC HANDLING CHARACTERISTICS. DID NOT SHUTDOWN ENGINE. DIVERTED. IN FLT LANDING WEIGHT CALCULATED AT 46990. R & R LT THRUST REVERSER PDU IAW AMM 78-32-03. OPS CHECK GOOD, REMOOct 23, 2010 · N413AW · Cndair CL6002B19 · Engine Thrust ReverserSDR A6WA201040304Unknown · malfunctionedWHILE WAITING TO CAPTURE GLIDE SLOPE, AP PITCHED UP 15 DEGREES, TURNED OFF AUTO PILOT AND RETUREND TO NORMAL FLIGHT. REENGAGED AP AND AP FUNCTIONED NORMALLY. PERFORMED ELEVATOR SERVO SPIN TEST IAW AMM 22-11-00. SERVO SPIN TEST GOOD AT THIS TIME, AUTOPILOT RApr 25, 2010 · N413AW · Cndair CL6002B19 · Autopilot SystemSDR A6WA200940124Actuator · failedFLAPS FAILED AT 41 DEGREES WHEN SELECTED TO 45 DEGREES. BRAKE TEMPS 4,3,4,4. REMOVED AND REPLACED RT INBD OUTER FLAP ACTUATOR. (K)Mar 15, 2009 · N413AW · Cndair CL6002B19 · Trailing Edge Flap ActuatorSDR A6WA200940145Retainer · corrodedMAIN AVIONICS DOOR SEAL RETAINERS (4EA) FOUND CORRODED. MAIN AVIONICS DOOR SEAL RETAINERS (4 EA) REPLACED IAW SRM 51-42-06. (K)Mar 5, 2009 · N413AW · Cndair CL6002B19 · Electrical/Electronic Compartment DoorsSDR A6WA200940117Fairing · wornLT WING, FLAP STUB FAIRING WORN LT WING, FLAP STUB FAIRING REPLACED IAW SRM 51-42-06. (K)Mar 5, 2009 · N413AW · Cndair CL6002B19 · Trailing Edge FlapsSDR A6WA200940149Stiffener · damagedPASSENGER DOOR AFT WEB + AFT TEE STIFFENER FOUND BUCKLED AND BENT. NEW PASSENGER AFT WEB + AFT TEE STIFFENERS INSTALLED IAW SRM 51-42-06. (K)Mar 4, 2009 · N413AW · Cndair CL6002B19 · Passenger/Crew DoorsSDR A6WA200940146Sill · corrodedSERVICE DOOR LOWER SILL, STEP PLATE CORRODED. CORROSION ON SERVICE DOOR LOWER SILL, STEP PLATE REMOVED IAW SRM 51-21-06 AND FOUND OUT OF LIMITS IAW SRM 53-21-23, SERVICE DOOR LWR SILL STEP PLATE REPLACED IAW SRM 51-41-04. (K)Mar 3, 2009 · N413AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200940099Skin · corrodedCORROSION ON UPPER PLANK ACCESS DOOR CUTOUT OF 640AT REO 601R-57-21-1076. (K)Mar 3, 2009 · N413AW · Cndair CL6002B19 · Wing, Plate/SkinSDR A6WA200940098Skin · corrodedCORROSION ON UPPER PLANK ACCESS DOOR CUT OUT OF 640BT. REO 601R57-21-1076.Mar 3, 2009 · N413AW · Cndair CL6002B19 · Wing, Plate/SkinSDR A6WA200940100Skin · corrodedCORROSION ON UPPER PLANK ACCESS DOOR CUTOUT OF 540AT REO 601R-57-21-1076. (K)Mar 3, 2009 · N413AW · Cndair CL6002B19 · Wing, Plate/SkinSDR A6WA200940168Housing · crackedCARGO DOOR HSG FOUND CRACKED 2 PLACES. CARGO DOOR HANDLE HSG REMOVED IAW SRM 51-42-21. CARGO DOOR HANDLE HSG INSTALLED IAW SRM 51-42-21. (K)Mar 2, 2009 · N413AW · Cndair CL6002B19 · Cargo/Baggage DoorsSDR A6WA200940150Mount · crackedPAX DOOR POWER ASSIST MOTOR STIFFENER MOUNT CRACKED. PAX DOOR POWER ASSIST MOTOR STIFFENER MOUNT REPLACED IAW SRM 51-42-06. (K)Feb 25, 2009 · N413AW · Cndair CL6002B19 · Passenger/Crew DoorsSDR A6WA200940148Pressure Blkhd · crackedCRACK FOUND ON FWD PRESSURE BULKHEAD FS 202.75, LBL 23.71 AROUND PARKING BRAKE CABLE (CRACK LENGTH 1.000) CRACK ON FWD PRESSURE BULKHEAD FS 202.75, LBL 23.71. REPAIRED IAW CRJ 200 601R-53-11-563. (K)Feb 25, 2009 · N413AW · Cndair CL6002B19 · Fuselage Main, BulkheadSDR A6WA200940147Bulkhead · crackedCRACK FOUND ON PILOT BULKHEAD FS 280, RBL 9 (CRACK LENGTH .500) CRACK ON PILOT BULKHEAD AT FS 280, RBL 9. REPAIRED IAW REO 601R-53-11-171, REV D. EDDY CURRENT PERFORMED ON CUT-OUT AND FABRICATD PARTS IAW REO 601R-53-11-171, REV D. (K)Feb 25, 2009 · N413AW · Cndair CL6002B19 · Fuselage Main, BulkheadSDR A6WA200840623Bulkhead · crackedMWC 6 FS 621 PRESSURE BULKHEAD WEB THAT SURROUNDS THE LINTEL ATTACHMENT FITTING IS CRACKED APPROX 1" LONG. PERFORMED A REPAIR BY CUTTING OUT SECTION OF WEB, FABRICATING AND INSTALLING REPAIR PARTS IAW BOMBARDIER, INC REO 601R-53-61-1230 REV D.Dec 4, 2008 · N413AW · Cndair CL6002B19 · Fuselage Main, BulkheadSDR A6WA200840428Wire Harness · unknownRT OUTBOARD MLG TIRE FLAT. SUSPECT ANTI-SKID PROBLEM. REMOVED AND REPLACED RIGHT OUTBOARD GEAR HARNESS ASSEMBLY IAW AWAC SUPP 06-051, OPS CHECK GOOD AT THIS TIME. (A)May 24, 2008 · N413AW · Cndair CL6002B19 · Landing Gear System WiringSDR A6WA200840051A/C Pack · malfunctionedRT PACK PRESSURE UNCONTROLLABLE, FOLLOWS ENGINE POWER SETTINGS, FALLS OFF LINE AT HIGH POWER SETTINGS. (K)Jan 23, 2008 · N413AW · Cndair CL6002B19 · Cabin Cooling SystemSDR A6WA200740129Support Angle · crackedCARGO DOOR SUPPORT BEAM ANGLE THAT ATTACHES TO REAR PRESSURE BULKHEAD IS CRACKED APPROX .5 INCH IN LENGTH. MAINTENANCE REMOVED CRACKED ANGLE AND INSTALLED NEW ANGLE P/N 601R35056-109 IAW CRJ SRM 51-42-21. (M)Mar 13, 2007 · N413AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200740125Angle · crackedAFT EQUIPMENT COMPARTMENT FS 621 TO 625 OBLIQUE ANGLE ON RIGHT SIDE CRACKED .5 INCH LONG. MAINTENANCE CRACKED ANGLE AND INSTALLED NEW ANGLE P/N 601-35012-52, IAW CRJ SRM 51-42-06. (M)Mar 12, 2007 · N413AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200740124Angle · crackedAFT EQUIPMENT COMPARTMENT FS 621 TO 625 OBLIQUE ANGLE ON LEFT SIDE CRACKED 1.5 INCH LONG. MAINTENANCE REMOVED CRACKED ANGLE AND INSTALLED NEW ANGLE P/N 601-35012-51 IAW CRJ SRM 51-42-06. (M)Mar 12, 2007 · N413AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200740128Skin · corrodedRIGHT WING INBOARD FUEL PANEL 640BB FOUND CORROSION AROUND WING PLANK APPROX .005 INCH DEEP IN NON-CRITICAL AREA. MAINTENANCE REPAIRED CORROSION BY BLENDING IAW BOMBARDIER REO 601R-57-21-030 REV F. (M)Mar 9, 2007 · N413AW · Cndair CL6002B19 · Wing, Plate/SkinSDR A6WA200740127Skin · corrodedLEFT WING OUTBOARD FUEL PANEL 550BB FOUND CORROSION AROUND WING PLANK APPROX .005 INCH DEEP IN NON-CRITICAL AREA. MAINTENANCE REPAIRED CORROSION BY BLENDING IAW BOMBARDIER REO 601R-57-030 REV F. (M)Mar 9, 2007 · N413AW · Cndair CL6002B19 · Wing, Plate/SkinSDR A6WA200740126Skin · corrodedRIGHT WING OUTBOARD FUEL PANEL 650B FOUND CORROSION AROUND WING PLANK APPROX .005 INCH DEEP IN NON-CRITICAL AREA. MAINTENANCE REPAIRED CORROSION BY BLENDING IAW BOMBARDIER REO 601R-57-030 REV F. (M)Mar 9, 2007 · N413AW · Cndair CL6002B19 · Wing, Plate/SkinSDR A6WA200740121Floor Support · crackedFS 280 AFT FLOOR SUPPORT ANGLE P/N 600-34017 CRACKED APPROX .3 INCH LONG OUTBOARD OF LBL 9.0. MAINTENANCE REPAIRED CRACKED FLOOR SUPPORT ANGLE P/N 600-34017 BY CUTTING OUT DAMAGE AND INSTALLING REPAIR ANGLE IAW BOMBARDIER REO 601R-53-11-138 REV C. (M)Mar 8, 2007 · N413AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200740120Angle · crackedLEFT FS 280 INBOARD AND OUTBOARD FLOOR ANGLES CRACKED APPROX .1 INCH LONG AT LBL 9.0. MAINTENANCE REMOVED CRACKED ANGLES AND INSTALLED NEW ANGLES P/N 601R31113-57 IAW CRJ SRM 51-42-06 AND 51-42-21. (M)Mar 8, 2007 · N413AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200740119Floor Support · crackedRIGHT FS 280 INBOARD AND OUTBOARD FLOOR SUPPORT ANGLES CRACKED APPROX .1 INCH LONG AT RBL 9.0. MAINTENANCE REMOVED CRACKED ANGLES AND INSTALLED NEW ANGLES P/N 601R31113-58 IAW CRJ SRM 51-42-06, 51-42-21. (M)Mar 8, 2007 · N413AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200740110Angle · crackedLT FS 484 INTERCOSTAL PREVIOUS REPAIR ANGLE AT LBL 36 CRACKED APPROXIMATELY .1 INCH LONG. MAINTENANCE INSTALLED NEWLY FABRICATED ANGLE IAW BSC STANDARD REPAIR 601R53-0030A AND BOMBARDIER REO 601R-53-41-059A REV A. (M)Mar 7, 2007 · N413AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200740109Angle · crackedRIGHT FS 484 INTERCOSTAL PREVIOUS REPAIR ANGLE AT RBL 36 CRACKED APPROXIMATELY .1 INCH LONG. MAINTENANCE INSTALLED NEWLY FABRICATED ANGLE IAW BSC STANDARD REPAIR 601R-53-0030A AND BOMBARDIER REO 601R-53-121-059 REV A. (M)Mar 7, 2007 · N413AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200740108Floor Support · crackedRIGHT FS 460 FLOOR SUPPORT FITTING P/N 600-31068-19 CRACKED APPROXIMATELY .3 INCH LONG AT OUTBOARD SIDE RBL 9. MAINTENANCE REMOVED CRACKED FITTING RIGHT FS 460 OUTBOARD SIDE RBL 9. DRILLED UP AND ALODINED NEW FITTING PART NR 600-31068-19. FITTING AND FASTENMar 7, 2007 · N413AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200740107Angle · crackedLEFT FS 484 INTERCOSTAL ANGLE AT LBL 27 CRACKED APPROXIMATELY .1 INCH LONG. MAINTENANCE INSTALLED NEWLY FAB`D ANGLE IAW BSC STANDARD REPAIR 601R.Mar 7, 2007 · N413AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200640333Extinguisher · lowFOUND CARGO BOTTLE LOW CAUTION MESSAGE ON TAXI, COMPLIED WITH QRH. REMOVED AND REPLACED CARGO FIRE EXTINGUISHER PER AMM 26-25-01. (M)Aug 20, 2006 · N413AW · Cndair CL6002B19 · Fire Bottle, FixedSDR A6WA200640226A/C Pack · malfunctionedABORTED TAKEOFF DUE TO RT PACK HIGH PRESSURE. ABORTED BELOW 40 KNOTS. CREW PERFORMED ENGINE RUN IAW MEL. NO RT PACK HIGH PRESSURE OCCURRED. AIRCRAFT OK FOR RETURN TO SERVICE. (K)Jun 4, 2006 · N413AW · Cndair CL6002B19 · Cabin Cooling SystemSDR A6WA200540283Warning System · activatedPASSENGER DOOR MASTER CAUTION AND AURAL `DOOR` CAME ON AFTER TAKEOFF AT APPROXIMATELY 500 AGL. COMPLIED WITH QRH AND RETURNED TO LAND. INTERROGATED PSEU, FOUND CODES D116, D117 AND D113. ALL INDICATIONS NORMAL. ALL ALIGNMENT MARKS NORMAL. NO FAULTS NOTED.Aug 13, 2005 · N413AW · Cndair CL6002B19 · Door Warning SystemSDR A6WA200540208Coalescer Bag · dirtyJET FUEL ODOR IN COCKPIT. SUSPECT DIRTY COALESCER BAG FOR NR 1 PACK, PLACED ON MEL AND PLACARDED. REMOVED AND REPLACED NR 1 COALESCER SOCK IAW 21-51-13. OPS CHECK GOOD. REMOVED FROM MEL AND REMOVED PLACARD. (M)Jun 17, 2005 · N413AW · Cndair CL6002B19 · Humidity Control SystemSDR A6WA200540120Bushing · out of positionLEFT AFT MLG TRUNNION BUSHING MIGRATED .006. REMOVED AND REPLACED LEFT AFT MLG TRUNNION BUSHING WITH 2ND OVERSIZED BUSHING P/N 601R-57-21-003-23 IAW BOMARDIER REO 601R-57-21-0003 REV B. (M)Mar 19, 2005 · N413AW · Cndair CL6002B19 · Wing, Landing Gear Attach FittingsSDR A6WA200540121Spar · misdrilledDUE TO HOLES SPACING ON RT LOWER WING SPAR AT WS 148, JOINT STRAP 601R100465-4 S/B CANNOT BE INSTALLED IAW SB 601R-57-037. REPAIRED RT WING SPAR AT WS 148, SHIFTED CUTLINE ON T/E RT WING AT WS 148. FABRICATED A NEW DOUBLE JOINT STRAP OUT OF 2024-T3.050 PO NRMar 19, 2005 · N413AW · Cndair CL6002B19 · Wing SparSDR A6WA200540122Rib · crackedLT HAND MLG WHEEL WELL AT SS 48.30, FS 523.8, BATT RIB IS CRACKED 1.2500 INCH LONG. REPAIRED LT WING BATT RIB AT WS 53.60 IAW MFG REO. (K)Mar 16, 2005 · N413AW · Cndair CL6002B19 · Wing, Rib/BulkheadSDR A6WA200540100Intercostal · crackedLT INTERCOSTAL AT FS 484.0 AT LBL 36 CRACKED, .5 INCH LONG. PERFORMED A REPAIR AT 484.0 LBL 36 BY CUTTING OUT DAMAGED AREA AND INSTALLING NEW ANGLE IAW REO. (K)Mar 16, 2005 · N413AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200540102Floorbeam · crackedRIGHT CARGO FLOOR SUPPORT ANGLE AT FS 621 CRACKED .5 INCH LONG. (M) REMOVED CRACKED SECTION OF FLOOR SUPPORT ANGLE AT FS 621 RT AND INSTALLED REPAIR ANGLE IAW MDG REO. (K)Mar 16, 2005 · N413AW · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR A6WA200540104Rib · crackedLEFT MLG WHEEL WELL AT SS 48.30 FS 523.8 BATT RIB IS CRACKED 1.25 INCH LONG. (M) REPAIRED LT WING BATT RIB AT WS 53.60 IAW MFG REO. (K)Mar 16, 2005 · N413AW · Cndair CL6002B19 · Fuselage Main, Longeron/StringerSDR A6WA200540103Floor Support · crackedLEFT CARGO FLOOR SUPPORT ANGLE AT FS 621 CRACKED AT 1 INCH. (M) REMOVED CRACKED SECTION OF FLOOR SUPPORT ANGLE AT FS 621 LT AND INSTALLED REPAIR ANGLE IAW MFG REO. (K)Mar 16, 2005 · N413AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200540101Intercostal · crackedRIGHT INTERCOSTAL AT FS 484 AT RBL 36 CRACKED 1 INCH LONG. (M) PERFORMED A REPAIR AT FS484, RBL 36 BY CUTTING OUT DAMAGED AREA AND INSTALLING NEW ANGLE IAW REO. (K)Mar 16, 2005 · N413AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200540099Drag Angle · crackedPASSENGER DOOR AFT DRAG ANGLE CRACKED. REPAIRED PAX DOOR AFT DRAG ANGLE IAW REO 601R-52-11-513 REV A BY CUTTING OUT (CRACKED ANGLE AND INSTALLING NEW ANGLE).Mar 15, 2005 · N413AW · Cndair CL6002B19 · Passenger/Crew Doors
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