N423AW

Service difficulty reports · 165

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 = 'N423AW' 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 A6WA201240760Engine · malfunctionedAPPLICATION OF TAKE OFF POWER, FELT VIBRATION IN AIRFRAME FOLLOWED BY LT ENGINE LOW OIL PRESSURE CAS MESSAGE. ABORTED TAKE OFF AT LESS THAN 20 KTS. PULLED ACFT OFF RUNWAY, NOTICED ITT WAS FULL SCALE AND N1 AND N2 VIB MESSAGES APPEARED. LEFT ENGINE REPLACEMEAug 3, 2012 · N423AW · Cndair CL6002B19 · Engine (Turbine/Turboprop)SDR A6WA201240731Shaft · crackedSERVICE DOOR OUTER HANDLE WILL NOT STOW FROM OUTSIDE OR INSIDE. INSPECTED SERVICE DOOR FOUND OUTER HANDLE SHAFT CRACKED. DOOR OPERATES PROPERLY FORM INSIDE REF LP 228429/4 FOR MEL.Jul 28, 2012 · N423AW · Cndair CL6002B19 · Service DoorsSDR A6WA201240057Actuator · malfunctionedON DEPARTURE, WHILE GEAR WAS IN TRANSIT, RECEIVED INBD ANTI-SKID MESSAGE, FOLLOWED BY GEAR DISAGREE WARNING. MESSAGE CLEARED WITHIN 20 SECONDS OF GEAR UP SELECTION. HAD NO RED GEAR INDICATION. BOTH MESSAGES CLEARED WITHOUT CREW ACTIONS. NO FURTHER INDICATIJan 6, 2012 · N423AW · Cndair CL6002B19 · Landing Gear ActuatorSDR A6WA201240055Priority Valve · malfunctionedAT 400 FT GEAR INTRANSIT, INBD AS MESSAGE APPEARED THEN GEAR DISAGREE WITHIN 10 SECONDS OF INITIAL GEAR UP SELECTION. NO RED INDICATIONS. BOTH MSGS CLEARED WITHOUT CREW ACTION. NORMAL EXTENSION AND NORMAL LANDING. NO INDICATIONS NOW. TROUBLESHOT AND R & RJan 5, 2012 · N423AW · Cndair CL6002B19 · Landing Gear Retraction/Extension SystemSDR A6WA201141148Handle · defectiveSERVICE DOOR HARD TO OPEN AND CLOSE FROM OUTSIDE. REMOVED AND REPLACED OUTER SERVICE DOOR HANDLE, CLEANED DOOR SEAL AND FRAME IAW AMM 52-41-03, OPS CHECK GOOD.Dec 29, 2011 · N423AW · Cndair CL6002B19 · Service DoorsSDR A6WA201141064Scissor Link · disconnectedON TAKE OFF RECEIVED A GEAR DISAGREE, NOSE GEAR WANRING WOW CAUTION AND NWS CAUTION, COMPLIED WITH QRH ALL MESSAGES CLEARED EXCEPT FOR WOW. GROUND CREW REPORTED SCISSORS DISCONNECTED. PERFORMED GVI OF NOSE GEAR, NOSE WHEEL WELL, AND NOSE TIRES. INSPECTED NODec 3, 2011 · N423AW · Cndair CL6002B19 · Nose/Tail Landing Gear Attach SectionSDR A6WA201140610Seal · leakingCLIMBING THROUGH FL 250, RECEIVED CABIN ALTITUDE CAUTION MESSAGE FOLLOWED IMMEDIATELY BY CABIN ALTITUDE WARNING. INITIATED TO FL 100 PERFORMED ALL APPROPRIATE CHECKLIST. DECLARED EMERGENCY AND LANDED. TROUBLESHOT SYS TO PRIMARY OUTFLOW VALVE BLEEDING AIR WHJul 19, 2011 · N423AW · Cndair CL6002B19 · Cargo/Baggage DoorsSDR A6WA201140820Bracket · crackedHYDRAULIC BRAKE SYSTEM NR 3 BRAKE ACCUMULATOR FWD BRACKET CRACKED. R & R BRACKET IAW SRM 51-42-06.Jul 14, 2011 · N423AW · Cndair CL6002B19 · Fuselage, Equipment Attach FittingsSDR A6WA201140822Seat Track · corrodedSEAT TRACK LBL 27, FS 559+112 TO 621 HAS CORROSION AT THE NUTPLATE HOLES. REMOVED AND FABRICATED SEAT TRACK . INSTALLED NEW SEAT TRACK AT IAW REO 601R-53-61-3778, REV.Jul 13, 2011 · N423AW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR A6WA201140823Bracket · crackedRT WHEEL WELL INBD OTBD HYD LINE BRACKETS 2 EA CRACKED. R & R WITH 2 EA SERVICEABLE BRACKETS IAW SRM 51-42-06.Jul 10, 2011 · N423AW · Cndair CL6002B19 · Fuselage, Equipment Attach FittingsSDR A6WA201140825Rib · crackedRT MLG BATT RIB CRACKED. REPAIR IAW REO 601R-57-51-046.Jul 10, 2011 · N423AW · Cndair CL6002B19 · Wing, Rib/BulkheadSDR A6WA201140821Cargo Track · corrodedCARGO TRACK CORRODED. REMOVED UNSERVICEABLE AND INSTALL SERVICEABLE.Jul 9, 2011 · N423AW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR A6WA201140826Web · crackedPAX DOOR AFT STAIRCASE WEB CRACKED AT SECOND STEP CUTOUT DAMAGED AREA ON AFT STAIRCASE THEN FABRICATED AND INSTALLED NEW PARTS IAW REO 601R-52-11-702, REV C.Jul 8, 2011 · N423AW · Cndair CL6002B19 · Passenger/Crew DoorsSDR A6WA201140824Bracket · crackedLEFT WHEEL WELL INBD HYDRAULIC LINE BRACKET CRACKED. REPLACED WITH SERVICEABLE BRACKET IAW SRM 51-42-06.Jul 7, 2011 · N423AW · Cndair CL6002B19 · Fuselage, Equipment Attach FittingsSDR A6WA201040772Bulkhead · crackedCRACK INDICATION AT WL 58.70 AND RBL9 REO601R5341260 REV E TO BE ACCOMPLISHED IAW AWAC JC 4MFG50672 AND 601R5341609 REV B AS NEEDED. REPAIRED CRACK ON FS 559 BULKHEAD AT WL 58.70 AND RBL 9 BY INCOPR OF REO 601R-53-41-260 REV E AND REO 601R-53-41-609, REV B7 DOct 10, 2010 · N423AW · Cndair CL6002B19 · Wing, Rib/BulkheadSDR A6WA201040829Bracket · wornSTUB FAIRING (RT) ATTACH BRACKET ON WING IS WORN. R & R RT STUB FAIRING ATTACH BRACKET ON WING IAW SRM 51-42-21.Oct 9, 2010 · N423AW · Cndair CL6002B19 · Wing Miscellaneous StructureSDR A6WA201040771Skin · dentedRT WING L/E MIDDLE SECTION, IS DENTED AT THE CTR. REFORMED DENT TO CONTOUR BY PUSHING DENT IAW SRM 57-41-31. DENT MEASURES 1.5 IN L X 1.0 IN W X .004 IN.Oct 8, 2010 · N423AW · Cndair CL6002B19 · Wing, Plate/SkinSDR A6WA200940755Actuator · malfunctionedUNCOMMANDED RUDDER DEFLECTION IN FLIGHT, YAW DAMPNER 1 DISENGAGED. NO FURTHER UNCOMMANDED MOVEMENTS. R & R LT YAW DAMPNER LINEAR ACTUATOR. RIGGING AND OPS TEST GOOD REF AMM 22-22-01.Nov 11, 2009 · N423AW · Cndair CL6002B19 · Autopilot SystemSDR A6WA200940546Fcu · malfunctionedENG NR 1 W/N GO ABOVE 71.3 PERCENT N1 ON TAKEOFF POWER. ABORTED TAKEOFF BELOW 80 KTS, BRAKE TEMPS 2-2-2-2. SELECTED ENG SPEED CONTROL SYS OFF. C/W ENG RUNS WITH CREW ASSISTANCE BOTH ENGINES ENG RUNS WITH CREW ASSISTANCE BOTH ENGINES MADE AND SUSTAINED POWERSep 14, 2009 · N423AW · Cndair CL6002B19 · Engine (Turbine/Turboprop)SDR A6WA200940472Attach Fitting · crackedCLIP AT FS 484.00, LBL 27.00 CRACKED. CLIP AT FS 484.00, LBL 27.00, REPLACED IAW SRM 200 51-42-21 AND 51-42-06. (K)Aug 7, 2009 · N423AW · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR A6WA200940468Attach Fitting · crackedUNDERFLOOR FS 484.00 AND LBL 36.00 CLIP CRACKED. UNDER FLOOR FS 484 AND LBL 36 REPAIRED IAW REO 601R-53-41-059 REV A. (K)Aug 5, 2009 · N423AW · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR A6WA200940457Bracket · crackedLT TAIL PIPE FAIRING FWD BRACKET OF COVER ASSY CRACKED. LT TAIL PIPE FAIRING FWD BRACKET OF COVER ASSY. REPLACED IAW SRM 51-42-06. (K)Aug 4, 2009 · N423AW · Cndair CL6002B19 · Engine Collector/Tailpipe/NozzleSDR A6WA200940456`Seat · crackedBACKREST ASSY 210 LT AND 230 RT OF CO-PILOT SEAT CRACKED. BACKREST ASSY 210 LT AND 230 RT OF COPILOT SEAT REPLACED IAW SRM 51-42-10. (K)Aug 4, 2009 · N423AW · Cndair CL6002B19 · Flight Compartment EquipmentSDR A6WA200940471Angle · crackedPAX DOOR ASSIST MOTOR LOWER ANGLE (WHEN DOOR OPEN) CRACKED .500 INCH. PAX DOOR ASSIST MOTOR LWR ANGLE (WHEN DOOR OPEN) REPLACED IAW SRM 51-42-06. (K)Aug 4, 2009 · N423AW · Cndair CL6002B19 · Passenger/Crew DoorsSDR A6WA200940463Seal · crackedRT FLIGHT SPOILER SURFACE OTBD METAL SEAL CRACKED. RT FLIGHT SPOILER SURFACE OTBD METAL SEAL REPLACED IAW SRM 51-42-06 AND 51-42-21. (K)Aug 4, 2009 · N423AW · Cndair CL6002B19 · SpoilersSDR A6WA200940466Bulkhead · crackedFWD PRESSURE BULKHEAD IS CRACKED AT FS 202.75, LBL27.5, WL 69.00 AND QTY 1 ELONGATED HOLE EXISTS IN WEB AND STIFFNER FS 202.75, LBL 9.00, WL 69.00. FWD PRESSURE BULKHEAD REPAIRED AT FS 202.75, WL 69.00 AND QTY 1 ELONGATED HOLE REPAIRE IN WEB AND STIFFNER FS 2Aug 2, 2009 · N423AW · Cndair CL6002B19 · Fuselage Main, BulkheadSDR A6WA200940460Bracket · crackedBRACKET CRACKED AT FS 621, AFT OF PRESSURE BULKHEAD, NEAR STR 14 LT BRACKET AT FS 621, AFT OF PRESSURE BULKHEAD, NEAR STR 14 LT REPAIRED IAW REO 601R-53-61-100 AND REO 601R-53-61-422. (K)Jul 31, 2009 · N423AW · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR A6WA200940461Bracket · crackedBRACKET CRACKED AT FS 621, AFT OF PRESSURE BULKHEAD, NEAR STR 14 RT BRACKET AT FS 621 AFT OF PRESSURE BULKHEAD, NEAR STR 14 RT REPAIRED IAW REO 601R-53-61-100 AND REO 601R-53-61-422. (K)Jul 31, 2009 · N423AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200940454Floorbeam · crackedUPPER AFT ANGLE AT FS 280.00, LBL 11.00, WL 72 IS CRACKED. UPPER AFT ANGLE AT FS 280.00, LBL 11.00, WL 72 REPAIRED IAW REO 601R-53-11-138. (K)Jul 30, 2009 · N423AW · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR A6WA200940453Retainer · corrodedMAIN AVIONICS DOOR SEAL RETAINERS CORRODED. MAIN AVIONICS DOOR SEAL RETAINERS REPLACED IAW SRM 51-42-06. (K)Jul 30, 2009 · N423AW · Cndair CL6002B19 · Electrical/Electronic Compartment DoorsSDR A6WA200940470Angle · crackedPRESSURE BULKHEAD LOWER FRAME CAP ANGLE IS CRACKED IN THE RADIUS. PRESSURE BULKHEAD LOWER FRAME CAP ANGLE REPAIRED IAW REO 601R-53-41-1022 AND REO 601R-53-41-260, REV C. (K)Jul 30, 2009 · N423AW · Cndair CL6002B19 · Fuselage Main, BulkheadSDR A6WA200940458Floor Support · crackedFLOOR EDGE MEMBER CRACKED AT FS 605, LBL 45, WHERE RIVET ATTACHED TO FLOORBEAM. (CRACK LENGTH .250 INCH) FLOOR EDGE MEMBER REPAIR AT FS 605, LBL 45 IAW REO 601R-53-61-433. (K)Jul 28, 2009 · N423AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200940465Skin · corrodedMAIN COMPARTMENT DOOR CUT-OUT INTERNAL SKIN FWD AND AFT SIDE CORRODED. MAIN AVIONIC COMPARTMENT DOOR CUT-OUT INTERNAL SKIN FWD AND AFT SIDE REPAIRED IAW REO 601R-53-21-676, REV A. (K)Jul 28, 2009 · N423AW · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR A6WA200940464Sill · corrodedCARGO BAY FLOOR SILL IS CRACKED AT FS 574.00, LBL 44.00, WL 72.00, CRACK LENGTH IS .350". CARGO BAY FLOOR SILL FS 574.00, LBL 44.00, WL 72.00, REPAIRED IAW REO 601R-53-61-1741. (K)Jul 28, 2009 · N423AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200940469Bulkhead Web · crackedAFT PRESSURE BULKHEAD WEB IS CRACKED ABOVE CARGO DOOR TRACK AT F/S 621.0, LBL 27, WL 130, REO 601R-53-61-1541 REV B CARRIED OUT. (K)Jul 28, 2009 · N423AW · Cndair CL6002B19 · Fuselage Main, BulkheadSDR A6WA200940459Sill · corrodedCARGO DOOR SILL AT LBL 45 CORRODED FROM FS 574 TO 621 AROUND STOW PLATE ATTACHING HOLES. CORROSION ON CARGO DOOR SILL AT LBL 45 FROM FS 574 TO FS 621 AROUND STOW PLATE ATTACHING HOLES, REMOVED IAW SRM 51-21-06. (K)Jul 27, 2009 · N423AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200940462Seat Track · corrodedLT FLOOR SEAT RAIL CORRODED BTW FS 349.00 AND FS 409.00, LBL 9.0 LT FLOOR RAIL REPLACED BTW FS 349.00 AND FS 409.00, LBL 9.00 IAW AMM TASK 53-01-400-802. (K)Jul 27, 2009 · N423AW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR A6WA200940455Crossbeam · crackedLOWER RADIUS OF CROSSBEAM AT FS 280.00, LBL 9.00, WL 72.00 IS CRACKED. REPAIR CARRIED OUT IAW REO 601R-53-11-171. (K)Jul 26, 2009 · N423AW · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR A6WA200940271Pressure Blkhd · crackedMWC 136501-2 - AFT PRESSURE BLKHD WEB AT FS 621 LINTEL LOCATION IS CRACKED. AFT PRESSURE BULKHD FS 621 REPAIRED IAW REO 601R-53-61-1230, REV D. (K)May 22, 2009 · N423AW · Cndair CL6002B19 · Fuselage Main, BulkheadSDR A6WA200940103Display · malfunctionedCAPT PFD WENT BLANK ON INITIAL TAKEOFF ROLL. ABORTED TAKEOFF PRIOR TO 80 KNOTS. BRAKE TEMP NORMAL. PERFORMED OPS TEST CHECK OUT IAW AMM 24-25-00-710-801. NO DEFECTS NOTED AT THIS TIME ACFT OK FOR SERVICE. (K)Feb 11, 2009 · N423AW · Cndair CL6002B19 · Central DisplaySDR A6WA200840073Structure · damagedDAMAGE ON LT FUSALAGE AT STA 220. REPAIRED CUTOUT ON LT FUSELAGE IAW REO 601R-53-11-1332. (K)Jan 29, 2008 · N423AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200840072Skin · tornPAX DOOR STAIR HAVE APPROX 1.5 IN X 1.5 IN TEAR IN FWD FACE SKIN AT FWD HANDRAIL DOWN STOP BRACKET POINT. REPAIRED IAW REO 601R-52-11-702, REV A. (K)Jan 28, 2008 · N423AW · Cndair CL6002B19 · Passenger/Crew DoorsSDR A6WA200740416Bulkhead · crackedFORWARD PRESSURE BULKHEAD AT FS 202.75 CRACKED AT HYDRAULIC SYS NR 3 RT IB BRAKE FITTING LT LOWER SIDE. (K) MAINTENANCE REPAIRED BULKHEAD IAW BOMBARDIER SERVICES CORP EO 601R-53-12466. (M)Jul 25, 2007 · N423AW · Cndair CL6002B19 · Fuselage Main, BulkheadSDR A6WA200740399Floor Support · crackedLT FS 280 FLOOR SUPPORT CLIPS CRACKED APPROX .2 INCH LONG AT LBL 9 IB AND OB LOCATIONS. (K) MAINTENANCE REMOVED AND INSTALLED SERVICEABLE CLIPS TWO P/N 601R3113-57 IAW BSC STANDARD REPAIR 601R-53-0057A AND CRJ 200 SRM 51-42-21 AND 51-42-13. (M)Jul 15, 2007 · N423AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200740398Frame · crackedFS 280 FRAME CRACKED APPROX 2 INCH LONG OB AT RBL 9, BELOW W/L 73. (K) MAINTENANCE REMOVED DAMAGED SECTION AND INSTALLED REPAIR IAW BOMBARDIER REO 601R-53-11-171. (M)Jul 15, 2007 · N423AW · Cndair CL6002B19 · Fuselage Main, FrameSDR A6WA200740397Floor Support · crackedRT FS 280 FLOOR SUPPORT CLIPS CRACKED APPROX .2 INCHES LONG AT RBL 9, IB AND OB LOCATIONS. (K) MAINTENANCE REMOVED AND REPLACED SUPPORT CLIPS IAW BSC STANDARD REPAIR 601R-53-0057A AND CRJ 200 SRM 51-42-21. (M)Jul 15, 2007 · N423AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200740396Channel · crackedU-CHANNEL AT BOTTOM OF CARGO DOOR FWD ROLLER TRACK IS CRACKED .2500 INCH LONG. (K) MAINTENANCE REMOVED AND REPLACED U-CHANNEL IAW CRJ 200 SRM 51-42-06. (M)Jul 15, 2007 · N423AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200740395Angle · crackedFS 625.0 INTERCOSTAL OBLIQUE ANGLE (UPPER) CRACKED. (K) MAINTENANCE REMOVED AND REPLACED INTERCOSTAL P/N 601-35012-51 IAW BOMBARDIER REO 601R-53-61-422. (M)Jul 15, 2007 · N423AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200740394Angle · crackedLT FS 484 INTERCOSTAL PREVIOUS REPAIR ANGLE AT LBL 36 CRACKED APPROX .1INCH LONG UNDER CABIN FLOOR PANEL 261DLF. (K) MAINTENANCE REMOVED CRACKED ANGLE, FABRICATED AND INSTALLED NEW ANGLE IAW BSC STANDARD REPAIR 601R-53-0030A AND REO 601R-53-41-059. (M)Jul 15, 2007 · N423AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200740393Intercostal · crackedRT FS 484 INTERCOSTAL CRACKED AT RBL 36 APPROX .1 INCH LONG UNDER CABIN FLOOR PANEL 262DRH. (K) MAINTENANCE REMOVED CRACKED ANGLE, FABRICATED AND INSTALLED NEW ANGLE IAW BSC STANDARD REPAIR 601R-53-0030A AND REO 601R-53-41-059. (M)Jul 15, 2007 · N423AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
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