N449AW

Service difficulty reports · 195

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 = 'N449AW' 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 A6WA200840496Stiffener · crackedPAX DOOR AFT STIFFENER ON AFT WEB 601R3117745-7 CRACKED. PAX DOOR AFT STIFFENER ON AFT WEB REPLACED IAW SRM 51-42-06 & SRM 51-42-13. (A)Jun 9, 2008 · N449AW · Cndair CL6002B19 · Passenger/Crew DoorsSDR A6WA200840494Sill · corrodedCARGO DOOR LOWER SILL FS 579-621 CORRODED. CORROSION REMOVED IAW CRJ 200 SRM 51-21-06. (A)Jun 9, 2008 · N449AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200840493Sill · corrodedSERVICE DOOR LOWER SILL PLATE CORRODED. CORROSION ON SERVICE DOOR LOWER SILL PLATE REMOVED IAW CRJ 200 SRM 51-21-06. (A)Jun 9, 2008 · N449AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200840492Attach Fitting · corrodedCARGO DOOR NET ATTCHMENT FITTING AT FS 615 LBL 40 CORRODED. CORROSION REMOVED IAW CRJ 200 SRM 51-21-06. (A)Jun 9, 2008 · N449AW · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR A6WA200840499Floorbeam · crackedCROSSBEAM AT PILOTS BULKHEAD CRACKED. CROSS BEAM REPAIRED IAW REO 601R-53-11-171 REV D SCHEME B. (A)Jun 8, 2008 · N449AW · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR A6WA200840497Attach Fitting · crackedCROSSBEAM OF PILOTS BULKHEAD OUTBOARD CLIP CRACKED FS 280 LBL 9. CLIP AT CROSS BEAM OF PILOTS BULKHEAD FS 280, LBL 9 REPLACED IAW CRJ 200 SRM 51-42-06. (A)Jun 7, 2008 · N449AW · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR A6WA200840498Floorbeam · crackedCROSSBEAM AT PILOTS BULKHEAD CRACKED. REPAIRED IAW REO 601R-53-11-171 REV D SCHEME B. (A)Jun 6, 2008 · N449AW · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR A6WA200840489Bulkhead · crackedFWD PRESSURE BULKHEAD AT FS 202, LBL 23.71, WL 69.00 IS CRACKED. FWD PRESSURE BULKHEAD AT FS 202.00, LBL 23.71 WL 69.00 REPAIRED IAW REO 601R-53-11-563. (A)Jun 6, 2008 · N449AW · Cndair CL6002B19 · Fuselage Main, BulkheadSDR A6WA200840488Bracket · crackedON RT ENGINE INLET BRACKET FOUND CRACKED AT STATION XN155.845 NEAR 5 O`CLOCK POSITION (LOOKING FWD). RT ENGINE BRACKET AT STATION XN 138.845 NEAR 5 O’CLOCK POSITION (LOOKING FWD) REPLACED IAW CRJ 200 SRM 51-42-06 & SRM 51-42-13. (A)Jun 6, 2008 · N449AW · Cndair CL6002B19 · Engine Cowling SystemSDR A6WA200840486Support Bracket · crackedHYDRAULIC SUPPORT BRACKET (P/N 601R75262-153) CRACKED IN RT MLG BAY. HYDRAULIC SUPPORT BRACKET IN RT MLG BAY IAW REO 601R-53-42-007. (A)Jun 6, 2008 · N449AW · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR A6WA200840485Support Bracket · crackedHYDRAULIC SUPPORT BRACKET (P/N 601R75262-159) CRACKED IN LT MLG BAY. HYDRAULIC SUPPORT BRACKET REPLACED IN LT MLG BAY IAW REO 601R-53-42-007. (A)Jun 6, 2008 · N449AW · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR A6WA200840504Sill · corrodedPAX DOOR LOWER SILL CORRODED FS 310.00 AND FS 349.00. CORROSION ON PAX DOOR LOWER SILL BLENDED IAW CRJ 200 SRM 51-21-06. (A)Jun 5, 2008 · N449AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200840487Sill · crackedCARGO BAY FLOOR SILL FOUND CRACKED AT FS 574.00. CARGO BAY FLOOR SILL AT FS 574.00 REPAIRED IAW REO 601R-53-61-1741. (A)Jun 5, 2008 · N449AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200840501Shaft · corrodedCREW ESCAPE HATCH OUTER HANDLE SHAFT IS CORRODED. CREW ESCAPE HATCH OUTER HANDLE SHAFT REPLACED IAW CMM 52-22-03. (A)Jun 3, 2008 · N449AW · Cndair CL6002B19 · Emergency ExitsSDR A6WA200840495Support Bracket · crackedNR 2 HYDRAULIC MANIFOLD SUPPORT BRACKET AT FS 718.00 RT CRACK FOUND IN AFT LOWER CORNER. NR 2 HYDRAULIC MANIFOLD SUPPORT BRACKET AT FS 718.00 RT REWORKED IAW REO 601R-53-62-031. (A)Jun 2, 2008 · N449AW · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR A6WA200840417Pump · failedIN FLIGHT RECEIVED SPOILERONS FAULT STATUS MESSAGE AND INBOARD GROUND SPOILER FAULT STATUS MESSAGE. AFTER HYDRAULIC PUMP 2B REPLACEMENT REF MEL 182321/3 OPS TESTED SPOILER SYS PER AMM 27-60-00 NO DEFECTS NOTED. PERFORMED SYSTEM BITE ON SECU NR 1 AND NR 2 ALLMay 14, 2008 · N449AW · Cndair CL6002B19 · Hydraulic Pump (Electric/Engine), MainSDR A6WA200840380Buss · shortedRECIEVED MASTER CAUTIOIN AC SERVICE BUSS, RAN QRH AND CONTINUED IN ARI AND ON GROUND, MESSAGE IS INTERMITTENT, POSSIBLE ELECTRICAL ODOR IN COCKPIT, PULLED CIRCUIT BREAKER PANEL 2, S2. R&R ACFT SERVICE BUS SENSE RELAY K5XD REF WDM 24-50-00. OPS CHECK GOOD IAWMay 3, 2008 · N449AW · Cndair CL6002B19 · AC Power Distribution SystemSDR A6WA200840366Windshield · crackedFIRST OFFICERS WINDSHIELD SHATTERED (OUTER PANE) ON CLIMBOUT AT 9000 FT COMPLIED WITH QRH AND LANDED WITHOUT INCIDENT IN RDU. REMOVED AND REPLACED FIRST OFFICER`S WINDSHIELD IAW 56-11-01, OPS CHECK GOOD, LEAK CHECK GOOD. (A)Apr 28, 2008 · N449AW · Cndair CL6002B19 · Flight Compartment WindowsSDR A6WA200840484Support Bracket · crackedHYDRAULIC SUPPORT BRACKET (P/N 601R75262-157) CRACKED IN RT MLG BAY. HYDRAULIC SUPPORT BRACKET REPLACED IN RT MLG BAY IAW REO 601R-53-42-007. (A)Apr 6, 2008 · N449AW · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR A6WA200840483Intercostal · crackedINTERCOSTAL AT FS 484.0, WL 72.0, LBL 36 IN CRACKED. INTERCOSTAL REPAIRED IAW REO 601R-53-41-059. (A)Apr 6, 2008 · N449AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200840482Intercostal · crackedINTERCOSTAL AT FS 484.0, WL 72.0, RBL 36.0 IS CRACKED. INTERCOSTAL REPAIRED IAW REO 601-53-41-059. (A)Apr 6, 2008 · N449AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200840481Intercostal · crackedINTERCOSTAL FS 484.0 WL 72.0, LBL 27.0 ANGLE IS CRACKED. CORRECTIVE ACTION IN PROGRESS. (A)Apr 6, 2008 · N449AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200840067Ahrs · malfunctionedCOMPLETE NR 1 AHRS FAILURE IN FLIGHT. COMPLIED WITH QRH. NO ALTITUDE OR COMPASS INFORMATION. AFTER REVERSIONARY SLELECTION TO NR 2, ALL DISPLAY INFO WAS NORMAL ON CAPTAINS SIDE. (K)Feb 11, 2008 · N449AW · Cndair CL6002B19 · Integrated Flight SystemSDR A6WA200840004Flap · failedFLAPS FAILED ON RETRACTION AFTER LANDING. RT FLAP INDICATES -0- DEGREES, LT FLAP INDICATES 22 DEGREES. C/W FLAP RESET, FLAP FAIL DID NOT CLEAR. FOUND FLAPS COVERED WITH ICE AND SNOW, PUT AC IN HANGAR TO THAW. PERFORMED RESET IAW AWAC SUPPLEMENT 98-018B AND Jan 1, 2008 · N449AW · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR A6WA200740613Ballast · faultyELECTRICAL SMOKE ODOR IN AREA OF ROW 3, AT GATE NO PASSENGERS ONBOARD. IDENTIFIED BAD BALLAST FOR 4DF CEILING LIGHT. REMOVED AND REPLACED CEILING LIGHT 4DF POWER UNIT/DIMMER (111B) IAW CRJ200 AMM 33-21-04. OPS CHECK GOOD. (M)Nov 9, 2007 · N449AW · Cndair CL6002B19 · Passenger Compartment LightingSDR A6WA200740093Solenoid · leakingFUEL LEAK AND RUNNING DOWN BELLY SURFACE UNDER TAIL. FOUND APU FUEL SOLENOID LEAKING DRAINING OUT FUSELAGE BELLY DRAIN. DEACTIVATED APU, NO LEAK NOTED, REMOVED AND REPLACED FUEL SOLENOID AND O-RING AT LOWER ELBOW FITTING IAW AMM 49-31, NO LEAKS NOTED. (K)Mar 7, 2007 · N449AW · Cndair CL6002B19 · APU Engine Fuel and ControlSDR A6WA200740039Flap System · jammedON APPROACH INTO YOW, FLAPS FAIL CAS MESSAGE FAILED AT 0 DEGREES, COMPLIED WITH QRH. LANDED AT APPROXIMATELY 40,600 LBS, CREW DID NOT CALL IN DISCREPANCY. NO HES/RTO INSPECTION REQUIRED. INTERROGATED FECU, FECU SHOWS FLAP FAIL WAS DUE TO JAM ON LEFT WING. Jan 31, 2007 · N449AW · Cndair CL6002B19 · Trailing Edge FlapsSDR A6WA200740036Indicator · malfunctionedDURING TAKEOFF STANDBY INDICATED AIRSPEED INDICATED 0 TO 80 KNOTS. ABORTED TAKEOFF. MAX BTMS READINGS WERE 4444 WEIGHT = 43,000 LBS IAS NR 1 AND NR 2 INDICATED NORMAL. REMOVED AND REPLACED STANDBY ALT/IAS IAW 34-12-01, PERFORMED PITOT STATIC LEAK CHECK, OPSJan 22, 2007 · N449AW · Cndair CL6002B19 · Altimeter, Barometric/EncoderSDR A6WA200740030Flap System · malfunctionedWHEN SELECTING FLAPS 30 DEGREES ON APPROACH, FLAP FAIL CAUTION MESSAGE ILLUMINATED, FLAPS REMAINED AT 20 DEGREES. LOCAL MAINTENANCE VISUAL INSPECTED FLAPS RESET C/B`S PER AMM SUPPLEMENT 98-018A, FLAPS OPERATE NORMALLY. PLACED ON 72 HOUR WATCH. (M)Jan 17, 2007 · N449AW · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR A6WA200640412Bpsu · faultyFLAPS FAILED AT ZERO DEGREES WHEN SELECTED ON APPROACH. CROSS REFERENCE: A6WA200740030 - FOUND EVIDENCE OF WATER IN RT NR 3 AND NR 4 FLEX DRIVE SHAFT, CLEANED FLEX DRIVE SHAFTS NR 3 AND NR 4. (K) WHEN SELECTING FLAPS FROM 8 DEGREES TO 20 DEGREES, A FLAP CAUTDec 7, 2006 · N449AW · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR A6WA200640362Windshield · crackedFIRST OFFICERS WINDSCREEN IS CRACKED, FL220, CRUISE, WINDOW HEAT ON. REPLACED FIRST OFFICERS WINDSHIELD IAW CRJ AMM 56-10-00, OPS TEST GOOD. (M)Oct 10, 2006 · N449AW · Cndair CL6002B19 · Flight Compartment WindowsSDR A6WA200640344Connector · dirtyDOOR MOTOR CONTINUOUSLY RUNNING WITH DOOR SHUT. INSPECTED AND CLEANED PASSENGER DOOR ASSIST MOTOR CONNECTOR IAW CH 52. OPS CHECK GOOD AT THIS TIME.Sep 5, 2006 · N449AW · Cndair CL6002B19 · Door System WiringSDR A6WA200640301Lamp · inoperativeEMERGENCY FLOOR LIGHTING FORWARD SECTION DOES NOT ILLUMINATE. FOUND ELECTRICAL CONNECTIONS SWAPPED. RECONNECTED ELECTRICAL CONNECTIONS. TEST CARRIED OUT PER AMM 33-51-00-710-801 SATISFACTORILY. (M)Jul 27, 2006 · N449AW · Cndair CL6002B19 · Emergency LightingSDR A6WA200640286Skin · corrodedFOUND LEFT WING PLANK ACCESS CUTOUT FLANGE AT FUEL PANEL 540FB, HOLE NR 8 AT WS 139 HAS MINOR CORROSION APPROX .003 INCH DEEP ON 90 PERCENT OF CIRCUMSTANCE. REPAIRED THE LEFT WING LOWER PLANK PANEL CUTOUTS IAW BSC EO 601R-57-9567A. (M)Jul 18, 2006 · N449AW · Cndair CL6002B19 · Wing, Plate/SkinSDR A6WA200640285Skin · corrodedFOUND LEFT WING PLANK ACCESS CUTOUT FLANGE AT FUEL PANEL 510AB HOLE NR 2 AT WS 11.00 HAS MINOR CORROSION APPROX .002 INCH DEEP ON 60 PERCENT OF CIRCUMFERENCE. MAINTENANCE REPAIRED THE LEFT WING PLANK FUEL PANEL CUTOUT IAW BSC EO 601R-57-9567A. (M)Jul 18, 2006 · N449AW · Cndair CL6002B19 · Wing, Plate/SkinSDR A6WA200640283Floorbeam · crackedFOUND LEFT SIDE FS 621 FLOORBEAM ANGLE CRACKED APPROX 1.3 INCH LONG. MAINTENANCE REMOVED DAMAGED PORTION OF LT SIDE FS 621 FLOOR SUPPORT ANGLE REO 601R-53-61-117. IAW REO 601R-53-61-117 REV C. (M)Jul 17, 2006 · N449AW · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR A6WA200640282Floorbeam · crackedFOUND RIGHT SIDE FS 621 FLOORBEAM ANGLE CRACKS APPROX .7 INCH LONG. MAINTENANCE REMOVED DAMAGED PORTION OF RIGHT SIDE 621 FS FLOOR SUPPORT ANGLE IAW REO 601R-53-61-117 COMPLETED REPAIR OF RIGHT FS 621 ANGLE USING 2024 T3 .090 INCH P/N 601R53-61-117-2 AND 601RJul 17, 2006 · N449AW · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR A6WA200640300Handle · lack of lubeCREW ESCAPE HATCH OUTER HANDLE RELEASE BUTTON WON`T DEPLOY. CLEANED DIRT AND DEBRIS FROM RELEASE BUTTON AND OUTER HANDLE AND LUBED OUTER HANDLE AND RELEASE BUTTON. (M)Jul 16, 2006 · N449AW · Cndair CL6002B19 · Emergency ExitsSDR A6WA200640284Angle · crackedFOUND FS 625 LEFT OBLIQUE ANGLE IS CRACKED APPROX .75 INCH. MAINTENANCE REPLACED FS 625 LT OBLIQUE ANGLE P/N 601-35012-51 WITH NEW IAW CRJ SRM 51-42-06. (M)Jul 14, 2006 · N449AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200640173Generator · malfunctionedGEN NR 2 OFFLINE 15 SECONDS AFTER TURNING IT ON, WILL NOT RESET. (M)May 1, 2006 · N449AW · Cndair CL6002B19 · AC Generation SystemSDR A6WA200540225Check Valve · malfunctionedLEFT ENGINE OIL PRESSURE MASTER WARNING IN FLIGHT. REMOVED LEFT ENGINE OIL REPLENISHMENT CHECK VALVE. INSTALLED CHECK VALVE TAGGED REPAIR, P/N 2810044-101, S/N 972. ADDED 5 QUARTS TO LEFT ENGINE. OIL TANK SERVICED TO 5 1/2 FULL RED AMM 79-12-13. NO LEAKS Jul 1, 2005 · N449AW · Cndair CL6002B19 · Engine Oil System (Airframe Furnished)SDR A6WA200540024Warning System · malfunctionedUPON GEAR RETRACTION, NOSE DOOR END GEAR DISAGREE WARNING MESSAGE ILLUMINATED. CYCLED NLG WITH LINKS ATTACHED OPS CHECK GOOD OK FOR RETURN TO SERVICE IAW. (K)Jan 28, 2005 · N449AW · Cndair CL6002B19 · Landing Gear Position and WarningSDR A6WA200540007Skin · gougedFOUND DENT/GOUGE IN LEFT SIDE AFT FUSELAGE SKIN AT FS 612, BETWEEN STRINGERS 24L AND 25L. MEASURES 2 INCH BY 1.8 INCH BY .040 INCH DEEP. PERFORMED A MAJOR REPAIR B4 CUTTING AWAY DAMAGED SKIN AND INSTALLING PN EXTERNAL DOUBLER IAW CRJ SRM 53-00-31 REPAIR NR 1Jan 2, 2005 · N449AW · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR A6WA200540006Intercostal · crackedFOUND RIGHT SIDE FS 621-625.3 INTERCOSTAL AT STRINGER 14R IS CRACKED IN RADIUS .6 INCH LONG. REMOVED CRACKED INTERCOSTAL AND REPLACED WITH NEW INTERCOSTAL IAW CRJ200 SRM 51-42-06. (M)Dec 26, 2004 · N449AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200440145Computer · malfunctionedON COMMAND OF AUTOPILOT DISENGAGEMENT, PITCH CONTROL DID NOT DISENGAGE FOR APPROX 5-10 SECONDS.Oct 10, 2004 · N449AW · Cndair CL6002B19 · Autopilot System
Back to N449AW