N465AW

Service difficulty reports · 170

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 = 'N465AW' 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 A6WA200740424Angle · crackedLT 484 ANGLE IS CRACKED AT LBL 36 APPROX .5 INCH LONG. (K) MAINTENANCE REPAIRED ANGLE IAW BOMBARDIER REO 601R-53-41-059 REV A AND BOMBARDIER STANDARD REPAIR 601R-53-0030A. (M)Jul 27, 2007 · N465AW · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR A6WA200740423Angle · crackedLT 484 ANGLE IS CRACKED AT LBL 27 APPROX .5 INCHES LONG. (K) MAINTENANCE REPAIRED ANGLE IAW BOMBARDIER REO 601R-53-41-059 REV A AND BOMBARDIER STANDARD REPAIR 601R-53-0029B. (M)Jul 27, 2007 · N465AW · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR A6WA200740422Angle · crackedRT 484 ANGLE IS CRACKED AT RBL 27 APPROX 1 INCH LONG. (K) MAINTENANCE REPAIRED ANGLE IAW BOMBARDIER REO 601R-53-41-059 REV A AND BOMBARDIER STANDARD REPAIR 601R-53-0029B. (M)Jul 27, 2007 · N465AW · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR A6WA200740421Angle · crackedRT 484 ANGLE IS CRACKED AT RBL 36 APPROX .25 INCH LONG. (K) MAINTENANCE REPAIRED ANGLE IAW BOMBARDIER REO 601R-53-41-059 REV A AND BOMBARDIER STANDARD REPAIR 601R-53-0030A. (M)Jul 27, 2007 · N465AW · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR A6WA200740419Channel · crackedHYDRAULIC PRESSURE TRANSDUCER HAT CHANNEL CRACKED APPROX .1 LONG IN LT MLG WHEEL WELL CEILING. (K) MAINTENANCE REMOVED AND REPLACED HAT CHANNEL P/N 601R75262-159 IAW CRJ 200 SRM 51-42-06. (M)Jul 27, 2007 · N465AW · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR A6WA200740418Angle · crackedRT OBLIQUE ANGLE AT STA 625.00 HAS A .5 INCH CRACKED IN RADIUS. (K) MAINTENANCE INSTALLED NEW ANGLE IAW CRJ SRM 51-42-06. (M)Jul 26, 2007 · N465AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200740417Angle · crackedLT OBLIQUE ANGLE AT STA 625 HAS .5 INCH CRACKED IN RADIUS. (K) MAINTENANCE INSTALLED NEW ANGLE CRJ SRM 51-42-06. (M)Jul 26, 2007 · N465AW · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR A6WA200740224Unknown · unknownFLAPS FAIL CAUTION MESSAGE INFLIGHT AFTER FLAP 8 TAKEOFF AFTER FLAP RETRACTION ALT, MOVED FLAP HANDLE TO ZERO, FLAPS STAYED AT 8. AIRSPEED 170 KTS OAT 21 DEGREES C. PERFORMED FLAPS FAIL CHECKLIST AND FLAPS 8 LANDING. TOUCHDOWN 164 KTS AT 100/MIN. COMPLIED May 11, 2007 · N465AW · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR A6WA20074022Unknown · unknownFLAPS FAIL CAUTION MESSAGE AND FLAPS FAIL AT 0 DEGREES. PERFORMED FLAP RESET PROCEDURE IAW AWAC SUPPLEMENT 98-018B STEPS 1.3 AND 1.4, FLAPS RESET. AIRCRAFT RELEASED FOR SERVICE, NO SDU LIGHTS ILLUMINATED AT THIS TIME. (M)May 1, 2007 · N465AW · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR A6WA200740225Bracket · crackedLEFT HYDRAULIC TRANSDUCER BRACKET, P/N 601R75262-159, CRACKED APPROXIMATELY .1 INCH LONG IN LEFT MLG WHEEL WELL CEILING. INSTALLED NEW BRACKET IAW CRJ SRM 51-42-06. (M)Apr 15, 2007 · N465AW · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR A6WA200740154Door · openPERFORMED AIR RETURN AFTER N1 FAN VIBRATION ON NR 2 ENGINE ASSOCIATED WITH AIRFRAME VIBRATION. VERTICAL DESCENT RATE LESS THAN 360 FPM AT TOUCHDOWN. LANDING WEIGHT 51,000 LBS. OVERWEIGHT LANDING INSPECTION NOT REQUIRED. RT ENGINE UPPER TRANSLATING COWL OPEMar 25, 2007 · N465AW · Cndair CL6002B19 · Nacelle/Pylon, Main FrameSDR A6WA200740118Flap · malfunctionedAFTER TAKEOFF WHILE RETRACTING FLAPS FROM 20 DEGREES. COMPLIED WITH QRH, FLAPS FAIL CAUTION MESSAGE ON ED1. COMPLIED WITH SUPPLEMENT 98-018A, NO FLAP TWISTING, SKEWING OR DEFORMATION NOTED. RESET CIRCUIT BREAKER ONCE, MESSAGE CLEARED, FLAPS OPERATE NORMALLYMar 12, 2007 · N465AW · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR A6WA200740032Element · malfunctionedANTI-ICE DUCT MESSAGE WITH DUCT FAIL IN SWITCH LIGHT WITH WING ANTI-ICE LIGHT ON. COMPLIED WITH QRH, SELECTED 14TH STAGE BLEEDS AND WING ANTI-ICE OFF. MESSAGE CLEARED. WHEN 14TH STAGE BLEEDS SELECTED ON AND WING ANTI-ICE TO STANDBY, MESSAGE DID NOT REAPPEARJan 18, 2007 · N465AW · Cndair CL6002B19 · Ice/Rain Protection SystemSDR A6WA200640403Sensor · failedMESSAGE DURING FLAP RETRACTION ON CLIMBOUT, FLAP FAIL AT ZERO. FOUND LT BRAKE POSITION SENSOR UNIT HARD FAILED. REPLACED BPSU IAW AMM 27-51-10. FLAPS CHECK GOOD. (K)Dec 4, 2006 · N465AW · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR A6WA200640364Carbon Seal · leakingRT ENGINE OIL LOW PRESSURE ILLUMINATED EN ROUTE, WITH THROTTLE RETARDED, OIL PRESSURE DROPPED FROM 48 TO 28 PSI. ENGINE WAS SHUTDOWN MANUALLY. PERFORMED ENGINE OIL CONSUMPTION CHECK PER AWAC SUPPLEMENT 06-025. FOUND STARTER CARBON SEAL LEAKING. REMOVED ANDOct 11, 2006 · N465AW · Cndair CL6002B19 · Turbine Engine Oil SystemSDR A6WA200640352Windshield · failedFIRST OFFICERS FRONT WINDSCREEN SHATTERED, CRACKED AFTER TAKEOFF AND SHATTERED PRIOR TO 4000 FEET. HEAT WAS SELECTED ON. REMOVED AND REPLACED FIRST OFFICERS RT WINDSHIELD. OPS CHECK GOOD. (M)Sep 15, 2006 · N465AW · Cndair CL6002B19 · Flight Compartment WindowsSDR A6WA200540286Skin · lightning strikeFUSELAGE SKIN HAS SUSTAINED LIGHTNING STRIKE DAMAGE AT FS 654.5 BETWEEN STR 26R AND 27R. REPAIRED DAMAGED AREA BY INSTALLING AN EXTERNAL DOUBLER AT FS 654.5 BETWEEN STR 26R AND 27R IAW EO AND SRM. (K)Aug 16, 2005 · N465AW · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR A6WA200540287Skin · crackedPASSENGER DOOR AFT SKIN DAMAGED AND INTERNAL STIFFENER CRACKED BELOW SKIN RIGHT STIFFENER CRACKED COMPLETELY IN HALF 1.5 INCH. INSTALLED REPAIR FILLER AND DOUBLE IAW BRAS EO 601R-52-7054A. (M)Aug 15, 2005 · N465AW · Cndair CL6002B19 · Passenger/Crew DoorsSDR A6WA200540288Support Beam · crackedCARGO DOOR SUPPORT BEAM MEMBER ANGLE, P/N 601R35050-109, CRACKED AT PRESSURE BULKHEAD FS 621, LBL 34.42. FABRICATED NEW CARGO DOOR SUPPORT BEAM ANGLE IAW CRJ200 SRM 51-30-06 AND BOMBARDIER DRAWING NR 601R35050, INSTALLED ANGLE IAW CRJ200SRM 51-42-21. (M)Aug 12, 2005 · N465AW · Cndair CL6002B19 · Fuselage Main, StructureSDR A6WA200440047Door · openDURING CLIMB-OUT, EXPERIENCED EXTREMELY LOUD NOISE FROM NOSE OF AIRCRAFT. RETURN TO FIELD. FOUND GROUND SERVICE DOOR OPEN. INSPECTED AND NO DAMAGE NOTED. CLOSED AND SECURED DOOR. NO FURTHER OCCURRENCES OR DEFECTS. (M)Apr 19, 2004 · N465AW · Cndair CL6002B19 · Fluid Service Doors
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