N447AW

Service difficulty reports · 175

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 = 'N447AW' 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 A6WA200940086Fitting · crackedFWD UPPER FITTING ON CARGO FOUND CRACK FWD UPPER FITTING ON CARGO DOOR REPLACED IAW SRM 51-42-13. (K)Feb 2, 2009 · N447AW · Cndair CL6002B19 · Cargo/Baggage DoorsSDR A6WA200940093Cable · out of positionPILOTS RT PEDAL LEVER FOULING WITH PARKING BRAKE CABLE. LEVER CAN’T RETURN TO FULL FWD POSITION THIS CAN CAUSE BRAKE PRESSURE ON RT SIDE. PARKING BRAKE CABLE RE-ROUTED IAW AMM TASK 32-45-01-400-801 AND AWAC SUPPLEMENT 06-027A. (K)Feb 2, 2009 · N447AW · Cndair CL6002B19 · Landing Gear Brake SystemSDR A6WA200940065Drag Angle · crackedPAX DOOR AFT DRAG ANGLE FOUND CRACKED PAX DOOR AFT DRAG ANGLE REPAIRED IAW REO 601R-52-11-513, REV A. (K)Feb 2, 2009 · N447AW · Cndair CL6002B19 · Passenger/Crew DoorsSDR A6WA200940063Panel · crackedPAX DOOR AFT SIDE PANEL FOUND CRACK (ZONE 2 AND ZONE 3) (CRACK LENGTH .300) PAX DOOR AFT SIDE PANEL REPAIR CARRIED OUT IAW REO 601R-52-11-700, REV A. (K)Feb 2, 2009 · N447AW · Cndair CL6002B19 · Passenger/Crew DoorsSDR A6WA200940059Panel · crackedPAX DOOR FWD SIDE PANEL FOUND CRACK (ZONE 2) (CRACK LENGTH .250) PAX DOOR FWD SIDE PANEL REPAIRED IAW REO 601R-52-11-702. (K)Feb 2, 2009 · N447AW · Cndair CL6002B19 · Passenger/Crew DoorsSDR A6WA200840600Bulkhead · crackedAFT PRESSURE BULKHEAD WEB AT FS 621.00 AT THE LINTEL INSTALLATION IS CRACKED. AFT PRESSURE BULKHEAD WEB AT FS 621.00 LINTEL INSTALLATION REPAIRED IAW CRJ 200 REO 601R-53-61-1230 REV D.Oct 21, 2008 · N447AW · Cndair CL6002B19 · Fuselage Main, BulkheadSDR A6WA200840547Flap System · failedFLAPS FAIL CAUTION CAS MESSAGE IN FLIGHT WHEN SELECTING 8 DEGREES. LT AND RT INDICATE NORMAL LANDING, BRAKES ALL GREEN. PERFORMED FLANGE RELAY PROCEDURE IAW AWAC SUPP 98-018B STEPS 1.3 AND 1.4. FLAPS RESET. ACFT RELEASED FOR SERVICE.Jul 22, 2008 · N447AW · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR A6WA200840538Scavenge Pump · failedAT CRUISE, AT FL310, LT OIL PRESSURE WARNING MESSAGE, OIL PRESSURE WENT TO 15-20 PSI. RAN QRH, AT IDLE PSI RETURNED TO APPROX 30 PSI FOR LESS THAN 1 MINUTES. THEN RECEIVED LT OIL PRESSURE WARNING AGAIN AND PERFORMED LT ENGINE SHUTDOWN. ENGINE WINDMILLED FORJul 7, 2008 · N447AW · Cndair CL6002B19 · Turbine Engine Oil SystemSDR A6WA200740643Unknown · smokeSMOKE AND ELECTRICAL FIRE ODOR COMING FROM F/O`S SIDE PANEL NEAR WINDSHIELD. FOUND FLOOD LIGHT ON F/O`S SIDE INOPERATIVE AND CIRCUIT BREAKER FOR FLOOD LIGHT POPPED. INSPECTED WIRE HARNESS, NO DEFECTS NOTED. (M)Dec 2, 2007 · N447AW · Cndair CL6002B19 · Air Distribution SystemSDR A6WA200740460Actuator · malfunctionedDURING TAKEOFF/LANDING, ELEVATOR REQUIRES GREATER THAN NORMAL FORCE TO MOVE AFT, NO BINDING FELT. REMOVED AND REPLACED FIRST OFFICERS PITCH FEEL LINEAR ACTUATOR IAW AMM 27-31-23. OPERATIONAL CHECK GOOD. (M)Aug 15, 2007 · N447AW · Cndair CL6002B19 · Elevator Control SystemSDR A6WA200740043Floorbeam · crackedFOUND RIGHT SIDE CARGO FLOOR ANGLE AT FS 621 BULKHEAD CRACKED APPROX .5 INCH LONG. (M) MAINTENANCE REPAIR CRACK IAW REO 601R-53-61-117 REV C BY INSTALLING REPAOR ANGLE AND STRAPS. (K)Jan 25, 2007 · N447AW · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR A6WA200740047Skin · corrodedRT WING LOWER PLANK FUEL TANK ACCESS DOOR CUT OUT HOLE NR 8 (PNL 640FB) HAS MINOR CORROSION AT IB AND OB ENDS APPROX 3 INCH LONG BY .003 INCH DEEP AT IB END AND 1.25 INCH LONG BY .002 INCH DEEP AT OB END. BOTH IN NON-CRITICAL AREA. (M)MAINTENANCE REPAIRED WIJan 24, 2007 · N447AW · Cndair CL6002B19 · Wing, Plate/SkinSDR A6WA200740046Skin · corrodedRT WING LOWER PLANK FUEL TANK ACCESS DOOR CUT OUT HOLE NR 2 (610AB) HAS MINOR PITTING AT IB END IN AN AREA APPROX 1.5 INCH LONG BY .005 INCH DEEP IN NON-CRITICAL AREA. (M) MAINTENANCE REPAIRED WING PLANK HOLE NR 2 (610 AB) IAW REO 601R-57-21-030 REV F AND EOJan 24, 2007 · N447AW · Cndair CL6002B19 · Wing, Plate/SkinSDR A6WA200740045Skin · corrodedFOUND LEFT WING LOWER PLANK FUEL TANK ACCESS DOOR CUTOUT HOLE NR 2 (PNL 510AB, HAS MINOR PITTING AT INBOARD END IN AN AREA APPROX 3 INCHES LONG BY .005 INCH DEEP IN NON-CRITICAL AREA. (M) MAINTENANCE REPAIRED WING PLANK HOLE NR 2 (510AB) IAW REO 601R-57-21-0Jan 24, 2007 · N447AW · Cndair CL6002B19 · Wing, Plate/SkinSDR A6WA200740044Skin · corrodedFOUND LT WING LOWER PLANK FUEL TANK ACCESS DOOR CUTOUT HOLE NR 16 PN. 550HB, HAS MINOR PITTING AT IB END IN AN AREA APPROX 3.25 INCH LONG BY .003 INCH DEEP IN NON-CRITICAL AREA. (M) MAINTENANCE REPAIRED WING PLANK HOLE NR 16 (550 HB) IAW REO 601R-57-21-030 Jan 24, 2007 · N447AW · Cndair CL6002B19 · Wing, Plate/SkinSDR A6WA200740049Angle · crackedFOUND RT SIDE FS 621 TO FS 625.30 INTERCOSTAL AT STRINGER 14R IS CRACKED NEAR RADIUS APPROX .50 INCH LONG NEAR RADIUS. MAINTENANCE REPLACED CRACKED INTERCOSTAL WITH NEW INTERCOSTAL PN 601-35012-52 IAW SRM 51-42-06. (K)Jan 20, 2007 · N447AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200740048Intercostal · crackedFOUND LEFT SIDE FS 621 TO FS 625.30 INTERCOSTAL AT STRINGER 14L IS CRACKED NEAR RADIUS APPROX 1.1 INCH LONG. (M)Jan 20, 2007 · N447AW · Cndair CL6002B19 · Wing Miscellaneous StructureSDR A6WA200640399Isolation Valve · leakingCARGO BOTTLE LOW MASTER CAUTION MESSAGE ILLUMINATED. REMOVED AND REPLACED LT CARGO FIRE BOTTLE, FOUND BOTTLE WAS THERMALLY DISCHARGED, CAUSED BY A LEAK ON THE 10TH STAGE ISOLATION VALVE CLAMP, TIGHTENED CLAMPS, NO LEAKS, REF AMM. (K)Dec 1, 2006 · N447AW · Cndair CL6002B19 · Extinguishing SystemSDR A6WA200740042Angle · crackedFOUND LEFT SIDE FS 621 TO 625.30 INTERCOSTAL AT STRINGER 14L CRACKED APPROX 1.1 INCH LONG NEAR RADIUS. (M) MAINTENANCE REMOVED AND REPLACED OBLIQUE ANGLE IAW SRM 51-40-11 AND 51-42-06. (K)Nov 25, 2006 · N447AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200640316Mechanism · lack of lubeUNABLE TO OPEN SERVICE DOOR FROM OUTSIDE. LUBED SERVICE DOOR IAW 12-20-52, OPS CHECK GOOD. (M)Aug 13, 2006 · N447AW · Cndair CL6002B19 · Service DoorsSDR A6WA200640125Warning Light · illuminatedICE CAUTION LIGHT ILLUMINATED AT 80 KNOTS. ABORTED TAKEOFF, BRAKE APPLICATION AT 100 KNOTS. ICE CAUTION EXTINGUISHED 30 SECONDS AFTER LEAVING RUNWAY. MAX BTMS READINGS: 1=6, 2=5, 3=5, 4=6. PERFORMED FUNCTIONAL TEST OF THE ICE DETECTOR AMM, FOUND OK, REMOVEMar 30, 2006 · N447AW · Cndair CL6002B19 · Ice DetectionSDR A6WA200540166Warning System · activatedON TAKEOFF, ABORTED TAKEOFF DUE TO SPOILERON CONFIG WARNING. NOTE SPEED 60 KNOTS, BTMS HIGHEST READING 4 AND 2. SENT MECHANIC FROM IAS TO BTV. PERFORMED FUNCTION CHECK OF SECU SYSTEM, AND BITE CHECK. ALL CHECKED GOOD PER 27-61-05. (M)May 8, 2005 · N447AW · Cndair CL6002B19 · Drag Control SystemSDR A6WA200540045Bushing · migratedRT MAIN LANDING GEAR AFT TRUNNION BUSHING IS MIGRATED .045 INCH. REMOVED MIGRATED BUSHING AND INSTALLED 1ST OVERSIZED BUSHING IAW BOMBARDIER REO 601R-57-21-003 REV B. (M)Feb 10, 2005 · N447AW · Cndair CL6002B19 · Main Landing GearSDR A6WA200540046Bushing · migratedFOUND LT MAIN LANDING GEAR AFT TRUNNION BUSHING IS MIGRATED .041 INCH. REMOVED MIGRATED BUSHING AND INSTALLED 1ST OVERSIZED BUSHING IAW BOMBARDIER REO 601R-57-21-003 REV B. (M)Feb 10, 2005 · N447AW · Cndair CL6002B19 · Main Landing GearSDR A6WA200440229Odor · detectedRAMPER SMELLED BURNED PLASTIC WHEN OPENING CARGO DOOR. VISUALLY INSPECTED CARGO BAY, COULD NOT SMELL ANY PLASTIC SMELL. CARGO FAN OPS TESTED GOOD AND PERFORMED OPS TEST OF SMOKE DETECTOR IAW AMM. OPS CHECK GOOD. (M)Dec 11, 2004 · N447AW · Cndair CL6002B19 · Cargo Compartments
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