N443AW

Service difficulty reports · 182

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 = 'N443AW' 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 A6WA20094001AActuator · failedLOG 196278/2 - ON APPROACH, FLAPS FAIL CAUTION MSG. FLAPS STUCK AT ZERO DEGREES. C/W QRH, AIR DIVERSION. LANDED OK, NORMAL BRAKING. REMOVED AND REPLACED FLAP ACTUATORS.Jan 16, 2009 · N443AW · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR A6WA200940019Actuator · failedLOG 196278/2 - ON APPROACH, FLAPS FAIL CAUTION MSG. FLAPS STUCK AT ZERO DEGREES. C/W QRH, AIR DIVERSION. LANDED OK, NORMAL BRAKING. REMOVED AND REPLACED FLAP ACTUATORS.Jan 16, 2009 · N443AW · Cndair CL6002B19 · Trailing Edge Flap ActuatorSDR A6WA200840589Landing Gear · unknownON GEAR RETRACTION, GEAR DISAGREE WARNING MESSAGE. SUSPECT NOSE GEAR FAULT. LANDED AT 41,000 LBS AND BRAKING WAS NORMAL. SERVICED MLG AND NLG IAW AMM 12-12-32, PERFORMED GEAR EXTENSION AND RETRACTION CHECK AS REQUIRED. OPS CHECK GOOD. (K)Sep 14, 2008 · N443AW · Cndair CL6002B19 · Landing Gear Retraction/Extension SystemSDR A6WA200840358Bulkhead · crackedREAR PRESSURE BULKHEAD WEB CRACK FS 621 LBL 45 BTWN WL 106.17 AND WL (LINTEL ATTACHMENT FITTING). REAR PRESSURE BULKHEAD WEB FS 621 LBL 45 BTWN WL 106.17 AND WL 113.33 REPAIRED IAW REO 601R-53-61-1230 REV D.Apr 19, 2008 · N443AW · Cndair CL6002B19 · Fuselage Main, BulkheadSDR A6WA200840354Plate · corrodedCORROSION ON FLOOR LANDING PLATE AROUND NUT PLATES HOLES BTWN FS 574 TO FS 621 AND AT LBL 44. CORROSION REMOVED ON FLOOR LANDING PLATE AROUND NUT PLATES HOLES BTWN FS 574 TO FS 621 AND AT LBL 44 IAW SRM 51-21-06.Apr 19, 2008 · N443AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200840352Bulkhead · dentedDENT EXIST ON FLIGHT COMPARTMENT BULKHEAD FS 280 RBL 9 WL 93.0 FLIGHT COMPARTMENT BULKHEAD REPAIRED IAW REO 601R-53-11-1376.Apr 19, 2008 · N443AW · Cndair CL6002B19 · Fuselage Main, BulkheadSDR A6WA200840356Channel · crackedCHANNEL CRACK AT FS 574 FWD TRACK OF CARGO DOOR. CRACKED CHANNEL REPLACED IAW SRM 51-42-06.Apr 18, 2008 · N443AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200840355Bracket · crackedBRACKET CRACKED ON BULKHEAD AT FS 621 WL 107 (CRACK LENGTH .500") BRACKET FABRICATED AS PER SAMPLE AND REPLACED AT FS 621 WL 107 IAW SRM 51-42-21.Apr 16, 2008 · N443AW · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR A6WA200840342Hinge · crackedCARGO DOOR STEP PLATE ONE HINGE CRACKED (FWD). CARGO DOOR STEP PLATE ONE HINGE (FWD) REPLACED IAW SRM 51-42-06. .Apr 16, 2008 · N443AW · Cndair CL6002B19 · Fuselage, Door HingeSDR A6WA200840340Intercostal · crackedCRACK FOUND AT FS 484 RBL 36 WL 72. - - INTERCOSTAL REPAIRED AT FS 484, RBL 36, WL 72 IAW REO 601R-53-41-059 REV A. (S)Apr 16, 2008 · N443AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200840339Intercostal · crackedCRACK FOUND AT FS 484 LBL 36 WL 72. (M) INTERCOSTAL REPAIRED AT FS 484, LBL 36, WL 72 IAW REO 601R-53-41-059 REV A.Apr 16, 2008 · N443AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200840353Structure · crackedCRACK EXIST ON PASSENGER DOOR EDGE MEMBER. PAX DOOR CRACKS REPAIRED IAW REO 601R-52-11-279.Apr 15, 2008 · N443AW · Cndair CL6002B19 · Passenger/Crew DoorsSDR A6WA200840345Floorbeam · crackedFLOOR LANDING PLATE CRACKED AT FS 605, LBL 43. DAMAGE CUTOUT, NDT PERFORMED ON CUTOUT, REDUNDANT HOLE PLUGGED IAW REO 601R-53-61-433.Apr 14, 2008 · N443AW · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR A6WA200840341Plate · crackedFLOOR LANDING PLATE CRACKED AT FS 605, LBL 42. - - DAMAGE CUTOUT, NDT PERFORMED ON CUTOUT, REDUNDANT HOLE PLUGGED IAW REO 601R-53-61-433. .Apr 14, 2008 · N443AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200840332Sill · crackedCARGO BAY FLOOR SILL CRACKED APPROX .200 IN AT FS 574. REPAIRED IAW CRJ 200 REO 601R-53-61-1741. (M)Apr 14, 2008 · N443AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200840357Bulkhead · crackedCRACK FOUND ON PRESSURE BULKHEAD FS 202.75 LBL 23.71 AROUND PARKING BRAKE. CRACK PRESSURE BULKHEAD REPAIRED IAW REO 601R-53-11-563.Apr 12, 2008 · N443AW · Cndair CL6002B19 · Fuselage Main, BulkheadSDR A6WA200840344Frame · crackedCRACK FOUND ON FRAME FS 280 RBL 9 WL 73. FRAME AT FS 280, RBL 9, WL 73 REPAIRED IAW RWO 601R-53-11-171 REV "D" SCHEME "B". .Apr 12, 2008 · N443AW · Cndair CL6002B19 · Fuselage Main, FrameSDR A6WA200840343Frame · crackedCRACK FOUND ON FRAME 280, LBL 9 WL 73.00. - - FRAME AT FS 280 LBL 9 WL 73.00 REPAIRED IAW REO 601R-53-11-171 REV "D" SCHEME B. .Apr 12, 2008 · N443AW · Cndair CL6002B19 · Fuselage Main, FrameSDR A6WA200740025Flap System · failedWHILE IN FLIGHT, FLAPS FAILED AT ZERO WHILE ATTEMPTING TO EXTEND. LANDED FLAPS AT ZERO. NORMAL BRAKING ACTION. BRAKE TEMPS READ 5, 5, 5, 6. RESET PER AMM SUPPLEMENT 98-018A. PLACED ON 72 FLAP WATCH. (M) COMPLIED WITH AMM SUPPLEMENT 98-018A, NO FURTHER IJan 14, 2007 · N443AW · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR A6WA200740009Flap System · unknownFLAPS FAIL YELLOW CAUTION MESSAGE IN FLIGHT. LANDED AT FLAPS ZERO. (M)Jan 9, 2007 · N443AW · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR A6WA200740002Pseu · unknownSERVICE DOOR CAUTION MESSAGE IN FLIGHT. CAME ON AT ABOUT 1000 AGL, THEN EXTINGUISHED, AND CAME ON AGAIN AT ABOUT 5 TO 7000 FEET INDICATED MSL. INSPECTED SERVICE DOOR, NO DAMAGE OR DEFECTS NOTED. PRESSURIZED AIRCRAFT TO 4.0 PSI, NO FAULTS FOUND. INTERCHANGEDec 29, 2006 · N443AW · Cndair CL6002B19 · Door Warning SystemSDR A6WA200640354Switch · malfunctionedSTAB TRIM 1 AND 2 DISENGAGED INFLIGHT DURING MANUAL TRIM ACTUATIONS. REMOVED AND REPLACED CAPT TRIM DISCONNECT SWITCH AFTER TESTING IAW AWAC SUPPLEMENT NR 05-029. WORK PERFORMED IAW CRJ AMM 27-4, OPS CHECK GOOD. (M)Sep 25, 2006 · N443AW · Cndair CL6002B19 · Stabilizer Position IndicatingSDR A6WA200640297Solenoid Valve · malfunctionedON DEPARTURE FROM BNA FLT 3818, STEERING INOPERATIVE CAUTION MESSAGE ILLUMINATED, COMPLIED WITH QRH, NO FURTHER ACTION. EMERGENCY LANDING DECLARED BY CREW. REMOVED AND REPLACED NOSEWHEEL STEERING SELECTOR VALVE IAW CRJ AMM 32-51-25. OPS AND LEAK CHECK GOOD.Jul 28, 2006 · N443AW · Cndair CL6002B19 · Landing Gear Retraction/Extension SystemSDR A6WA200640177Anchor · crackedPAX DOOR AFT CABLE ANCHOR ASSY, P/N 601R380741-3 IS CRACKED, APPROX 1.5 INCH IN LENGTH. REMOVED AND REPLACED AFT COUNTERBALANCE ASSY ANCHOR FITTING WITH NEW P/N 601R31976-1, IAW CRJ-200 AMM 52-11-17 AND SB 601R-52-116 REV C. (M)May 3, 2006 · N443AW · Cndair CL6002B19 · Passenger/Crew DoorsSDR A6WA200640166Drag Angle · crackedPAX DOOR AFT DRAG ANGLE CRACKED AT PULLEY BRACKET APPROX 7 INCHES LONG. REPAIRED PAX DOOR AFT DRAG ANGLE IAW BOMBARDIER REO 601R-52-11-513 REV A. (M)May 1, 2006 · N443AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200640165Intercostal · crackedFOUND RT SIDE FS 621 TO FS 625.3 INTERCOSTAL AT STRINGER 14R IS CRACKED NEAR RADIUS APPROX 1.1 INCH LONG. REMOVED AND INSTALLED NEW INTERCOSTAL P/N 601-35012-52 AT FS 621 TO FS 625.3, STRINGER 14R, IAW CRJ-200 SRM 51-42-06. (M)Apr 30, 2006 · N443AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200640164Intercostal · crackedFOUND LEFT SIDE FS 621 TO FS 625.3 INTERCOSTAL AT STRINGER 14L IS CRACKED NEAR RADIUS APPROX 1.0 INCH LONG. REMOVED AND INSTALLED NEW LEFT INTERCOSTAL, P/N 601-35012-51, AT FS 621 TO 625.3, STRINGER 14L, IAW CRJ-200 SRM 51-42-06. (M)Apr 30, 2006 · N443AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200640163Rib · crackedFOUND LT WS 53.60 BATT RIB ASSEMBLY HAS A .5 INCH CRACK AT TOP CORNER. REPAIRED BATTERY RIB BY REMOVING DAMAGED AREA AND INSTALLING REPAIR ANGLE DOUBLE AND FILLER IAW BOMBARDIER REO 601R-57-51-046 REV B. (M)Apr 30, 2006 · N443AW · Cndair CL6002B19 · Wing, Rib/BulkheadSDR A6WA200540125Line · chafedSMELL STRONG FUEL ODOR IN CABIN. REMOVED AND REPLACED CHAFED LINE FROM FUEL SOLENOID TO APU BURNER CAN. REMOVED AND REPLACED AIR PACK COALESCER SOCKS, RAN ENGINES AIRCRAFT OK FOR SERVICE. (M)Mar 25, 2005 · N443AW · Cndair CL6002B19 · APU Engine Fuel and ControlSDR A6WA200440199Floorbeam · crackedTHE LT AND RT SIDE UNDER FLOORBEAM STRUCTURE IS CRACKED AT FSL73, LBL40 AND RBL40. REMOVED CRACKED AREA AND INSTALLED REPAIR PARTS IAW REO.Dec 2, 2004 · N443AW · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR A6WA200440005Smoke Detector · false activationSMOKE TOILET CAS MESSAGE ON TAXI, COMPLIED WITH QRH. FIRE DEPARTMENT INSPECTED LAV, NO EVIDENCE OF SMOKE OR FIRE. INSTALLED SMOKE DETECTOR AFT LAV, TESTED OK. REMOVED FROM MEL. (M)Jan 10, 2004 · N443AW · Cndair CL6002B19 · Smoke DetectionSDR A6WA200340104Engine · malfunctionedABORTED TAKEOFF, 140 KNOTS NR 2 ENGINE N2 DROPPED OFF TO APPROX 50-60 PERCENT. ON TAKEOFF ROLL, BRAKE MAX TEMPS WERE 11, 9, 7, 8 ABORTED TAKEOFF, TAKEOFF AT 1655Z MARKED FDR AT 1704Z. PERFORMED ACCELERATION/DECELERATION CHECKS AND POWER ASSURANCE CHECKS, NO Jun 24, 2003 · N443AW · Cndair CL6002B19 · Engine (Turbine/Turboprop)
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