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 A6WA202206098191Steering Sys · warning messageSTEERING INOP CAUT MSG ABOUT 15 MIN AFTER TO. C/W QRH MSG RETURNED AFTER STEERING SWITCH RESET. ATTEMPTED MULTIPLE CYCLES OF STEERING SWITCH NO FIX. AFTER CONFIGURING A/C FOR LANDING CYCLED STEERING SWITCH TO ON CAUT MSG REMAINED CLEARED LANDED WITH NORMAL STEJun 9, 2022 · N443AW · Cndair CL6002B19 · Steering UnitSDR A6WA202205178182Bonding Plate · corrodedRH ENGINE PYLON, TOP SIDE, OUTBOARD BONDING PLATE HAS CORROSION. REMOVE AND REPLACED BONDING PLATE ON RH AFT PYLON TOPSIDE, BONDING CHECK GOOD. PRIMED AND TOP COAT. IAW CRJ-200 SRM 51-45-15, AMM 51-80-00-760-803, SRM 51-25-06, AND 51-25-16 SUPP 15-335 ***AIRCMay 17, 2022 · N443AW · Cndair CL6002B19 · Nacelle/Pylon, Plate/SkinSDR A6WA202205178183Frame · corrodedFS605.00 AFT SIDE OF FRAME FROM STR27 TO 23R HAS EVIDENCE OF CORROSION FURTHER CLEANING AND EVALUATION IS REQUIRED CLEANED AND REMOVED FRAME PN 601R36026-27S AT FS605, REPLACED FRAME AT FS605 IAW CRJ-200 SRM 51-26-00, 51-42-21, 51-42-06, AND 51-40-11 ****AIRCRMay 17, 2022 · N443AW · Cndair CL6002B19 · Fuselage Main, FrameSDR A6WA202203188133None · noneLOST RUDDER TRIM IN FLIGHT. RUDDER TRIM FULL DEFLECTION NL. RUDDER TRIM SWITCH WILL NOT MOVE NR. A/C CONTROLLABLE WITH RH RUDDER INPUT. DIVERTED TO BUF, SMOOTH LANDING AT 47,100LBS ***AIRCRAFT REMOVED FROM SERVICE*** R&R AILERON/RDR TRIM PANEL IAW AMM 27Mar 18, 2022 · N443AW · Cndair CL6002B19 · Flight Control SystemSDR A6WA202107287843Power Supply · inoperativeFLAPS FAIL AT ZERO DEGREES ON APROACH WHEN SELECTED FROM 0 TO 8, FLAPS DID NOT MOVE. LANDING WEIGHT APROX 45000 LBS, SMOOTH UNEVENTFUL LANDING, MAX BTMS 7556. AIRCRAFT REMOVED FROM SERVICE. REF WO 307503 MX WC 2-19 FOR TBS AND CORRECTIVES (LH AND RH BJul 28, 2021 · N443AW · Cndair CL6002B19 · Trailing Flap Position Indicating SystemSDR A6WA202107277840Flap System · failedREF 347659-2 AFTER TAKEOFF, REC FLAP FAIL CAUTION MSG DURING FLAP RETRACTION FROM FLAPS 8 TO FLAPS 0. CW AWA SUP 98-018I RESET FAILED WHEN MOVING HANDLE FROM 8 TO 0 TO BEGIN 5 FLAP CYCLES ***AIRCRAFT REMOVED FROM SERVICE*** MX IN PROGRESSJul 25, 2021 · N443AW · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR A6WA202107207831Flap System · malfunctionedDURING APPROACH AND FLAPS SET TO ZERO, RECIEVED A FLAPS FAIL CAUTION. 44 PASSENGERS, FO WAS FLYING, NO OBSERVERS. CAPTAIN STATED DURING DEBRIEF THAT IT WAS A NORMAL ILS APPROACH AT 10 CENTER AND 210 KIAS. LOWERED GEAR AT 200 KIAS. CAPTURED GLIDESLOPE AT 17Jul 17, 2021 · N443AW · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR A6WA202107207832Flap System · malfunctionedFLAP FAIL AT 0, FLAPS ALREADY ON MEL, FN 3917 EMERGENCY DECLARED BY CREW. AS THEY TURNED ONTO AN EXTENDED FINAL INTO ORD, FO FLYING, WENT UNDER 180, SELECTED FLAPS TO 8 & RECEIVED A FLAP MASTER CAUTION, FLAPS NEVER MOVED OUT OF 0. RAN QRH & DECLARED EMERGENCJul 17, 2021 · N443AW · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR A6WA202107157827Control Unit · malfunctionedDURING THE APPROACH TO KORD, THE FLIGHT CREW EXPERIENCED A FLAP FAILURE AND DISCONTINUED THE APPROACH. THE CREW COMPLETED REQUIRED CHECKLISTS, DECLARED AN EMERGENCY WITH ATC, COMMUNICATED WITH THE FLIGHT ATTENDANT, PASSENGERS AND DISPATCH THEN RETURNED AND LANJul 15, 2021 · N443AW · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR A6WA202106077798Flap System · stuckAFTER SELECTING FLAPS ZERO AFTER TAKEOFF, RECEIVED FLAPS FAIL CAUTION MESSAGE. FLAPS STUCK AT 3 DEG LEFT & 4 DEG RIGHT. IAS AT TIME OF FLAP FAIL WAS 200 KTS, OAT OF 27 DEG C, & TIME NOTED IN AIR WAS 1 MINUTE. (BLOCK 2) PERFORMED FLAP RESET PROCEDURE IAW SUPP 9Jun 6, 2021 · N443AW · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR A6WA202106047794Bpsu · failedAT FL 300 AND MACH . FLAPS FAILED AT ZERO. AIRCRAFT REMOVED FROM SERVICE. LEFT BPSU REPLACED, OPS CHECK GOOD.Jun 4, 2021 · N443AW · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR A6WA202106047793Bpsu · failedFL 240 RECEIVED FLAPS FAIL CAUTION MSG C/W QRH FLAPS FAILED AT 0 DEGREES. DECLARED AN EMERGENCY AND LANDED WITH NO ISSUES IN IAD. C/W FIM RESET IAW AWAC SUP 98-18I BOX 12 FLAP RESET, AND PLACED ON MEL AIRCRAFT REMOVED FROM SERVICE. R&R LFT BPSU IAW AMJun 3, 2021 · N443AW · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR A6WA2020032647244Skin · dentedPERFORM PERMANENT REPAIR TO R/H L/E BETWEEN WS 226 TO WS 242 THAT MEASURES 2.0"L X 2.5" W X .037"D. "AIRCRAFT REMOVED FROM SERVICE" DENT AT WS 242 REFORMED TO ORIGINAL CONTOUR AND HFEC WITH NO CRACK INDICATIONS. REF ASAP EA# AWAC-CRJ257-01476 REV IR DTD 03/Mar 14, 2020 · N443AW · Cndair CL6002B19 · Wing, Plate/SkinSDR A6WA2020032547237Doubler · corrodedSUPPLEMENTAL, CLOSET ASSY HAS CORROSION ON LWR SILL BY MOUNT POINT. AIRCRAFT REMOVED FROM SERVICE. MANUFACTURED PART ITEMS 55 & 75 AND REPLACED ITEMS 35 AND 65. REF ASAP EA AWAC-CRJ225-01480 REV IR DTD 3/21/20.Mar 6, 2020 · N443AW · Cndair CL6002B19 · Passenger Compartment EquipmentSDR A6WA2020032547240Cable · frayedL1 DOOR MAIN PAX DOOR POWER ASSIST CABLE IS FRAYED. "AIRCRAFT REMOVED FROM SERVICE" REMOVED AND REPLACED L1 MAIN PAX DOOR POWER ASSIST CABLE REF CRJ-200 AMM 52-11-00Mar 6, 2020 · N443AW · Cndair CL6002B19 · Passenger/Crew DoorsSDR A6WA2020032647242Vane · cracked#2 ENGINE THRUST REVERSER CASCADE AT 12 O'CLOCK POSITION HAS A CRACKED VANE. "AIRCRAFT REMOVED FROM SERVICE" REMOVED AND REPLACED 12 O'CLOCK POS CASCADE ON #2 ENG REF CRJ 299 AMM 78-33-01. REV 60Mar 4, 2020 · N443AW · Cndair CL6002B19 · Engine Thrust ReverserSDR A6WA2020032647243Skin · dentedPERFORM REPAIR TO L/H FUSELAGE SKIN BETWEEN FRAMES FS 544 TO FS 559 & S9L TO S10L FOR 1-OFF DENT THAT MEASURES 2.4"L X .5"W X .128"D. "AIRCRAFT REMOVED FROM SERVICE" CUTOUT DAMAGED AREA. HFEC PERFORMED AROUND CUTOUT. REPAIR DOUBLER FABRICATED FROM 2024-T3 Mar 4, 2020 · N443AW · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR A6WA202002147179Bracket · damagedAFTER T/O SELECTED GEAR UP GOT GEAR DISAGREE AND NOSE DOOR OPEN (W) MS GS AND NOSE GEAR WOULD NOT RETRACT. RAN QRH FOR NOSE DOOR OPEN ALL (W) MSGS DISAPPEARED AIRCRAFT REMOVED FROM SERVICE INSPECTED NLG DOORS, NO DEFECTS NOTED,Feb 13, 2020 · N443AW · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR A6WA2019112147021Bpsu · malfunctionedSHORTLY AFTER DEPARTURE, THE FLIGHT CREW RECEIVED A FLAP FAIL CAUTION MESSAGE. THE CREW DECLARED AN EMERGENCY AND RETURNED TO KORD WITHOUT FURTHER INCIDENT. FLAPS FAIL CAS MSG MOVING FLAP LEVERS FROM 8 TO 0 AFTER TAKE OFF PERFROMED FLAP FAIL RESET PROCEDURES INov 16, 2019 · N443AW · Cndair CL6002B19 · Trailing Flap Position Indicating SystemSDR A6WA2019110546972Pitot Line · contaminatedDURING CLIMB OUT IN MODERATE ICING RECEIVED IAS AND ALT YELLOW BOX MSG"S ON BOTH PFD'S AND OTHER ASSOCIATED MSG'S. NO PITOT OR STATIC HEAT FAILURES. COULD NOT ISOLATE EITHER ADC, BOTH APPEARED INOP. RECEIVED ADC TEMP DISAGREE CAUTION AFTER 10 MIN. ALL MSG'S CLNov 2, 2019 · N443AW · Cndair CL6002B19 · Pitot/Static SystemSDR A6WA2019020846371Windshield · crackedLEFT WINDSHIELD ARCED AT FL 280 CW QRH. APPEARS TO BE CRACKED. LH WINDSCREEN MIDDLE PANE IS CRACKED ALMOST FULL WIDTHFeb 6, 2019 · N443AW · Cndair CL6002B19 · Flight Compartment WindowsSDR A6WA2018101246109Warning System · activatedOUT OF 15,000FT IN DECENT RECEIVED DYD 1 LO PRESS CAUTION C/W QRH PROBLEM DID NOT RESOLVE. PRESSURE WENT FROM 1800PSI TO 500PSI IN 2 MINUTES. TURNED ACMP OFF, PUMP RAN FOR APPROX 3 MINUTES. EDP RAN FOR APPROX 15 MINUTES AT LO PRESS.Oct 10, 2018 · N443AW · Cndair CL6002B19 · Hydraulic Pressure IndicatorSDR A6WA201846019Warning Message · illuminated4826 WHILE TRANSFERING BLEEDS TO THE ENGINES AFTER T/O CHECKLIST RECEIV ED LH PACK HI PRESSURE CAUTION MSG. CW QRH PROCEEDURE. MSG REMAINED. ON CLIMB WITH LG ENGINE AT BELOW 60% N1 RECEIVED LH PACK OVERPRESSURERE DUCED LH ENGINE TO 57% N1 AND CYCLED PACK SW. Aug 30, 2018 · N443AW · Cndair CL6002B19 · Cabin Cooling SystemSDR A6WA2018042445778Latch · crackedLEFT LRU DOOR AFT LATCH STRUCTURE IS CRACKED.Apr 18, 2018 · N443AW · Cndair CL6002B19 · DoorsSDR A6WA2018042445779Bulkhead · crackedAFT PRESSURE BULKHEAD ABOVE AFT CARGO DOOR TRACK AT UPPER END IS CRACKED .Apr 18, 2018 · N443AW · Cndair CL6002B19 · Fuselage Main, BulkheadSDR A6WA201845775Fitting · crackedBATH TUB FITTING AT BS 461, OTBD SIDE OF LBL 9 IS CRACKED.Apr 16, 2018 · N443AW · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR A6WA201845774Hinge · crackedPAX DOOR LOWER FOLDING STEP HINGE CRACKED.Apr 14, 2018 · N443AW · Cndair CL6002B19 · Passenger/Crew DoorsSDR A6WA2018041645773Drag Angle · crackedPAX DOOR HAD A CRACKED AFT DRAG ANGLE.Apr 14, 2018 · N443AW · Cndair CL6002B19 · Passenger/Crew DoorsSDR A6WA2018041645770Skin · dentedLEFT INBD FLAP LOWER SKIN DENTED AT FLAP STATION 54.5 APPROXIMATELY 4 INCHES FROM TRAILING EDGE.Apr 13, 2018 · N443AW · Cndair CL6002B19 · Trailing Edge FlapsSDR A6WA2018041645769Bracket · crackedRIGHT MLG WHEEL WELL PRESSURE TRANSDUCER BRACKET IS CRACKED. REPLACED THE BRACKET IAW SRM 51-42-06.Apr 11, 2018 · N443AW · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR A6WA2018041645771Retainer · crackedL/H PYLON PANEL 412BT SEAL RETAINER CRACKED. REPAIRED THE SEAL RETAINER IAW SUPP 16-363.Apr 10, 2018 · N443AW · Cndair CL6002B19 · Nacelle/Pylon, Main FrameSDR A6WA2018041645772Retainer · crackedLEFT LOWER PYLON PANEL 412DB SEAL RETAINER IS CRACKED. REPAIRED THE SEAL RETAINER IAW 16-363.Apr 10, 2018 · N443AW · Cndair CL6002B19 · Nacelle/Pylon, Main FrameSDR A6WA2018042445777Angle · damagedANGLE DAMAGED AT BS 280 TO 295, STRINGERS 2L TO 4L, REPAIRED IAW REO 601R31522.Apr 3, 2018 · N443AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA2018012545575Anti-Ice Valve · defectiveCLIMBOUT RECEIVED LEFT COWL ANTI-ICE CAUTION MESSAGE WITH COWL ANTI-ICE SELECTED OFF. C/W QRH MESSAGE CLEARED AT 84% N2. RETURNED FOR A NORMAL LANDING UNDER LANDING WEIGHT.Jan 16, 2018 · N443AW · Cndair CL6002B19 · Air Intake Anti/De-Ice SystemSDR A6WA2017103045366Actuator · malfunctionedUNCOMMANDED YAW, ONCE DURING CLIMB AND ONCE IN CRUISE. SLIGHT YAW AND NO CROSSWIND OR TAILWIND NOTICED. NO MESSAGE POSTED, AUTOPILOT ENGAGED. REMOVED AND REPLACED LEFT YAW DAMPER LINEAR ACTUATOR IAW AMM 22-22-01. OPS CHECKED GOOD.Oct 21, 2017 · N443AW · Cndair CL6002B19 · Autopilot SystemSDR A6WA2017022244801B-Nut · leakingDURING DESCENT WITH APU OFF AND BOTH PACKS SELECTED TO AUTO, CREW REPORTED STRONG FUEL ODOR IN CABIN AND COCKPIT. PERFORMED VISUAL INSPECTION OF AFT EQUIPMENT BAY AIR CONDITIONING DUCTS, NO DEFECTS NOTED. FOUND A B-NUT FITTING ON APU FUEL CONTROL UNIT LEAKING Feb 16, 2017 · N443AW · Cndair CL6002B19 · APU Engine Fuel and ControlSDR A6WA201744756Unknown · odorEXHAUST SMELL AND SMOKE IN CABIN WITH BOTH PACKS ON AND APU RUNNING.Jan 16, 2017 · N443AW · Cndair CL6002B19 · Air Distribution SystemSDR A6WA2016122844686Skin · damagedFUSELAGE SKIN DAMAGED AT BS 559+112 TO 574, STRINGERS 14 TO 16R.Dec 22, 2016 · N443AW · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR A6WA2016122844687Stringer · damagedSTRINGER 15R DAMAGED BETWEEN BS 559+112 AND 574Dec 22, 2016 · N443AW · Cndair CL6002B19 · Fuselage Main, Longeron/StringerSDR A6WA201644324Inverter · inoperativeFLIGHT NUMBER 4041. EMERGENCY LIGHTS BETWEEN ROWS 5D AND 8D, AND EMERGENCY EXIT ROW 8F LOWER GREEN EXIT SIDEWALL SIGN NOT ILLUMINATING. R & R THE NR 3 INVERTER IAW AMM 33-51-07. OPS CHECKED GOOD.Sep 12, 2016 · N443AW · Bombdr CL6002D15 · Emergency LightingSDR A6WA201644276Light · inoperativeFLIGHT 3862. LEFT LOWER EXIT LIGHT ROW 8 INOPERATIVE. FLOOR LIGHT ROWS 2-5 INOPERATIVE CYCLED EMERG LIGHT SWITCH. EMERGENCY LIGHTS OPS CHECK GOOD IAW AMM 33-51Aug 29, 2016 · N443AW · Cndair CL6002B19 · Emergency LightingSDR A6WA201644143Heat Exchanger · unserviceableON CLIMBOUT, RECEIVED HIGH OIL TEMP OF 151, FLASHING YELLOW, CW QRH OIL TEMP AGAIN CLIMBED IN TO CAUTION RANGE, FOLLOWED QRH PROCEDURES, ACCOMPLISHED SINGLE ENGINE PROCEDURES, OIL TEMP AND PRESSURE CLIMBING PRIOR TO ENGINE SHUTDOWN, OIL PRESSURE NEVER EXCEEDEJul 24, 2016 · N443AW · Cndair CL6002B19 · Engine Oil CoolerSDR A6WA201643858Skin · damagedREPAIR RT HORIZONTAL STAB, LOWER SKIN TEMP REPAIR IAW REO 601R-55-11-520. PERFORM PERMANENT REPAIR AS REQUIRED.May 7, 2016 · N443AW · Cndair CL6002B19 · Horizontal Stabilizer, Plate/SkinSDR A6WA201643857Support Angle · crackedRBL 9 IN NLG WW HAS A CRACKED SUPPORT ANGLE TOP OF RBL 9 POST. REPLACED ANGLE AT RBL 9 & FS 202.75 IN NLG BAY IAW SRM 51-42-06.May 7, 2016 · N443AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA201643859Spar · damagedREPAIR RT HORIZONTAL STAB AT RIB 9. TEMP REPAIR COMPLIED WITH IAW REO 601R-55-11-519. PERFORM PERMANENT REPAIR.May 7, 2016 · N443AW · Cndair CL6002B19 · Horizontal Stabilizer, Spar/RibSDR A6WA201643852Skin · chafedBOTH SIDES OF RUDDER LE ARE HEAVILY CHAFED.May 6, 2016 · N443AW · Cndair CL6002B19 · Rudder, Plate/SkinSDR A6WA201643856Strap · damagedINSTALLED NEW FUEL PRESS BOX, REQUIRED STRAP REPLACEMENT.May 6, 2016 · N443AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA201643853Seat Track · corrodedSEAT RAIL LBL 27 OTBD FLANGE HAS CORROSION AFT OF FS 559+112.May 6, 2016 · N443AW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR A6WA201643848Support Bracket · crackedPASSENGER ENTRY DOOR SUPPORT WHEEL BRACKET CRACKED.May 6, 2016 · N443AW · Cndair CL6002B19 · Passenger/Crew DoorsSDR A6WA201643849Angle · crackedRIGHT WINDSHIELD SIDE POST LOWER OTBD ANGLE CLIP IS CRACKED IN FLIGHT DECK.May 6, 2016 · N443AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
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