N441ZW

Service difficulty reports · 186

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 = 'N441ZW' 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 A6WA202608098905Window · overtemp2062 - R WINDOW HEAT CAUTION IN FLIGHT C/W QRH AND RETURNED TO ATW. AIRCRAFT REMOVED FROM SERVICE. REF W/O 348445, WC 1&2 FOR R&R OF SIDE WINDOW RH AND HEATER CONTROLLER. OPS CHECK AND LEAK CHECK GOOD. IAW AMM 56-12-01.Aug 9, 2026 · N441ZW · Cndair CL6002B19 · Windshield/Door Rain/Ice RemovalSDR A6WA202405128747Flap System · faultedWHILE ON APPROACH TO KORD, AT 3500 FEET, THE CREW SELECTED FLAPS 8 AND RECEIVED A FLAP FAIL MESSAGE AT 0 DEGREES. THEY INITIATED A GO AROUND, DECLARED AN EMERGENCY WITH ATC, COMPLIED WITH THE QRH AND BRIEFED THE PASSENGERS. THEY LANDED WITHOUT FURTHER ISSUE ONMay 12, 2024 · N441ZW · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR A6WA202401158715Skin · dentedDENT ON LEFT AFT FUSELAGE SKIN AT FS755.00 TO 67.5% SPAR DATUM S24L. AIRCRAFT REMOVED FROM SERVICE EVALUATED DENT ON AFT FUSELAGE SKIN AT FS755.00 Ï¿½ 67.5% SPAR DATUM AND S21L TO S23L. ACCOMPLISHED DOUBLER REPAIR IAW EA AWAC-CRJ253-02025 REV IR DATED 01/Jan 15, 2024 · N441ZW · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR A6WA202401138701Structure · corroded20090 335262 453-280-600 MFG00716 HRS 64.15. AIRCRAFT HAS BEEN REMOVED FROM SERVICE. CORROSION AT 7 PLACES ON REAR PRESSURE BULKHEAD FRAME CAP FROM FS574 TO FS605. ALL AT RBL41.75. ORIGINAL MATERIAL THICKNESS 0.050Ï¿½.Ï¿½ P1 - L= 1.300Ï¿½ X W= 0.900Ï¿½ XJan 13, 2024 · N441ZW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA202401088693Strap · corrodedCORROSION ON FLOOR STRUCTURE RH STRAP PN 601R31025-29 AT FS 559.00 AND RBL27 - 42. ***** AIRCRAFT REMOVED FROM SERVICE *****Jan 8, 2024 · N441ZW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA202401088694Strap · corrodedCORROSION ON FLOOR STRUCTURE RH STRAP PN 601R31025-29 AT FS 559.00 AND LBL27 - 45. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND INSTALLED FLOOR STRUCTURE RH STRAP PN 601R31025-29 AT FS 559.00 AND LBL27 - 42 WITH FABRICATED NEW STRAP WITH MATERIAL 7075-T6, TJan 8, 2024 · N441ZW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA2022092658309Actuator · faultedRECEIVED GEAR DISAGREE AND LH MLG INDICATED RED ON SELECTION OF GEAR DOWN. APROX 1500 FT. CW QRH LH MLG REMAINED UNSAFE. CW TOWER FLYBY. GEAR APPEARED TO BE DOWN AND LOCKED. EMERG GEAR HANDLE WAS PULLED. LANDED WITHOUT INCEIDENT. AFTER LANDING NOTED THE PROX Sep 25, 2022 · N441ZW · Cndair CL6002B19 · Landing Gear Door ActuatorSDR A6WA202208128271None · noneAFTER T/O UPON SELECTING THE LANDING GEAR HANDLE UP RECEIVED WARNING MSG, NOSE DOOR OPEN AND GEAR DISAGREE. PERFORMED GEAR EMER EXTENSION PER QRH BOTH WARNING MSG'S CLEARED AND GEAR SHOWED NORMAL DOWN. (CONT) LP 337510/1 MSG 'S APPEARED ALMOST IMMEDIATELY AFAug 12, 2022 · N441ZW · Cndair CL6002B19 · Landing Gear SystemSDR A6WA202112068000None · noneDURING CLIMB THROUGH 18,000 NOTICED CABIN ALT INCREASING AT APROX 2000 FT PER MIN, ECS PAGE SHOWED BOTH L & R 10TH STAGE VALVES CLOSED. INITIATED DECENT TO 0,000 FT (BLK 3) AT APROX 12,000 FT RECEIVED CABIN ALT CAUTION MSG C/W QRH LEFT L&R 10 TH STAGE VALVEDec 4, 2021 · N441ZW · Cndair CL6002B19 · Pneumatic SystemSDR A6WA2020052087263Bpsu · malfunctionedSHORTLY AFTER TAKEOFF, THE FLIGHT CREW RECEIVED A FLAP FAIL CAUTION MESSAGE. THE CREW REVIEWED THE QRH, CONTACTED DISPATCH AND ATC, DECLARED AN EMERGENCY AND CONTINUED TO DESTINATION WITH AN OTHERWISE NORMAL LANDING. RECEIVED FLAPS FAIL AT 8 DEG WHEN COMPLETINMay 18, 2020 · N441ZW · Cndair CL6002B19 · Trailing Flap Position Indicating SystemSDR A6WA2020012447133Angle · corrodedSERVICE DOOR LWR SILL FS 319 TO FS 349 HAS MULTIPLE AREAS OF CORROSION REMOVED, FABRICATED AND INSTALLED ANGLE 601R38303-105 FROM 7075-T6 REF CRJ 200 SRM 53-21-23 REV. 37. AIRCRAFT REMOVED FROM SERVICE. REMOVED, FABRICATED AND INSTALLED ANGLE 601R38303-105 FJan 7, 2020 · N441ZW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA202001247132Structure · corrodedENTRY DOOR INNER STRUCTURE FROM FS 311.75 TO 347.25 HAS CORROSION. ITEMS AS IDENTIFIED REF CRJ 200 SRM 52-10-14 ITEM 1 FORMER INNER, FS 320.10 601R31902-455, ITEM 18 FORMER 601R31902-409, ITEM 19 FORMER 601R31902-13, ITEM 25 INTERCOSTAL 601R31902-318, ITEM 26 Jan 6, 2020 · N441ZW · Cndair CL6002B19 · Passenger/Crew DoorsSDR A6WA2020012247125Bonding Plate · corrodedNR 2 PYLON UPPER TRAILING EDGE, TWO BONDING PLATES HAD CORROSION. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACE BOTH BONDING PLATES IAW SRM TEMP REV 51-42, SRM 51-42-10, & 51-25-00 REV 37.Jan 6, 2020 · N441ZW · Cndair CL6002B19 · Nacelle/Pylon, Main FrameSDR A6WA2020012247123Control Cable · frayedRIGHT OTBD AILERON FUSELAGE CONTROL CABLE IS FRAYED AT THE RT REAR QUADRANT. AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE O/B AILERON FUSELAGE CONTROL CABLE AND ACCOMPLISHED RIGGING IAW AMM 27-00-00 & 27-11-00, REV 60. ACCOMPLISHED AILERON TJan 4, 2020 · N441ZW · Cndair CL6002B19 · Aileron Control SystemSDR A6WA2019100146890Warning Message · illuminatedAFTER ROTATION RECEIVED STEERING INOP CAUTION AFTER GEAR RETRACTION, GEAR INDICATED UP/LOCKED. AT 700FT AGL RECEIVED WOW INPUT CAUTION C/W QRH FOR NWS MESSAGE REMAINED. DECLARED AN EMERGENCY AND LANDING IN IAD WAS UNEVENTFUL.Sep 27, 2019 · N441ZW · Cndair CL6002B19 · Landing Gear Steering SystemSDR A6WA2019012446327Aileron · corrodedLEFT AILERON OUT BOARD PCU ATTACHMENT POINT ON AILERON FOUND TO HAVE CORROSION.Jan 24, 2019 · N441ZW · Cndair CL6002B19 · AileronsSDR A6WA2018060845872Warning Message · false activationRECEIVED NOSE GEAR DOOR OPEN WARNING MESSAGE IN A TURN AT 200 KTS. AT 230 KTS THE MESSAGE CLEARED. WHEN TRUE AIRSPEED IS ABOVE 250 MESSAGE CAME BACK. APPEARS DOOR IS NOT OPEN. NOSE LANDING GEAR FORWARD DOOR SENSOR RIGGING WITHIN LIMITS IAW AMM 32-00-00. PEJun 5, 2018 · N441ZW · Cndair CL6002B19 · Landing Gear Position and WarningSDR A6WA2018060545869Proximity Sensor · failedNOSE DOOR OPEN WARNING INFLIGHT AT 14,000FT. MESSAGE CLEARED AT 230KTS . REMOVED & REPLACED NLG DOOR LT FWD PROXIMITY SENSOR IAW AMM 32-61-05, OPS CHECKED GOOD.Jun 4, 2018 · N441ZW · Cndair CL6002B19 · Landing Gear Position and WarningSDR A6WA2018053045854Window · crackedON ARRIVAL, HEARD A NOISE SIMILAR TO A BIRDSTRIKE AND NOTICED THE FIRST OFFICER`S WINDOW CRACKED. RECEIVED A WINDOW HEAT MESSAGE. COMPLIED WITH QRH. REDUCED SPEED TO 205 KIAS. DECLARED EMERGENCY. LANDED NORMALLY. CHANGED THE WINDOW.May 30, 2018 · N441ZW · Cndair CL6002B19 · Flight Compartment WindowsSDR A6WA201845679Warning Message · illuminated3769 INFLIGHT RECIEVED NWS INOP CAUTION MSG COMPLIED WITH QRH MSG PERSISTED LANDED WITH NWS INOP. COMPLIED WITH FIM RESET MSG CLEAREDMar 8, 2018 · N441ZW · Cndair CL6002B19 · Landing Gear Steering SystemSDR A6WA2018022145644Warning System · activatedRECEIVED LEFT HAND ANTI ICE CAUTION AFTER TAKEOFF. COMPLIED WITH QRH, MESSAGE DID NOT CLEAR. COWL SHOWED AMBER ON ANTI-ICE SYNOPTIC, COWL ANTI ICE SOV SHOWED CLOSED. LANDING WEIGHT 47,000LBS.Feb 19, 2018 · N441ZW · Cndair CL6002B19 · Air Intake Anti/De-Ice SystemSDR A6WA201845601Pump · inoperative3762 GEAR DISAGREE WARNING MESSAGE ON RETRACTION. C/W QRH. RETURNED TO ATW. CHANGED HYD PUMP AND DRAG BRACE. TEST NOT COMPLETED.Jan 30, 2018 · N441ZW · Cndair CL6002B19 · Hydraulic Pump (Electric/Engine), MainSDR A6WA2018012545596Bulkhead · damagedREAR PRESSURE BULKHEAD FORWARD FACE DAMAGED IN MULTIPLE LOCATIONS. SCREW DAMAGE. REPAIRED.Jan 24, 2018 · N441ZW · Cndair CL6002B19 · Fuselage Main, BulkheadSDR A6WA2018012545597Access Panel · damagedPANEL 332AB SCREW HOLE ELONGATED.Jan 24, 2018 · N441ZW · Cndair CL6002B19 · Horizontal Stabilizer, Plate/SkinSDR A6WA201845593Threshold · corrodedSERVICE DOOR THRESHOLD IS CORRODED.Jan 22, 2018 · N441ZW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA2018012545592Stringer · crackedSTR 3L IS CRACKED JUST FWD OF FRAME 379, IN THE CABIN.Jan 21, 2018 · N441ZW · Cndair CL6002B19 · Fuselage Main, Longeron/StringerSDR A6WA2018012545589Angle · cracked280 BEAM UPPER ANGLE STRIP IS SUSPECTED TO BE CRACKED JUST O/B OF RBL9, IN THE CABIN BELOW FLOOR.Jan 21, 2018 · N441ZW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA201845590Angle · damagedLOWER REPAIR ANGLES AT FS280 AND LBL12 AND RBL12 ARE DAMAGED.Jan 21, 2018 · N441ZW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA2018012545591Fitting · crackedBATHTUB FITTING IS CRACKED AT THE O/B SIDE OF LBL9 AT FS461, IN THE MAIN CABIN.Jan 21, 2018 · N441ZW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA2018012545594Support · corrodedPAX DOOR CUT OUT STRUCTURE CORRODED, FS 310.00 TO 349.00 STR 18L. REPLACED ANGLE SUPPORT IAW SRM 51-42-06, 51-42-21, 53-21-23.Jan 20, 2018 · N441ZW · Cndair CL6002B19 · Fuselage Main, StructureSDR A6WA2018012545585Angle · crackedANGLE CLIP IS CRACKED AT THE I/B SIDE OF RBL 36 AT FS 484 IN THE CABIN BELOW THE FLOOR.Jan 20, 2018 · N441ZW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA2018012545581Intercostal · corrodedINTERCOSTAL AT FS 319 - FS 333 AND STR 22L CORRODED.Jan 20, 2018 · N441ZW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA2018012545582Frame · crackedFRAME 605 IS CRACKED IN 2 SPOTS ABOVE AND BELOW STR 9L IN THE CARGO BAY.Jan 19, 2018 · N441ZW · Cndair CL6002B19 · Fuselage Main, FrameSDR A6WA2018012545578Rib · crackedLT PYLON LOWER RIB CRACKED AT FS605.Jan 19, 2018 · N441ZW · Cndair CL6002B19 · Nacelle/Pylon, Frame/Spar/RibSDR A6WA201845584Angle · crackedFS280 FWD UPPER ANGLE IS CRACKED.Jan 18, 2018 · N441ZW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA2018012545583Angle · crackedLT OBLIQUE ANGLE CRACKED ON AFT PRESSURE BULKHEAD.Jan 18, 2018 · N441ZW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA2018012545587Retainer · crackedCRACKED SEAL RETAINER ON PYLON PANEL 412BT.Jan 17, 2018 · N441ZW · Cndair CL6002B19 · Nacelle/Pylon Miscellaneous StructureSDR A6WA2018012545586Retainer · crackedPANEL 422BT SEAL RETAINER CRACKED.Jan 17, 2018 · N441ZW · Cndair CL6002B19 · Nacelle/Pylon Miscellaneous StructureSDR A6WA2018012545579Seat Track · corrodedSEAT TRACK ON LBL 9 HAS CORROSION BETWEEN FS 605 AND FS 621, IN THE CARGO BAY.Jan 15, 2018 · N441ZW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR A6WA2018012545580Fitting · crackedANGLE CLIP CRACKED AT THE O/B SIDE OF RBL 27 AT FS 484 IN THE CABIN BELOW THE FLOOR.Jan 15, 2018 · N441ZW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA2018011745567Fitting · crackedPANEL 422BT DIVIDER PANEL CLIP CRACKED. REPLACED CLIP IAW SRM 51-40-11, 51-42-06.Jan 15, 2018 · N441ZW · Cndair CL6002B19 · Nacelle/Pylon Miscellaneous StructureSDR A6WA2018011745570Tie Down · corrodedCARGO NET TIE DOWN FITTINGS CORRODED FROM FS 574.00 TO 605.00, LBL9. REPLACED FITTINGS IAW SRM 53-61-49, 51-41-02.Jan 14, 2018 · N441ZW · Cndair CL6002B19 · Cargo CompartmentsSDR A6WA201845568Door Sill · crackedCARGO DOOR OPENING LOWER SILL IS CRACKED AT FS 605.00. REPAIRED SILL IAW REO 601R-53-61-433 REV-C.Jan 13, 2018 · N441ZW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA2018011745569Tie Down · corrodedCARGO NET TIE DOWN FITTINGS CORRODED AT FS 559+96 AND 574.00, LBL27. REPLACED TIE DOWNS IAW SRM 53-61-49, 51-41-02.Jan 13, 2018 · N441ZW · Cndair CL6002B19 · Cargo CompartmentsSDR A6WA2017112745430Landing Gear · malfunctionedRECEIVED A GEAR UP DISAGREE AND NOSE DOOR WARNING AFTER TAKE OFF. COMPLIED WITH QRH, NOSE WHEEL DID NOT RETRACT, MLG UP AND LOCKED, NOSE SHOWING DOWN AND LOCKED. REMOVED AND REPLACED NOSE LANDING GEAR BRACKET SUB ASSY, RIGHT PROXIMITY SENSORS, WOW NR 2 ANDNov 17, 2017 · N441ZW · Cndair CL6002B19 · Nose/Tail Landing GearSDR A6WA2017092645306Beam · damagedDURING SCHEDULED INSPECTION OF THE AFT PRESSURE BULKHEAD, INSPECTION FOR THE CARGO DOOR CROSS BEAM DAMAGED. DAMAGE WAS CAUSED BY THE CARGO DOOR CABLE.Sep 24, 2017 · N441ZW · Cndair CL6002B19 · Fuselage Main, BulkheadSDR A6WA2017092645307Bulkhead Web · crackedDURING SCHEDULED INSPECTION OF THE AFT PRESSURE BULKHEAD, A CRACK WAS FOUND AT LBL 28 JUST ABOVE THE TOP OF THE CARGO DOOR TRACK.Sep 23, 2017 · N441ZW · Cndair CL6002B19 · Fuselage Main, BulkheadSDR A6WA2017092645308Bulkhead · damagedDURING SCHEDULED INSPECTION OF THE AFT PRESSURE BULKHEAD, DAMAGE WAS FOUND AT BS 621, RBL 36.2, WL 103. DAMAGE WAS CAUSED BY A SCREW PROTRUDING THROUGH THE CARGO BAY LINERS AND CONTACTING THE BULKHEAD SURFACE.Sep 23, 2017 · N441ZW · Cndair CL6002B19 · Fuselage Main, BulkheadSDR A6WA201745164Bpsu · malfunctionedFLAPS FAILED CAUTION MESSAGE DURING CRUISE AT 31,000 FT. FLAPS INDICATED ZERO. NO FLAP HANDLE INPUTS. REPLACING THE RT BPSU.Aug 6, 2017 · N441ZW · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR A6WA201745162Flap System · malfunctionedDURING CRUISE FLT AT 28000 FT RECEIVED FLAP FAIL CAUTION MESSAGE. COMPLIED WITH QRH & FLAPS SHOW ZERO. PERFORMED FLAP RESET PROCEDURE IAW 98-018G BOX 11 & FLAPS RESET.Aug 5, 2017 · N441ZW · Bombdr CL6002D15 · Trailing Edge Flap Control System
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