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 A6WA201040322Fitting · crackedFS 280 FLOOR SUPPORT LBL INBD CLIP IS CRACKED. R & R CLIP PN 601R3111357 IAW REO 601R-53-11-138, REV NC.Apr 27, 2010 · N441ZW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA201040323Fitting · crackedFS 280 FLOOR SUPPORT RBL 9 INBD CLIP IS CRACKED. R & R CLIP IAW SRM.Apr 27, 2010 · N441ZW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA201040292Plate · crackedCARGO DOOR LANDING PLATE CRACKED AT FS 589. REPAIRED LANDING PLATE IAW 601R-53-61-433, REV B.Apr 26, 2010 · N441ZW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA201040328Lug · gougedRT INBD FLAP HINGE BOX AFT LUGS ON WING ARE GOUGED (DWG 601R10315 REF). REPAIRED DAMAGED LUGS ON TR INBD FLAP, INBD HINGE BOX AFT LUGS IAW REO 601R-57-21-1276.Apr 24, 2010 · N441ZW · Cndair CL6002B19 · Trailing Edge FlapsSDR A6WA201040291Intercostal · crackedRT FS 484 INTERCOSTAL, INBD CLIP APPEARS CRACKED. RBL 27 R & R UNIT SERVICEABLE CLIP PN 601R31171-9, PO 961346 AT RT FS 484, RBL 27. INBD SIDE ALL WORK DONE IAW REO 601R-53-41-059, REV B AND SRM 51-25-16.Apr 22, 2010 · N441ZW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA201040276Coalescer Bag · odorAFTER APU START UP JET-A SMELL IN COCKPIT. R & R PACK NR 1 COALESCER IAW 21-51-13 IAW AMM 21-51-13. OPS CHECK GOOD, SUSPECT APU OVER OIL SERVICED, CLEANED UP OIL, NO LEAKS.Mar 23, 2010 · N441ZW · Cndair CL6002B19 · Humidity Control SystemSDR A6WA201040232Apu · odorAFTER APU START-UP, JET A SMELL IN COCKPIT. R & R NR 1 PACK COALESCER IAW AMM 21-51-13. OPS CK GOOD, SUSPECT APU OIL OVERSERVICED, CLEANED UP OIL, NO LEAKS NOTED.Mar 23, 2010 · N441ZW · Cndair CL6002B19 · APU Core EngineSDR A6WA200940013Pcu · out of rigDURING FLT AN ABNORMAL AMOUNT OF LT AILERON TRIM WAS REQUIRED F/O WINGS LEVEL FLIGHT, FLT CTL POS IND, LT AILERON UP AND RT AILERON CTR. FOUND LT AILERON PCU OUT OF RIG. RIGGED LT AILERON PCU IAW AMM 27-11-00. OPS CHECK GOOD AT THIS TIME. (K)Jan 11, 2009 · N441ZW · Cndair CL6002B19 · Aileron Control SystemSDR A6WA200840370Bracket · crackedLT ENGINE INLET, QTY (2) BRACKETS CRACKED AT 4 & 5 O`CLOCK POSITION NEAR LOWER OUTBOARD T/R ACTUATOR (LOOKING AFT). QTY (2) BRACKETS AT 4 & 5 O`CLOCK POSITION NEAR THE LOWER OUTBOARD T/R ACTUATOR OF THE LT ENGINE INLET REPLACED IAW CRJ 200 SRM 51-42-06. (S)Apr 22, 2008 · N441ZW · Cndair CL6002B19 · Nacelle/Pylon, Attach FittingsSDR A6WA200840369Bulkhead · crackedREAR PRESSURE BULKHEAD CRACKED AROUND LINTER FITTING ATTACHMENT POINT. REPAIRED IAW CRJ 200 REO 601R-53-61-1230 REV D. (S)Apr 21, 2008 · N441ZW · Cndair CL6002B19 · Fuselage Main, BulkheadSDR A6WA200840368Web · crackedCRACK FOUND ON WEB STRUCTURE FS 280 RBL 9. REPAIRED IAW REO 601R-53-11-171 REV D. (S)Apr 21, 2008 · N441ZW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200840367Bracket · crackedBRACKET CRACK ON FS 280 LBL 9 ON FLOOR STRUCTURE. ON FS 280 LBL 9 ON FLOOR STRUCTURE (2) BRACKET REPLACED IAW SRM 51-42-21 AND SRM 51-42-06. (S)Apr 21, 2008 · N441ZW · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR A6WA200840280Flap System · inoperativeFLAPS FAILED AT 20 DEGREES, COMPLIED WITH QRH, LANDED DCA. LANDED NORMAL, MAX BTMS READING 4 FOR ALL BRAKES. RESET PER AWAC SUPPLEMENT 98-018B. (M)Mar 30, 2008 · N441ZW · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR A6WA200840181Light · shortedBOTH CAPTAIN AND FIRST OFFICER MAP LIGHTS ARE OUT, CBP2 U6 POPPED. RECYCLED BREAKER ONCE, FIRST OFFICER MAP LIGHT SPARKED AND SHORTED WHEN MOVED, CBP2 U6 POPPED AGAIN. (M)Mar 16, 2008 · N441ZW · Cndair CL6002B19 · Flight Compartment LightingSDR A6WA200840097Brake Assy · malfunctionedFLAPS HALF SPEED MESSAGE ON ED2. REMOVED AND REPLACED MOTOR BRAKE UNIT IAW 27-52-05. OPS CHECK GOOD AT THIS TIME. (M)Feb 18, 2008 · N441ZW · Cndair CL6002B19 · Trailing Flap Position Indicating SystemSDR A6WA200840096Detector · malfunctionedON SHORT FINAL FLAPS FAILED AT 45 DEGREES. RAN QRH. NO FURTHER PROBLEMS. REMOVED AND REPLACED SKEW DETECTION UNIT IAW AMM 27-51-15. OPS CHECK GOOD IAW AMM 27-54-00. (K)Feb 17, 2008 · N441ZW · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR A6WA200840015Warning System · activatedNOSE GEAR DISAGREE WHEN GEAR RETRACTED. NOSE GEAR SHOWED RED, ALSO HEARD CLICKING NOISE BELOW FEET. AIR RETURN TO BTV, UPON GEAR EXTENSION GEAR SHOWED 3 GREEN DOWN AND LOCKED. (K)Feb 16, 2008 · N441ZW · Cndair CL6002B19 · Landing Gear Position and WarningSDR A6WA200840060Flap · stuckINFLIGHT, FLAPS STUCK AT 42 DEGREES WHEN SELECTED 45 DEGREES. AFTER 10 MINUTES, FLAPS WENT TO 45 DEGREES, NO FAULT MESSAGES ILLUMINATED. (K)Feb 1, 2008 · N441ZW · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR A6WA200840058Flap · failedFLAPS FAIL CAUTION IN FLIGHT. FLAPS FAILED AT 40 DEGREES. EMERGENCY LANDING DECLARED. LANDING UNEVENTFUL. COMPLIED WITH RESET PROCEDURE IAW AWAC SUPPLEMENT 98-108B STEPS 1.3 AND 1.4, FLAPS SYSTEM RESET OK. (K)Feb 1, 2008 · N441ZW · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR A6WA200840059Bpsu · faultyFLAPS FAIL CAS MESSAGE, BOTH FLAPS INDICATE 42 DEGREES. PERFORMED FLAPS RESET PROCEDURE IAW AWAC SUPPLEMENT 98-018B STEPS 1.3 AND 1.4 FLAPS RESET OK. (FERRIED TO ORF DUE TO HISTORY) LT BPSU WON`T STAY IN RIG. REMOVED AND REPLACED LT PBSU IAW AMM 27-51-10-. Jan 31, 2008 · N441ZW · Cndair CL6002B19 · Trailing Flap Position Indicating SystemSDR A6WA200840007Trim System · malfunctionedON CLIMBOUT WITH FLAPS 8 DEGREES, STAB AND MACH TRIM WOULDN`T REMAIN ENGAGED. COMPLIED WITH QRH, RE-ENGAGED STAB AND MACH TRIM, BOTH DISENGAGED AND WOULDN`T REENGAGE. SET FLAPS TO 2- DEGREES, RETURNED TO DEPARTURE. REMOVED AND REPLACED FO`S HORIZONTAL STAB Jan 4, 2008 · N441ZW · Cndair CL6002B19 · Stabilizer Control SystemSDR A6WA200740648Pcu · unknownEXCESSIVE LEFT DOWN AILERON TRIM REQUIRED FOR LEVEL FLIGHT, REQUEST INSPECTION. REMOVED AND REPLACED NR 1 AILERON PCU PER AMM 27-14-01, OPS AND LEAK CHECK GOOD. RIG CHECK PER AMM 27-11-00, RIG CHECK GOOD. (M)Nov 27, 2007 · N441ZW · Cndair CL6002B19 · Aileron Control SystemSDR A6WA200640388Door Seal · unknownSERVICE DOOR DIFFICULT TO LATCH AND UNLATCH. REMOVED AND REPLACED SERVICE DOOR SEAL IAW 52-41-07. (K)Nov 19, 2006 · N441ZW · Cndair CL6002B19 · Service DoorsSDR A6WA200640155Floor Support · crackedFOUND CARGO FLOOR SUPPORT ANGLE AT FS 621 CRACKED APPROX .5 INCH RIGHT SIDE. MAINTENANCE REPAIRED RT FS 621 FLOOR SUPPORT ANGLE BY REMOVING DAMAGED ANGLE AND INSTALLING NEW ANGLES AND STRAP IAW BOMBARDIER REO 601R-53-61-117 REV C. (M)Apr 16, 2006 · N441ZW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200640154Floor Support · crackedFOUND CARGO FLOOR SUPPORT ANGLE AT FS 621 CRACKED APPROX .5 INCH LEFT SIDE. MAINTENANCE REPAIRED LT FS 621 FLOOR SUPPORT ANGLE BY REMOVING DAMAGED ANGLE AND INSTALLING NEW ANGLES AND STRAP IAW BOMBARDIER REO 601R-53-61-117 REV C. (M)Apr 16, 2006 · N441ZW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200640153Intercostal · crackedFOUND INTERCOSTAL CRACKED AT FS 484 RBL 36 IN UPPER RADIUS. MAINTENANCE REPAIRED FS 484.0 INTERCOSTAL AT RBL 36 BY REMOVING DAMAGED FLANGE AREA, FABRICATING NEW ANGLE ABD INSTALLING IAW BOMBARDIER REO 601R-53-41-059 REV A AND BSC STANDARD REPAIR 601R-53-0030AApr 16, 2006 · N441ZW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200640152Angle · crackedFOUND ANGLE CRACKED AT FS 484 RBL 27 IN UPPER CORNER APPROX .5 INCH IN RADIUS. MAINTENANCE FABRICATED REPAIR ANGLE FROM MATERIAL P/N 56144-14 IAW BSC STANDARD REPAIR 601R-53-0029 AND INSTALLED ANGLE AT FS 484 RBL 27 IAW BOMBARDIER AEROSPACE REO 601R-53-41-059Apr 16, 2006 · N441ZW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200640151Angle · crackedFOUND FS 625 OBLIQUE ANGLE IS CRACKED .500 INCH LONG. MAINTENANCE REMOVED CRACKED ANGLE AND INSTALLED NEW ANGLE P/N 601-35012-51, IAW CRJ SRM 51-42-06. (M)Apr 14, 2006 · N441ZW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200640069Actuator · inoperativeBETWEEN GEAR RETRACTION AND EXTENSION, HEARD FLAPPING SOUND FROM NOSE AREA. REMOVED AND REPLACED NLG DOOR ACTUATOR. (K)Feb 5, 2006 · N441ZW · Cndair CL6002B19 · Landing Gear Door ActuatorSDR A6WA200440201Skin · lightning strikePERFORMED PERMANENT REPAIR TO LIGHTNING STRIKE DAMAGE AT FS 280 TO FS 349 ALONG STRINGER L26 (5) LOCATIONS. PERFORMED PERMANENT REPAIR TO FUSELAGE AT FS 280 TO FS 349 ALONG STRINGER 26L IAW EO 601R-53-5672.Nov 26, 2004 · N441ZW · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR A6WA200440202Angle · crackedRT FS 484.00 AT RBL 36 ANGLE CRACKED.Nov 26, 2004 · N441ZW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200440196Skin · lightning strikePERMANENT REPAIR TO LIGHTNING STRIKE DAMAGE AT FS 755, STRINGER 25L. REPAIRED DAMAGE BY ENLARGING FASTENER HOLE TO .1875 INCH AND INSTALLED RIVET MS2042AD6 IAW BRAS WO 601R-53-5674.Nov 26, 2004 · N441ZW · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR A6WA200440195Intercostal · crackedINTERCOSTAL CRACKED IN RADIUS APPROX 1.1 INCH LONG, FS 621- FS 625.1, STR 14R. REMOVED CRACKED ANGLE, INSTALLED NEW ANGLE PN 601-35012-52 USING MS20470AS5 RIVETS IAW CRJ SRM 57-040-06.Nov 24, 2004 · N441ZW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200440130Control Unit · failedFLAP FAIL MESSAGE ILLUMINATED AT 13000 FT, COMPLIED WITH QRH PERFORMED ZERO FLAP LANDING, BRAKES APPLIED AT LESS THAN 80 KNOTS, MAX BRAKES TEMP INDICATION WAS '2'. TOUCHDOWN AT 172 KNOTS. REMOVED AND REPLACED FECU IAW AMM 27-51-05. COMPLIED WITH OPS CHECK OSep 7, 2004 · N441ZW · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR A6WA200340197Control Handle · failedUNCOMMANDED FLAP ACTUATION IN FLIGHT AT CRUISE 0-6 DEGREES WITH FLAP SETTING ZERO ALL OTHER SETTINGS NORMAL OPERATION. REMOVED AND REPALCED FECU AND FLAP HANDLE. (M)Dec 20, 2003 · N441ZW · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR A6WA200340137Tail Cone · damagedDAMAGE TO TAIL CONE, RESULTING IN DELAMINATION OF INNER AND OUTER SKINS AND CORE DAMAGE. REPAIR, FABRICATED SKIN PLIES TWO EACH AND EXTRA PLY ONE EACH FOR EACH DAMAGED SKIN FROM KEVLAR 49 STYLE 281 FABRICATED PREPEG CMS532-01. EXTRA PLY TO EXTEND .5 INCHES PSep 18, 2003 · N441ZW · Cndair CL6002B19 · Aerodynamic Fairings
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