N414ZW

Service difficulty reports · 203

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 = 'N414ZW' 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 A6WA201040898Structure · crackedPAX DOOR STAIR STRUCTURE IS CRACKED NEXT TO FWD HANDRAIL 1 BRACKET CUT OUT CRACKED SECTION AND FABRICATED NEW SECTION IAW REO 601R-52-11-702, REV C, REPAIR Z.Nov 27, 2010 · N414ZW · Cndair CL6002B19 · Passenger/Crew DoorsSDR A6WA201040899Drag Angle · crackedPAX DOOR AFT DRAG ANGLE CRACKED. REMOVED CRACKED SECTION OF AFT DRAG ANGLE, THE INSTALLED NEW SERVICEABLE SECTION IAW B/A REO 601R-52-11-513, REV A.Nov 27, 2010 · N414ZW · Cndair CL6002B19 · Passenger/Crew DoorsSDR A6WA201040891Anchor Fitting · corrodedRT WINDSCREEN ANCHOR FITTING IS CORRODED. R & R TR WINDSCREEN ANCHOR FITTING IAW AMM 20-21-07.Nov 27, 2010 · N414ZW · Cndair CL6002B19 · Passenger Compartment EquipmentSDR A6WA201040873Skin · chafedLT LOWER CORE COWL CHAFED FROM BLOCKER DOOR NEXT TO FWD LATCHES BLENDED DAMAGE IAW REO 601R-71-12-232, REV D AND WAS FOUND TO BE WITHIN ALLOWABLE LIMITS. DAMAGE MEASURES 4.00 LONG, 0.25 WIDE AND .007 DEEP. TREATED AREA IAW CMM 20-01-11 AND SRM 51-25-06.Nov 23, 2010 · N414ZW · Cndair CL6002B19 · Nacelle/Pylon, Plate/SkinSDR A6WA201140028Cargo Track · corrodedBAGGAGE COMPARTMENT TIE DOWNS NR2 AND NR3 ON LBL 27 AND NR1 AND NR2 ON LBL9 ARE CORRODED. R & R 2EA TIE DOWNS ON LBL 9.0 & 2 EA TIE-DOWNS ON LBL 27.0 IAW SRM 51-41-02.Nov 22, 2010 · N414ZW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR A6WA201040892Hinge · damagedLT NR2 ELEVATOR HINGE ON BOTH ELEVATOR AND HORIZ STABILIZER HAVE MINOR TOOLING DAMAGE. B.ENDED OUT MINOR TOOLING DAMAGE IAW REO 601R-55-11-061, REO 601R-55-21-080.Nov 21, 2010 · N414ZW · Cndair CL6002B19 · Elevator StructureSDR A6WA201040872Bulkhead · chafedAFT SIDE OF RT 280 BULKHEAD CHAFED FROM GALLEY ACCESS DOOR. CUT OUT DAMAGE FROM AFT RT SIDE 280 BULKHEAD, BLENDED CHAFED AREA ON CHANNEL IAW REO 601R-53-11-1727 FAB, WEB FILLER AND WEB DOUBLER PRIMED TOP COAT INSTALLED PART IAW REO 601R-11-1727, REV D.Nov 21, 2010 · N414ZW · Cndair CL6002B19 · Fuselage Main, BulkheadSDR A6WA201140029Frame · crackedFRAME STA 484, LBL27 INBD CLIP IS CRACKED IN UPPER CORNER. REMOVED UNERVICEABLE CLIP, DUPLICATED AND INSTALLED SERVICEABLE CLIP IAW SRM 51-42-00, 51-42-21, 53-41-43.Nov 10, 2010 · N414ZW · Cndair CL6002B19 · Fuselage Main, FrameSDR A6WA201040756Overheat Loop · malfunctionedGOT ANTI-ICE DUCT WARNING MESSAGE RT AFTER TAKEOFF. RAN QRH. ANTI-ICE SELECTED OFF AND SYNOPTIC PAGE SHOWED RT FUSELAGE RED. R & R BLEED LEAK DETECTOR LOOP A15WK IAW 36-21-04. OPS CK OF BLEED AIR LEAK DETECTION SYS GOOD AT THIS TIME.Oct 4, 2010 · N414ZW · Cndair CL6002B19 · Overheat DetectionSDR A6WA200840629Vane · gougedLT WING INBD FLAP, VANE LEADING EDGE GOUGED AT 3 PLACES. 1ST GOUGE AT FLAP STA 57.00 WIDTH .500", LENGTH 1", DEPTH .030". 2ND GOUGE AT FLAP STA 105 WIDTH .500", LENGTH 1.00", DEPTH .007". 3RD GOUGE AT FLAP STA 141 WIDTH .500" LENGTH 1.00", DEPTH .010". LT Dec 8, 2008 · N414ZW · Cndair CL6002B19 · Trailing Edge FlapsSDR A6WA200840632Stop · crackedBUTE DOOR HINGE PANEL 694KB STOP ASSY CRACKED. .550" L X .300 W X .090 D STOP ASSY ON BUTE DOOR HINGE PANEL 694KB R&R IAW CRJ200 SRM 51-42-06 AND 51-23-00.Dec 7, 2008 · N414ZW · Cndair CL6002B19 · DoorsSDR A6WA200840626Visor · crackedVERTICAL STAB. LT UPPER VISOR CRACKED AND BENT. CRACK .250 LONG. VERTICAL STAB LT UPPER VISOR REPLACED IAW CRJ 200Dec 5, 2008 · N414ZW · Cndair CL6002B19 · Vertical StabilizerSDR A6WA200840637Stringer · corrodedSTRINGER 27 FOUND CORRODED BTW FS 333. TO FS 349. CORROSION ON STR 27 BTW FS 333 TO FS 349. REMOVED IAW SRM 51-12-00. EDDY CURRENT PERFORMED ON BLEND OUT AREA, NO CRACKS FOUND. SURFACE FINISH RESTORED.Dec 5, 2008 · N414ZW · Cndair CL6002B19 · Fuselage Main, Longeron/StringerSDR A6WA200840634Skin · gougedRT WING INBD FLAP VANE L/E SKIN AT STA 57.00 GOUGED OVER LIMITS IAW REO 601R-57-52-004. RT WING INBD FLAP VANE LEADING EDGE AT STA 57.00 REPLACED IAW SRM 51-42-13.Dec 4, 2008 · N414ZW · Cndair CL6002B19 · Trailing Edge FlapsSDR A6WA200840643Stiffener · crackedCRACK FOUND ON PAX DOOR MOTOR ASSIST STIFFENER AFT WEB. PAX DOOR MOTOR ASSIST STIFFENER AFT WEB REPLACED IAW SRM 51-42-06 AND 51-42-13.Dec 3, 2008 · N414ZW · Cndair CL6002B19 · Passenger/Crew DoorsSDR A6WA200840636Bulkhead · crackedCRACK FOUND ON PILOT BULKHEAD FS 280 RBL 9. CRACK LENGTH IS .500. PILOT BULKHEAD FS 280 RBL 9 REPAIRED IAW CRJ 200 REO 601R-53-11-171 REV D.Dec 3, 2008 · N414ZW · Cndair CL6002B19 · Fuselage Main, BulkheadSDR A6WA200840628Bracket · crackedCRACK FOUND ON BRACKET FS 280 LBL 9 INBD CRACK LENGTH IS .250. BRACKET AT FS 280 LBL 9 REMOVED IAW SRM 51-54-13 AND 51-42-21. NEW BRACKET ST FS 280 LBL INSTALL IAW SRM 51-42-20.Dec 3, 2008 · N414ZW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200840627Bracket · crackedCRACK FOUND ON BRACKET FS 280 RBL 9 INBD CRACK LENGTH IS .200. BRACKET AT FS 280 RBL 9 REMOVED IAW SRM 51-42-13 AND 51-42-21. NEW BRACKET AT FS RBL 9 INSTALL IAW 51-42-20.Dec 3, 2008 · N414ZW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200840633Attach Fitting · crackedCRACK FOUND ON INTERCOSTAL CLIP AT FS 484 RBL 27. CRACK LENGTH IS .400. INTERCOSTAL CLIP AT FS 484 RBL 27 R&R.Dec 3, 2008 · N414ZW · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR A6WA200840642Scuff Plate · corrodedSERVICE DOOR LOWER SCUFF PLATE FOUND CORRODED, 3 PLACES APPROX .500 X .500, .026 DEEP. CORROSION REMOVED IAW SRM 51-21-26 AND FOUND OUT OF LIMITS IAW SRM 53-00-00. LOWER SERVICE DOOR SCUFF PLATE REPLACED IAW SRM 51-41-02.Dec 2, 2008 · N414ZW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200840635Lever · gougedGOUGE FOUND ON PAX DOOR PULL IN LEVER, FWD UPPER PACK DOOR PULL IN LEVER REPLACED IAW AMM 20-21-00-910-801.Dec 2, 2008 · N414ZW · Cndair CL6002B19 · Passenger/Crew DoorsSDR A6WA200840491Regulator · out of rigAIRCRAFT REQUIRES 50% LT AILERON TRIM FOR LEVER FLIGHT, THE YOKE HAS LT TO RT SLOP FEEL ON FINAL APPROACH. THE YOKE HAD TO BE MOVED APPROXIMATELY 2-3 INCHES BEFORE RESPONSE. (A) RIGGED LT AND RT AILERON TENSION REGULATORS & RIGGED LT AND RT AILERON OUTBOARD Jun 8, 2008 · N414ZW · Cndair CL6002B19 · Aileron Control SystemSDR A6WA200740008Aileron · ratchetingNOTICEABLE HANGUP/LATCH IN AILERON ROLL CONTROL ON BOTH YOKES NEAR NEUTRAL POSITION, NOTICED IN FLIGHT, 6000-7000 FT WHILE HAND FLYING. (M)Jan 9, 2007 · N414ZW · Cndair CL6002B19 · Aileron Control SystemSDR A6WA200640422Channel · crackedRIGHT MLG WHEEL WELL HYDRAULIC TRANSDUCER HAT CHANNEL P/N 601R75262-157 CRACKED APPROX .2 INCH LONG. MAINTENANCE REPAIRED IAW BSC EO 601R-53-0044E BY REMOVING DAMAGED BRACKET FABRICATING NEW BRACKET AND INSTALLING. (M)Dec 29, 2006 · N414ZW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200640423Channel · crackedLEFT MLG WHEEL WELL HYDRAULIC TRANSDUCER HAT CHANNEL P/N 601R75262-159 CRACKED APPROX .2 INCHE LONG. MAINTENANCE REMOVED AND REPLACED CHANNEL IAW BSC SR 601R-53-0044E. (M)Dec 29, 2006 · N414ZW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200640392Shutoff Valve · malfunctionedON TAKEOFF ROLL CAUTION MESSAGE FOR LT AND RT HIGH PACK PRESSURE, ABORT TAKEOFF. C/W QRH. RAN UP 2ND TIME AND BOTH HI PRESS CAUTION MESSAGE AGAIN. REMOVED AND REPLACED BOTH PRSOV VALVES IAW AMM, OPS CHECK GOOD. REMOVED PN 32156222, RT SN 1319 (TT 9618 HRS)Nov 27, 2006 · N414ZW · Cndair CL6002B19 · Cabin Cooling SystemSDR A6WA200640349Stringer · damagedPIT DAMAGE ON STRINGER NR 7L OF FS 409 DAMAGE IS .011 DEEP LOCATED .250 BELOW RIVET ROW. MAINTENANCE REPAIRED DAMAGE IAW SRM 53-00-31, 51-12-00 AND EO 601R-53-9798. (M)Sep 7, 2006 · N414ZW · Cndair CL6002B19 · Fuselage Main, Longeron/StringerSDR A6WA200540290Selector Valve · inoperativeON APPROACH, WHEN SELECTED GEAR DOWN GOR (GEAR DISAGREE AND NOSE DOOR) MASTER WARNING. NLG INDICATED UP AND LOCKED MLG DOWN. CYCLED GEAR WITH SAME INDICATIONS. PERFORMED QRH AND OBTAINED 3 GREEN. REMOVED AND REPLACED NLG SELECTOR VALVE AMM. OPS CHECK GOODAug 18, 2005 · N414ZW · Cndair CL6002B19 · Landing Gear Retraction/Extension SystemSDR A6WA200540127Line · chafedHYDRAULIC NR 1 LOW PRESSURE MESSAGE INFLIGHT ON CLIMBOUT. QUANTITY INDICATES ZERO. REMOVED AND REPLACED HYDRAULIC SUPPLY LINE TO CASE DRAIN ASSY REF 29-11-02, RAN ENGINE LEAK CHECK. OPS CHECK GOOD. (K)Mar 27, 2005 · N414ZW · Cndair CL6002B19 · Hydraulic System, MainSDR A6WA200540062Angle · crackedFOUND RT FS 621 ANGLE IS CRACKED. REPAIRED RT FS 621 ANGLE IAW BOMBARDIER REO 601-53-61-117 REV A. (M)Feb 2, 2005 · N414ZW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200540067Angle · crackedFOUND LEFT FS 621 ANGLE IS CRACKED. REPAIRED LEFT FS 621 ANGLE IAW BRAS EO 601R-53-61-117. (M)Feb 2, 2005 · N414ZW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200540041Skin · dentedSKIN IS DENTED ON THE LT SIDE SKIN PANEL BETWEEN RS 108.25 AND 113.98 THE DENT MEASURES 2.2 INCHES LONG X 2 INCHES WIDE. PERFORMED A MAJOR REPAIR TO THE RUDDER SKIN ON LT SIDE BY TRIMMING OUT DAMAGE, LPI, FABED DOUBLER AND INSTALLED IAW EO. (K)Feb 2, 2005 · N414ZW · Cndair CL6002B19 · Rudder, Plate/SkinSDR A6WA200540040Fastener · mislocatedUNABLE TO ACHIEVE EDGE DISTANCE ON JOINT STRAP (PN 601R1004654) WHILE COMPLYING WITH SB 601R57037 DUE TO EXISTING FASTENER BEING MISLOCATED. PERFORMED A MAJOR ALTERATION TOO, BY SHIFTING THE CUTLINE TO PROVIDE MINIMUM EDGE DISTANCE ON THE EXISTING FASTENERS, Feb 2, 2005 · N414ZW · Cndair CL6002B19 · FastenersSDR A6WA200540066Angle · crackedPAX DOOR AFT DRAG ANGLE IS CRACKED 2 INCHES LONG JUST FORWARD OF DOOR ASSIST PULLEY MOUNT. REPAIRED ANGLE BY INSTALLING SPLICE ANGLE P/N 601R31772-5 AND IAW BOMBARDIER, INC REO 601R-52-11-513. (M)Jan 31, 2005 · N414ZW · Cndair CL6002B19 · Passenger/Crew DoorsSDR A6WA200540029Angle · crackedLT FS 621.00 ANGLE IS CRACKED. CUT AWAY DAMAGED SECTION OF ANGLE AND INSTALLED A REPAIR ANGLE IAW REO. (K)Jan 31, 2005 · N414ZW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200540065Angle · crackedLEFT FS 484 ANGLE AT LBL 36 IS CRACKED. REPAIRED LEFT FS 484 ANGLE IAW BRAS REO 601R-53-41-059. (M)Jan 30, 2005 · N414ZW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200540064Angle · crackedRT FS 484 ANGLE AT RBL 36 IS CRACKED. REPAIRED RT FS 484 ANGLE IAW BRAS EO 601R-53-41-059. (M)Jan 30, 2005 · N414ZW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200540063Angle · crackedFOUND RT FS 484 ANGLE AT RBL 27 IS CRACKED. REPAIRED RT FS 484 ANGLE IAW BRAS EO 601R-53-41-059. (M)Jan 30, 2005 · N414ZW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200540028Skin · corrodedMWC 170 CORROSION EXISTS ON LOWER WING PLANK UNDER FUEL PANEL 510AB. PERFORMED A MAJOR REPAIR BY REMOVING CORROSION IAW REO. (K)Jan 27, 2005 · N414ZW · Cndair CL6002B19 · Wing, Plate/SkinSDR A6WA200540027Skin · corrodedFOUND CORROSION ON RT LOWER WING PLANK UNDER THE FOLLOWING FUEL PANELS 640BB AND 650GB. PERFORMED A MAJOR REPAIR BY REMOVING CORROSION IAW REO. (K)Jan 27, 2005 · N414ZW · Cndair CL6002B19 · Wing, Plate/SkinSDR A6WA200540061Floor Support · crackedFOUND CABIN FLOOR SUPPORT STRUCTURE AT FS 280, RBL 9 BOTH CLIPS ARE CRACKED IN RADIUS AT TOP. REPAIRED CABIN FLOOR SUPPORT STRUCTURE AT FS 280 RBL 9 IAW BRAS EO 601R-53-5924. (M)Jan 26, 2005 · N414ZW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200540025Bushing · migratedLT MAIN LANDING GEAR AFT TRUNNION BUSHING IS MIGRATED .007 INCH. REMOVED MIGRATED BUSHING AND INSTALLED A 2ND OVERSIZED BUSHING MODIFIED TO A 1ST OVERSIZED BUSHING IAW BOMBARDIER EO 601R-57-21-003 REV B AND EO 601R-57-5907A. (M)Jan 26, 2005 · N414ZW · Cndair CL6002B19 · Main Landing GearSDR A6WA200540032Floor Support · crackedCABIN FLOOR SUPPORT STRUCTURE AT FS280, LBL 9.0. THE OB CLIP IS CRACKED IN RADIUS AT TOP. (K) REMOVED CRACKED CLIP AND INSTALLED NEW FABRICATED CLIP IAW BRAS EO 601R-53-5924. (M)Jan 26, 2005 · N414ZW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200540026Bushing · migratedRT MLG AFT TRUNNION BUSHING IS MIGRATED .046 INCH. REMOVED MIGRATED BUSHING AND INSTALLED 2ND OVERSIZED BUSHING MODIFIED TO A 1ST OVERSIZED IAW EO.Jan 26, 2005 · N414ZW · Cndair CL6002B19 · Main Landing Gear Attach SectionSDR A6WA200540068Sill · crackedFOUND CARGO DOOR SILL PLATE AT FS 589 CRACKED. REPAIRED CARGO DOOR SILL PLATE IAW BOMBARDIER REO 601R-53-61-433. (M)Jan 25, 2005 · N414ZW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200540031Intercostal · crackedRT SIDE FS621 THROUGH FS623.3 INTERCOSTAL AT STR 14R IS CRACKED IN RADIUS APPROXIMATELY 1.1 INCH LONG. REMOVED AND REPLACED FS 621-625.3 INTERCOSTAL ANGLE AT STRINGER 14R IAW BRAS EO 601R-53-5933. (M) (K)Jan 24, 2005 · N414ZW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200540030Intercostal · crackedLT SIDE FS621 THROUGH FS 625.3 INTERCOSTAL AT STR 14L IS CRACKED IN RADIUS APPROXIMATELY 1.0 INCH LONG. (K) REMOVED AND REPLACED FS 621-625.3 INTERCOSTAL ANGLE AT STRINGER 14L IAW BRAS EO 601R-53-5933. (M)Jan 24, 2005 · N414ZW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200440200Bpsu · out of rigFLAPS FAIL AT 20 DEGREES. 49700 LBS. LANDING WEIGHT LIGHT BREAKING. 5 MAX BTMS READING, LIGHT TOUCHDOWN. FOUND LT AND RT BRAKE POSITION SENSOR UNITS (BPSU) BOTH OUT OF RIG. RIGGED LT AND RT BPSU`S REF AMM, FLAPS OPS GOOD.Dec 9, 2004 · N414ZW · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR A6WA200340198Tube · failedNR 2 HYDRAULIC LOW PRESSURE LIGHT ILLUMINATED, FLUID INDICATES ZERO. REMOVED AND REPLACED HYDRAULIC TUBE ASSEMBLY. (M)Dec 21, 2003 · N414ZW · Cndair CL6002B19 · Hydraulic System, MainSDR A6WA200340090Striker · damagedPASSENGER DOOR SEAL STRIKER AT FS 310 IS DAMAGED MIDWAY TOP TO BOTTOM. REPAIRED DAMAGED PASSENGER DOOR SEAL STRIKER AT FS 310 IAW BOMBARDIER REO 601R-52-11-008 REV B. (M)May 28, 2003 · N414ZW · Cndair CL6002B19 · Passenger/Crew Doors
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