N427ZW

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 = 'N427ZW' 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 A6WA201040024Handle · crackedCARGO DOOR HANDLE ASSY IS CRACKED (.600") CARGO DOOR HANDLE REPLACED IAW SRM 51-42-21 AND DWG PL601R35027.Nov 27, 2009 · N427ZW · Cndair CL6002B19 · Cargo/Baggage DoorsSDR A6WA201040027Bulkhead · mislocatedQTY (1) REDUNDANT HOLE AND QTY (2X) DRILL MARKS EXISTS IN PRESSURE BULKHEAD WEB AT FS 559.00, RBL 22.5, WL 50.0 QTY (1) REDUNDANT HOLE AND QTY (2X) DRILL MARKS REPAIRED IAW REO 601R-53-41-1117.Nov 27, 2009 · N427ZW · Cndair CL6002B19 · Fuselage Main, BulkheadSDR A6WA201040017Sill · corrodedCARGO DOOR FLOOR SILL UPPER AND LOWER SURFACES AROUND NUT PLATES CORRODED. CARGO DOOR FLOOR SILL REPAIRED IAW REO 601R-53-61-1574, REV A.Nov 26, 2009 · N427ZW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA201040019Retainer · corrodedMAIN AVIONIC DOOR AFT SEAL RETAINERS IS CORRODED. MAIN AVIONIC DOOR AFT SEAL RETAINERS REPLACED IAW SRM 51-42-06.Nov 26, 2009 · N427ZW · Cndair CL6002B19 · Electrical/Electronic Compartment DoorsSDR A6WA201040029Intercostal · crackedPREVIOUSLY REPAIRED INTERCOSTAL ANGLE AT FS 484.00, LBL 36.00 CRACKED. INTERCOSTAL ANGLE AT FS 484.00, LBL 36.00, REPLACED IAW REO 601R-53-41-059, REV B.Nov 25, 2009 · N427ZW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA201040018Sill · crackedCARGO DOOR FLOOR SILL CRACKED UNDER STOW PLATE BRACKET AT FS 574.00 (LENGTH .250" X 2) CARGO FLOOR SILL UNDER STOW PLATE BRACKET AT FS 574.00 REPAIRED IAW REO 601R-53-61-1741 REV N/C.Nov 24, 2009 · N427ZW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA201040009Lens · crackedRT WING POSITION LIGHT LENS IS CRACKED AT SEVERAL FASTENER HOLES. CRACK LENGTHS ARE BTWN .100" AND .300". RT WING POSITION LIGHT LENS REPLACED IAW TASK 57-30-01-400-801, SUPPLEMENT NO: 07-009.Nov 24, 2009 · N427ZW · Cndair CL6002B19 · Exterior LightingSDR A6WA201040028Attach Fitting · crackedINTERCOSTAL CLIP AT FS 484.00, RBL 27.00 CRACKED (LENGTH .250") INTERCOSTAL CLIP AT FS 484.00, RBL 27.00. REPLACED IAW SRM 51-42-08 AND SRM 51-42-21.Nov 24, 2009 · N427ZW · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR A6WA201040012Bulkhead · crackedCRACK FOUND ON FWD PRESSURE BULKHEAD AT FS 202.75, LBL 23.71, WL 69 IN PARKING BRAKE CABLE AREA. FWD PRESSURE BULKHEAD AT FS 202.75, LBL 23.71, WL 69, REPAIRED IAW REO 601R-53-11-563.Nov 20, 2009 · N427ZW · Cndair CL6002B19 · Fuselage Main, BulkheadSDR A6WA200940658Intercostal · crackedINTERCOSTAL FOUND CRACKED BEHIND AFT PRESSURE BULKHEAD AT WL 100.5, LBL 48, FL 621.00. REPLACEMENT INTERCOSTAL FABRICATED AND INSTALLED IAW SRM 51-42-06 AND 51-42-20. (K)Sep 27, 2009 · N427ZW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200940659Track · crackedCRACK FOUND AT FS 621.00, LBL 27.50, WL 130.00 AT THE END OF CARGO DOOR TRACK. FS 621.00, LBL 27.50, WL 130.00 AT THE END OF CARGO DOOR TRACK REPAIRED IAW REO 601R-53-61-1541, REV B. (K)Sep 24, 2009 · N427ZW · Cndair CL6002B19 · Cargo/Baggage DoorsSDR A6WA200940657Bulkhead · crackedCRACKS FOUND AT LINTEL FITTING OF THE AFT PRESSURE BULKHEAD. REPAIR PERFORMED AT LINTEL FITTING AT THE AFT PRESSURE BULKHEAD REO 601R-53-61-1230 REV D. (K)Sep 24, 2009 · N427ZW · Cndair CL6002B19 · Fuselage Main, BulkheadSDR A6WA200940412Uplock · malfunctionedAFTER GEAR RETRACTION, GEAR DISAGREE MESSAGE DISPLAYED (AFTER APPROX 10-15 SECS) AFTER GEAR LEVER MOVEMENT LT MAIN GEAR NOT SAFE INDICATION. C/W QRH LANDING EXTENDED AND INDICATED DOWN AND LOCKED. VISUALLY INSP ALL 3 LANDING GEAR. FOUND NO EVIDENCE OF HYD LJul 17, 2009 · N427ZW · Cndair CL6002B19 · Landing Gear Position and WarningSDR A6WA200840653Windshield · crackedLOG 198420/2 CAPTAINS SIDE WINDSHIELD SHATTERED INFLIGHT COMPLIED WITH QRH. R&R CAPTS SIDE WINDSHIELD IAW CRJ AMM 56-11-01. REF W/O 130800 W/C NR 1 FOR LEAK CHECK AND OPS CHECK.Dec 29, 2008 · N427ZW · Cndair CL6002B19 · Flight Compartment WindowsSDR A6WA200840610Flap · malfunctionedTHRU 10,000 FT FLAPS FAIL MSG. FLAPS FAILED AT ZERO, AIRSPEED WAS 250 KIAS. COMPLIED WITH QRH LANDED NORMAL. COMPLIED WITH FLAPS RESET IAW AWAC SUPP 98-018B FLAPS OPS CHECK GOOD.Nov 17, 2008 · N427ZW · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR A6WA200840182Aileron · stuckIN FLIGHT, 4 SECONDS AFTER DISCONNECTION AUTOPILOT, AILERONS STUCK AND MOMENTARILY AILERONS COULD NOT BE TURNED LEFT OR RIGHT, ON 4 MILE FINAL. (M)Mar 14, 2008 · N427ZW · Cndair CL6002B19 · Aileron Control SystemSDR A6WA200740664Hinge · crackedRT SIDE BUTE DOOR 694JB PIANO HINGE CRACKED. HINGE REPLACED ON BUTE DOOR 694JB IAW CRJ 200, SRM 51-42-06 AND PAINTED IAW CRJ 200, SRM 51-25-01. (K)Nov 19, 2007 · N427ZW · Cndair CL6002B19 · Wing Miscellaneous StructureSDR A6WA200740639Floorbeam · crackedCRACK EXIST ON FLOORBEAM FS 280 RBL 9 OUTBOARD CRACK ON FLOORBEAM .750 INCH. FLOORBEAM REPAIRED IAW CRJ 200 REO 601R-53-11-1171. (M)Nov 16, 2007 · N427ZW · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR A6WA200740633Structure · damagedCRACK ON FORWARD AND AFT PASSAGE DOOR EDGE MEMBER DAMAGED REPAIRED ON FORWARD AND AFT PASSENGER DOOR EDGE MEMBER IAW CRJ 200 REO 601R-52-11-279 REV NC. (M)Nov 16, 2007 · N427ZW · Cndair CL6002B19 · Passenger/Crew DoorsSDR A6WA200740665Fitting · gougedGOUGE ON FWD PAX DOOR ALIGNMENT FITTING .750 X .200, .020 DEEP. FWD PAX DOOR ALIGNMENT FITTING REPLACED IAW CRJ 200, SRM 51-42-06. (K)Nov 16, 2007 · N427ZW · Cndair CL6002B19 · Passenger/Crew DoorsSDR A6WA200740662Bracket · crackedCRACK EXIST ON BRACKET OF INTERCOSTAL, FS 484, LBL 27, CRACK DIMENTION ON BRACKET , 1 INCH. BRACKET OF INTERCOSTAL AT FS 484, LBL 27 REPLACED IAW REO 601R-53-41-059. (K)Nov 16, 2007 · N427ZW · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR A6WA200740661Intercostal · crackedCRACK EXIST ON INTERCOSTAL AND BRACKET FS 484, RBL 27 AND RBL 36 CRACK DIMENTION OF INTERCOSTAL 1 INCH AND BRACKET .500 INCH. INTERCOSTAL AT FS 484, RBL 36 REPAIRED IAW REO 601R-53-41-059 BRACKET AT FS 484, RBL 27, REPLACED IAW REO 601R-53-41-059. (K)Nov 16, 2007 · N427ZW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200740659Intake Duct · crackedAPU INTAKE DUCT CRACKED. APU INTAKE DUCT REPLACED IAW AMM. (K)Nov 16, 2007 · N427ZW · Cndair CL6002B19 · Airborne Auxiliary Power Unit (APU) SystemSDR A6WA200740642Exhaust Duct · corrodedAPU EXHAUST LIPS CRACKED AT 5 O`CLOCK AND 6 O`CLOCK. APU EXHAUST REPLACED IAW AMM 49-81-01-400-801. (K)Nov 16, 2007 · N427ZW · Cndair CL6002B19 · APU Exhaust SystemSDR A6WA200740641Floorbeam · crackedCRACK EXIST ON BRACKET OF FLOORBEAM, FS 280, LBL 9 AND RBL 9 CRACK ON BRACKET IS 1 INCH. NEW SERVICEABLE BRACKETS INSTALL AT FS 280.00, LBL 9.0 AND RBL 9.0 IAW SRM 51-42-06. (K)Nov 16, 2007 · N427ZW · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR A6WA200740635Hinge · corrodedFOUND PAX DOOR FOLDING STEP (UPPER) HINGE CORRODED. PAX DOOR FOLDING STEP HINGE INSTALLED IAW SRM 51-41-00. (M)Nov 16, 2007 · N427ZW · Cndair CL6002B19 · Entrance StairsSDR A6WA200740634Drag Angle · crackedFOUND CRACK ON AFT DRAG ANGLE OF PASSENGER DOOR AIRSTAIRS. JOB PERFORMED ON AFT DRAG ANGLE OF PASSENGER DOOR AIRSTAIRS IAW REO 601R-57-11-513. (M)Nov 16, 2007 · N427ZW · Cndair CL6002B19 · Passenger/Crew DoorsSDR A6WA200740640Bracket · crackedLT MLG WHEEL WELL HYD SUPPORT BRACKET CRACKED. LT MLG WHEEL WELL HYD SUPPORT BRACKET REPLACED.Nov 15, 2007 · N427ZW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200740667Support Bracket · crackedRT MLG WHEEL WELL FWD HYD SUPPORT BRACKET CRACKED. RT MLG WHEEL WELL FWD HYDRAULIC SUPPORT BARCKET REPLACED IAW CRJ 200 SRM 51-42-06. (K)Nov 15, 2007 · N427ZW · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR A6WA200740666Support Bracket · crackedRT MLG WHEEL WELL, AFT HYD SUPPORT BRACKET IS CRACKED. RT MLG WHEEL WELL AFT HYD SUPPORT BRACKET REPLACED IAW CRJ 200, SRM 51-42-06. (K)Nov 15, 2007 · N427ZW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200740663Skin · dentedRT WING IB L/E FOUND SCRATCHED AND DENTED OVER LIMITS IAW CRJ200 SRM. NEW SKIN INSTALLED IAW CRJ SRM 51-40-11 AND SRM 51-41-04. (K)Nov 15, 2007 · N427ZW · Cndair CL6002B19 · Wing, Plate/SkinSDR A6WA200740660Bracket · crackedCRACK EXIST ON BRACKET FS 625, LT STR 14L. BRACKET AT FS 625, STR 14L REPLACED IAW, SRM 51-42-06. (K)Nov 15, 2007 · N427ZW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200740632Sill · corrodedFOUND SERVICE DOOR CUT-OUT LOWER SILL PLATE CORRODED P/N NR 601R38957-19. NEW SERVICEABLE LOWER SILL PROTECTIVE PLATE INSTALLED IAW CRJ 200 SRM 51-41-02. (M)Nov 15, 2007 · N427ZW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200740503Fan · odorREQUEST INSPECTION FOR SMOKE ODOR IN COCKPIT. HEARD GRINDING NOISE FROM DISPLAY OR ARNIC FAN. INSPECTED AIRCRAFT AND TESTED AVIONIC COOLING SYSTEM PER CRJ AMM 21-24-00-710-801. REPLACED DISPLAY FILTER. COULD NOT DUPLICATE PROBLEM. NO SMOKE ODOR. NO NOISESep 10, 2007 · N427ZW · Cndair CL6002B19 · Air Distribution FanSDR A6WA200740188Unknown · odorSTRONG FUEL ODOR IN COCKPIT AFTER ENGINE SHUTDOWN, APU IS RUNNING. PERFORMED INSPECTION OF FUEL LINES AND FUEL DRAINS, NO FUEL ODORS OR LEAKS DETECTED AT THIS TIME, OK FOR RETURN TO SERVICE. (K)Apr 6, 2007 · N427ZW · Cndair CL6002B19 · Air Distribution SystemSDR A6WA200640370Control Unit · malfunctionedON LANDING ROLL OUT, UNCOMMANDED ELEVATOR TRIM ACTUATION TO 9.8 UNITS NOSE UP. INTERROGATED MDC NO FAULTS FOUND. FUNCTION TEST OF HSTCU GOOD, NO EVIDENCE OF MOISTURE INGRESS. REMOVED AND REPLACED HSTCU, FUNCTION CHECK GOOD. FDR TO BE DOWNLOADED IN ORF. CAOct 26, 2006 · N427ZW · Cndair CL6002B19 · Stabilizer Control SystemSDR A6WA200640360Connector · looseLEFT ENGINE OIL PRESSURE WARNING CAS MESSAGE ILLUMINATED INTERMITTENTLY THROUGHOUT APPROACH. OIL PRESSURE AND TEMP REMAINED NORMAL, ON PRIMARY EICAS, LOWEST READING 49 PSI. CHECKED ENGINE OIL LEVEL, FOUND FULL. INSPECTED LT ENGINE NO EVIDENCE OF OIL LEAKAGEOct 11, 2006 · N427ZW · Cndair CL6002B19 · Engine Oil System WiringSDR A6WA200640229Roller · out of adjustSERVICE DOOR HANDLE HARD TO OPEN. ADJUSTED SERVICE DOOR ROLLER STOPS, AMM, OPS CHECK GOOD. (K)Jun 3, 2006 · N427ZW · Cndair CL6002B19 · Service DoorsSDR A6WA200540333Pivot Assy · seizedHORIZONTAL STABILIZER RT OUTER PIVOT PIN FOUND TO BE SEIZED IN OUTER BUSHING CAUSING BUSHING TO ROTATE IN LUG. MAINTENANCE REMOVED AND REPLACED HORIZONTAL STABILIZER RT OUTER BUSHING AND REAMED THE LUG TO 2ND OVERSIZE IAW SB. (K)Nov 27, 2005 · N427ZW · Cndair CL6002B19 · Horizontal Stabilizer StructureSDR A6WA200540334Skin · corrodedLT WING LOWER PLANK FUEL TANK ACCESS DOOR CUTOUT FOR PANEL 540CB HAS MINOR CORROSION ON OB 5 INCH LONG X .1250 INCH WIDE AND .002 INCH DEEP AND IB 4 INCH LONG X .1250 INCH WIDE AND .002 INCH DEEP. MAINTENANCE PERFORMED A MAJOR REPAIRED TO LT WING LOWER PLANK Nov 22, 2005 · N427ZW · Cndair CL6002B19 · Wing, Plate/SkinSDR A6WA200540340Rib · crackedAWAC WO 89248, MWC 143. LT BATT RIB ASSY AT WS 53.60 UPPER AFT RADIUS IS CRACKED 2 INCH LONG. INSTALLED REPAIR DOUBLER AND FILLER IAW REO. (K)Nov 21, 2005 · N427ZW · Cndair CL6002B19 · Wing, Rib/BulkheadSDR A6WA200540331Intercostal · crackedRT SIDE FS 621.00 TO FS 625.30 INTERCOSTAL AT STR 14R IS CRACKED NEAR RADIUS APPROX 1.0 INCH LONG. MAINTENANCE REPLACED INTERCOSTAL IAW SRM. (K)Nov 21, 2005 · N427ZW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200540332Intercostal · crackedLT SIDE FS621 TO 625.30 INTERCOSTAL AT STR 14L IS CRACKED NEAR RADIUS APPROX 1.1 INCH LONG. MAINTENANCE REPLACED INTERCOSTAL IAW SRM. (K)Nov 21, 2005 · N427ZW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200540311Idg · lack of lubeIDG NR 1 CAUTION MESSAGE AT TAKEOFF THRUST ABORTED TAKEOFF BELOW 40 KNOTS BTMS INDICATES 3, 3, 4, 4 LIGHT BRAKING. NO HIGH ENERGY STOP INSPECTION REQUIRED IAW 05-51-27 P601. COMPLIED WITH (M) ACTION FOR MEL 24-11-01-01 PLACARDED. SERVICED IDG NR 1 WITH OIL Sep 28, 2005 · N427ZW · Cndair CL6002B19 · Alternator-Generator DriveSDR A6WA200540182Tube · leakingHYDRAULIC NR2 SYSTEM PRESSURE LOSS FOLLOWED BY LOSS OF QTY. NR2 SYSTEM, COMPLIED WITH QRH. INSPECTED AND FOUND HYD PRESSURE LINE NR2 IN APU BAY LEAKING, ALSO ENG DRIVEN HYD PUMP NR 2 FAILED. REMOVED/REPLACED ENGINE DRIVE HYD PUMP NR 2. REMOVED AND REPLACEDMay 25, 2005 · N427ZW · Cndair CL6002B19 · Hydraulic System, MainSDR A6WA200540016Flex Line · leakingOXYGEN LOW PRESSURE. WHILE TROUBLESHOOTING FOUND LINE (PN 3801950110) TO CAPTAINS MASK BOX LEAKING. REMOVED AND REPLACED OXYGEN FLEX LINE TO BOTTOM OF CAPTAINS SIDE OXYGEN MASK RETAINER BOX TO COCKPIT FLOOR. LEAK CHECK GOOD. (K)Jan 8, 2005 · N427ZW · Cndair CL6002B19 · Crew Oxygen SystemSDR A6WA200440176Odor · detectedFUEL SMELL UPON START UP OF APU ON GROUND BEFORE BLEEDS ARE TRANSFERRED. COMPLIED WITH (CM) ACTION PLACARDED AND PLACED ON MEL. TROUBLESHOT APU FUEL SYSTEM RAN APU AND ACM NO FUEL ODOR DETECTED. NO LEAKS DETECTED. RETURN TO SERVICE. REMOVED OFF MEL. (K)Nov 7, 2004 · N427ZW · Cndair CL6002B19 · Air Distribution SystemSDR A6WA200440180Odor · detectedFUEL SMELL UPON START UP OF APU ON GROUND BEFORE BLEEDS ARE TRANSFERRED. MAINTENANCE VERIFIED NO FUEL OR OIL LEAKS IN APU BAY. TROUBLESHOT APU FUEL SYSTEM. RAN APU AND AIR CYCLE MACHINE. NO FUEL SMELL DETECTED AND NO LEAKS.Nov 7, 2004 · N427ZW · Cndair CL6002B19 · Air Distribution SystemSDR A6WA200440043Bushing · failedWHILE REMOVING RT MLG FOR FITTING REPLACEMENT, IT WAS DISCOVERED THAT RT MLG AFT TRUNNION BUSHING IS MIGRATED. REMOVED MIGRATED BUSHING, INSTALLED 2ST OVERSIZE BUSHING AND LINE REAMED TO 2.4379 INCH ALL WORK DOEN IAW BRAS EO 601R-32-4827 AND MFG SB 601R-32-05Apr 13, 2004 · N427ZW · Cndair CL6002B19 · Landing Gear Retraction/Extension SystemSDR A6WA200440042Bushing · failedWHILE REMOVING LT MLG FOR FITTING REPLACEMENT IT WAS DISCOVERED THAT LT MLG AFT TRUNNION BUSHING IS MIGRATED. REMOVED MIGRATED BUSHING, INSTALLED 1ST OVERSIZE BUSHING AND LINE REAMED TO 2.4379 INCHES ALL WORK DONE IAW BRAS EO 601R-32-4827 AND MFG SB 601R-32-0Apr 13, 2004 · N427ZW · Cndair CL6002B19 · Landing Gear Retraction/Extension System
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