N433AW

Service difficulty reports · 259

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 = 'N433AW' 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 A6WA201040062Panel · crackedFWD CORNER OF PANEL 326BL CRACKED OFF. (VISOR PANEL FAIRING). TRIMMED DAMAGE IAW REO 601R-55-32-246.Dec 18, 2009 · N433AW · Cndair CL6002B19 · Vertical Stabilizer, Plate/SkinSDR A6WA201040059Structure · crackedPAX DOOR LOWER AFT EDGE MEMBER IS CRACKED. REPAIRED DAMAGE ON PAX DOOR LOWER AFT EDGE MEMBER IAW REO 601-51-11-279.Dec 18, 2009 · N433AW · Cndair CL6002B19 · Passenger/Crew DoorsSDR A6WA201040069Seat Track · wornPILOTS INBD AND OTBD SEAT RAILS WORN. REMOVED AND REPLACED PILOTS INBD AND OTBD SEAT RAILS IAW SRM 51-42-21.Dec 17, 2009 · N433AW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR A6WA201040070Seat Track · wornCO-PILOTS INBD AND OTBD SEAT RAILS ARE WORN. REMOVED AND REPLACED CO-PILOTS INBD AND OTBD SEAT TRACKS IAW SRM 51-42-21.Dec 17, 2009 · N433AW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR A6WA201040055Stiffener · crackedAPU ENCLOSURE DOOR EXTERNAL STIFFENERS CRACKED AT UPPER WELD. REPAIRED CRACKS (2 EA) IAW REO 601R-49-11-070.Dec 15, 2009 · N433AW · Cndair CL6002B19 · APU Cowling/ContainmentSDR A6WA201040058Floorbeam · crackedFS 280, FLOOR SUPPORT UPPER CAP CRACKED AT RBL 10.0 AND LBL 10.0. REPAIRED IAW REO 601R-53-11-136.Dec 14, 2009 · N433AW · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR A6WA201040065Attach Angle · corrodedATTACH ANGLE AT FS 320.10 IN LWR PAX DOOR CORRODED RII REQUIRED. REMOVED CORRODED ATTACH ANGLES, DUPLICATED PARTS AND INSTALLED NEW SERVICEABLE PARTS.Dec 14, 2009 · N433AW · Cndair CL6002B19 · Passenger/Crew DoorsSDR A6WA201040066Attach Angle · corrodedATTACH ANGLES AT FS 338.00 IN LWR PAX DOOR CORRODED. REMOVED CORRODED ATTACH ANGLE, DUPLICATED PART AND INSTALLED NEW SERVICEABLE ANGLE.Dec 14, 2009 · N433AW · Cndair CL6002B19 · Passenger/Crew DoorsSDR A6WA201040056Support Angle · crackedFS 280 FWD SUPPORT ANGLE BENEATH COCKPIT FLOORBOARD 221ALF CRACKED. REMOVED DAMAGE ANGLE, DUPLICATED SERVICEABLE ANGLE AND INSTALLED SERVICEABLE ANGLE.Dec 14, 2009 · N433AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA201040005Bracket · crackedHYD SYS NR 1 PRESSURE/RETURN FILTER MANIFOLD MOUNT BRACKET CRACKED IN LOWER AFT RADIUS. REPAIRED HYD SYS NR 1 PRESSURE/RETURN MANIFOLD MOUNT BRACKET IAW REO 601R-53-62-031. (K)Dec 12, 2009 · N433AW · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR A6WA2010400004Angle · crackedLT WING OTBD ATTACH ANGLE UNDER ACCESS PANEL 520ML IS CRACKED. REMOVED CRACKED ATTACH ANGLE FROM LT WING OTBD UNDER ACCESS PANEL 520ML AND INSTALLED SERVICEABLE BRACKET PN 600-12045-11 IAW SRM 51-41-061.Dec 10, 2009 · N433AW · Cndair CL6002B19 · Wing Miscellaneous StructureSDR A6WA201040004Angle · crackedLT WING OTBD ATTACH ANGLE UNDER ACCESS PANEL 520 ML CRACKED. REMOVED CRACKED ATTACH ANGLE FROM LT WING, OTBD UNDER ACCESS PANEL 520 ML AND INSTALLED SERVICEABLE BRACKET PN 600-12045-11, IAW SRM 51-41-061. (K)Dec 10, 2009 · N433AW · Cndair CL6002B19 · Wing Miscellaneous StructureSDR A6WA201040002Stiffener · crackedRT JETPIPE 2ND RIB CRACKED. REAPRED RT JETPIPE 2ND RIB IAW CMM TASK 78-11-00-300-810-A01. REPAIR SRS 042.Dec 9, 2009 · N433AW · Cndair CL6002B19 · Engine Collector/Tailpipe/NozzleSDR A6WA201040003Panel · crackedLT OTBD L/E INNER SKIN PANEL CRACKED. REPLACED LT OTBD L/E INNER SKIN PANEL IAW SRM 51-42-06 AND SRM 51-42-13. (K)Dec 9, 2009 · N433AW · Cndair CL6002B19 · Wing, Plate/SkinSDR A6WA200940679Mechanism · lack of lubePASSENGER DOOR DIFFICULT TO OPEN FROM OUTSIDE. INSPECTED AND LUBED PASSENGER DOOR LATCHING MECHANISM. OPS CK GOOD IAW AMM 52-11-00-05. (K)Oct 12, 2009 · N433AW · Cndair CL6002B19 · Passenger/Crew DoorsSDR A6WA200940550Door · stuckPAX DOOR WILL NOT OPEN FROM OUTSIDE. HART TO OPEN FROM INSIDE PLACARDED AND PLACED ON MEL. INSTALLED NEW HANDLE LATCH ASSY IAW AMM 52-11-21 HANDLE NOW WORKS BUT DOOR IS STILL HARD TO OPEN. FURTHER T/S REQUIRED. STOWED AND OPERATED INNER AND OUTER HANDLE OSep 15, 2009 · N433AW · Cndair CL6002B19 · Passenger/Crew DoorsSDR A6WA200940448Seal · missingLOUD SQUEAL COMING FROM SERVICE DOOR WHEN PSI`D AT ALTITUDE. FOUND 2 AREAS ON SERVICE DOOR SEAL STRIKER MISSING SEALANT. REAPPLIED MISSING SEALANT IAW AMM 51 STANDARD PRACTICES. (K)Jul 28, 2009 · N433AW · Cndair CL6002B19 · Service DoorsSDR A6WA200940175Computer · malfunctionedREFUEL SPR WILL NOT FUEL WING TANKS IN AUTO OR MANUAL. REMOVED AND REPLACED FUEL SYS COMPUTER, OPS CHECK GOOD. REMOVED AND REPLACED REFUEL/DEFUEL PANEL. OPS CHECK GOOD. REMOVED AND REPLACED REFUEL/DEFUEL PANEL HARNESS. OPS CHECK GOOD. 3 TANKS CONFIG COMPUTApr 1, 2009 · N433AW · Cndair CL6002B19 · Fuel StorageSDR A6WA200840645Retaining Clip · out of positionWHILE SERVICING APU SMELL NOTICED OPENED PANEL RAN APU. FOUND APU INLET BELLOWS RETAINING CLIP RT SIDE SLID AFT AND CHAFED HOLE IN METERED FUEL LINE TO NOZZLES. DRIPS ON IGNITER BOX. R&R FUEL LINE, REPOSITIONED RETAINING CLIP AND PLACED SPIRAL WRAP ON FUEL Dec 15, 2008 · N433AW · Cndair CL6002B19 · APU Engine Fuel and ControlSDR A6WA200840581Door · stuckCREW REPORTS PASSENGER DOOR UNABLE TO OPEN FROM OUTSIDE. INSPECTED PASSENGER DOOR LATCH MECHANISM, INNER AND OUTER HANDLES PER AMM 52-11-02, 52-11-03. REMOVED PUSH-PULL RODS AND CLEANED AND LUBED ROD ENDS. REMOVED, CLEANED AND LUBED INNER AND OUTER HANDLES Aug 20, 2008 · N433AW · Cndair CL6002B19 · Passenger/Crew DoorsSDR A6WA200840401Control Column · looseREQUEST INSPECTION OF FIRST OFFICER`S CONTROL COLUMN FOR SUSPECTED EXCESSIVE PLAY IN NEUTRAL POSITION. PERFORMED OPS CHECK OF ELEVATOR CONTROL SYSTEM USING PITCH FEEL CHECK IAW AWAC SUPPLEMENT 2006-004A. OPS CHCEK GOOD. NO DEFECTS NOTED. (A)May 13, 2008 · N433AW · Cndair CL6002B19 · Control Column SectionSDR A6WA200840351O-Ring · leakingSTRONG FUEL ODOR THROUGHOUT CABIN AND COCKPIT SOMETIME AFTER APU STARTED ON ARRIVAL. FOUND APU FUEL LINE LEAKING. WITH APU OFF, FUEL LEAK STOPS. REF 201527/4 FOR MEL. R&R LOWER SOV ELBOW & O-RING IAW AMM 49-31-01. OPS AND LEAK CHECK GOOD.Apr 20, 2008 · N433AW · Cndair CL6002B19 · APU Engine Fuel and ControlSDR A6WA200840218Handle · damagedPARKING BRAKE HANDLE OCCASIONALLY SLIPS OUT OF POSITION. (M)Mar 18, 2008 · N433AW · Cndair CL6002B19 · Landing Gear Brake SystemSDR A6WA200740674Hinge · crackedPAX DOOR UPPER FOLDING STEP, LOWER HINGE IS CRACKED. PAX DOOR UPPER FOLDING STEP, LOWER HINGE REPLACED IAW SRM 51-41-00. (K)Dec 6, 2007 · N433AW · Cndair CL6002B19 · Fuselage, Door HingeSDR A6WA200740677Floor Support · crackedCRACK FOUND ON FLOOR STRUCTURE FS 621, LBL 45 CRACK LENGTH IS .500 INCH. FLOOR SUPPORT AT FS 621.00 LBL 45 REPAIRED IAW REO 601R-53-61-117, REV C. (K)Nov 30, 2007 · N433AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200740676Floor Support · corrodedCORROSION FOUND ON FLOOR SUPPORT FS 589 TO 621, LBL 27. JOB PERFORMED ON FLOOR SUPPORT FS 589 TO 621, LBL 27 IAW REO 601R-53-61-2439. (K)Nov 30, 2007 · N433AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200740673Drag Angle · crackedPAX DOOR STAIR ASSY, AFT DRAG ANGLE IS CRACKED. REPAIRED IAW CRJ200, REO 601R-52-11-513 REV (A). (K)Nov 30, 2007 · N433AW · Cndair CL6002B19 · Passenger/Crew DoorsSDR A6WA200740672Floorbeam · crackedFLOORBEAM AT FS 280 IS CRACKED AT LBL 9 AND RBL 9 CRACK AT LBL 9 IS .400 INCH CRACK AT RBL 9 IS 1.200 INCH. (M) FLOORBEAM REPAIRED IAW REO 601R-53-11-171 REV D. (K)Nov 30, 2007 · N433AW · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR A6WA200740671Bracket · crackedCRACK FOUND ON 4 BRACKET FS 280 LBL 9 AND RBL 9 CRACK LENGTH IS 1 INCH. (M) 3 BRACKETS REPLACED ON FS 280, LBL 9, OB AND IB AND RBL 9 OB IAW REO 601R-53-11-171 REV-D. BRACKET REPLACED ON FS 280, RBL 9, IB IAW CRJ 200, SRM 51-42-06. (K)Nov 30, 2007 · N433AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200740668Angle · crackedLT AND RT ANGLES CRACKED ON REAR PRESSURE BULKHEAD AFT SURFACE. (M) LT AND RT ANGLES ON AFT PRESSURE BULKHEAD (AFT FACE) AT FS 622, WL 73 TO 75, BTW STR 16 AND 17 INSTALLED AS IAW SRM 51-42-20. (K)Nov 30, 2007 · N433AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200740675Bulkhead · crackedCRACK FOUND ON T FWD PRESSURE BULKHEAD PARKING BRAKE CABLE HOLE APPROX .650 INCH LONG. FWD PRESSURE BULKHEAD AT FS 202.00, LBL 23.71. REPAIRED IAW REO 601R-53-11-563. (K)Nov 29, 2007 · N433AW · Cndair CL6002B19 · Fuselage Main, BulkheadSDR A6WA200740669Support Channel · crackedFOUND CARGO DOOR FORWARD TRACK LOWER SUPPORT CHANNEL P/N 601R35050-25 FOUND CRACK APPROX .500 LONG 1 EACH. (M) CARGO DOOR FWD TRACK, LOWER SUPPORT CHANNEL. FABRICATED IAW SRM 51-24-16, CRACKED SUPPORT CHANNEL REMOVED IAW SRM 51-42-06, FABRICATED SUPPORT CHANov 29, 2007 · N433AW · Cndair CL6002B19 · Passenger/Crew DoorsSDR A6WA200740670Structure · crackedON PAX DOOR, CRACK FOUND ON PASSENGER EDGE MEMBER. (M) PAX DOOR ON PASSENGER EDGE MEMBER REPAIRED IAW REO 601R-52-11-279. (K)Nov 28, 2007 · N433AW · Cndair CL6002B19 · Passenger/Crew DoorsSDR A6WA200740622Dcu · malfunctionedRIGHT ENGINE N2 FLUCTUATION INFLIGHT. COMPLIED WITH QRH. N2 SPIKE OVER 104 PERCENT AT LEAST TWO TIMES WITH POWER REDUCED. OAT -6. NO VIBE GAUGE INDICATION. DIVERTED TO ORF. FOUND DCU NR 2 CAUSING N2 FLUCTUATING INDICATION. REMOVED AND REPLACED DCU NR 2 Nov 15, 2007 · N433AW · Cndair CL6002B19 · Central ComputersSDR A6WA200740461Door · lack of lubeUNABLE TO OPEN MAIN PASSENGER DOOR. AFTER MULTIPLE ATTEMPTS, DOOR OPENED. OPERATED DOOR SEVERAL TIMES. DOOR APPEARS TO OPERATE NORMALLY. PLACED ON MEL. REF LOG 177995/2 CLEANED AND LUBED PASSENGER DOOR. PERFORMED OPS CHECK OF PASSENGER DOOR SEVERAL TIMESAug 19, 2007 · N433AW · Cndair CL6002B19 · Passenger/Crew DoorsSDR A6WA200740310Apu · smokeAFTER TRANSFERRING BLEEDS TO APU, THERE WAS A FAINT ODOR IN THE COCKPIT, ENGINES AT IDLE, (SMOKE TOILET) MESSAGE ON ED 1. MESSAGE CLEARED ON RUNWAY. FA REPORTS SMOKE AT CEILING AT ROW 11 AND 12. REPORTS SMOKE AT CEILING AT ROW 11 AND 12 REMOVED AND REPLACEDJun 16, 2007 · N433AW · Cndair CL6002B19 · Airborne Auxiliary Power Unit (APU) SystemSDR A6WA200740309Unknown · odorLAV SMOKE TOILET MESSAGE APPEARED ON FINAL APPROACH. F/A REPORTED SMOKE AND STRONG ELECTRICAL ODOR COMING FROM CENTER OVERHEAD. APU AND PACKS ON. SMOKE DISSIPATED 3-5 MINUTES AFTER INDICATION. REMOVED CEILING PANELS. INSPECTED LIGHT FIXTURES AND WIRING. Jun 16, 2007 · N433AW · Cndair CL6002B19 · Air Distribution SystemSDR A6WA200740226Wire · shortedCPLT ROLL COMMAND MESSAGE ON ED2 IN FLIGHT. GREEN CPLT ROLL LIGHT ILLUMINATED ON GLARESHIELD. COMPLIED WITH QRH. ROLL DISCONNECT HANDLE PULLED. EMERGENCY LANDING DECLARED. (M) [07-20-07] ISOLATED SHORT TO IB L/E (LT) REPAIRED WIRE CN619A22 AND CN620AZMay 12, 2007 · N433AW · Cndair CL6002B19 · Instrument System WiringSDR A6WA200640421Angle · crackedRUDDER SYSTEM (MID SPAR) ANGLE P/N 600-92638-1 AT LEFT AFT SIDE OF VS 67.5 PERCENT FRAME CRACKED APPROX .5 INCH LENGTH AT TOP INBOARD ATTACH RIVET. MAINTENANCE FABRICATED NEW ANGLE FROM 7075T6511 PO NR 74697/1 PER DRAWING 600-92638 AND INSTALLED IAW CRJ SRM 5Dec 17, 2006 · N433AW · Cndair CL6002B19 · Horizontal Stabilizer StructureSDR A6WA200640420Attach Angle · crackedATTACHMENT ANGLE P/N 600-12025-8 FOR RIGHT WING L/E PANEL 620JT CRACKED AT UPPER AND LOWER CORNER WS 139.54 CRACKS APPROX .2 INCHES LONG. MAINTENANCE REPLACED ATTACHMENT ANGLE WITH NEW.Dec 17, 2006 · N433AW · Cndair CL6002B19 · Wing, Attach FittingsSDR A6WA200640419Attach Angle · crackedATTACHMENT ANGLE P/N 600-12045-12 FOR WING L/E PANEL 630JT CRACKED AT UPPER AND LOWER CORNERS WS 149.58 CRACKS APPROX .2 INCH LONG. MAINTENANCE REPLACED ATTACHMENT ANGLE WITH NEW P/N 600-12045-12 IAW CRJ200 AMM 20-21-00-910-801. (M)Dec 17, 2006 · N433AW · Cndair CL6002B19 · Wing, Attach FittingsSDR A6WA200640299Pdu · contaminatedLEFT THRUST REVERSER UNSAFE CAUTION MESSAGE AND POSSIBLE DEPLOYMENT AT ROTATION. AIRCRAFT SHUDDERED. MESSAGE CLEARED AT 1000 FEET, NORMAL FLIGHT THEREAFTER. REMOVED AND REPLACED NR 1 ENGINE THRUST REVERSER POWER DRIVE PDU 9PDU FULL OF WATER, DRAINED UPON ARJul 31, 2006 · N433AW · Cndair CL6002B19 · Engine Thrust ReverserSDR A6WA200640302Door · lack of lubePASSENGER DOOR WILL NOT OPEN FROM OUTSIDE. PLACARDED AND PLACED ON MEL. INSPECTED AND FOUND SEVERAL PUSH RODS SEIZED UP. APPLIED LUBRICANT TO AFFECTED AREAS IAW CRJ 12-20-52, OPS CHECK GOOD AT THIS TIME. REMOVED FROM MEL. (M)Jul 31, 2006 · N433AW · Cndair CL6002B19 · Passenger/Crew DoorsSDR A6WA200640174A/C Pack · odorWHEN AIRBORNE NOTICED EXHAUST ODOR FROM GASPERS IN FLIGHT DECK, LEFT PACK UNRESPONSIVE TO MANUAL OR AUTO MODE. TEMP 23 DEGREES CELSIUS, REDUCED AIRFLOW IN FLIGHT DECK WITH LT PACK ON. SHUTDOWN LT PACK PROCEEDED WITH SINGLE PACK. NO MESSAGE NOTED. ODOR CLEAMay 1, 2006 · N433AW · Cndair CL6002B19 · Cabin Cooling SystemSDR A6WA200640092Actuator · malfunctionedFLAPS FAIL CAS MESSAGE IN FLIGHT. FLAPS STUCK AT ZERO LANDING WEIGHT 42,000 LBS. BTMS MAX READING 2, ALL IN GREEN. PLACED ON 72 HOUR FLAP WATCH, FECU NEEDS INTERROGATION. REPLACED RIGHT FLAP ACTUATORS AND FLEX DRIVE SHAFTS. (M)Feb 18, 2006 · N433AW · Cndair CL6002B19 · Trailing Edge Flap ActuatorSDR A6WA200640071Drive Shaft · failedIB TO MSP FLAP FAIL MESSAGE ILLUMINATED WHEN FLAP SELECTED TO 8 DEGREES. ACCOMPLISHED ZERO FLAP LANDING IAW CHECKLIST. HIGHEST TEMP= 5- ALL GREEN. REMOVED AND REPLACED LT FLEX SHAFT 1 THRU 4 IAW AMM. OPS CHECK GOOD AT THIS TIME. (K)Feb 10, 2006 · N433AW · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR A6WA200540365Skin · corrodedLT WING LOWER PLANK ACCESS HOLE NR2 UNDER PNL 510AB AT WS 12.245 HAS CORROSION ON IB SIDE APPROX 3 INCH L X .1 INCH W X .004 DEEP IN NON CRITICAL AREA. MAINTENANCE REPAIRED WING PLANK ACCESS HOLE AT WS 12.245 IAW REO. (K)Dec 18, 2005 · N433AW · Cndair CL6002B19 · Wing, Plate/SkinSDR A6WA200540364Skin · damagedDAMAGE TO FUSELAGE SKIN AT FS640-FS700 STRINGER 18, 19 LT SIDE. MAINTENANCE REMOVED DAMAGE SKIN BETWEEN FS 640- FS 700 AND STRINGER 18 - 19L. FABRICATED DOUBLER AND FILLERS AND INSTALLED IAW EO. (K)Dec 17, 2005 · N433AW · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR A6WA200540154Selector Valve · malfunctionedGEAR DISAGREE WARNING IN FLIGHT COMPLIED WITH QRH, LANDED NORMAL. REMOVED AND REPLACED GEAR SELECTOR VALVE IAW AMM 32-33-10. PERFORMED GEAR EXTENSION AND RETRACTION TEST IAW AMM 32-30-00. LEAK AND OPS CHECK GOOD. (M)Apr 11, 2005 · N433AW · Cndair CL6002B19 · Landing Gear Retraction/Extension SystemSDR A6WA200540148Outflow Valve · malfunctionedAFTER TAKEOFF, AIRCRAFT WOULD NOT PRESSURIZE. RETURNED TO ORD. PER MEL 21-24-06-02 SECURED OVERBOARD VALVE IN THE CLOSED POSITION. PERFORMED OPS TEST, NO DISCREPANCIES NOTED. (M)Apr 8, 2005 · N433AW · Cndair CL6002B19 · Pressure Regulator/Outflow Valve
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