N450AW

Service difficulty reports · 232

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 = 'N450AW' 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 A6WA200940091Floorbeam · crackedUPPER AFT ANGLE AT FS 280.00, LBL 9.0 FOUND CRACKED (CRACK LENGTH 1.000 IN). REPAIR PERFORMED AT UPPER AFT ANGLE AT FS 280.00, LBL 9.0 IAW REO 601R 53-11-138 REV, NC. (K)Feb 27, 2009 · N450AW · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR A6WA200940089Structure · crackedVERTICAL STAB, LT UPPER VISOR IS CRACKED. VERTICAL STAB, LT UPPER VISOR REPLACED IAW SRM 51-41-04. (K)Feb 27, 2009 · N450AW · Cndair CL6002B19 · Vertical StabilizerSDR A6WA200940088Fitting · crackedFS 484.00, RBL 27, QTY (1) ONE CLIP IS CRACKED (CRACK LENGTH: 0.500 INCH) F/S 484.00, RBL 27, CLIP REMOVED AND REPLACED IAW SRM 51-42-06 AND SRM 51-42-20. (K)Feb 26, 2009 · N450AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200940092Frame · crackedLWR OF FRAME CRACKED AT 280.00, RBL 9.00 (CRACK LENGTH 1.250 IN) LWR AREA OF FRAME WEB AT 280.00, RBL 9.00 REPAIRED IAW REO 601R-53-11-171 REV D. SCHEME A NOTES 4-13. (K)Feb 25, 2009 · N450AW · Cndair CL6002B19 · Fuselage Main, FrameSDR A6WA200940090Drag Angle · crackedPAX DOOR AFT DRAG ANGLE CRACKED PAX DOOR AFT DRAG ANGLE REPAIRED IAW REO 601R-52-11-513, REV A. (K)Feb 25, 2009 · N450AW · Cndair CL6002B19 · Passenger/Crew DoorsSDR A6WA200940161Plate · cracked(2) CRACKS FOUND ON CARGO LOWER SILL, FS 589 AND FS 605. LOWER SILL LANDING PLATE BTW FS 589 AND FS 605 REPAIRED IAW REO 601R-53-61-433. (K)Feb 23, 2009 · N450AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200940087Channel · crackedCRACK FOUND ON CARGO DOOR TRACK LOWER CHANNEL FS 574. REMOVED AND REPLACED CARGO DOOR LOWER CHANNEL PN 601R-35050-25 IAW SRM 51-42-06, SL 2529.Feb 23, 2009 · N450AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200840602Bulkhead · crackedAFT PRESSURE BULKHEAD WEB FS 621.00 AT THE LINTEL ATTACHMENT INSTALLATION IS CRACKED. AFT PRESSURE BULKHEAD WEB FS 621.00 LINTLE INSTALLATION REPAIRED IAW REO 601R-53-61-1230 REV D.Oct 28, 2008 · N450AW · Cndair CL6002B19 · Fuselage Main, BulkheadSDR A6WA200840536Handle · dirtyUNABLE TO OPEN SERVICE DOOR FROM OUTSIDE, HANDLE WILL NOT POP OUT WHEN PUSH BUTTON IS PUSHED. CLEANED SERVICE DOOR HANDLE AND LUBED IAW AMM 52-41-03, OPS CHECK GOOD. (A)Jul 3, 2008 · N450AW · Cndair CL6002B19 · Service DoorsSDR A6WA200840360Seal · leakingAT 8,000 FT HIGH PITCH WHISTLE FROM PASSENGER DOOR, FLIGHT ATTENDANT REPORTS CURTAIN SUCKED TO THE DOOR, PRESSURIZATION INDICATED 3,000 FT CLIMB, RETURNED TO MHT. R&R PAX DOOR SEAL IAW 52-11-10. OPS CHECK GOOD. PRESSURIZATION CHECK GOOD.Apr 23, 2008 · N450AW · Cndair CL6002B19 · Passenger/Crew DoorsSDR A6WA200840252Control Panel · malfunctionedRECEIVED LEFT AND RIGHT WING ANTI-ICE CAUTION MESSAGES, IN STANDBY RECEIVED LEFT AND RIGHT WING ANTI-ICE CAUTION MESSAGES INTERMITTENTLY. LANDING WEIGHT 44,000 LBS. REMOVED AND REPLACED ANTI-ICE CONTROL PANEL IAW 20-12-21, OPS CHECK GOOD. AVIONICS REPORTS SMar 27, 2008 · N450AW · Cndair CL6002B19 · Airfoil Anti/De-ice SystemSDR A6WA200840010Seal · obstructedSERVICE DOOR DIFFICULT TO OPEN. CLEANED DEBRIS FROM DOOR SEAL. DOOR OPERATES OK AT THIS TIME. (K)Jan 8, 2008 · N450AW · Cndair CL6002B19 · Service DoorsSDR A6WA200740462Control Unit · malfunctionedWITH FLAPS AT ZERO, PITCH CONTROL FORCE UNUSUALLY HIGH, FLAPS OUT TO ZERO HAS NORMAL CONTROL FORCE. REMOVED AND REPLACED BOTH PITCH FEEL SIMULATOR UNITS PER AMM TASK 27-31-20-000-801. PERFORMED CONTROL COLUMN FEEL FORCE AND CENTERING CHECK PER AMM TASK 27-3Aug 20, 2007 · N450AW · Cndair CL6002B19 · Elevator Tab Control SystemSDR A6WA200740098Bulkhead · crackedVISUAL INDICATION OF CRACK IN FWD PRESSURE BULKHEAD FS202.75, WL69.0, LBL23.71 (JUST BELOW PARKING BRAKE CABLE). MEASURES APPROX 1.0 INCH LONG. MAINTENANCE CUT-OUT DAMAGED AREA AND INSTALLED REPAIR DOUBLER IAW REO 601R-53-11-563. (K)Mar 4, 2007 · N450AW · Cndair CL6002B19 · Fuselage Main, BulkheadSDR A6WA200740097Anchor Fitting · crackedPAX DOOR ANCHOR FITTING (FWD) PN 601R380742-3 IS CRACKED. MAINTENANCE REPLACED PAX DOOR ANCHOR FITTING (FWD) PN 601R3807423 IAW AMM 52-11-17-400-803. (K)Mar 2, 2007 · N450AW · Cndair CL6002B19 · Passenger/Crew DoorsSDR A6WA200740096Anchor Fitting · crackedPAX DOOR ANCHOR FITTING (AFT) PN 601R3807413 IS CRACKED. MAINTENANCE REPLACED PAX DOOR ANCHOR FITTING (AFT) PN 601R3807413 IAW AMM 52-11-17-400-803. (K)Mar 2, 2007 · N450AW · Cndair CL6002B19 · Passenger/Crew DoorsSDR A6WA200740087Intercostal · crackedFS 484 INTERCOSTAL CRACKED AT RBL 36. MAINTENANCE DAMAGED FLANGE AND INSTALLED REPAIR ANGLE IAW REO 601R-53-41-059 REV A AND BSC STANDARD REPAIR 601R-53-0030A. (K)Feb 27, 2007 · N450AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200740086Angle · crackedAFT EQUIPMENT COMPARTMENT FS 625.00 OBLIQUE ANGLE. RT IS CRACKED 2 INCH LONG IN AFT RADIUS MAINTENANCE REMOVED OLD CRACKED 625 OBLIQUE ANGLE, INSTALLED NEW SERVICEABLE ANGLE, PN 601-35012-52 IAW SRM 51-42-06. (K)Feb 26, 2007 · N450AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200740085Angle · crackedAFT EQUIPMENT COMPARTMENT FS 625.00 OBLIQUE ANGLE LT CRACKED 2 INCHES LONG IN AFT RADIUS. MAINTENANCE REMOVED OLD CRACKED 625 OBLIQUE ANGLE, INSTALLED NEW SERVICEABLE ANGLE PN 601-35012-51 IAW SRM 51-42-06. (K)Feb 26, 2007 · N450AW · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR A6WA200740079Intercostal · crackedFOUND FS 484 INTERCOSTAL ANGLE CRACKED APPROX .1 INCH LONG AT BL 27. (M) MAINTENANCE REMOVED AND REPLACED ANGLE IAW BSC STANDARD REPAIR 601-53-0029B. (K)Feb 22, 2007 · N450AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200740078Angle · crackedFOUND FS 484 INTERCOSTAL CRACKED APPROX .1 INCH LONG AT LBL 36. (M) MAINTENANCE REMOVED DAMAGED FLANGE AND INSTALLED REPAIR ANGLE IAW REO 601R-53-41-059 REV A AND BSC STANDARD REPAIR 601R-53-0030A. (K)Feb 22, 2007 · N450AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200740077Floor Support · crackedFOUND RT FLOOR SUPPORT ANGLE IS CRACKED 1 INCH AT FS 621, WL 73, RBL 41. (M) MAINTENANCE REPAIRED FLOOR SUPPORT ANGLE AT FS 621 IAW REO 601R-53-61-117 REV C.Feb 22, 2007 · N450AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200740076Floor Support · crackedFOUND LT FLOOR SUPPORT ANGLE IS CRACKED 1 INCH AT FS 621, WL 73, LBL 41. (M) MAINTENANCE REPAIRED CRACKED FLOOR SUPPORT ANGLE BY REMOVING DAMAGED AREA AND INSTALLING REPAIR ANGLE AND STRAP IAW REO 601R-53-61-117 REV C. (K)Feb 22, 2007 · N450AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200740075Channel · crackedFOUND LT MLG WHEEL WELL HYDRAULIC TRANSDUCER HAT CHANNEL P/N 601R75262-159 CRACKED APPROX .05 INCH LONG. (M) MAINTENANCE REMOVED AND REPLACED CHANNEL PN 601R75262-159 IAW SRM 51-42-06. (K)Feb 21, 2007 · N450AW · Cndair CL6002B19 · Hydraulic System, MainSDR A6WA200740074Channel · crackedFOUND RIGHT MLG WHEEL WELL HYDRAULIC TRANSDUCER HAT CHANNEL P/N 601R75262-157 CRACKED APPROX .1 INCH LONG. (M) MAINTENANCE REMOVED AND REPLACED BRACKET PN 601R75262-157 IAW SRM 51-42-06. (K)Feb 21, 2007 · N450AW · Cndair CL6002B19 · Hydraulic System, MainSDR A6WA200740073Support Bracket · crackedFOUND RT MLG WHEEL WELL HYDRAULIC LINE SUPPORT BRACKET P/N 601R75262-155 CRACKED APPROX .1 INCH LONG. (M) MAINTENANCE REMOVED AND REPLACED BRACKET ASSY PN 601R75262-153 IAW SRM 51-42-06.Feb 21, 2007 · N450AW · Cndair CL6002B19 · Hydraulic System, MainSDR A6WA200740068Fitting · crackedIB AND OB CLIPS AT FS 280, LBL 9.0, FLOOR SUPPORT BEAM ARE CRACKED IN RADIUS APPROX .30 INCH LON EACH. (K) MAINTENANCE REMOVED AND REPLACED IB AND OB CLIPS PN 601R31113-57 IAW SRM 51-42-06, SRM 51-42-20 AND BSC STANDARD REPAIR 601R-53-0057A. (K)Feb 19, 2007 · N450AW · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR A6WA200740067Fitting · crackedIB AND OB CLIPS AT FS 280, RBL 9.0, FLOOR SUPPORT BEAM ARE CRACKED IN RADIUS APPROX .30 INCHES LONG EACH. (K) MAINTENANCE REMOVED AND REPLACED IB AND OB CLIPS PN 601R31113-58 IAW SRM 51-42-06, SRM 51-42-20 AND BSC STANDARD REPAIR 601R-53-0057A. (K)Feb 19, 2007 · N450AW · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR A6WA200540209Window · crackedLT SIDE WINDOW CRACKED IN COCKPIT (ON APPROACH). REMOVED AND REPLACED LT SIDE WINDOW IAW MM. (K)Jun 17, 2005 · N450AW · Cndair CL6002B19 · Flight Compartment WindowsSDR A6WA200440154Cover · unsecureIN FLIGHT, LOW OIL PRESSURE ILLUMINATED NR 1 ENGINE OIL PRESSURE FLUCTUATED AT CLIMB AND IDLE SETTINGS. AC RETURNED TO FIELD AT 32,000 FT. PRESSURE DROPPED TO 25 PSI THROTTLE BACK PRESSURE TO 60 PERCENT AT 33,000 FT PRESSURE FLUCTUATED 40 PERCENT-50 PERCENT-Oct 17, 2004 · N450AW · Cndair CL6002B19 · Engine (Turbine/Turboprop)SDR A6WA200440156Odor · detectedIN FLIGHT, STARTED APU, SMELLED JET FUEL, TURNED APU OFF- NO MESSAGES DISPLAYED. INSPECTED TAIL COMPARTMENT AND APU COMPARTMENT FOR LEAKAGE. FOUND NONE. RUNUP APU. OPS CHECK IAW MM 49-10-00. AIRCRAFT OK FOR SERVICE.Oct 16, 2004 · N450AW · Cndair CL6002B19 · Airborne Auxiliary Power Unit (APU) SystemSDR A6WA200440080Elbow · leakingAIR VENT IN COCKPIT AND CABIN EMITTING A OIL LIKE ODOR, SMELLS LIKE KEROSENE, STRONGER AT TIMES THAN OTHERS WITH NO RELATION TO POWER SETTINGS. FOUND APU FUEL SOV SOLENOID LEAKING FROM LOWER ELBOW FITTING INSTALLED NEW PACKING ON ELBOW FITTING, OPS CHECK GOODJun 13, 2004 · N450AW · Cndair CL6002B19 · APU Engine Fuel and Control
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