N465AW

Service difficulty reports · 170

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 = 'N465AW' 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 A6WA201745056Frame · corrodedFRAME BS 349 HAS CORROSION ON THE FWD AND AFT SIDE BETWEEN STRINGER 26L AND 26R.Jun 13, 2017 · N465AW · Cndair CL6002B19 · Fuselage Main, FrameSDR A6WA2017061445054Fitting · corrodedLBL 27 AFT FITTING IS CORRODED AT OTBD NUTPLATE LOCATION AT BS 618.Jun 13, 2017 · N465AW · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR A6WA2017061445055Frame · crackedFRAME BS 333 CRACKED AT STRINGER 2L.Jun 11, 2017 · N465AW · Cndair CL6002B19 · Fuselage Main, FrameSDR A6WA2017061245050Stringer · crackedSTRINGER 3L CRACKED AT BS 379.Jun 10, 2017 · N465AW · Cndair CL6002B19 · Fuselage Main, Longeron/StringerSDR A6WA2017061945047Bracket · crackedRIGHT INTERCOSTAL BRACKET CRACKED ON THE AFT REAR PRESSURE BULKHEAD AT BS 621. REPLACED INTERCOSTAL IAW SRM 51-41-21.Jun 9, 2017 · N465AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA2017061245048Floorbeam · crackedFLIGHT DECK FLOORBEAM CRACKED ON THE FWD SIDE OF BS 280, RBL9. REPLACED THE FLOORBEAM ANGLE IAW SRM 51-42-06, AND 51-42-21.Jun 9, 2017 · N465AW · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR A6WA2017061245046Retainer · crackedSEAL RETAINER CRACKED ON PANEL 422BT. REPAIRED THE SEAL RETAINER IAW SUP 16-363.Jun 2, 2017 · N465AW · Cndair CL6002B19 · Nacelle/Pylon, Main FrameSDR A6WA2017060545040Structure · crackedPAX DOOR EDGE MEMBER HAS A CRACK ON FWD END. REPAIRED IAW REO 601R-52-11-279, REV NC.Jun 2, 2017 · N465AW · Cndair CL6002B19 · Passenger/Crew DoorsSDR A6WA201744728Engine · power lossAT 31,000 FEET LOST 5% N1 ON RIGHT ENGINE WITH SLIGHT YAW. LASTED 2-3 SECONDS, THEN CONDITION CORRECTED ITSELF WITH NO INPUT FROM THE CREW. N1 WAS SET TO 85 % AT TIME OF ROLLBACK, AND SPEED SWITCHES WERE SELECTED ON. NO ABNORMAL CAUTIONS OR MESSAGES PRESENT DUJan 7, 2017 · N465AW · Cndair CL6002B19 · Engine (Turbine/Turboprop)SDR A6WA201644258Flap System · malfunctionedFLAPS FAIL DURING CLIMB OUT, AT FLT LEVEL 230, 280 KNOTS FLAPS AT 0 WITH NO MOVEMENT OR SELECTION TO FLAPS. COMPLIED WITH QRH, MESSAGE PERSISTED. DIVERTED AND DECLARED EMERGENCY. RESET FLAPS IAW FIM 27-50-00 AND SET FLAPS AT 20 DEGREES.Aug 22, 2016 · N465AW · Cndair CL6002B19 · Trailing Flap Position Indicating SystemSDR A6WA201644251Flap · malfunctionedFLAP FAIL CAUTION MESSAGE DURING CRUISE CLIMB, FLAPS AT ZERO DEGREES, PERFORMED FLAP RESET PROCEDURE IAW SUPP 98-18G, BOX 12, FLAPS RESET. NOTED BY MAINTENANCE.Aug 21, 2016 · N465AW · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR A6WA201643960Unknown · smokeCARGO SMOKE WARNING OCCURRED AT GATE. RAMP VERIFIED SMOKE PRESENT IN CARGO BAY WHEN OPENING DOOR.May 31, 2016 · N465AW · Cndair CL6002B19 · Air Distribution SystemSDR A6WA201643663Thrust Reverser · lack of lubeIN FLIGHT RECEIVED RT REV UNLOCK MSG. COMPLIED WITH QRH. DIVERTED & LANDED BELOW 47000 LBS & MAX BTMS WAS 4454. DEACTIVATED RT TR IAW SUP 15-046, M ACTION COMPLIED WITH. PERFORMED TR LUBE IAW SUPP 14-118A. OPERATIONS CHECKED GOOD AT THIS TIME. REMOVED PLMar 6, 2016 · N465AW · Cndair CL6002B19 · Engine Thrust ReverserSDR A6WA201643586Adg · deployed FLIGHT NR 4026, IMMEDIATELY AT TAKEOFF, LOUD NOISE FROM FRONT OF ACFT, NO CAUTIONS, OR WARNINGS. ELEC SYNOPTIC SHOWED ADG DEPLOYED. ADG DEPLOYED AT APPROX 145 KNOTS, MAX OF 200 KNOTS ON RETURN. ADG DEPLOYED APPROX 14 MINUTES. PERFORMED VISUAL INSPECTION OFeb 14, 2016 · N465AW · Cndair CL6002B19 · AC Generator-AlternatorSDR A6WA201543012Computer · failedFLIGHT 9365, 3848CXL 3951 CBP1 N5 & CBP2 H14 POPPED. ELEC BURNING SMELL IN COCKPIT & GALLEY. AHRS WAS INTERMITTENT THEN HARD FAIL. R & R AHRS COMPUTER. OPERATIONS CHECKED GOOD IAW AMM 34-21-01. CB DID NOT POP OR ELEC ODOR NOTED AT THIS TIME. SN OFF 3393 Aug 28, 2015 · N465AW · Cndair CL6002B19 · Integrated Flight SystemSDR A6WA201542799Light · inoperativeFLIGHT NR 3849, EMER FLOOR LIGHT STRIP INOPERATIVE AFT OF ROW 8.May 31, 2015 · N465AW · Cndair CL6002B19 · Emergency LightingSDR A6WA201542779Angle · crackedLT UPPER OBLIQUE ANGLE ON SF621 BULKHEAD CRACKED.May 23, 2015 · N465AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA201542782Bracket · crackedBRACK TRANSDUCER BRACKET IN LT WW IS CRACKED.May 23, 2015 · N465AW · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR A6WA201542778Stringer Clip · crackedFS 280 STRINGER 3L CLIPS ARE CRACKED.May 23, 2015 · N465AW · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR A6WA201542775Floorbeam · crackedUPPER CAP ON FS 280 FLOORBEAM IS CRACKED AT RBL 9 & 12.May 23, 2015 · N465AW · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR A6WA201542777Fitting · crackedOUTER CLIP CRACKED AT FS 280 LBL 9, BOTH CLIPS CRACKED AT LBL 9.May 23, 2015 · N465AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA201542776Skin · dentedLEFT AFT FUSELAGE SKIN HAS PROTRUDING DENT AT FS 712.00.May 23, 2015 · N465AW · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR A6WA201542780Fitting · chafedHORIZONTAL STAB LT & RT OTBD PIVOT FITTING ON STAB IS GOUGED & SCORED.May 23, 2015 · N465AW · Cndair CL6002B19 · Horizontal Stabilizer Miscellaneous StructureSDR A6WA201542781Stiffener · crackedWING STIFFENER IN RT WW AT WS 48 IS CRACKED.May 23, 2015 · N465AW · Cndair CL6002B19 · Wing Miscellaneous StructureSDR A6WA201542783Drag Angle · cracked55378-8000-0016 PAX DOOR AFT DRAG ANGLE IS CRACKED.May 23, 2015 · N465AW · Cndair CL6002B19 · Passenger/Crew DoorsSDR A6WA201542771Structure · crackedNOSE WW CUT OUT AFT RT CORNER IS CRACKED.May 22, 2015 · N465AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA201542788Handle · crackedPAX DOOR INNER HANDLE CRACKED.May 21, 2015 · N465AW · Cndair CL6002B19 · Passenger/Crew DoorsSDR A6WA201542770Bulkhead · crackedFS 202 BULKHEAD CRACKED APPROX 3" LONG AT CUT OUT FOR PARKING BRAKE CABLE.May 21, 2015 · N465AW · Cndair CL6002B19 · Fuselage Main, BulkheadSDR A6WA201542789Seal Depressor · gougedSERVICE DOOR SEAL STRIKER GOUGED.May 19, 2015 · N465AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA201542762Fitting · crackedLEFT WINDSHIELD POST LOWER FITTING IS CRACKED.May 19, 2015 · N465AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA201542759Fitting · crackedRIGHT FS 484.00 CLIPS ARE CRACKED AT BL 27.00.May 19, 2015 · N465AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA201542761Support Angle · crackedLOWER SUPPORT ANGLE FOR CARGO COMPARTMENT CURTAIN HANGAR SUPPORT ON AFT END HAS A CRACK ON OTBD END.May 19, 2015 · N465AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA201542760Fitting · crackedFLIGHT COMPARTMENT RT SIDE WINDOW POST LOWER FITTING IS CRACKED.May 19, 2015 · N465AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA201542382Cover · unsecureEMERGENCY LIGHT FLOOR TRACK COVER AT ROW 1C - D COMING OFF.Feb 8, 2015 · N465AW · Cndair CL6002B19 · Emergency LightingSDR A6WA2014073141817Engine · failedAPU AUTOSHUTDOWN FLAME OUT. FIRST OFFICER FOUND METAL DEBRIS NEAR APU EXHAUST. INSPECTED & FOUND INTERNAL APU FAILURE, CLEANED & SECURED AREA. APU IS CONSIDERED INOPERABLE.Jul 28, 2014 · N465AW · Cndair CL6002B19 · APU Core EngineSDR A6WA2013071041046Skin · damagedSKIN SURROUNDING PANEL 132AL HAS TWO PLACES THAT HAS SCREW BITE MARKS. BLENDED OUT DAMAGE ON RT FUSELAGE SKIN IAW REO 601R-53-11-2529, REV B.Jul 5, 2013 · N465AW · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR A6WA20134M1045Skin · damagedSKIN HAS ONE SCREW HOLE THAT ELONGATED AT THE 12:00 POSITION. REPAIRED RT FUSELAGE SKIN IAW REO 601R-53-11-2529, REV B.Jul 5, 2013 · N465AW · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR A6WA2013071041062Mount · crackedSERVICE DOOR SWITCH MOUNT IS CRACKED. R & R MOUNT ON SERVICE DOOR IAW SRM 51-41-02 AND 51-42-21.Jul 2, 2013 · N465AW · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR A6WA20134M1055Skin · crackedRUDDER RT LOWER FWD SKIN IS CRACKED AND DENTED. R & R SKIN.Jul 2, 2013 · N465AW · Cndair CL6002B19 · Rudder, Plate/SkinSDR A6WA2013071041052Tie Down · corrodedBULKHEAD TIE DOWNS AT 559+80 LBL 9 AND 27 AND RBL 9 AND 27 HAVE CORROSION. BLENDED OUT OF LIMITS, R & R.Jul 1, 2013 · N465AW · Cndair CL6002B19 · Fuselage Main, BulkheadSDR A6WA2013071041058Trunnion · damagedDURING COLD WORKING OF MLG FOUND TWO OVERSIZED HOLES 1 ON LT & 1 ON RT LOWER MLG TRUNNION FLANGE. REPAIRED DISCREPANT HOLES ON LT & RT MLG TRUNNION FLANGE. IAW REO 601R-57-21-1963.Jun 29, 2013 · N465AW · Cndair CL6002B19 · Wing, Landing Gear Attach FittingsSDR A6WA2013071041050Bulkhead · chafedRT AFT FS 280 BULKHEAD CHAFED. REPAIRED IAW REO 601R-53-11-1727. REV E.Jun 29, 2013 · N465AW · Cndair CL6002B19 · Fuselage Main, BulkheadSDR A6WA2013071041048Heat Shield · damagedAPU AFT HEAT SHIELD HAS SIX SCREWS PULLED THRU. FABRICATE AND INSTALLED HEAT SHIELD IAW SRM 51-24-16, SRM 51-21-11,SRM 51-25-06 AND SRM 51-40-11.Jun 29, 2013 · N465AW · Cndair CL6002B19 · APU Cowling/ContainmentSDR A6WA2013071041056Bracket · gougedGOUGE ON UPPER T/E BRACKET ON RT PYLON L/E PANEL 421 AL IS OUT OF LIMITS DUE TO PROXIMITY TO FASTENER HOLE. R & R.Jun 28, 2013 · N465AW · Cndair CL6002B19 · Nacelle/Pylon Miscellaneous StructureSDR A6WA2013071041054Panel · chafedVISOR PANEL NR 326 BL DISTORTED (BENT) CHAFED BEYOND LIMITS. REPLACED WITH SERVICEABLE VISOR PANEL.Jun 28, 2013 · N465AW · Cndair CL6002B19 · Wing StructureSDR A6WA2013071041047Sill · corrodedPAX DOOR LOWER SILL HAS MULTIPLE AREAS OF CORROSION FOUND TO BE OUT OF ALLOWABLE LIMITS. R & R PAX DOOR LOWER SILL IAW SRM.Jun 28, 2013 · N465AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA2013071041061Seal · crackedLT FLIGHT SPOILER WING T/E SEAL IS CRACKED. R & R.Jun 27, 2013 · N465AW · Cndair CL6002B19 · SpoilersSDR A6WA2013071041059Vane · crackedRT FLAP VANE L/E CRACKED. BLENDED 2 AREAS WITHIN LIMITS BLENDED INBD L/E OUT OF LIMITS CHANGED INBD L/E SKIN.Jun 27, 2013 · N465AW · Cndair CL6002B19 · Trailing Edge FlapsSDR A6WA2013071041064Skin · chafedINNER SKIN CHAFED OUT OF LIMITS. REPLACED INNER SKIN.Jun 26, 2013 · N465AW · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR A6WA2013071041063Support Bracket · crackedFWD LOWER SUPPORT BRACKET FOR CARGO BAY DOOR WAS CRACKED. R & R IAW SRM 51-42-06 & 51-41-02.Jun 26, 2013 · N465AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
Back to N465AW