N406AW, cancelled Jun 25, 2019

Service difficulty reports · 161

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 = 'N406AW' AND deregistration_id = 'N406AW-2019-06-25'
  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 A6WA201543414Wire Harness · defectiveSTEERING INOPERATIVE CAUTION IN FLIGHT. COMPLIED WITH QRH, MSG PERSISTED. R & R NLG HARNESS & LT ROTARY VOLTAGE DIFFERENTIAL TRANSDUCER. OPERATIONS CHECKED GOOD.Dec 28, 2015 · N406AW · Cndair CL6002B19 · Landing Gear System WiringSDR A6WA201543368Warning System · activatedRECEIVED GEAR DISAGREE WARNING ALONG WITH WOW INPUT CAUTION ON CLIMB OUT. TRIED TO RECYCLE GEAR WITH NO CHANGE. LEFT THE GEAR IN DOWN POSITION. GEAR SHOWED DOWN & 3 GREEN. RAN QRH FOR GEAR DISAGREE WARNING. PERFORMED MANUAL EXTENSION AS PRECAUTION & LANDEDec 16, 2015 · N406AW · Cndair CL6002B19 · Landing Gear Position and WarningSDR A6WA201543149Handle · lack of lubePASSENGER DOOR WILL NOT OPEN FROM OUTSIDE. INSPECTED PAX DOOR OUTER HANDLE & CLEARANCES IAW AMM 52-11-03, NO VISUAL DEFECTS NOTED. DOOR WILL NOT OPEN FROM OUTSIDE. HANDLE EXTENDS, BUT WILL NOT ROTATE. LUBED PAX DOOR HANDLE, PIN & BELL CRANK ASSEMBLIES IAW AOct 19, 2015 · N406AW · Cndair CL6002B19 · Passenger/Crew DoorsSDR A6WA201543048Light · inoperativeFORWARD FACING EMER EXIT SIGN AT ROW 8, LIGHTS BURNED OUT.Sep 10, 2015 · N406AW · Cndair CL6002B19 · Emergency LightingSDR A6WA201543042Apu · unknownFLIGHT 3945, APU WILL NOT START IN THE AIR. HEAVY FUEL ODOR OCCURS AFTER START ON THE GND WITH BOTH PACKS ON. COMPLIED WITH CM ACTION PLACARDED & PLACED ON MEL.Sep 7, 2015 · N406AW · Cndair CL6002B19 · APU Core EngineSDR A6WA201542620Seal · failedAT 30,000 FT RECEIVED LOUD NOISE COMING FROM SERVICE DOOR. PRESSURIZATION WAS NORMAL, NO DOOR WARNING INDICATIONS. NOISE COMES FROM LOWER RT SIDE. FLIGHT ATTENDANT REPORTS VIBRATION & FELT LIKE AIR WAS COMING FROM DOOR. DECLARED AN EMER & DIVERTED. R & RApr 11, 2015 · N406AW · Cndair CL6002B19 · Service DoorsSDR A6WA201341324Unknown · odorWITH PACKS ON THERE IS A STRONG FUEL SMELL IN THE AIRPLANE WITH APU ON.Feb 8, 2015 · N406AW · Cndair CL6002B19 · Air Distribution SystemSDR A6WA201442091Light · inoperativeEMERGENCY FLOOR TRACK LIGHTS ROW 8 - 12 INOPERATIVE.Oct 27, 2014 · N406AW · Cndair CL6002B19 · Emergency LightingSDR A6WA201442048Warning System · activatedDESCENDING THROUGH 20,000' ALL CRTS EXCEPT ED1 & 2 WENT BLANK. FMS WENT BLANK. FMS, FD MAP CAUTION, FMS NOT AVAILABLE. G/S WARNING APPEARED. THROUGH 10,000' APU BATTERY CHARGER STATUS MSG APPEARED.Oct 12, 2014 · N406AW · Cndair CL6002B19 · Central ComputersSDR A6WA201441978Light · inoperativeFLOOR TRACK EMER LIGHTS 2 - 5 WILL NOT ILLUMINATE.Sep 17, 2014 · N406AW · Cndair CL6002B19 · Emergency LightingSDR A6WA201441902Trim System · out of adjustON DEPARTURE LEVELING OFF AT 8,000 FT UNCOMMANDED FULL RT RUDDER TRIM. AUTO PILOT HAD BEEN ENGAGED FOR 2 MINUTES. COMPLIED WITH QRH DISCONNECTED AUTO PILOT & YAW DAMP. DISCOVERED RUDDER TRIM WAS AT FULL RT WITH NO INPUT FROM THE KNOB. KNOB WAS CENTERED. AAug 27, 2014 · N406AW · Cndair CL6002B19 · Rudder Tab Control SystemSDR A6WA201441592Mount Bracket · crackedFWD LT NOSE HYD COMPARTMENT BRAKE ACCUMULATOR FWD OTBD MOUNT BRACKET CRACKED. R & R WITH SERVICEABLE PART, PN 601R75250-55 IAW SRM 51-40-11 & 51-42-21.May 26, 2014 · N406AW · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR A6WA201441590Floor Support · corrodedLBL 27 FLOORBEAM CAP CORRODED AROUND NUTPLATE HOLES, FS 574 TO 621. R & R FLOORBEAM CAP WITH SERVICEABLE SECTION IAW SRM 51-40-11 & 51-42-21.May 25, 2014 · N406AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA201441571Door Sill · corrodedPAX DOOR LWR SILL IS CORRODED BETWEEN FS 315 TO FS 344. R & R WITH NEW SERVICEABLE SILL ANGLE IAW SRM 51-41-02, 51-42-06 & 51-42-13.May 23, 2014 · N406AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA201441572Skin · chafedLEFT INBD FLAP VANE LE SKIN IS CHAFED AT 3 LOCATIONS. REMOVED & REPLACED INBD & CTR FLAP VANE LE SKIN IAW SRM 51-42-13 & 51-40-11.May 23, 2014 · N406AW · Cndair CL6002B19 · Trailing Edge FlapsSDR A6WA201441573Door Frame · crackedPAX DOOR AFT FRAME AT FS 338 IS CRACKED UNDER PREVIOUS REPAIR. REMOVED CRACKED FRAME & REPLACED WITH NEW SERVICEABLE FRAME IAW REO 601R-52-11-402 REV H.May 22, 2014 · N406AW · Cndair CL6002B19 · Fuselage Main, StructureSDR A6WA201441588Mount Bracket · crackedEXTERNAL SERVICES PANEL ASSEMBLY UPPER MOUNT BRACKET CRACKED. R & R EXTERNAL SERVICES PANEL UPPER MOUNT BRACKET WITH SERVICEABLE PART, PN 601R51590-13 IAW SRM 51-40-11 & 51-42-06.May 20, 2014 · N406AW · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR A6WA201441560Fitting · corrodedRIGHT WINDSCREEN LWR FITTINGS HAVE CORROSION ON LWR SIDE. R & R UNSERVICEABLE FITTINGS & INSTALLED NEW SERVICEABLE FITTINGS IAW SRM 51-41-02.May 18, 2014 · N406AW · Cndair CL6002B19 · Passenger Compartment EquipmentSDR A6WA201441587Skin · damagedCOMPLIED WITH CARD 4DMI16358 REPAIR LT ELEVATOR DAMAGE NR 12 & 13 601R-51-00-293. PERFORMED PERMANENT REPAIR IAW SRM 55-20-00 FIG 204.May 17, 2014 · N406AW · Cndair CL6002B19 · Elevator, Plate/SkinSDR A6WA201441565Cleat · corrodedPAX DOOR LWR SILL FWD & AFT CLEATS ARE CORRODED. REMOVED FWD & AFT CLEATS ON LWR PAX DOOR SILL & INSTALLED NEW SERVICEABLE CLEATS IAW SRM 51-42-06.May 17, 2014 · N406AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA201441574Skin · gougedUPPER SURFACE OF LWR WING PLANK IS GOUGED AT WS 88.5. REPAIRED GOUGED UPPER SURFACE OF LWR WING PLANK IAW REO 601R--57-21-2192 DATED 5-21-14.May 16, 2014 · N406AW · Cndair CL6002B19 · Wing, Plate/SkinSDR A6WA201441589Frame · corrodedLOWER SECTION OF FS 605 FRAME HAS CORROSION. REPAIRED FRAME FS 605 IAW EA 15-2014-122 REV C DATED 5/24/2014.May 16, 2014 · N406AW · Cndair CL6002B19 · Fuselage Main, FrameSDR A6WA201441561Cleat · corrodedSERVICE DOOR CUT OUT THRESHOLD CLEATS HAVE CORROSION ATTACHED FASTENERS. REMOVED CORRODED FASTENERS & INSTALLED NEW SERVICEABLE FASTENERS IAW AMM 20-24-00.May 16, 2014 · N406AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA201441558Rib · crackedLEFT BATTERY RIB CRACKED ON FWD END. REMOVED CRACKED RIB & INSTALLED SERVICEABLE BATTERY RIB IAW REO 601R-57-51-046 REV B.May 16, 2014 · N406AW · Cndair CL6002B19 · Wing, Rib/BulkheadSDR A6WA201441591Housing · chafedSERVICE DOOR HANDLE HOUSING CHAFED. R & R HANDLE HOUSING WITH SERVICEABLE PART, PN 119935-1 IAW SRM 51-40-11 & 51-42-21.May 15, 2014 · N406AW · Cndair CL6002B19 · Service DoorsSDR A6WA201441562Fitting · crackedCLIPS AT FS 280 & STRINGER 3L CRACKED. REMOVED UNSERVICEABLE CLIP & INSTALLED SERVICEABLE CLIP IAW SRM 51-42-06, 51-41-02, 51-42-06 & 51-42-21.May 15, 2014 · N406AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA201441559Fitting · crackedCLIP AT FS 280 & STRINGER 3L CRACKED. REMOVED CRACKED CLIP & INSTALLED SERVICEABLE CLIP IAW SRM51-41-11 & 51-41-02.May 15, 2014 · N406AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA201441553Angle · crackedLEFT & RIGHT OBLIQUE ANGLES IN AEB ARE CRACKED. R & R CRACKED RT OBLIQUE ANGLE WITH NEW SERVICEABLE ANGLE IAW SRM 51-40-11 & 51-42-21. SEE W C 54596-3000-0004 FOR REMOVAL & REPLACEMENT OF LT OBLIQUE ANGLE.May 14, 2014 · N406AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA201441549Drag Angle · crackedLEFT DRAG ANGLE COMMON TO BATTERY RIB CRACKED AT AFT END. R & R CRACKED LT DRAG ANGLE WITH NEW SERVICEABLE DRAG ANGLE IAW SRM 51-42-21, 51-40-11 & 51-25-16.May 14, 2014 · N406AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA201441548Drag Angle · crackedPAX DOOR DRAG ANGLE FWD OF POWER ASSIST PULLEY BRACKET IS CRACKED. REPAIRED PAX DOOR DRAG ANGLE IAW REO 601R-52-11-513 REV A.May 14, 2014 · N406AW · Cndair CL6002B19 · Passenger/Crew DoorsSDR A6WA201441547Skin · crackedEXTERNAL LWR FUSELAGE SKIN AT AFT NLG CUT OUT ON BOTH LT & RT CORNERS ARE CRACKED. REPAIRED NLG WW CUT OUT IAW REO 601R-53-11-048 REV C 10-1-08.May 14, 2014 · N406AW · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR A6WA201441554Attach Fitting · corrodedSERVICE DOOR FWD SILL ATTACH AT FRAME IS CORRODED. R & R WITH NEW SERVICEABLE PART IAW SRM 51-42-21.May 13, 2014 · N406AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA201441552Angle · crackedLEFT LWR OBLIQUE ANGLE CRACKED ON AFT SIDE OF 621 BULKHEAD. R & R LWR OBLIQUE ANGLE WITH NEW SERVICEABLE ANGLE IAW SRM 51-42-21.May 13, 2014 · N406AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA201441551Drag Angle · crackedRIGHT DRAG ANGLE COMMON TO BATTERY RIB IS CRACKED. R & R RT DRAG ANGLE IAW SRM 51-42-21.May 13, 2014 · N406AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA201441550Mount Bracket · crackedEXTERNAL SERVICE PANEL 122CR CUT OUT LWR MOUNT BRACKET FOR SERVICE BOX CRACKED. REMOVED CRACKED MOUNT BRACKET & INSTALLED NEW BRACKET IAW SRM 51-42-13 & 51-40-11.May 13, 2014 · N406AW · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR A6WA201441600Post · crackedVERTICAL POST AT RBL 18 ON FS 409+128 BULKHEAD IS CRACKED AT LOWER END, OTBD AFT FLANGE. REPAIRED RBL 18 OTBD POST AT FS 409+128 IAW REO 601R-53-41-056 REV F DATED 2011/09/02.May 11, 2014 · N406AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA201441586Skin · dentedLEFT ELEVATOR HAS 4 DENTS ON LOWER SURFACE. REPAIRED 2 DENTS IAW SRM 55-20-00 FIG 204 & FOUND 2 DENTS TO BE IN LIMITS IAW SRM 55-20-00 FIG 101.May 11, 2014 · N406AW · Cndair CL6002B19 · Elevator, Plate/SkinSDR A6WA201441543Seat Track · corrodedCABIN NR 1 FLOOR SEAT TRACK CORRODED AT FWD END OF LBL 9 FS 364.00. REMOVED CORRODED SEAT TRACK & REPLACED WITH NEW SERVICEABLE SEAT TRACK IAW AMM 53-01-11.May 11, 2014 · N406AW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR A6WA201441542Seat Track · corrodedCABIN NR 1 FLOOR SEAT TRACK CORRODED AT FWD END RBL 9 AT FS 364.00. REMOVED CORRODED FLOOR SEAT TRACK & REPLACED WITH NEW SERVICEABLE FLOOR SEAT TRACK IAW SRM 53-01-11.May 11, 2014 · N406AW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR A6WA201441544Seat Track · corrodedSEAT TRACK AFT OF 9G TIE DOWN AT FS 559+112 HAS CORROSION AROUND FASTENERS HOLES. REMOVED UNSERVICEABLE SEAT TRACK & INSTALLED A NEW SERVICEABLE TRACK IAW SRM 53-01-11.May 10, 2014 · N406AW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR A6WA201441541Angle · corrodedFS 280.00 FLOOR ANGLES CORRODED & RBL 9 OTBD CLIP CRACKED. REPAIRED FWD 7 AFT FLOOR ANGLES AT FS 280 RBL 9 - LBL9. R & R OTBD CLIP AT FS 280 & RBL 9 IAW SRM 51-21-06, 53-00-00 & REO 601R-53-11-171 REV D.May 10, 2014 · N406AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA201441113Apu · shutdownTURNED APU GENERATOR ON, APU AUTO SHUTDOWN. HEAVY SMELL OF JET FUEL & SMOKE FROM EXHAUST. ACTION TAKEN IN PROGRESS. Feb 6, 2014 · N406AW · Cndair CL6002B19 · APU Core EngineSDR A6WA201312104046Fuel Sys · leaking3847 WITH PACKS ON THERE IS A STRONG FUEL SMELL IN THE AIRPLANE WITH APU ON. FOUND FUEL LEAK BY FUEL CONTROL. R, OPERATIONS & LEAK CHECKED GOOD AT THIS TIME NO FUEL SMELL NOTED IN CABIN.Dec 8, 2013 · N406AW · Cndair CL6002B19 · APU Engine Fuel and ControlSDR A6WA201303014018Warning System · activatedFLAPS FAIL CAUTION MSG DURING RETRACTION AFTER LANDING. PERFORMED FLAP RESET PROCEDURE IAW AWAC SUP 98-18E BOX 12. FLAPS RESET. PLACARD AND PLACED ON MEL.Mar 1, 2013 · N406AW · Cndair CL6002B19 · Trailing Flap Position Indicating SystemSDR A6WA201301234011Windshield · damagedIN FLIGHT SAW SPARKING AND MELTING ON LEFT WINDSHIELD. COMPLIED WITH QRH. TURNED WINDSHIELD HEAT OFF, SPARKS STOPPED. COORDINATED WITH DISPATCH AND ATC, RETURNED TO LAND AT DCA. LANDING WEIGHT 39,000. NO FURTHER INCIDENT. REPLACED LEFT WINDSHIELD.Jan 23, 2013 · N406AW · Cndair CL6002B19 · Flight Compartment WindowsSDR A6WA201240805Bpsu · failedFLAPS FAILED WHEN SELECTED 20-30. FLAPS STAYED AT 20 DEGREES. REPLACED RT BPSU PER 27 51 OPS CK GOOD.Aug 15, 2012 · N406AW · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR A6WA201240772Bpsu · failedFLAPS FAILED IN FLT AT 20 DEGREES WHEN 30 DEGREES WAS SELECTED. PERFORMED FLAP RESET PROCEDURE IAW SUPPLEMENT 98-18E BOX 12, FLAPS RESET. FOUND REPEAT BPSU FAULT CODES IN FECU, REPLACED LT BPSU IAW AMM 27-51. OPS CK GOOD.Aug 14, 2012 · N406AW · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR A6WA201240645Warning Message · false activationCARGO BOTTLE LOW CAUTION MESSAGE IN FLIGHT, NO INDICATION OF FIRE/SMOKE. INSPECTED CARGO BAY, NO EVIDENCE OF FIRE/SMOKE. NO BOTTLE DISCHARGE.Jun 30, 2012 · N406AW · Cndair CL6002B19 · Fire Protection SystemSDR A6WA201240535Panel · crackedRT ENGINE PYLON PANEL 422AB HAS CRACKED SEAL RETAINER. REMOVED UNSERVICEABLE RT ENG PYLON PANEL 422AB SEAL RETAINER AND INSTALLED SERVICEABLE SEAT RETAINER IAW SRM 51-42-06.May 11, 2012 · N406AW · Cndair CL6002B19 · Nacelle/Pylon, Plate/SkinSDR A6WA201240534Bracket · brokenT2 SENSE LINE BRACKET BROKEN, SUPPORT BRACKET FOR THE T2 SENSE LINE ON TOP OF THE ENGINE. REMOVED ENG INLET AND INSTALLED A NEW SERVICEABLE BRACKET.May 4, 2012 · N406AW · Cndair CL6002B19 · Nacelle/Pylon Miscellaneous Structure
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