N463AW

Service difficulty reports · 190

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 = 'N463AW' 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 A6WA202605268889Drive Assy · failedFLAPS FAILED CAUTION MSG ON APPROACH. FLAPS FAILED AT ZERO DEG. C/W FIM RESET, RESET FAILED. AIRCRAFT REMOVED FROM SERVICE. INSPECTED FLAP SKEW DETECTOR IAW FIM 27-50-00. FAULTS NOTED FOR FECU POWER 1 AND 2 AND LH OUTBD PANEL SKEW L4 AND L3. DEACTIVATED SKEW May 26, 2026 · N463AW · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR A6WA202602208881Door · bindingLEFT OVERWING EXIT WILL NOT OPEN FREELY. AIRCRAFT REMOVED FROM SERVICE. PERFORMED OPS CHECK OF OVERWING EMGERGENCY EXIT IAW AMM 52-21-00. PERFORMED OPS CHECK OF OVERWING EMGERGENCY EXIT IAW AMM 52-21-00. DOOR OPENS AND CLOSES FREELY, COMPLIED WITH CM ACTFeb 20, 2026 · N463AW · Cndair CL6002B19 · Emergency ExitsSDR A6WA202309198653Unknown · unknownGEAR DISAGREE ON RETRACTING GEAR AT 220 KTS. AT FLAPS 0, HYD PUMPS IN AUTO 3B TO ON. MESSAGES ENCOUNTERED DURRING GO AROUND. (MOC NOTE GO AROUND WAS FOR UNSTABLE APPROCH) *****AIRCRAFT REMOVED FROM SERVICE******** CW M ACTION FOR MEL 32-30-01 REF 359659/3 Sep 19, 2023 · N463AW · Cndair CL6002B19 · Landing Gear Retraction/Extension SystemSDR A6WA202308148647Wire Harness · unknownAFTER TAKE-OFF, AFTER SELECTING GEAR UP, GOT GEAR DISAGREE WITH NOSE GEAR SHOWING DOWN. COMPLETED QRH TO EXTEND GEAR, GEAR SHOWED DOWN WITH THREE GREEN. NOSE GEAR INDICATION REMAINED GREEN WHOLE FLIGHT. HYD QTY, PRESSURE AND TEMPS NORMAL.AIRCRAFT REMOVED FROM Aug 14, 2023 · N463AW · Cndair CL6002B19 · Landing Gear System WiringSDR A6WA202308068645Unknown · unknownRECEIVED GEAR DISAGREE WARNING MESSAGE AFTER TAKE-OFF AND NOSE DOOR OPEN WARNING MESSAGE. FLAPS AT 8. RECEIVED 3 GREEN AFTER SELECTING GEAR DOWN WITH MANUAL RELEASE HANDLE AND GEAR LEVER PER QRH. AIRCRAFT REMOVED FROM SERVICE. R & R BENT NLG CENTERING PROX SAug 6, 2023 · N463AW · Cndair CL6002B19 · Main Landing GearSDR A6WA202306298632Unknown · unknownON SHORT FINAL FA REPORTED SMOKE/SMELL FROM ROW 8CD. CHEMICAL SMELL LASTED FOR ABOUT 5MINS AFTER LANDING TO OPENING THE PAX DOOR AIRCRAFT REMOVED FROM SERVICE. INSPECTED CABIN. ALL OVERHEAD AND SIDEWALL LIGHTING OPS NORMAL. INSPECTED AND CLEANED TEMP SENSOJun 29, 2023 · N463AW · Cndair CL6002B19 · Cabin Cooling SystemSDR A6WA202305178609Unknown · unknownON-TAKE OFF AFTER GEAR RETRACTION RECEIVED NOSE DOOR OPEN AND GEAR DISAGREE MASTER WARNING APPROXIMATELY 6 SECONDS AFTER SELECTING GEAR UP. (BLK 2) NOSE LANDING GEAR SHOWED RED ON EICAS MANUAL RELEASE WAS USED. DID NOT ENCOUNTER ICING OR TURBULENCE HYD PUMPS TMay 17, 2023 · N463AW · Cndair CL6002B19 · Nose/Tail Landing GearSDR A6WA202212058464Doubler · noneDURING INCORPORATION OF REO 601R-53-61-1240 REPAIR AND MODIFICATION TO THE FS621.00 PRESSURE BULKHEAD WEB, FOUND EXISTING DOUBLER PN 601R-53-61-5768-1 INSTALLED AT FS621.00 AND LBL9.50 TO LBL27.50, WL74 TO WL87.4. *****AIRCRAFT REMOVED FROM THE SERVICE********Dec 5, 2022 · N463AW · Cndair CL6002B19 · Fuselage Structure (General)SDR A6WA202212058462Skin · chafedWEAR DAMAGE TO THE FUSELAGE EXTERNAL SKIN PN 601R35004-405 AT FS682.00 - FS700.00 AND STR 15R. ********AIRCRAFT REMOVED FROM SERVICE*********** BLENDED WEAR DAMAGE TO THE FUSELAGE EXTERNAL SKIN PN 601R35004-405 AT FS682.00 - FS700.00 AND STR 15R. DIMENSIONS LDec 5, 2022 · N463AW · Cndair CL6002B19 · Fuselage Structure (General)SDR A6WA202212058459Skin · dentedTWO DENTS ON FORWARD FUSELAGE SKIN PN 601R31022-61 AT FS319.00-FS333.00 AND STR 25L - STR 26L. DENT DIMENSIONS: D5- L = 0.600Ï¿½ X W = 0.600Ï¿½ X D = 0.009Ï¿½, FS280.00+13 D6- L = 0.600Ï¿½ X W = 0.500Ï¿½ X D = 0.008Ï¿½, FS280.00+14 ORIGINAL MATERIAL THICKNESDec 5, 2022 · N463AW · Cndair CL6002B19 · Fuselage Floor PanelSDR A6WA202212058457Skin · dentedTHREE DENTS ON FORWARD FUSELAGE SKIN PN 601R31022-61 AT FS280.00-FS295.00 AND STR 25L - STR 26L. DENT DIMENSIONS: D1- L = 0.250Ï¿½ X W = 0.200Ï¿½ X D = 0.004Ï¿½, FS280.00+13 D2- L = 0.400Ï¿½ X W = 0.325Ï¿½ X D = 0.007Ï¿½, FS280.00+14 D3- L = 0.350Ï¿½ X W = 0Dec 5, 2022 · N463AW · Cndair CL6002B19 · Fuselage Floor PanelSDR A6WA202212058458Skin · dentedONE DENT ON FORWARD FUSELAGE SKIN PN 601R31022-61 AT FS310.00-FS319.00 AND STR 25L - STR 26L. DENT DIMENSIONS: D4- L = 0.825Ï¿½ X W = 0.800Ï¿½ X D = 0.008Ï¿½, FS310.00+9 ORIGINAL MATERIAL THICKNESS 0.063Ï¿½. ****AIRCRAFT REMOVED FROM SERVICE****** VERIFIEDDec 5, 2022 · N463AW · Cndair CL6002B19 · Fuselage Floor PanelSDR A6WA202212058456Doubler · dentedDENT TO FORWARD FUSELAGE SKIN FS280.0 TO FS310.0 AND STR 11-14 RHS. ****AIRCRAFT REMOVED FROM SERVICE******* PERFORMED A PERMANENT REPAIR FOR TEMPORARY REO 601R-53-21-3568 TO A DENT TO FORWARD FUSELAGE SKIN FS280.0 TO FS310.0 AND STR 11-14 RHS. FABRICATED DOUDec 5, 2022 · N463AW · Cndair CL6002B19 · Fuselage Floor PanelSDR A6WA202212058453Seat Track · corrodedCORROSION ON CABIN FLOOR SEAT TRACK PN 601R35031-263 AT FS559.00 TO FS621.00 AND RBL27.0. ***** AC REMOVED FROM SERVICE ***** CORROSION EXCEEDED SRM LIMITS AND REMOVED AND REPLACED CABIN FLOOR SEAT TRACK PN 601R35031-263 AT FS559.00 TO FS621.00 AND RBL27.0. SEDec 5, 2022 · N463AW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR A6WA2023013058452Drag Angle · crackedPAX DOOR AFT PANEL DRAG ANGLE IS CRACKED AT PULLEY BRACKET AREA AT FS339.50. AIRCRAFT REMOVED FROM SERVICE. REPAIRED DRAG ANGLE WITH FABRICATION OF NEW ANGLE, DIMENSIONS L= 21.500Ï¿½ W= 1.600Ï¿½. PERFORMED HFEC WITH NO INDICATIONS. RESTORED PROTECTIVE FINISHDec 5, 2022 · N463AW · Cndair CL6002B19 · Passenger/Crew DoorsSDR A6WA202207308300None · noneNOSE GEAR DISAGREE MESSAGE APPEARED AFTER LANDING GEAR WAS MOVED TO UP POSITION. RAN QRH, MESSAGE PERSIST. MANUALLY DEPLOY GEAR AND MESSAGE CLEARED. NOSE DOOR OPEN WARNING MESSAGE APPEARED AFTER GEAR DISAGREE MESSAGE WAS DISPLAYED. NO GEAR BOXES WERE RED, ONLAug 25, 2022 · N463AW · Cndair CL2151A10 · Landing Gear SystemSDR A6WA202203318157None · none****SUPPLEMENTAL INFORMATION**** FLAPS FAIL CAUTION MESSAGE IN CRUISE AT FL 300. QRH COMPLETED. PERFORMED FLAP RESET PROCEDURE IAW AWAC SUPPLEMENT 98-18I BOX 12. FLAPS RESET, PLACARDED AND PLACED ON MEL AIRCRAFT REMOVED FROM SERVICEPERFORMED Mar 31, 2022 · N463AW · Cndair CL6002B19 · Trailing Flap Position Indicating SystemSDR A6WA202112178028Flap System · faultedRECEIVED FLAPS FAIL CAUTION MESSAGE AFTER INTIAL DECENT. C/W QRH & PROCEDED TO LAND AT DESTINATION. FLAPS WERE AT ZERO POSITION. PERFORMED FLAP RESET PROCEDURE IAW SUP 98-18I BOX 12. FLAPS RESET. CAPTAIN WAS THE FLYING PILOT. DURING DECENT AT 5,000 FT & FLADec 17, 2021 · N463AW · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR A6WA202110247930None · noneFO'S FRONT WINDSHIELD IS CRACKED, OUTER PLY. ***AIRCRAFT REMOVED FROM SERVICE*** REMOVED FO WINDSHIELD AND COMPLETED INSTALLATION UP TO SUBTASK 56-11-01-430-007, STEP D. REF 348762/1 FOR COMPLETION OF TASKS P/N: NP139321-18, S/N OFF: 1107H5903, S/N ON: Oct 24, 2021 · N463AW · Cndair CL6002B19 · Window/Windshield SystemSDR A6WA202107297841Seal · lack of lubeAFTER TAXIING INTO GATE, UNABLE TO OPEN MAIN CABIN DOOR FROM INSIDE OR OUTSIDE. ***AIRCRAFT REMOVED FROM SERVICE*** CLEANED, INSPECTED, AND LUBED PAX DOOR SEAL IAW AWAC SUP 19-152A. OPS CHECK GOOD AT THIS TIME. OPERATED FROJul 28, 2021 · N463AW · Cndair CL6002B19 · Passenger/Crew DoorsSDR A6WA2019090546840Support Bracket · crackedRT HYDRAULIC MANIFOLD SUPPORT BRACKET AFT LOWER CORNER CRACKED. REMOVED AND REPLACED RT HYDRAULIC MANIFOLD SUPPORT BRACKET IAW REO 601R 53-62-031 REV A.Sep 4, 2019 · N463AW · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR A6WA2019090546839Seat Track · corrodedFLOOR SEAT TRACK #4 ON RBL9 HAS CORROSION. REMOVED AND REPLACED FLOOR SEAT TRACK #4 RBL 9 IAW SUPPLEMENT 19-254.Sep 4, 2019 · N463AW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR A6WA2019090546841Skin · chafedBOTTOM LEADING EDGE OF RIGHT AILERON SKIN CHAFING. REMOVED AND REPLACED RT AILERON LOWER CENTER LEADING EDGE SKIN IAW SRM 51-42-06 AND 51-42-21.Sep 4, 2019 · N463AW · Cndair CL6002B19 · AileronsSDR A6WA2019090546838Skin · corrodedFUEL ACCESS CUTOUT 510AB SHOWS SIGNS OF FRETTING. REPAIRED FUEL ACCESS CUTOUT 510AB IAW EA# AWAC-CRJ257-01318 REVA.Sep 3, 2019 · N463AW · Cndair CL6002B19 · Wing, Plate/SkinSDR A6WA2019090546832Intercostal · crackedINTERCOSTAL WHICH BUTTS UP TO AIRCARFT SKIN ON AFT SIDE OF 621 BULKHEAD AT STRINGER 14L APPEARS CRACKED. REMOVED AND REPLACED STRINGER 14L INTERCOSTAL IAW SRM 51-42-06 AND 51-42-21.Sep 3, 2019 · N463AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA2019090546835Intercostal · corrodedEVIDENCE OF CORROSION ON PAX DOOR INTERCOSTAL THAT IS ABOVE LATCH MECH BOX. REMOVED AND REPLACED INTERCOSTAL IAW SRM 51-42-06, 51-42-21 AND 51-42-13.Sep 3, 2019 · N463AW · Cndair CL6002B19 · Passenger/Crew DoorsSDR A6WA2019090546836Post · cracked409+128 VERTICAL POST AT RBL 18 IS CRACKED ON RIGHT SIDE AT AFT INBOARD ANGLE AT 6TH FASTENER FROM TOP. REMOVED AND REPLACED VERTICAL POST ASSEMBLY AT FS 409+128 AT RBL 18 IAW GREO 601R-53-41-889 REV D.Sep 3, 2019 · N463AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA2019090546833Door Sill · corrodedRT FLOOR SILL HAS CORROSION BETWEEN FS 559+80 AND FS 589 ON UPPER AND LOWER SURFACES. REMOVED AND REPLACED RT FLOOR SILL AT WL 73.50 AND FS 559+87 TO 559+118 IAW SRM 51-42-21 AND 51-42-06.Sep 3, 2019 · N463AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA2019090546831Support Beam · gougedPERFORM PERMANENT REPAIR FOR CARGO BAY DOOR TRACK SUPPORT BEAM. REPLACED CARGO DOOR SUPPORT BEAM IAW SRM 51-42-20. THIS COMPLIES WITH DMI 22614.Sep 1, 2019 · N463AW · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR A6WA2019090446830Bracket · crackedAFTER REMOVAL OF CARGO BAY DOOR TRACK SUPPORT BEAM BRACKET ON 621 FWD SIDE CRACKED IN TWO PLACES. REMOVED AND REPLACED CARGO DOOR BEAM BRACKET IAW SRM 51-42-21 AND SRM T/R 51-42.Sep 1, 2019 · N463AW · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR A6WA2019090546834Skin · chafedRIGHT INBOARD FLAP VANE, INBOARD SKIN HAS CHAFING. REPLACED RIGHT I/B FLAP VANE I/B LEADING EDGE IAW SRM 51-42-13.Aug 31, 2019 · N463AW · Cndair CL6002B19 · Trailing Edge FlapsSDR A6WA2019090446828Skin · crackedPAX DOOR INNER SKIN CRACKED AT DOOR DATUM 6, FS335. REPAIRED PAX DOOR INNER SKIN IAW SUPP. 19-248.Aug 31, 2019 · N463AW · Cndair CL6002B19 · Passenger/Crew DoorsSDR A6WA2019090446829Seat Track · corrodedRIGHT FLOOR SEAT TRACK #5 CORRODED. REPLACED SEAT TRACK #5 IAW AMM 53-01-11.Aug 30, 2019 · N463AW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR A6WA2019090446827Seat Track · corrodedRIGHT FLOOR SEAT TRACK #3 CORRODED. REPLACED SEAT TRACK IAW AMM 53-01-11.Aug 30, 2019 · N463AW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR A6WA2019090446826Fitting · crackedFS 202.75 IN NLG WHEEL WELL RBL9 POST UPPER CLIP IS CRACKED. REPLACED CLIP IAW SRM 51-42-06.Aug 29, 2019 · N463AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA2019083046817Bracket · crackedFS469.00, RBL 45 FAIRING ATTACH BRACKET IS CRACKED. REMOVED AND REPLACED FS469.00, RBL 45 FAIRING ATTACH BRACKET IAW SRM 51-42-06.Aug 29, 2019 · N463AW · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR A6WA2019083046812Threshold · corrodedSERVICE DOOR LOWER SILL THRESHOLD CORRODED. REPLACED SERVICE DOOR LOWER SILL THRESHOLD IAW CRJ200 SRM TR 51-42.Aug 29, 2019 · N463AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA2019083046819Bracket · crackedFS449.00,LBL 45 FAIRING ATTACH BRACKET CRACKED. REPLACED BRACKET IAW SRM 51-42-06.Aug 29, 2019 · N463AW · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR A6WA2019083046818Bracket · crackedFS461.00, RBL45 FAIRING ATTACH BRACKET CRACKED. REPLACED BRACKET IAW SRM 51-42-06.Aug 29, 2019 · N463AW · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR A6WA2019083046821Bracket · crackedRIGHT MLG BAY VOLUMETRIC FUSE BRACKET, LINE BRACKET CRACKED. REPLACED BRACKET IAW SRM 51-42-06.Aug 29, 2019 · N463AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA2019083046820Bracket · crackedFS469.00, LBL45 FAIRING SUPPORT ATTACH BRACKET CRACKED. REPLACED BRACKET IAW CRJ 200 SRM 51-42-06.Aug 29, 2019 · N463AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA2019083046815Intercostal · crackedINTERCOSTAL ON AFT SIDE OF 621 BULKHEAD AT STR 15L IS CRACKED. REPLACED INTERCOSTAL IAW SRM 51-42-06, 51-42-21.Aug 28, 2019 · N463AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA2019083046816Intercostal · crackedINTERCOSTAL AT FS621.00 STR 16L IS CRACKED ON AFT SIDE OF BULKHEAD. REPLACED INTERCOSTAL IAW CRJ 200 SRM 51-42-06, 51-42-21.Aug 28, 2019 · N463AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA2019083046813Skin · crackedFS235.00, STR 26L NLG CUT OUT IS CRACKED. REPAIRED NLG CUT OUT IAW REO 601R-53-11-101 REV-E.Aug 28, 2019 · N463AW · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR A6WA2019082846808Skin · crackedFS 235 STR 26R NLG CUTOUT HAS A CRACK INDICATION REPAIR ACCOMPLISHED ON AAR N/R WO 1017605 1000/0005Aug 27, 2019 · N463AW · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR A6WA2019082746807Cargo Track · corrodedCARGO FLOOR TRACK CORRODED AT 559+78 TO 559+95, LBL27. OUT OF LIMITS PER SRM 53-21-49, REPLACED TRACK IAW AMM 53-01-11.Aug 25, 2019 · N463AW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR A6WA2019082746804Web · crackedFS 193,LBL30 TRU WEB IS CRACKED. REPAIRED WEB IAW REO 601R-53-11-111 REV-NC.Aug 24, 2019 · N463AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA2019082746806Seat Track · corrodedLEFT SIDEWALL SEAT TRACK NR 5 CORRODED. OUT OF LIMITS PER REO 601R-53-00-055 REV-C REPAIR B. REPLACED LEFT SIDEWALL SEAT TRACK 5 IAW AMM 53-01-11.Aug 24, 2019 · N463AW · Cndair CL6002B19 · Fuselage, Door HingeSDR A6WA2019802746800Vertical Support · cracked409+128 VERTICAL POST AT BL 0 IS CRACKED ON BOTH RIGHT AND LEFT SIDES AT AFT ANGLE, 6TH FASTENER FROM TOP. REPLACED ANGLES ON THE VERTICAL POST IAW SRM 51-42-06 AND REO 601R-53-41-889 REV-D.Aug 22, 2019 · N463AW · Cndair CL6002B19 · Fuselage Main, StructureSDR A6WA2019082746799Angle · crackedFS 484, LBL36 I/B CLIP CRACKED. REPLACED CLIP IAW REO 601R-53-41-059 REV-B.Aug 21, 2019 · N463AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
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