N405AW

Service difficulty reports · 198

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 = 'N405AW' 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 A6WA202103107711Strap · damagedFORWARD PRESSURE BULKHEAD AT FS 202.75 CENTER POST AFT STRAP HAS TOOLING MARKINGS/ GOUGES JUST BELOW THE LOWER FASTENER OF WINDSHIELD LEFT LOWER CENTER POST FITTING, NEED TO COORDINATE WITH ENGINEERING AS REQUIRED FOR DISPOSITION. ***AIRCRAFT REMOVED FROM SEMar 7, 2021 · N405AW · Cndair CL6002B19 · Fuselage Main, BulkheadSDR A6WA202103097708Skin · corrodedCORROSION ON LOWER RIGHT HAND TCAS ANTENNA AREA ***AIRCRAFT REMOVED FROM SERVICE*** REMOVED CORROSION AT LWR R/H TCAS ANTENNA AREA, 5.5"L X 2.20"W X 0.008"D. IN LIMITS IAW ASAP EA# AWAC CRJ253-01583 REV IR DATED 3/8/2021. HFEC INSPECTION PERFORMED WITH NO IMar 5, 2021 · N405AW · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR A6WA202103087700Floorbeam · corrodedCORROSION COMMON TO PRESSURE FLOOR ANGLE AT FS461, RBL 42 ***AIRCRAFT REMOVED FROM SERVICE*** REMOVED CORROSION ON PRESSURE FLOOR ANGLE FS461, RBL 42, PERFORMED HFEC INSPECTION WITH NO INDICATIONS EVALUATED BLEND AND FOUND WITHIN LIMITS REF REO601R-53-41-66Mar 4, 2021 · N405AW · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR A6WA202103087693Skin · corrodedCORROSION COMMON TO PRESSURE FLOOR SILL AT FS439.00+2, RBL 42 ***AIRCRAFT REMOVED FROM SERVICE*** REMOVED CORROSION ON PRESSURE FLOOR SILL FS439.00+2, RBL 42, PERFORMED HFEC INSPECTION WITH NO INDICATIONS, PERFORMED UT THICKNESS CHECK, REMAINING MATERIAL WITMar 4, 2021 · N405AW · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR A6WA202103087703Floorbeam · corrodedCORROSION COMMON TO PRESSURE FLOOR ANGLE AT FS473.15+4.5, RBL 43 ***AIRCRAFT REMOVED FROM SERVICE*** REMOVED CORROSION ON PRESSURE FLOOR ANGLE FS473.15+4.5, RBL 43, PERFORMED HFEC INSPECTION WITH NO INDICATIONS. EVALUATED BLEND AND FOUND WITHIN LIMITS REF RMar 4, 2021 · N405AW · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR A6WA202103087699Floorbeam · corrodedCORROSION COMMON TO PRESSURE FLOOR ANGLE AT FS439.00+5, RBL 42 ***AIRCRAFT REMOVED FROM SERVICE*** REMOVED CORROSION ON PRESSURE FLOOR ANGLE FS439.00+5, RBL 42, PERFORMED HFEC INSPECTION WITH NO INDICATIONS EVALUATED BLEND AND FOUND WITHIN LIMITS REF REO601Mar 4, 2021 · N405AW · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR A6WA202103087702Floorbeam · corrodedCORROSION COMMON TO PRESSURE FLOOR ANGLE AT FS473.15+15, RBL 43 ***AIRCRAFT REMOVED FROM SERVICE*** REMOVED CORROSION ON PRESSURE FLOOR ANGLE FS473.15+15, RBL 43, PERFORMED HFEC INSPECTION WITH NO INDICATIONS. EVALUATED BLEND AND FOUND WITHIN LIMITS REF REOMar 4, 2021 · N405AW · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR A6WA202103087695Floorbeam · corrodedCORROSION COMMON TO PRESSURE FLOOR SILL AT FS499.00+10.5, LBL 43 ***AIRCRAFT REMOVED FROM SERVICE*** REMOVED CORROSION ON PRESSURE FLOOR ANGLE FS499.00+10.5, LBL 43, PERFORMED HFEC INSPECTION WITH NO INDICATIONS, PERFORMED UT THICKNESS CHECK, REMAINING MATERMar 4, 2021 · N405AW · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR A6WA202103087701Floorbeam · corrodedCORROSION COMMON TO PRESSURE FLOOR ANGLE AT FS461.00+7, RBL 42 ***AIRCRAFT REMOVED FROM SERVICE*** REMOVED CORROSION ON PRESSURE FLOOR ANGLE FS461.00+7, RBL 42, PERFORMED HFEC INSPECTION WITH NO INDICATIONS. EVALUATED BLEND AND FOUND WITHIN LIMITS REF REO60Mar 4, 2021 · N405AW · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR A6WA202103087694Floor Support · corrodedCORROSION COMMON TO PRESSURE FLOOR SILL AT FS 513.00+5.5, LBL 42 ***AIRCRAFT REMOVED FROM SERVICE*** REMOVED CORROSION ON PRESSURE FLOOR SILL FS 513.00+5.5, RBL 42, PERFORMED HFEC INSPECTION WITH NO INDICATIONS, PERFORMED UT THICKNESS CHECK, REMAINING MATERIMar 4, 2021 · N405AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA202103097707Skin · dentedOUTWARD DENT COMMON TO SKIN AT FS 625.3+5 TO 625.30+5.6, STR24L+4 TO STR ***AIRCRAFT REMOVED FROM SERVICE*** EVALUATED 2 OUTWARD DENTS: DENT 1) 0.200Ï¿½L X 0.200Ï¿½W X 0.004Ï¿½D. DENT 2) 0.500Ï¿½L X0.300Ï¿½W X 0.007Ï¿½D. FOUND TO BE WITHIN LIMITS PER SUPPLEMar 3, 2021 · N405AW · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR A6WA202103097709Skin · dented1 OUTWARD DENT COMMON TO SKIN AT FS672.20+6, STR 24R+ 2.5, 2 OUTWARD DENTS COMMON TO SKIN AT FS672.20+4.4 Ï¿½ FS672.20+6, STR 25R+1.8 - STR 25R+2.8. ***AIRCRAFT REMOVED FROM SERVICE*** ACCOMPLISHED FS REPAIR BETWEEN FS62.20 AND FS682.00, BETWEEN STR 24R AND Mar 3, 2021 · N405AW · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR A6WA202103087687Floorbeam · corrodedCORROSION COMMON TO PRESSURE FLOOR PANEL SILL NUTPLATE AT FS461.00+6, LBL 42 ***AIRCRAFT REMOVED FROM SERVICE*** REMOVED CORROSION FROM PRESSURE FLOOR PANEL SILL NUTPLATE AT FS461.00+6, LBL 42. HFEC INSPECTION PERFORMED WITH NO INDICATIONS NOTED. EVALUATED Mar 3, 2021 · N405AW · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR A6WA202103087681Skin · dentedOUTWARD DENT COMMON TO SKIN AT FS 625.30+17 TO STR22R+3.5 ***AIRCRAFT REMOVED FROM SERVICE*** EVALUATED OUTWARD DENT IN SKIN AT FS 625.30+17 AND STR 22R+3.5. HAND DRESSED DENT MEASURED 0.2"L X0.2"W X 0.004"D TO ORIGINAL CONTOUR REF ASAP EA # AWAC - CRJ253- Mar 3, 2021 · N405AW · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR A6WA202103087682Skin · dentedDENT IN FUSELAGE SKIN AT FRAME VS55.625% SPAR DATUM AND STR 10+1.5 ***AIRCRAFT REMOVED FROM SERVICE*** EVALUATED DENT AT FRAME VS 55.625% SPAR DATUM, DENT MEASURED .760"L X .420"W X .009"D. PERFORMED HAND DRESS ON FUSELAGE SKIN AT VS 55.625% BETWEEN STR1Mar 3, 2021 · N405AW · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR A6WA202103087686Floorbeam · corrodedCORROSION COMMON TO PRESSURE FLOOR ANGLE AT FS461.00+1, LBL 42 ***AIRCRAFT REMOVED FROM SERVICE*** REMOVED CORROSION ON PRESSURE FLOOR ANGLE AT FS 461.00+1, LBL 42, PERFORMED HFEC INSPECTION WITH NO INDICATIONS. PERFORMED UT THICKNESS CHECK AND FOUND TO BE Mar 3, 2021 · N405AW · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR A6WA202103087685Floorbeam · corrodedCORROSION COMMON TO FLOOR PANEL SILL AT FS 449.85+3, LBL 43. ***AIRCRAFT REMOVED FROM SERVICE*** REMOVED CORROSION FROM PRESSURE FLOOR PANEL SILL AT FS449.85+3, LBL 43. HFEC INSPECTION PERFORMED WITH NO INDICATIONS NOTED. EVALUATED BLEND AREA, FOUND TO BE Mar 3, 2021 · N405AW · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR A6WA202103087698Floorbeam · corrodedCORROSION COMMON TO PRESSURE FLOOR ANGLE AT FS544.00, LBL 42 ***AIRCRAFT REMOVED FROM SERVICE*** REMOVED CORROSION ON PRESSURE FLOOR ANGLE FS544.00, LBL 42, PERFORMED HFEC INSPECTION WITH NO INDICATIONS EVALUATED BLEND AND FOUND WITHIN LIMITS REF REO601R-53Mar 3, 2021 · N405AW · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR A6WA202103087690Floorbeam · corrodedCORROSION COMMON TO PRESSURE FLOOR PANEL SILL AT FS484.00+4, LBL 43 ***AIRCRAFT REMOVED FROM SERVICE*** REMOVED CORROSION FROM PRESSURE FLOOR PANEL SILL AT FS484.00+4, LBL 43. HFEC INSPECTION PERFORMED WITH NO INDICATIONS NOTED. EVALUATED BLEND AREA, REMAINMar 3, 2021 · N405AW · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR A6WA202103087704Skin · dentedINWARD DENT COMMON TO FS640.00+4 STR24+2.5 TO STR24+3.6. ***AIRCRAFT REMOVED FROM SERVICE*** PERFORMED EXTERNAL DOUBLER REPAIR FROM 0.063" 2024 T3 ON FUSELAGE SKIN AT FS 640.00+4 STR24+2.5 TO STR24+3 REF EA# AWAC - CRJ253-01577 REV IR DATED 3/6/2021.Mar 3, 2021 · N405AW · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR A6WA202103087691Floorbeam · corrodedCORROSION COMMON TO PRESSURE FLOOR ANGLE AT FS484.00+12, LBL 44 ***AIRCRAFT REMOVED FROM SERVICE*** REMOVED CORROSION ON PRESSURE FLOOR ANGLE AT FS 484.00+12, LBL 44, PERFORMED HFEC INSPECTION WITH NO INDICATIONS. PERFORMED UT THICKNESS CHECK AND FOUND TO BMar 3, 2021 · N405AW · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR A6WA202103087683Floorbeam · corrodedCORROSION COMMON TO PRESSURE FLOOR ANGLE AT FS424.00+2.5, LBL 36. ***AIRCRAFT REMOVED FROM SERVICE*** REMOVED CORROSION COMMON TO PRESSURE FLOOR ANGLE AT FS 424.00+2.5, LBL 36 HFEC INSPECTION PERFORMED WITH NO INDICATION. EVALUATION OF BLEND AREA FOUND TO BMar 3, 2021 · N405AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA202103087697Floor Support · corrodedCORROSION COMMON TO PRESSURE FLOOR SILL AT FS 529.00+9.5 TO FS529.00+11, LBL 42 ***AIRCRAFT REMOVED FROM SERVICE*** REMOVED CORROSION ON PRESSURE FLOOR ANGLE FS529.00+9.5 TO FS529.00+11, LBL 42, PERFORMED HFEC INSPECTION WITH NO INDICATIONS, PERFORMED UT THMar 3, 2021 · N405AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA202103087689Floor Support · corrodedCORROSION COMMON TO PRESSURE FLOOR PANEL SILL AT FS473.15+5, LBL 42 ***AIRCRAFT REMOVED FROM SERVICE*** REMOVED CORROSION FROM PRESSURE FLOOR PANEL SILL AT FS473.15+5, LBL 42. HFEC INSPECTION PERFORMED WITH NO INDICATIONS NOTED. EVALUATED BLEND AREA, REMAINMar 3, 2021 · N405AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA202103087692Floor Support · corrodedCORROSION COMMON TO PRESSURE FLOOR SILL AT NUTPLATE FS 513.00+9, RBL 42 ***AIRCRAFT REMOVED FROM SERVICE*** REMOVED CORROSION ON PRESSURE FLOOR SILL FS 513.00+9, RBL 42, PERFORMED HFEC INSPECTION WITH NO INDICATIONS, PERFORMED UT THICKNESS CHECK, REMAINING MMar 3, 2021 · N405AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA202103087705Floorbeam · corrodedCORROSION COMMON TO PRESSURE FLOOR ANGLE AT FS449.85+.5 LBL43. ***AIRCRAFT REMOVED FROM SERVICE*** REMOVED CORROSION ON PRESSURE FLOOR ANGLE AT FS449.85+.5, LBL43. PERFORMED HFEC WITH NO INDICATION. PERFORMED UT THICKNESS CHECK, FOUND TO BE WITH IN LIMITS REMar 3, 2021 · N405AW · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR A6WA202103087688Floorbeam · corrodedCORROSION COMMON TO PRESSURE FLOOR ANGLE AT FS473.15+4.5, LBL 42 ***AIRCRAFT REMOVED FROM SERVICE*** REMOVED CORROSION ON PRESSURE FLOOR ANGLE AT FS 473.15+4.5, LBL 42, PERFORMED HFEC INSPECTION WITH NO INDICATIONS. PERFORMED UT THICKNESS CHECK AND FOUND TOMar 3, 2021 · N405AW · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR A6WA202103087706Skin · dentedINWARD DENT COMMON TO SKIN AT FS718.00+14 TO FS718.00+16 STR16+1 AT FWD END TO STR16+.5 AT AFT END OF DENT. ***AIRCRAFT REMOVED FROM SERVICE*** HAND PASSED DENT COMMON TO SKIN AT FS 718.00+14 TO FS718.00+16, STR16+1 AT FWD END TO STR16+.5, REF EA# AWAC - CRMar 3, 2021 · N405AW · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR A6WA202103087684Floorbeam · corrodedCORROSION COMMON TO PRESSURE FLOOR ANGLE AT FS439.00+8, LBL44 ***AIRCRAFT REMOVED FROM SERVICE*** REMOVED CORROSION COMMON TO PRESSURE FLOOR ANGLE AT FS439.00+8 LBL 44. HFEC INSPECTION PERFORMED WITH NO INDICATIONS NOTED. EVALUATED BLEND AREA AND FOUND TO BMar 3, 2021 · N405AW · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR A6WA202103087696Floorbeam · corrodedCORROSION COMMON TO PRESSURE FLOOR SILL AT FS 513.00, LBL 42 ***AIRCRAFT REMOVED FROM SERVICE*** REMOVED CORROSION ON PRESSURE FLOOR ANGLE FS 513.00, LBL 42, PERFORMED HFEC INSPECTION WITH NO INDICATIONS, PERFORMED UT THICKNESS CHECK, REMAINING MATERIAL WITHMar 3, 2021 · N405AW · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR A6WA2019071246696Shutoff Valve · malfunctionedON DEPARTURE OUT OF ATW WITH ONE PACK ON MEL THE OTHER PACK INDICATED OVERPRESSURE. THE CAPTAIN OPTED TO RETURN TO ATW. RECORDED LOGBOOK DISCREPANCY: WHEN TRANSFERRING BLEEDS, APU SELECTED RIGHT 10TH STAGE BLEEDS REMAINED CLOSED, RIGHT PACK HI PRESSURE C/W QRJul 11, 2019 · N405AW · Cndair CL6002B19 · Cabin Cooling SystemSDR A6WA2019062146675Flap System · malfunctionedFLAP FAIL AT ZERO AT 8000FT ON ARRIVAL AFTER SELECTING FLAPS 8. PERFORMED RESET PER AWA SUP 98-018G. FLAPS FAILED AGAIN WHEN RETRACTING FROM 45 TO 30.Jun 20, 2019 · N405AW · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR A6WA2019030846458Intercostal · crackedAEB STR 13L INTERCOSTAL CRACKED. REPLACED.Mar 6, 2019 · N405AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA2019030546453Door Frame · crackedCARGO DOOR FWD SURROUND FRAME IS CRACKED IN THE RADIUS JUST BELOW THE FWD STOP UPPER FITTING. REPAIRED CARGO DOOR FWD SURROUND FRAME AT THE FWD UPER STOP FITTING IAW EA AWAC-CRJ252-01137 REV IR.Feb 22, 2019 · N405AW · Cndair CL6002B19 · Fuselage Main, StructureSDR A6WA2019012946343Fitting · damagedLEFT WING TRAILING EDGE FLAP ALIGNMENT FITTING DAMAGED. REPLACED FITTING IAW SUPP. 16-056.Jan 21, 2019 · N405AW · Cndair CL6002B19 · Trailing Edge FlapsSDR A6WA2019012146313Door Sill · corrodedRIGHT FLOOR SILL CORRODED FROM FS 559.00+48 TO 559.00+80. REPAIRED RIGHT FLOOR SILL IAW REO601R-53-00-526 REV-- AND EA 253-01141.Jan 19, 2019 · N405AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA2019012146312Door Frame · crackedCARGO DOOR PAN (FRAME) IS CRACKED. REPAIRED CARGO DOOR PAN IAW EA AWAC-CRJ253-01145 REV-IR .Jan 19, 2019 · N405AW · Cndair CL6002B19 · Cargo/Baggage DoorsSDR A6WA2019012146317Angle · corrodedPAX DOOR LOWER SILL ANGLE CORRODED. REPLACED PAX DOOR LOWER SILL ANGLE IAW SRM 51-42-02.Jan 19, 2019 · N405AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA2019011846306Stringer · crackedFUSELAGE SKIN CRACKED, FS 235.00, STR 26R. REPAIRED SKIN IAW REO 601R-53-11-048 REV-D.Jan 17, 2019 · N405AW · Cndair CL6002B19 · Fuselage Main, Longeron/StringerSDR A6WA2019011846298Rib · corrodedLEFT WING LEADING EDGE O/B, RIB CORRODED. REPLACED RIB IAW SRM 51-42-10, 51-42-06.Jan 17, 2019 · N405AW · Cndair CL6002B19 · Wing, Rib/BulkheadSDR A6WA2019011846305Fitting · crackedCARGO DOOR FWD LOWER DOOR STOP BACKUP FITTING CRACKED. REPLACED FITTING IAW SRM 51-42-06, 51-42-21.Jan 16, 2019 · N405AW · Cndair CL6002B19 · Fuselage Main, StructureSDR A6WA201946301Floorbeam · corrodedFLOORBEAM CAP CORRODED, FS569.00-621.00, LBL9. REPLACED CAP IAW REO 601R-53-61-3780 REV-A.Jan 16, 2019 · N405AW · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR A6WA2019011846299Floorbeam · corrodedFLOORBEAM CAP CORRODED AT FS569.00 TO 621.00, LBL27. REPLACED CAP IAW SRM 51-42-06, 51-42-21, 51-42-22, REO 601R-53-00-005 REV-B.Jan 15, 2019 · N405AW · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR A6WA2019011846302Web · crackedE&E BAY FLOOR WEB CRACKED, FS 193.00, LBL30. REPAIRED CRACK IAW REO 601R-53-11-111.Jan 15, 2019 · N405AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA2019011846300Angle · corroded280 BEAM AFT ANGLE CORRODED BETWEEN LBL12 AND RBL12. REPAIRED ANGLE IAW REO 601R-53-11-926 REV-D.Jan 14, 2019 · N405AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA201946303Floor Support · crackedFS 621.00 FLOOR SUPPORT ANGLE AT LBL43 IS CRACKED. REPAIRED FS 621.00, LBL43 ANGLE IAW REO 601R-53-61-117 REV-E.Jan 14, 2019 · N405AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA2019011846304Fitting · crackedNLG WHEEL WELL GS 202.00 BULKHEAD RBL 9 VERTICAL POST O/B CLIP IS CRACKED. REPLACED CLIP IAW SRM 51-42-06.Jan 13, 2019 · N405AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA2019011546291Floorbeam · corrodedFS 559+80, RBL9 O/B FLOORBEAM CAP CORRODED. REPLACED BEAM CAP IAW REO 601R-53-00-005 REV-B.Jan 11, 2019 · N405AW · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR A6WA2019011046284Angle · crackedAEB STR 14R OBLIQUE ANGLE CRACKED. REPLACED ANGLE IAW SRM 51-42-21.Jan 9, 2019 · N405AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA2019011046285Fitting · crackedFS589, LBL45 CLIP UNDER CARGO DOOR FLOOR SILL IS CRACKED. REPLACED CLIP IAW SRM 51-42-06, 51-42-21.Jan 9, 2019 · N405AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
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