# Service difficulty reports: N405AW

A list on [N405AW](https://openairdocs.org/aircraft/N405AW.md).

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

Page 1 of 4 · 198 reports

- [SDR A6WA202103107711](https://openairdocs.org/sdr/A6WA202103107711.md): Strap · damaged · Mar 7, 2021 · N405AW · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > FORWARD 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 SE
- [SDR A6WA202103097708](https://openairdocs.org/sdr/A6WA202103097708.md): Skin · corroded · Mar 5, 2021 · N405AW · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > CORROSION 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 I
- [SDR A6WA202103087700](https://openairdocs.org/sdr/A6WA202103087700.md): Floorbeam · corroded · Mar 4, 2021 · N405AW · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > CORROSION 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-53-41-66
- [SDR A6WA202103087693](https://openairdocs.org/sdr/A6WA202103087693.md): Skin · corroded · Mar 4, 2021 · N405AW · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > CORROSION 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 WIT
- [SDR A6WA202103087703](https://openairdocs.org/sdr/A6WA202103087703.md): Floorbeam · corroded · Mar 4, 2021 · N405AW · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > CORROSION 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 R
- [SDR A6WA202103087699](https://openairdocs.org/sdr/A6WA202103087699.md): Floorbeam · corroded · Mar 4, 2021 · N405AW · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > CORROSION 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 REO601
- [SDR A6WA202103087702](https://openairdocs.org/sdr/A6WA202103087702.md): Floorbeam · corroded · Mar 4, 2021 · N405AW · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > CORROSION 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 REO
- [SDR A6WA202103087695](https://openairdocs.org/sdr/A6WA202103087695.md): Floorbeam · corroded · Mar 4, 2021 · N405AW · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > CORROSION 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 MATER
- [SDR A6WA202103087701](https://openairdocs.org/sdr/A6WA202103087701.md): Floorbeam · corroded · Mar 4, 2021 · N405AW · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > CORROSION 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 REO60
- [SDR A6WA202103087694](https://openairdocs.org/sdr/A6WA202103087694.md): Floor Support · corroded · Mar 4, 2021 · N405AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > CORROSION 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 MATERI
- [SDR A6WA202103097707](https://openairdocs.org/sdr/A6WA202103097707.md): Skin · dented · Mar 3, 2021 · N405AW · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > OUTWARD 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 SUPPLE
- [SDR A6WA202103097709](https://openairdocs.org/sdr/A6WA202103097709.md): Skin · dented · Mar 3, 2021 · N405AW · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > 1 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
- [SDR A6WA202103087687](https://openairdocs.org/sdr/A6WA202103087687.md): Floorbeam · corroded · Mar 3, 2021 · N405AW · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > CORROSION 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
- [SDR A6WA202103087681](https://openairdocs.org/sdr/A6WA202103087681.md): Skin · dented · Mar 3, 2021 · N405AW · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > OUTWARD 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-
- [SDR A6WA202103087682](https://openairdocs.org/sdr/A6WA202103087682.md): Skin · dented · Mar 3, 2021 · N405AW · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > DENT 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 STR1
- [SDR A6WA202103087686](https://openairdocs.org/sdr/A6WA202103087686.md): Floorbeam · corroded · Mar 3, 2021 · N405AW · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > CORROSION 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
- [SDR A6WA202103087685](https://openairdocs.org/sdr/A6WA202103087685.md): Floorbeam · corroded · Mar 3, 2021 · N405AW · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > CORROSION 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
- [SDR A6WA202103087698](https://openairdocs.org/sdr/A6WA202103087698.md): Floorbeam · corroded · Mar 3, 2021 · N405AW · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > CORROSION 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-53
- [SDR A6WA202103087690](https://openairdocs.org/sdr/A6WA202103087690.md): Floorbeam · corroded · Mar 3, 2021 · N405AW · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > CORROSION 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, REMAIN
- [SDR A6WA202103087704](https://openairdocs.org/sdr/A6WA202103087704.md): Skin · dented · Mar 3, 2021 · N405AW · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > INWARD 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.
- [SDR A6WA202103087691](https://openairdocs.org/sdr/A6WA202103087691.md): Floorbeam · corroded · Mar 3, 2021 · N405AW · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > CORROSION 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 B
- [SDR A6WA202103087683](https://openairdocs.org/sdr/A6WA202103087683.md): Floorbeam · corroded · Mar 3, 2021 · N405AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > CORROSION 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 B
- [SDR A6WA202103087697](https://openairdocs.org/sdr/A6WA202103087697.md): Floor Support · corroded · Mar 3, 2021 · N405AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > CORROSION 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 TH
- [SDR A6WA202103087689](https://openairdocs.org/sdr/A6WA202103087689.md): Floor Support · corroded · Mar 3, 2021 · N405AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > CORROSION 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, REMAIN
- [SDR A6WA202103087692](https://openairdocs.org/sdr/A6WA202103087692.md): Floor Support · corroded · Mar 3, 2021 · N405AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > CORROSION 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 M
- [SDR A6WA202103087705](https://openairdocs.org/sdr/A6WA202103087705.md): Floorbeam · corroded · Mar 3, 2021 · N405AW · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > CORROSION 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 RE
- [SDR A6WA202103087688](https://openairdocs.org/sdr/A6WA202103087688.md): Floorbeam · corroded · Mar 3, 2021 · N405AW · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > CORROSION 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 TO
- [SDR A6WA202103087706](https://openairdocs.org/sdr/A6WA202103087706.md): Skin · dented · Mar 3, 2021 · N405AW · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > INWARD 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 - CR
- [SDR A6WA202103087684](https://openairdocs.org/sdr/A6WA202103087684.md): Floorbeam · corroded · Mar 3, 2021 · N405AW · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > CORROSION 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 B
- [SDR A6WA202103087696](https://openairdocs.org/sdr/A6WA202103087696.md): Floorbeam · corroded · Mar 3, 2021 · N405AW · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > CORROSION 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 WITH
- [SDR A6WA2019071246696](https://openairdocs.org/sdr/A6WA2019071246696.md): Shutoff Valve · malfunctioned · Jul 11, 2019 · N405AW · Cndair CL6002B19 · Cabin Cooling System
  > ON 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 QR
- [SDR A6WA2019062146675](https://openairdocs.org/sdr/A6WA2019062146675.md): Flap System · malfunctioned · Jun 20, 2019 · N405AW · Cndair CL6002B19 · Trailing Edge Flap Control System
  > FLAP 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.
- [SDR A6WA2019030846458](https://openairdocs.org/sdr/A6WA2019030846458.md): Intercostal · cracked · Mar 6, 2019 · N405AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > AEB STR 13L INTERCOSTAL CRACKED. REPLACED.
- [SDR A6WA2019030546453](https://openairdocs.org/sdr/A6WA2019030546453.md): Door Frame · cracked · Feb 22, 2019 · N405AW · Cndair CL6002B19 · Fuselage Main, Structure
  > CARGO 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.
- [SDR A6WA2019012946343](https://openairdocs.org/sdr/A6WA2019012946343.md): Fitting · damaged · Jan 21, 2019 · N405AW · Cndair CL6002B19 · Trailing Edge Flaps
  > LEFT WING TRAILING EDGE FLAP ALIGNMENT FITTING DAMAGED. REPLACED FITTING IAW SUPP. 16-056.
- [SDR A6WA2019012146313](https://openairdocs.org/sdr/A6WA2019012146313.md): Door Sill · corroded · Jan 19, 2019 · N405AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > RIGHT 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.
- [SDR A6WA2019012146312](https://openairdocs.org/sdr/A6WA2019012146312.md): Door Frame · cracked · Jan 19, 2019 · N405AW · Cndair CL6002B19 · Cargo/Baggage Doors
  > CARGO DOOR PAN (FRAME) IS CRACKED. REPAIRED CARGO DOOR PAN IAW EA AWAC-CRJ253-01145 REV-IR.
- [SDR A6WA2019012146317](https://openairdocs.org/sdr/A6WA2019012146317.md): Angle · corroded · Jan 19, 2019 · N405AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > PAX DOOR LOWER SILL ANGLE CORRODED. REPLACED PAX DOOR LOWER SILL ANGLE IAW SRM 51-42-02.
- [SDR A6WA2019011846306](https://openairdocs.org/sdr/A6WA2019011846306.md): Stringer · cracked · Jan 17, 2019 · N405AW · Cndair CL6002B19 · Fuselage Main, Longeron/Stringer
  > FUSELAGE SKIN CRACKED, FS 235.00, STR 26R. REPAIRED SKIN IAW REO 601R-53-11-048 REV-D.
- [SDR A6WA2019011846298](https://openairdocs.org/sdr/A6WA2019011846298.md): Rib · corroded · Jan 17, 2019 · N405AW · Cndair CL6002B19 · Wing, Rib/Bulkhead
  > LEFT WING LEADING EDGE O/B, RIB CORRODED. REPLACED RIB IAW SRM 51-42-10, 51-42-06.
- [SDR A6WA2019011846305](https://openairdocs.org/sdr/A6WA2019011846305.md): Fitting · cracked · Jan 16, 2019 · N405AW · Cndair CL6002B19 · Fuselage Main, Structure
  > CARGO DOOR FWD LOWER DOOR STOP BACKUP FITTING CRACKED. REPLACED FITTING IAW SRM 51-42-06, 51-42-21.
- [SDR A6WA201946301](https://openairdocs.org/sdr/A6WA201946301.md): Floorbeam · corroded · Jan 16, 2019 · N405AW · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > FLOORBEAM CAP CORRODED, FS569.00-621.00, LBL9. REPLACED CAP IAW REO 601R-53-61-3780 REV-A.
- [SDR A6WA2019011846299](https://openairdocs.org/sdr/A6WA2019011846299.md): Floorbeam · corroded · Jan 15, 2019 · N405AW · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > FLOORBEAM 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.
- [SDR A6WA2019011846302](https://openairdocs.org/sdr/A6WA2019011846302.md): Web · cracked · Jan 15, 2019 · N405AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > E&E BAY FLOOR WEB CRACKED, FS 193.00, LBL30. REPAIRED CRACK IAW REO 601R-53-11-111.
- [SDR A6WA2019011846300](https://openairdocs.org/sdr/A6WA2019011846300.md): Angle · corroded · Jan 14, 2019 · N405AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > 280 BEAM AFT ANGLE CORRODED BETWEEN LBL12 AND RBL12. REPAIRED ANGLE IAW REO 601R-53-11-926 REV-D.
- [SDR A6WA201946303](https://openairdocs.org/sdr/A6WA201946303.md): Floor Support · cracked · Jan 14, 2019 · N405AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FS 621.00 FLOOR SUPPORT ANGLE AT LBL43 IS CRACKED. REPAIRED FS 621.00, LBL43 ANGLE IAW REO 601R-53-61-117 REV-E.
- [SDR A6WA2019011846304](https://openairdocs.org/sdr/A6WA2019011846304.md): Fitting · cracked · Jan 13, 2019 · N405AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > NLG WHEEL WELL GS 202.00 BULKHEAD RBL 9 VERTICAL POST O/B CLIP IS CRACKED. REPLACED CLIP IAW SRM 51-42-06.
- [SDR A6WA2019011546291](https://openairdocs.org/sdr/A6WA2019011546291.md): Floorbeam · corroded · Jan 11, 2019 · N405AW · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > FS 559+80, RBL9 O/B FLOORBEAM CAP CORRODED. REPLACED BEAM CAP IAW REO 601R-53-00-005 REV-B.
- [SDR A6WA2019011046284](https://openairdocs.org/sdr/A6WA2019011046284.md): Angle · cracked · Jan 9, 2019 · N405AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > AEB STR 14R OBLIQUE ANGLE CRACKED. REPLACED ANGLE IAW SRM 51-42-21.
- [SDR A6WA2019011046285](https://openairdocs.org/sdr/A6WA2019011046285.md): Fitting · cracked · Jan 9, 2019 · N405AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FS589, LBL45 CLIP UNDER CARGO DOOR FLOOR SILL IS CRACKED. REPLACED CLIP IAW SRM 51-42-06, 51-42-21.

Next page: https://openairdocs.org/aircraft/N405AW/reports.md?page=2

## The whole list in SQL

Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS:

```sql
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
```

This list as a web page: https://openairdocs.org/aircraft/N405AW/reports

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