# Service difficulty reports: N463AW

A list on [N463AW](https://openairdocs.org/aircraft/N463AW.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 · 190 reports

- [SDR A6WA202605268889](https://openairdocs.org/sdr/A6WA202605268889.md): Drive Assy · failed · May 26, 2026 · N463AW · Cndair CL6002B19 · Trailing Edge Flap Control System
  > FLAPS 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
- [SDR A6WA202602208881](https://openairdocs.org/sdr/A6WA202602208881.md): Door · binding · Feb 20, 2026 · N463AW · Cndair CL6002B19 · Emergency Exits
  > LEFT 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 ACT
- [SDR A6WA202309198653](https://openairdocs.org/sdr/A6WA202309198653.md): Unknown · unknown · Sep 19, 2023 · N463AW · Cndair CL6002B19 · Landing Gear Retraction/Extension System
  > GEAR 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
- [SDR A6WA202308148647](https://openairdocs.org/sdr/A6WA202308148647.md): Wire Harness · unknown · Aug 14, 2023 · N463AW · Cndair CL6002B19 · Landing Gear System Wiring
  > AFTER 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
- [SDR A6WA202308068645](https://openairdocs.org/sdr/A6WA202308068645.md): Unknown · unknown · Aug 6, 2023 · N463AW · Cndair CL6002B19 · Main Landing Gear
  > RECEIVED 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 S
- [SDR A6WA202306298632](https://openairdocs.org/sdr/A6WA202306298632.md): Unknown · unknown · Jun 29, 2023 · N463AW · Cndair CL6002B19 · Cabin Cooling System
  > ON 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 SENSO
- [SDR A6WA202305178609](https://openairdocs.org/sdr/A6WA202305178609.md): Unknown · unknown · May 17, 2023 · N463AW · Cndair CL6002B19 · Nose/Tail Landing Gear
  > ON-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 T
- [SDR A6WA202212058464](https://openairdocs.org/sdr/A6WA202212058464.md): Doubler · none · Dec 5, 2022 · N463AW · Cndair CL6002B19 · Fuselage Structure (General)
  > DURING 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********
- [SDR A6WA202212058462](https://openairdocs.org/sdr/A6WA202212058462.md): Skin · chafed · Dec 5, 2022 · N463AW · Cndair CL6002B19 · Fuselage Structure (General)
  > WEAR 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 L
- [SDR A6WA202212058459](https://openairdocs.org/sdr/A6WA202212058459.md): Skin · dented · Dec 5, 2022 · N463AW · Cndair CL6002B19 · Fuselage Floor Panel
  > TWO 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 THICKNES
- [SDR A6WA202212058457](https://openairdocs.org/sdr/A6WA202212058457.md): Skin · dented · Dec 5, 2022 · N463AW · Cndair CL6002B19 · Fuselage Floor Panel
  > THREE 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 = 0
- [SDR A6WA202212058458](https://openairdocs.org/sdr/A6WA202212058458.md): Skin · dented · Dec 5, 2022 · N463AW · Cndair CL6002B19 · Fuselage Floor Panel
  > ONE 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****** VERIFIED
- [SDR A6WA202212058456](https://openairdocs.org/sdr/A6WA202212058456.md): Doubler · dented · Dec 5, 2022 · N463AW · Cndair CL6002B19 · Fuselage Floor Panel
  > DENT 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 DOU
- [SDR A6WA202212058453](https://openairdocs.org/sdr/A6WA202212058453.md): Seat Track · corroded · Dec 5, 2022 · N463AW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION 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. SE
- [SDR A6WA2023013058452](https://openairdocs.org/sdr/A6WA2023013058452.md): Drag Angle · cracked · Dec 5, 2022 · N463AW · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX 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 FINISH
- [SDR A6WA202207308300](https://openairdocs.org/sdr/A6WA202207308300.md): None · none · Aug 25, 2022 · N463AW · Cndair CL2151A10 · Landing Gear System
  > NOSE 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, ONL
- [SDR A6WA202203318157](https://openairdocs.org/sdr/A6WA202203318157.md): None · none · Mar 31, 2022 · N463AW · Cndair CL6002B19 · Trailing Flap Position Indicating System
  > ****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
- [SDR A6WA202112178028](https://openairdocs.org/sdr/A6WA202112178028.md): Flap System · faulted · Dec 17, 2021 · N463AW · Cndair CL6002B19 · Trailing Edge Flap Control System
  > RECEIVED 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 & FLA
- [SDR A6WA202110247930](https://openairdocs.org/sdr/A6WA202110247930.md): None · none · Oct 24, 2021 · N463AW · Cndair CL6002B19 · Window/Windshield System
  > FO'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:
- [SDR A6WA202107297841](https://openairdocs.org/sdr/A6WA202107297841.md): Seal · lack of lube · Jul 28, 2021 · N463AW · Cndair CL6002B19 · Passenger/Crew Doors
  > AFTER 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 FRO
- [SDR A6WA2019090546840](https://openairdocs.org/sdr/A6WA2019090546840.md): Support Bracket · cracked · Sep 4, 2019 · N463AW · Cndair CL6002B19 · Fuselage Main, Attach Fittings
  > RT HYDRAULIC MANIFOLD SUPPORT BRACKET AFT LOWER CORNER CRACKED. REMOVED AND REPLACED RT HYDRAULIC MANIFOLD SUPPORT BRACKET IAW REO 601R 53-62-031 REV A.
- [SDR A6WA2019090546839](https://openairdocs.org/sdr/A6WA2019090546839.md): Seat Track · corroded · Sep 4, 2019 · N463AW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > FLOOR SEAT TRACK #4 ON RBL9 HAS CORROSION. REMOVED AND REPLACED FLOOR SEAT TRACK #4 RBL 9 IAW SUPPLEMENT 19-254.
- [SDR A6WA2019090546841](https://openairdocs.org/sdr/A6WA2019090546841.md): Skin · chafed · Sep 4, 2019 · N463AW · Cndair CL6002B19 · Ailerons
  > BOTTOM 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.
- [SDR A6WA2019090546838](https://openairdocs.org/sdr/A6WA2019090546838.md): Skin · corroded · Sep 3, 2019 · N463AW · Cndair CL6002B19 · Wing, Plate/Skin
  > FUEL ACCESS CUTOUT 510AB SHOWS SIGNS OF FRETTING. REPAIRED FUEL ACCESS CUTOUT 510AB IAW EA# AWAC-CRJ257-01318 REVA.
- [SDR A6WA2019090546832](https://openairdocs.org/sdr/A6WA2019090546832.md): Intercostal · cracked · Sep 3, 2019 · N463AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > INTERCOSTAL 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.
- [SDR A6WA2019090546835](https://openairdocs.org/sdr/A6WA2019090546835.md): Intercostal · corroded · Sep 3, 2019 · N463AW · Cndair CL6002B19 · Passenger/Crew Doors
  > EVIDENCE 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.
- [SDR A6WA2019090546836](https://openairdocs.org/sdr/A6WA2019090546836.md): Post · cracked · Sep 3, 2019 · N463AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > 409+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.
- [SDR A6WA2019090546833](https://openairdocs.org/sdr/A6WA2019090546833.md): Door Sill · corroded · Sep 3, 2019 · N463AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > RT 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.
- [SDR A6WA2019090546831](https://openairdocs.org/sdr/A6WA2019090546831.md): Support Beam · gouged · Sep 1, 2019 · N463AW · Cndair CL6002B19 · Fuselage Main, Attach Fittings
  > PERFORM PERMANENT REPAIR FOR CARGO BAY DOOR TRACK SUPPORT BEAM. REPLACED CARGO DOOR SUPPORT BEAM IAW SRM 51-42-20. THIS COMPLIES WITH DMI 22614.
- [SDR A6WA2019090446830](https://openairdocs.org/sdr/A6WA2019090446830.md): Bracket · cracked · Sep 1, 2019 · N463AW · Cndair CL6002B19 · Fuselage Main, Attach Fittings
  > AFTER 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.
- [SDR A6WA2019090546834](https://openairdocs.org/sdr/A6WA2019090546834.md): Skin · chafed · Aug 31, 2019 · N463AW · Cndair CL6002B19 · Trailing Edge Flaps
  > RIGHT INBOARD FLAP VANE, INBOARD SKIN HAS CHAFING. REPLACED RIGHT I/B FLAP VANE I/B LEADING EDGE IAW SRM 51-42-13.
- [SDR A6WA2019090446828](https://openairdocs.org/sdr/A6WA2019090446828.md): Skin · cracked · Aug 31, 2019 · N463AW · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR INNER SKIN CRACKED AT DOOR DATUM 6, FS335. REPAIRED PAX DOOR INNER SKIN IAW SUPP. 19-248.
- [SDR A6WA2019090446829](https://openairdocs.org/sdr/A6WA2019090446829.md): Seat Track · corroded · Aug 30, 2019 · N463AW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > RIGHT FLOOR SEAT TRACK #5 CORRODED. REPLACED SEAT TRACK #5 IAW AMM 53-01-11.
- [SDR A6WA2019090446827](https://openairdocs.org/sdr/A6WA2019090446827.md): Seat Track · corroded · Aug 30, 2019 · N463AW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > RIGHT FLOOR SEAT TRACK #3 CORRODED. REPLACED SEAT TRACK IAW AMM 53-01-11.
- [SDR A6WA2019090446826](https://openairdocs.org/sdr/A6WA2019090446826.md): Fitting · cracked · Aug 29, 2019 · N463AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FS 202.75 IN NLG WHEEL WELL RBL9 POST UPPER CLIP IS CRACKED. REPLACED CLIP IAW SRM 51-42-06.
- [SDR A6WA2019083046817](https://openairdocs.org/sdr/A6WA2019083046817.md): Bracket · cracked · Aug 29, 2019 · N463AW · Cndair CL6002B19 · Fuselage Main, Attach Fittings
  > FS469.00, RBL 45 FAIRING ATTACH BRACKET IS CRACKED. REMOVED AND REPLACED FS469.00, RBL 45 FAIRING ATTACH BRACKET IAW SRM 51-42-06.
- [SDR A6WA2019083046812](https://openairdocs.org/sdr/A6WA2019083046812.md): Threshold · corroded · Aug 29, 2019 · N463AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > SERVICE DOOR LOWER SILL THRESHOLD CORRODED. REPLACED SERVICE DOOR LOWER SILL THRESHOLD IAW CRJ200 SRM TR 51-42.
- [SDR A6WA2019083046819](https://openairdocs.org/sdr/A6WA2019083046819.md): Bracket · cracked · Aug 29, 2019 · N463AW · Cndair CL6002B19 · Fuselage Main, Attach Fittings
  > FS449.00,LBL 45 FAIRING ATTACH BRACKET CRACKED. REPLACED BRACKET IAW SRM 51-42-06.
- [SDR A6WA2019083046818](https://openairdocs.org/sdr/A6WA2019083046818.md): Bracket · cracked · Aug 29, 2019 · N463AW · Cndair CL6002B19 · Fuselage Main, Attach Fittings
  > FS461.00, RBL45 FAIRING ATTACH BRACKET CRACKED. REPLACED BRACKET IAW SRM 51-42-06.
- [SDR A6WA2019083046821](https://openairdocs.org/sdr/A6WA2019083046821.md): Bracket · cracked · Aug 29, 2019 · N463AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > RIGHT MLG BAY VOLUMETRIC FUSE BRACKET, LINE BRACKET CRACKED. REPLACED BRACKET IAW SRM 51-42-06.
- [SDR A6WA2019083046820](https://openairdocs.org/sdr/A6WA2019083046820.md): Bracket · cracked · Aug 29, 2019 · N463AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FS469.00, LBL45 FAIRING SUPPORT ATTACH BRACKET CRACKED. REPLACED BRACKET IAW CRJ 200 SRM 51-42-06.
- [SDR A6WA2019083046815](https://openairdocs.org/sdr/A6WA2019083046815.md): Intercostal · cracked · Aug 28, 2019 · N463AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > INTERCOSTAL ON AFT SIDE OF 621 BULKHEAD AT STR 15L IS CRACKED. REPLACED INTERCOSTAL IAW SRM 51-42-06, 51-42-21.
- [SDR A6WA2019083046816](https://openairdocs.org/sdr/A6WA2019083046816.md): Intercostal · cracked · Aug 28, 2019 · N463AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > INTERCOSTAL AT FS621.00 STR 16L IS CRACKED ON AFT SIDE OF BULKHEAD. REPLACED INTERCOSTAL IAW CRJ 200 SRM 51-42-06, 51-42-21.
- [SDR A6WA2019083046813](https://openairdocs.org/sdr/A6WA2019083046813.md): Skin · cracked · Aug 28, 2019 · N463AW · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > FS235.00, STR 26L NLG CUT OUT IS CRACKED. REPAIRED NLG CUT OUT IAW REO 601R-53-11-101 REV-E.
- [SDR A6WA2019082846808](https://openairdocs.org/sdr/A6WA2019082846808.md): Skin · cracked · Aug 27, 2019 · N463AW · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > FS 235 STR 26R NLG CUTOUT HAS A CRACK INDICATION REPAIR ACCOMPLISHED ON AAR N/R WO 1017605 1000/0005
- [SDR A6WA2019082746807](https://openairdocs.org/sdr/A6WA2019082746807.md): Cargo Track · corroded · Aug 25, 2019 · N463AW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > CARGO 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.
- [SDR A6WA2019082746804](https://openairdocs.org/sdr/A6WA2019082746804.md): Web · cracked · Aug 24, 2019 · N463AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FS 193,LBL30 TRU WEB IS CRACKED. REPAIRED WEB IAW REO 601R-53-11-111 REV-NC.
- [SDR A6WA2019082746806](https://openairdocs.org/sdr/A6WA2019082746806.md): Seat Track · corroded · Aug 24, 2019 · N463AW · Cndair CL6002B19 · Fuselage, Door Hinge
  > LEFT 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.
- [SDR A6WA2019802746800](https://openairdocs.org/sdr/A6WA2019802746800.md): Vertical Support · cracked · Aug 22, 2019 · N463AW · Cndair CL6002B19 · Fuselage Main, Structure
  > 409+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.
- [SDR A6WA2019082746799](https://openairdocs.org/sdr/A6WA2019082746799.md): Angle · cracked · Aug 21, 2019 · N463AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FS 484, LBL36 I/B CLIP CRACKED. REPLACED CLIP IAW REO 601R-53-41-059 REV-B.

Next page: https://openairdocs.org/aircraft/N463AW/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 = 'N463AW' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N463AW/reports

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