# Service difficulty reports: N424AW

A list on [N424AW](https://openairdocs.org/aircraft/N424AW.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 · 156 reports

- [SDR A6WA202107227839](https://openairdocs.org/sdr/A6WA202107227839.md): Seat Track · corroded · Jul 22, 2021 · N424AW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > FOUND CORROSION ON SEAT TRACKS AT RBL 27 AND 9, AND LBL 9 FS559+84 TO 559+92 ***AIRCRAFT REMOVED FROM SERVICE*** R&R SEAT TRACKS AT RBL 27 AND 9, AND LBL 9 FS 559+84 TO FS 559+92
- [SDR A6WA202107207835](https://openairdocs.org/sdr/A6WA202107207835.md): Seat Track · corroded · Jul 20, 2021 · N424AW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > RH SIDE SEAT RAI AT FS 559+58 SEAT TRACK HAS AREA OF CORROSION ***AIRCRAFT REMOVED FROM SERVICE*** BLENDED AND FOUND TO BE WITHIN LIMITS
- [SDR A6WA202107207836](https://openairdocs.org/sdr/A6WA202107207836.md): Frame · corroded · Jul 20, 2021 · N424AW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > RH SIDE SEAT RAIL AT FS 559+58 SEAT TRACK HAS AREA OF CORROSION ***AIRCRAFT REMOVED FROM SERVICE*** BLENDED AND FOUND TO BE WITHIN LIMITS
- [SDR A6WA202106117802](https://openairdocs.org/sdr/A6WA202106117802.md): Filter · not reported · Jun 8, 2021 · N424AW · Cndair CL6002B19 · Cabin Cooling System
  > REF. 340633/3 RH PACK SHUT DOWN AFTER TRANSFER, LH PACK ON MEL, ***AIRCRAFT REMOVED FROM SERVICE*** R&R RH PRSOV FILTER IAW AMM 21-51, OPS CHECK GOOD. REMOVED PLACARD REMOVED FROM MEL.
- [SDR A6WA2019091046859](https://openairdocs.org/sdr/A6WA2019091046859.md): Angle · corroded · Sep 9, 2019 · N424AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > SERVICE DOOR CUTOUT LOWER SILL ANGLE IS CORRODED.
- [SDR A6WA2019091346847](https://openairdocs.org/sdr/A6WA2019091346847.md): Angle · corroded · Sep 5, 2019 · N424AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > PAX DOOR LOWER SILL ANGLE IS CORRODED AROUND CUTOUT FOR THE PROX SENSOR I/B SIDE.
- [SDR A6WA2019090446824](https://openairdocs.org/sdr/A6WA2019090446824.md): Post · cracked · Aug 30, 2019 · N424AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FS 409+128, LBL 18 VERT POST HAS CRACK INDICATIONS NOTED IN THE AFT FLANGE REDIUS AT WL 69 I/B SIDE.250 LONG, O/B SIDE.500 LONG. BOTH GREATER TAHN 50% FSH BOTH FAILED NDT ISP.
- [SDR A6WA2019090446825](https://openairdocs.org/sdr/A6WA2019090446825.md): Post · cracked · Aug 30, 2019 · N424AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FS 409+128 LBL 18 VERT POST HAS CRACK INDICATION NOTED IN THE AFT FLANGE RADIUS AT WL 69 I/B SIDE.250 LONG O/B SIDE.500 LONG. BOTH GREATER THAT 50%FSH BOTH FAILED NDT INSP>
- [SDR A6WA2019090946851](https://openairdocs.org/sdr/A6WA2019090946851.md): Floorbeam · corroded · Aug 29, 2019 · N424AW · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > LBL27 CARGO FLOORBEAM HAS CORROSION AROUND ONE NUTPLATE HOLE AT FS559+ 114.
- [SDR A6WA2019083046810](https://openairdocs.org/sdr/A6WA2019083046810.md): Seat Track · corroded · Aug 28, 2019 · N424AW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > CARGO LBL 27 SEAT RAIL BEAM IS CORRODED AROUND NUTPLATES OB FLANGE F.S. 574.00 TO F.S. 608.00.
- [SDR A6WA2019082746802](https://openairdocs.org/sdr/A6WA2019082746802.md): Web · cracked · Aug 18, 2019 · N424AW · Cndair CL6002B19 · Passenger/Crew Doors
  > PASSENGER DOOR AFT WEB HAS AN INDICATION NOTED AT FOOTPRINT OF O/B STIFFENER FOR POWER ASSIST MOTOR. 0.250" LONG BY 50%FSH, FAILED NDT.
- [SDR A6WA2019090946844](https://openairdocs.org/sdr/A6WA2019090946844.md): Post · cracked · Aug 17, 2019 · N424AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FS409+128 BL0 POST HAS CRACK INDICATIONS NOTED IN THE AFT FLANGE RADIUS AT WL69. LT SIDE.600" LONG, R/H SIDE.300" LONG. BOTH GREATER THAN 50% FSH, BOTH FAILED NDT INSPECTION.
- [SDR A6WA2019090946846](https://openairdocs.org/sdr/A6WA2019090946846.md): Post · cracked · Aug 17, 2019 · N424AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FS409+128 RBL18 VERT POST HAS CRACK INDICATIONS NOTED IN THE AFT FLANGE RADIUS AT WL69. I/B SIDE.250" LONG, O/B SIDE.600" LONG, BOTH GREATER THAN 50% FSH. FAILED NDT INSPECTION.
- [SDR A6WA2019090946845](https://openairdocs.org/sdr/A6WA2019090946845.md): Post · cracked · Aug 17, 2019 · N424AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FS409+128 RBL18 VERT POST HAS CRACK INDICATIONS NOTED IN THE AFT FLANGE RADIUS AT WL69. I/B SIDE.250" LONG, O/B SIDE.600" LONG, BOTH GREATER THAN 50 % FSH. FAILED NDT INSPECTION.
- [SDR A6WA2019090946843](https://openairdocs.org/sdr/A6WA2019090946843.md): Post · cracked · Aug 17, 2019 · N424AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FS409+128 BL0 POST HAS CRACK INDICATIONS NOTED IN THE AFT FLANGE RADIUS AT WL69. LT SIDE.600" LONG, RT SIDE.300" LONG. BOTH GREATER THAN 50% FSH. BOTH FAILED NDT INSPECTION.
- [SDR A6WA2019090946849](https://openairdocs.org/sdr/A6WA2019090946849.md): Bulkhead · cracked · Aug 15, 2019 · N424AW · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > FOUND REAR PRESSURE BULKHEAD WEB HAS 7 AREAS WITH MULTIPLE INDICATIONS NOTED. 1) LBL 18, WL 129 - 132.5, 60% FSH, 2) LBL 9.5, WL 131 - 133, 50% FSH, 3) RBL 18, WL 131 - 134.5, 50% FSH, 4) RBL 27.5, WL 129.5 - 131, 70% FSH, 5) RBL 27.5, WL 114 - 85.5, 60% FSH,
- [SDR A6WA2019082746801](https://openairdocs.org/sdr/A6WA2019082746801.md): Drag Angle · cracked · Aug 15, 2019 · N424AW · Cndair CL6002B19 · Passenger/Crew Doors
  > PASSENGER DOOR AFT DRAG ANGLE IS CRACKED IN PREVIOUS REPAIR.
- [SDR A6WA2019082746795](https://openairdocs.org/sdr/A6WA2019082746795.md): Skin · dented · Aug 14, 2019 · N424AW · Cndair CL6002B19 · Trailing Edge Flaps
  > RH INBD FLAP LOWER SKIN HAS A DENT ON O/B T/E APPROX 10 INCHES FROM THE O/B END OF FLAP
- [SDR A6WA2019082746803](https://openairdocs.org/sdr/A6WA2019082746803.md): Plate · corroded · Aug 13, 2019 · N424AW · Cndair CL6002B19 · Fuselage Main, Attach Fittings
  > SERVICE DOOR STEP PLATE IS CORRODED.
- [SDR A6WA2019030846456](https://openairdocs.org/sdr/A6WA2019030846456.md): Smoke Detector · out of position · Mar 7, 2019 · N424AW · Cndair CL6002B19 · Smoke Detection
  > SMOKE TOILET CAUTION AND AURAL TONE RECEIVED ON FINAL AT 2600 FT. AFTER LANDING, INSPECTION CREW NOTICED SMOKE DETECTOR WAS NOT FLUSH WITH BULKHEAD.
- [SDR A6WA2019020546359](https://openairdocs.org/sdr/A6WA2019020546359.md): Warning Message · illuminated · Jan 21, 2019 · N424AW · Cndair CL6002B19 · Brake Anti-Skid Section
  > AT LIFT OFF RECEIVED IB ANTISKID CAUTION MSG. MSG CLEARED AFTER G EAR RETRACTION. MSG RETURNED AFTER GEAR EXTENSION ON TOUCHDOWN AND CLEAR AGAIN ON TAXI IN.
- [SDR A6WA2018102646125](https://openairdocs.org/sdr/A6WA2018102646125.md): Warning System · activated · Oct 26, 2018 · N424AW · Cndair CL6002B19 · Landing Gear Position and Warning
  > AFTER T/O AND SELECTING GEAR LEVER IP, RECEIVED GEAR DISAGREE. NOSE GEAR DID NOT SHOW RETRACTED. C/W QRH. OPERATED MANUAL RELEASE AND SELECTED HANDLE DOWN. GEAR SHOWED 3 GREEN. RETURNED TO MKE. LANDING WEIGHT LESS THAN 46,000 LBS.
- [SDR A6WA201745168](https://openairdocs.org/sdr/A6WA201745168.md): Actuator · failed · Aug 6, 2017 · N424AW · Cndair CL6002B19 · Trailing Edge Flap Actuator
  > FLAPS FAILED AT 27 DEGREES DURING APPROACH. EMERGENCY DECLARED. REMOVED AND REPLACED THE LT FLAP ACTUATOR IAW AMM27-53-05. OPS CHECKED GOOD.
- [SDR A6WA201745102](https://openairdocs.org/sdr/A6WA201745102.md): Hinge · cracked · Jul 12, 2017 · N424AW · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR OUTER HANDLE FLAP HINGE FWD DOOR HINGE IS BROKEN. REPLACED PAX DOOR OUTER HANDLE FLAP HINGE ASSY IAW SRM 51-42-06.
- [SDR A6WA201745100](https://openairdocs.org/sdr/A6WA201745100.md): Attach Bracket · cracked · Jul 11, 2017 · N424AW · Cndair CL6002B19 · Fuselage Main, Attach Fittings
  > FLIGHT DECK CENTER WINDSHIELD POST LOWER ATTACH BRACKET CRACKED. REPLACED BRACKET IAW SRM 51-41-21.
- [SDR A6WA201745101](https://openairdocs.org/sdr/A6WA201745101.md): Attach Bracket · cracked · Jul 11, 2017 · N424AW · Cndair CL6002B19 · Fuselage Main, Attach Fittings
  > CENTER WINDSHIELD POST LOWER ATTACH BRACKET LT SIDE IS CRACKED. REPLACED BRACKET IAW SRM 51-41-21.
- [SDR A6WA2017071045088](https://openairdocs.org/sdr/A6WA2017071045088.md): Landing · cracked · Jul 8, 2017 · N424AW · Cndair CL6002B19 · Fuselage Main, Structure
  > GROUND AIR DOOR AFT LANDING IS CRACKED
- [SDR A6WA201745110](https://openairdocs.org/sdr/A6WA201745110.md): Frame · corroded · Jul 1, 2017 · N424AW · Cndair CL6002B19 · Fuselage Main, Frame
  > FRAME BS 394 CORRODED ON AFT SIDE BETWEEN STRINGER 26L AND 26R. REPAIRED THE FRAME IAW 17-156.
- [SDR A6WA2017072545130](https://openairdocs.org/sdr/A6WA2017072545130.md): Bulkhead · cracked · Mar 25, 2017 · N424AW · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > CRACKS FOUND ON AFT PRESSURE BULKHEAD AT LBL 36.2, WL 79.5, LBL.5, WL 127 - 132.5, LBL.5, WL107 - 115, AND LBL.5, WL 100.5 - 104.5.
- [SDR A6WA201644677](https://openairdocs.org/sdr/A6WA201644677.md): Connector · unsecure · Dec 19, 2016 · N424AW · Cndair CL6002B19 · Light System Wiring
  > EMERGENCY LIGHTS INOPERATIVE ROW 8 AND AFT. PERFORMED OPS CHECK ON EMERGENCY SYSTEM AND FOUND LOOSE CONNECTOR ON FLOOR LIGHT, SECURED THE CONNECTOR AND PERFORMED OPS CHECK, OPS CHECKED GOOD IAW AMM 33-50-00.
- [SDR A6WA201643999](https://openairdocs.org/sdr/A6WA201643999.md): Light · inoperative · Jun 15, 2016 · N424AW · Cndair CL6002B19 · Emergency Lighting
  > FLOOR EMERGENCY LIGHTS, ROW 8 AND AFT WILL NOT ILLUMINATE.
- [SDR A6WA201543061](https://openairdocs.org/sdr/A6WA201543061.md): Engine · malfunctioned · Sep 14, 2015 · N424AW · Cndair CL6002B19 · Engine (Turbine/Turboprop)
  > RECEIVED VIBRATION & HEARD LOUD BANG, THEN SAW N1 & N2 ON LT ENG DECREASING & ITT RISING UNTIL IT EXCEEDED 900 DEG C. PULLED LT ENG BACK TO IDLE UNTIL SHUTDOWN, CHECKLIST COULD BE COMPLETED. N1 & N2 CONTINUED TO ROTATION, ITT WENT TO ALMOST ZERO. VIBRATION
- [SDR A6WA201542980](https://openairdocs.org/sdr/A6WA201542980.md): Light · inoperative · Aug 12, 2015 · N424AW · Cndair CL6002B19 · Emergency Lighting
  > FLIGHT 3996, EMER FLOOR LIGHTS INOPERATIVE BETWEEN ROWS 6 - 8. REMOVED LIGHT STRIP ROW 6 - 8. INSPECTED CONNECTORS, NO DEFECTS. REINSTALLED FLOOR STRIP, LIGHTS STILL INOPERATIVE, SEE 266879 3 FOR MEL.
- [SDR A6WA201542963](https://openairdocs.org/sdr/A6WA201542963.md): Connector · loose · Jul 31, 2015 · N424AW · Cndair CL6002B19 · Light System Wiring
  > FLIGHT 3874 EMERGENCY PATH LIGHTING, ROWS 7 - 9 & LOWER EXIT SIGN WINDOW EXIT RIGHT SIDE INOPERATIVE. FOUND CONNECTOR LOOSE ON FLOOR TRACK LIGHTING ROW 9. CONNECTED WIRING IAW AMM 33-51-01. OPERATIONS CHECKED GOOD.
- [SDR A6WA201542919](https://openairdocs.org/sdr/A6WA201542919.md): Fitting · cracked · Jul 10, 2015 · N424AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > LBL 280 & RBL 9 INBD & OTBD CLIPS CRACKED.
- [SDR A6WA201542918](https://openairdocs.org/sdr/A6WA201542918.md): Angle · unknown · Jul 10, 2015 · N424AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > REPAIR & REINFORCEMENT FOR FS LOWER CAP ANGLES BL 9.00 & 18.00 LT & 7 RT.
- [SDR A6WA201542921](https://openairdocs.org/sdr/A6WA201542921.md): Support · cracked · Jul 10, 2015 · N424AW · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR SUPPORT WHEEL LEG IS CRACKED.
- [SDR A6WA201542898](https://openairdocs.org/sdr/A6WA201542898.md): Drag Angle · cracked · Jul 4, 2015 · N424AW · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR AFT DRAG ANGLE CRACKED FWD OF POWER ASSIST YOKE.
- [SDR A6WA201542888](https://openairdocs.org/sdr/A6WA201542888.md): Attach Fitting · cracked · Jul 1, 2015 · N424AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > STRINGER 3L ATTACHED CLIPS AT FS 280.00 BULKHEAD CRACKED.
- [SDR A6WA201542890](https://openairdocs.org/sdr/A6WA201542890.md): Angle · cracked · Jul 1, 2015 · N424AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > RIGHT SIDE FS 621 - 625 OBLIQUE ANGLE AFT OF 621 BULKHEAD AT STRINGER 14R CRACKED.
- [SDR A6WA201542887](https://openairdocs.org/sdr/A6WA201542887.md): Seat Track · chafed · Jul 1, 2015 · N424AW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > LT & RT SEAT TRACK AT FS 364 - 409 HAS CORROSION.
- [SDR A6WA201542891](https://openairdocs.org/sdr/A6WA201542891.md): Attach Bracket · cracked · Jul 1, 2015 · N424AW · Cndair CL6002B19 · Fuselage Main, Attach Fittings
  > LEFT LOWER NOSE COMPARTMENT FWD ATTACH BRACKET FOR UPPER HYD ACCUMULATOR IS CRACKED.
- [SDR A6WA201542889](https://openairdocs.org/sdr/A6WA201542889.md): Angle · cracked · Jul 1, 2015 · N424AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > LEFT WINDSHIELD SIDE POST SUPPORT LOWER OTBD MOUNT ANGLE IS CRACKED.
- [SDR A6WA201542910](https://openairdocs.org/sdr/A6WA201542910.md): Bulkhead · damaged · Jun 27, 2015 · N424AW · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > FS 559.00 LOWER BULKHEAD HAS A GOUGE & CRACK AT LBL 18.00.
- [SDR A6WA2015051942730](https://openairdocs.org/sdr/A6WA2015051942730.md): Engine · malfunctioned · May 13, 2015 · N424AW · Cndair CL6002B19 · Engine (Turbine/Turboprop)
  > RT ENGINE INDICATING 125 - 127 PSI IN CLIMB OUT & CRUISE. REDUCED THRUST TO 80% N1 & 86% N2 OIL PRESS PSI. INDICATES 86 PSI AT IDLE ON GROUND. REPLACED RT ENGINE. ALL CHECKED GOOD.
- [SDR A6WA201442005](https://openairdocs.org/sdr/A6WA201442005.md): Unknown · odor · Sep 27, 2014 · N424AW · Cndair CL6002B19 · Air Distribution System
  > ELECTRICAL BURNING SMELL EMANATING FROM CEILING AREA AROUND ROWS 5 & 6.
- [SDR A6WA201312194201](https://openairdocs.org/sdr/A6WA201312194201.md): Control Unit · faulty · Dec 16, 2013 · N424AW · Cndair CL6002B19 · Fire Detection
  > INFLIGHT RECEIVED MULTIPLE RT FIRE FAIL CAUTION MESSAGES & RECEIVED 1 RT ENG FIRE RED WARNING MESSAGE, ALL MESSAGES LASTED FOR 2 - 3 SEC. R & R FIRE OVERHEAT CONTROL UNIT IAW AMM 26-10-01, OPERATIONS CHECKED GOOD.
- [SDR A6WA2013082741159](https://openairdocs.org/sdr/A6WA2013082741159.md): Stop · damaged · Aug 21, 2013 · N424AW · Cndair CL6002B19 · Cargo/Baggage Doors
  > FWD UPPER CARGO DOOR STOP HAS ENLARGED HOLE. REPLACED PART.
- [SDR A6WA2013082741173](https://openairdocs.org/sdr/A6WA2013082741173.md): Handle · cracked · Aug 20, 2013 · N424AW · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR OUTER HANDLE IS CRACKED. R & R IAW EO E08/007/452, REV B.
- [SDR A6WA2013082741163](https://openairdocs.org/sdr/A6WA2013082741163.md): Hinge Fitting · damaged · Aug 20, 2013 · N424AW · Cndair CL6002B19 · Rudder Structure
  > RUDDER CENTER HINGE UPPER & LOWER FITTING BEARING TOLERANCE OUT OF LIMITS. R & R HINGE FITTING.

Next page: https://openairdocs.org/aircraft/N424AW/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 = 'N424AW' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N424AW/reports

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