# Service difficulty reports: N431AW

A list on [N431AW](https://openairdocs.org/aircraft/N431AW.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 6 · 254 reports

- [SDR A6WA202108177858](https://openairdocs.org/sdr/A6WA202108177858.md): Bushing · corroded · Aug 17, 2021 · N431AW · Cndair CL6002B19 · Elevator Structure
  > RH ELEVATOR OTBD HINGE BUSHING CORRODED. AIRCRAFT REMOVED FROM SERVICE. R & R BUSHING
- [SDR A6WA202103227722](https://openairdocs.org/sdr/A6WA202103227722.md): Antenna · detached · Mar 21, 2021 · N431AW · Cndair CL6002B19 · Air Collision Avoidance System
  > 3819 - THOUGHT AT FLIGHT LEVEL 330 MAIN CABIN DOOR SEAL FAILED, INITIALLY HELD PRESSURE THEN CABIN STARTED TO CLIMB, DESCENDED TO FLIGHT LEVEL 200 THEN COULDN'T HOLD PRESSURE. FOUND ANTENNA ABOVE FLIGHT DECK SEPARATED FROM FUSELAGE. TCAS DIRECTIONAL
- [SDR A6WA202103227723](https://openairdocs.org/sdr/A6WA202103227723.md): Pseu · malfunctioned · Mar 19, 2021 · N431AW · Cndair CL6002B19 · Brake Anti-Skid Section
  > 3954 - AFTER TAKEOFF RECEIVED ANTI SKID INBOARD CAUTION MESSAGE AND PROX SYS CHANNEL CAUTION MESSAGE. C/W QRH. ***AIRCRAFT REMOVED FROM SERVICE*** R+R THE PSEU IN REF TO THE CRJ200 AMM 32-61-04. ALL OPS CHECKS GOOD.ANTI SKID OPS CHECKS GOOD IN REF. TO T
- [SDR A6WA202103027671](https://openairdocs.org/sdr/A6WA202103027671.md): Warning Message · false activation · Feb 25, 2021 · N431AW · Cndair CL6002B19 · Door Warning System
  > AT CRUISE, RECEIVED PAX DOOR STOW CAUTION MESSAGE. COMPLIED WITH QRH, GREEN WITNESS MARKS ALIGN AND PRESSURIZATION NORMAL. MESSAGE REMAINED INTERMITTENT FOR REMAINDER OF FLIGHT. ***AIRCRAFT REMOVED FROM SERVICE*** PERFORMED OPERATIONAL CHECK OF PAX DOOR NO
- [SDR A6WA2020031647226](https://openairdocs.org/sdr/A6WA2020031647226.md): Switch · defective · Mar 12, 2020 · N431AW · Cndair CL6002B19 · Engine Thrust Reverser
  > LEFT THRUST REVERSER CAUTION IN FLIGHT - AIR RETURN "AIRCRAFT REMOVED FROM SERVICE" REF WORK ORDER 293027 FOR R/R OF STOW SWITCH AND OPS TEST ON WORK CARDS 15-THROUGH 19. REMOVED PLACARD, REMOVED FROM MEL
- [SDR A6WA2020030947216](https://openairdocs.org/sdr/A6WA2020030947216.md): Pdu · malfunctioned · Mar 6, 2020 · N431AW · Cndair CL6002B19 · Engine Thrust Reverser
  > L REV UNLOCK CAUTION IN FLIGHT. C/W IAC AND QRH. EMER STOW DID NOT CLEAR MESSAGE. REVERSER NOT USED ON LANDING. CAUTION REMAINS WITH ENGINE SHUT DOWN. AIRCRAFT REMOVED FROM SERVICE. R/R LH TR PDU IAW AMM 78-32-03 OPS CHECK GOOD AT THIS TIME.
- [SDR A6WA2019120647042](https://openairdocs.org/sdr/A6WA2019120647042.md): Pdu · faulty · Dec 4, 2019 · N431AW · Cndair CL6002B19 · Engine Thrust Reverser
  > SUPPLEMENTAL INFORMATION, DURING CLIMB OUT RECIEVED LT T/R UNLOCK CAUTION MSG. C/W QRH EMERG STOW WAS PRESSED. T/R STOWED VISUALLY VERIFIED ON GROUND. REV ICON AMBER, DID NOT EXTINGUISH. AIRCRAFT AIR RETURNED TO KORD FOR MX. REVERSER WAS DE-ACTIVATED AND
- [SDR A6WA2019110946985](https://openairdocs.org/sdr/A6WA2019110946985.md): Battery Pack · inoperative · Oct 21, 2019 · N431AW · Cndair CL6002B19 · Emergency Lighting
  > L/H LWR EMERGENCY LIGHT BY OVERWING EXIT WILL NOT ILLUMINATE. AIRCRAFT REMOVED FROM SERVICE FOUND BATTERY PACK PS2LY TO HAVE LOW VOLTAGE. CHARGED DEPLETED EMERGENCY BACK REF AWAC SUPPLEMENT 15-220B. PERFORMED SELF TEST OF EMERGENCY BATTERY PACK/CHARGER ASSY
- [SDR A6WA2019110946984](https://openairdocs.org/sdr/A6WA2019110946984.md): Skin · dented · Oct 16, 2019 · N431AW · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > SMALL DENT ON R/H AFT FUSELASGE TAIL SECTION APPROX FS 733 & R/H STRINGER 19 AIRCRAFT REMOVED FROM SERVICE REWORKED DENT ON R/H AFT FUSELAGE TAIL SECTION AT APPROX FSS 733 AND ABOVE S19R IN AN AREA OF 1" X 1" X.002"D FROM ORIGINAL DEPTH OF.012"D FOUND TO B
- [SDR A6WA2019110946980](https://openairdocs.org/sdr/A6WA2019110946980.md): Intercostal · cracked · Oct 15, 2019 · N431AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > APU DOOR INTERCOSTAL AT FS 654 TO FS 672.20 IS CRACKED AIRCRAFT REMOVED FROM SERVICE REPAIRED DOOR INTERCOSTAL AT FS654 TO FS 672.20 REF AIR WISCONSIN SUPPLEMENTAL NO. 13-0851B AND BOMBARDIER PL601R-53-62-225 AT STRINGER 4L. CUT OUT DAMAGED AREA, HFEC NO D
- [SDR A6WA2019110546968](https://openairdocs.org/sdr/A6WA2019110546968.md): Door Sill · corroded · Oct 14, 2019 · N431AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > R/H PRESSURE FLOOR SILL ASSY ON PAD UP AREA AT STA 449.88 & RBL 43 AND STA 461 & RBL 43 HAS SURFACE CORROSION AIRCRAFT REMOVED FROM SERVICE REMOVED SURFACE CORROSIONBY HAD AT BOTH STA 449.85 AND STA 461 & RBL 43. STA 449.85 HAD AN AREA OF 1.0" X 1.0" X.002"
- [SDR A6WA2019110946983](https://openairdocs.org/sdr/A6WA2019110946983.md): Seal · damaged · Oct 12, 2019 · N431AW · Cndair CL6002B19 · Emergency Exits
  > R/H OVERWING EMERGENCY EXIT DOOR SEAL HAS 2" TEAR ON BOTTOM SIDE AIRCRAFT REMOVED FROM SERVICE REPLACED SEAL ON R/H OVERWING EMERGENCY EXIT DOOR SEAL REF CRJ AMM 52-21-07
- [SDR A6WA2019110946982](https://openairdocs.org/sdr/A6WA2019110946982.md): Fairing · damaged · Oct 11, 2019 · N431AW · Cndair CL6002B19 · Engine Thrust Reverser
  > #1 I/B REVERSER STING FAIRING HAS MULTIPLE DAMAGE AND CRACKS AIRCRAFT REMOVED FROM SERVICE #1 ENG I/B REVERSER STING FAIRING HAS MULTIPLE DAMAGES AND CRACKS BEYOND LIMITS AND PART HAD TO BE REPLACED
- [SDR A6WA2019090446823](https://openairdocs.org/sdr/A6WA2019090446823.md): Unknown · malfunctioned · Aug 30, 2019 · N431AW · Cndair CL6002B19 · Cabin Cooling System
  > DURING CLIMB WHEN TRANSFERRING BLEEDS TO ENGINES RECEIVED RT PACK HIGH PRESS. C/W QRH PACK WORKED ON APU (NOT ON ENGINE) DER: ON CLIMB OUT WHEN TRANSFERRING BLEEDS TO ENGINE RECEIVED RT PACK HI PRESS CAUTION MESSAGE COMPLIED WITH QRH AND THE MESSAGE CLEARED.
- [SDR A6WA2019071746701](https://openairdocs.org/sdr/A6WA2019071746701.md): Warning System · false activation · Jul 15, 2019 · N431AW · Cndair CL6002B19 · Fire Bottle, Fixed
  > WHILE FLT LEVEL 250 IN ROUTE RECIEVED "AMBER CARGO BOTTLE LOW CAUTION MSG". C/W QRH DIVERTED TO KMSN FOR NORMAL LANDING. MSG CLEARED AT PARKING. PLACARED AND PLACED ON MEL.
- [SDR A6WA2019071646700](https://openairdocs.org/sdr/A6WA2019071646700.md): Warning System · false activation · Jul 15, 2019 · N431AW · Cndair CL6002B19 · Fire Bottle, Fixed
  > CARGO FIRE BOTTLE LOW INDICATION- WHILE AT FLT LEVEL 280 ENROUTE, RECEIVED AMBER CARGO BLT LO MESSAGE. C/W QRH & LANDED AT 47400 LBS LANDING WEIGHT. BTMS READS 3343. MESSAGE CLEARED BY ITSELF AT 3000 FEET. LANDING WAS NORMAL AND SMOOTH.
- [SDR A6WA2019040446528](https://openairdocs.org/sdr/A6WA2019040446528.md): Unknown · unknown · Mar 31, 2019 · N431AW · Cndair CL6002B19 · Flight Control System
  > ON APPROACH, THE AIRCRAFT EXPERIENCED AN UN-COMMANDED YAW MOTION. THE FLIGHT CREW REFERENCED THE QRH, STABILIZED THE AIRCRAFT, CONTACTED ATC AND DISPATCH, DECLARED AN EMERGENCY AND DIVERTED.
- [SDR A6WA2017091145271](https://openairdocs.org/sdr/A6WA2017091145271.md): Frame · corroded · Sep 9, 2017 · N431AW · Cndair CL6002B19 · Fuselage Main, Frame
  > FRAME BS 333 HAS CORROSION ON THE FWD AND AFT SIDE BETWEEN STRINGERS 22R AND 23R
- [SDR A6WA2017091145255](https://openairdocs.org/sdr/A6WA2017091145255.md): Post · cracked · Sep 6, 2017 · N431AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > BS 409+128 VERTICAL POST AT RBL 18 CRACKED ON INBD SIDE IN AFT RADIUS.
- [SDR A6WA2017091145259](https://openairdocs.org/sdr/A6WA2017091145259.md): Frame · corroded · Sep 6, 2017 · N431AW · Cndair CL6002B19 · Fuselage Main, Frame
  > FRAME BS 574 HAS CORROSION ON THE FWD AND AFT SIDE AROUND STRINGER 21L, IN THE CARGO BAY.
- [SDR A6WA2017091145256](https://openairdocs.org/sdr/A6WA2017091145256.md): Skin · cracked · Sep 6, 2017 · N431AW · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN PUNCTURED AT BS 640 - 654 AND STRINGERS 26R - 27R.
- [SDR A6WA2017091145258](https://openairdocs.org/sdr/A6WA2017091145258.md): Bracket · cracked · Sep 6, 2017 · N431AW · Cndair CL6002B19 · Fuselage Main, Attach Fittings
  > DURING LEAK CHECK OF #3 HYD RESERVOIR FOUND RESERVOIR AFT MOUNT BRACKET TO BE CRACKED
- [SDR A6WA2017091145267](https://openairdocs.org/sdr/A6WA2017091145267.md): Rib · cracked · Aug 28, 2017 · N431AW · Cndair CL6002B19 · Nacelle/Pylon, Main Frame
  > RIGHT PYLON LEADING EDGE FWD INTERNAL RIB CRACKED. REPAIRED IAW 14-252A.
- [SDR A6WA201745235](https://openairdocs.org/sdr/A6WA201745235.md): Angle · cracked · Aug 26, 2017 · N431AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > ANGLE AT THE CARGO DOOR BEAM, AFT SIDE OF BS 621 IS CRACKED. REPLACED THE ANGLE IAW SRM 51-42-21.
- [SDR A6WA2017091145272](https://openairdocs.org/sdr/A6WA2017091145272.md): Battery Pack · no test · Aug 21, 2017 · N431AW · Cndair CL6002B19 · Emergency Lighting
  > EMERGENCY LIGHT BATTERY PACK NR 3 FAILED OPERATIONAL TEST. REPLACED THE BATTERY PACK IAW AMM 33-51-04, OPS CHECKED GOOD IAW AMM 33-51-04-740-801.
- [SDR A6WA201745216](https://openairdocs.org/sdr/A6WA201745216.md): Stringer · corroded · Aug 21, 2017 · N431AW · Cndair CL6002B19 · Fuselage Floor Panel
  > STRINGER 21L HAS CORROSION BETWEEN FRAMES BS 574 AND 589.
- [SDR A6WA2017082245208](https://openairdocs.org/sdr/A6WA2017082245208.md): Angle · cracked · Aug 18, 2017 · N431AW · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > REAR PRESSURE BULKHEAD AFT SIDE HAS A CRACKED OBLIQUE ANGLE AT STRINGER 14R. REPLACED THE ANGLE IAW SRM 51-42-21, 51-40-11, 51-21-11, AND 51-25-06.
- [SDR A6WA2017082945234](https://openairdocs.org/sdr/A6WA2017082945234.md): Angle · cracked · Aug 17, 2017 · N431AW · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > FLOORBEAM ANGLE CRACKED AT BS 621 AT OTBD FLOOR SILL. REPLACED THE FLOORBEAM ANGLE IAW REO 601R-53-61-117, REV-D.
- [SDR A6WA2017082245206](https://openairdocs.org/sdr/A6WA2017082245206.md): Angle · cracked · Aug 14, 2017 · N431AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > ANGLE ON STRINGER 3L IS CRACKED, AFT OF BS 280. REPLACED THE ANGLE IAW SRM 51-24-16, AND 51-42-06.
- [SDR A6WA201745184](https://openairdocs.org/sdr/A6WA201745184.md): Angle · cracked · Aug 14, 2017 · N431AW · Cndair CL6002B19 · Fuselage Main, Structure
  > RIGHT FLIGHT DECK WINDOW LOWER AFT ANGLE CRACKED. REPLACED THE ANGLE IAW SRM 51-42-21.
- [SDR A6WA2017091145268](https://openairdocs.org/sdr/A6WA2017091145268.md): Angle · cracked · Aug 13, 2017 · N431AW · Cndair CL6002B19 · Nacelle/Pylon Miscellaneous Structure
  > LEFT PYLON ACCESS PANEL SUPPORT ANGLE CRACKED AT 605. REPAIRED IAW 14-252A.
- [SDR A6WA2017082945238](https://openairdocs.org/sdr/A6WA2017082945238.md): Angle · corroded · Aug 13, 2017 · N431AW · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > FLOORBEAM ANGLE CORRODED AT BS 621, RBL 9 TO RBL 27. REPAIRED THE FLOORBEAM ANGLE IAW EA CRJ253-00753 REV-IR.
- [SDR A6WA201745199](https://openairdocs.org/sdr/A6WA201745199.md): Stringer · cracked · Aug 12, 2017 · N431AW · Cndair CL6002B19 · Fuselage Main, Longeron/Stringer
  > STR 3L IS CRACKED JUST FWD OF FRAME 379.00. REPAIRED STRINGER 3L FWD OF FRAME 379.00 IAW SRM 53-00-03, 51-42-06, 51-25-16.
- [SDR A6WA2017082945233](https://openairdocs.org/sdr/A6WA2017082945233.md): Post · cracked · Aug 10, 2017 · N431AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > CRACKED VERTICAL POST AT BS 409+128, BL 0. REPLACED VERTICAL POST IAW SRM 51-42-06, AND REO 01R-53-41-889.
- [SDR A6WA2017082245212](https://openairdocs.org/sdr/A6WA2017082245212.md): Post · cracked · Aug 10, 2017 · N431AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > VERTICAL POST AT BS 409+128, LBL 18 IS CRACKED. REPLACED THE VERICAL POST IAW SRM 53-41-19, AND REO 601R-53-41-889 REV-B.
- [SDR A6WA201745240](https://openairdocs.org/sdr/A6WA201745240.md): Strap · corroded · Aug 9, 2017 · N431AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FLOOR SUPPORT STRAP CORRODED AT FS 559 TO 560, RBL 30 TO RBL 42. REPAIRED THE FLOOR STRAP IAW SRM 51-42-06, AND EA 00754, REV-IR.
- [SDR A6WA2017081645185](https://openairdocs.org/sdr/A6WA2017081645185.md): Floorbeam · cracked · Aug 9, 2017 · N431AW · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > FLOORBEAM ANGLE CRACKED AT BS 280, LBL 9, OTBD. REPLACED THE FLOORBEAM ANGLE IAW SRM 51-42-21, 51-41-11, 51-21-11, AND 51-25-06.
- [SDR A6WA2017081645187](https://openairdocs.org/sdr/A6WA2017081645187.md): Floorbeam · cracked · Aug 9, 2017 · N431AW · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > FLOOBEAM ANGLE CRACKED AT BS 280, RBL 9- INBD. REPLACED THE FLOORBEAM ANGLE IAW SRM 51-42-21.
- [SDR A6WA201745179](https://openairdocs.org/sdr/A6WA201745179.md): Door Sill · cracked · Aug 9, 2017 · N431AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > LT FLOOR SILL CRACKED AT FS 589.00 IN THE CARGO BAY. REPAIRED LT FLOOR SILL REO 601R-53-61-433 REV-C.
- [SDR A6WA201745180](https://openairdocs.org/sdr/A6WA201745180.md): Seat Track · corroded · Aug 9, 2017 · N431AW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > CARGO SEAT TRACK CORRODED AT FS 559+80 TO 559+96, LBL9. REPLACED CARGO SEAT TRACK IAW AMM 53-00-49, REO 601R-53-00-485 REV-B.
- [SDR A6WA201745189](https://openairdocs.org/sdr/A6WA201745189.md): Floorbeam · cracked · Aug 8, 2017 · N431AW · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > FLOORBEAM ANGLE CORRODED AT BS 280, LBL 9 TO RBL 9. REPLACED THE FLOORBEAM ANGLE IAW SRM 51-42-06.
- [SDR A6WA201745173](https://openairdocs.org/sdr/A6WA201745173.md): Support Bracket · cracked · Aug 8, 2017 · N431AW · Cndair CL6002B19 · Fuselage Main, Attach Fittings
  > RT OVERWING ACCESS PNL SUPPORT BRACKET AT FS 449.85 IS CRACKED.
- [SDR A6WA201745174](https://openairdocs.org/sdr/A6WA201745174.md): Support Bracket · cracked · Aug 8, 2017 · N431AW · Cndair CL6002B19 · Fuselage Main, Attach Fittings
  > RT OVERWING ACCESS PNL SUPPORT BRACKET AT FS 461.0 IS CRACKED.
- [SDR A6WA2017081145248](https://openairdocs.org/sdr/A6WA2017081145248.md): Attach Angle · corroded · Aug 7, 2017 · N431AW · Cndair CL6002B19 · Fuselage Main, Attach Fittings
  > MAIN CABIN FLOOR SILL ATTACH ANGLE CORRODED AT THE SERVICE DOOR. REPLACED ATTACH ANGLE IAW SRM 51-42-06, 51-42-13, 51-42-21, AND 51-40-11.
- [SDR A6WA2017082945237](https://openairdocs.org/sdr/A6WA2017082945237.md): Skin · damaged · Aug 7, 2017 · N431AW · Cndair CL6002B19 · Trailing Edge Flaps
  > LEFT INBD FLAP LOWER SKIN DAMAGED. REPLACED THE SKIN IAW SRM 51-42-13, 57-52-00, AND 51-40-11.
- [SDR A6WA2017081645186](https://openairdocs.org/sdr/A6WA2017081645186.md): Floorbeam · cracked · Aug 7, 2017 · N431AW · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > MAIN CABIN FLOORBEAM AT BS 280, RBL 9 HAS CRACKED ATTACH ANGLE. REPLACED THE FLOORBEAM ANGLE IAW SRM 51-42-21, 51-40-11, 51-24-36, 51-25-16, AND 51-25-06.
- [SDR A6WA201745188](https://openairdocs.org/sdr/A6WA201745188.md): Floorbeam · cracked · Aug 7, 2017 · N431AW · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > FLOORBEAM ANGLE CRACKED AT BS 280.00, LBL 9. REPLACED THE FLOORBEAM ANGLE IAW SRM 51-42-21.
- [SDR A6WA2017081645190](https://openairdocs.org/sdr/A6WA2017081645190.md): Floorbeam · corroded · Aug 7, 2017 · N431AW · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > MAIN CABIN FLOORBEAM CORRODED AT BS 280. LBL 9 TO RBL 9. REPAIRED THE FLOORBEAM IAW REO 601R-53-11-136 REV-A.
- [SDR A6WA201745203](https://openairdocs.org/sdr/A6WA201745203.md): Skin · chafed · Aug 6, 2017 · N431AW · Cndair CL6002B19 · Trailing Edge Flaps
  > LEFT I/B FLAP VANE HAS A CHAFE AT THE I/B STOP. REPLACED FLAP VANE LEADING EDGE IAW SRM 51-42-13.
- [SDR A6WA201744830](https://openairdocs.org/sdr/A6WA201744830.md): Warning System · activated · Mar 3, 2017 · N431AW · Cndair CL6002B19 · Door Warning System
  > RECEIVED SERVICE DOOR CAUTION MESSAGE ON CLIMB OUT AT 20,000 FEET AND THEN LOUD HISSING. PRECEDED BY "THUMP" COMING FROM SERVICE DOOR AREA. PRESSURIZATION REMAINED NORMAL HOWEVER HISSING WAS INTOLERABLE. C/W QRH, DECLARED EMERGENCY, RETURNED PHL. LANDING WAS S

Next page: https://openairdocs.org/aircraft/N431AW/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 = 'N431AW' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N431AW/reports

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