# Service difficulty reports: N412AW

A list on [N412AW](https://openairdocs.org/aircraft/N412AW.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 · 200 reports

- [SDR A6WA202107127824](https://openairdocs.org/sdr/A6WA202107127824.md): Strut · faulted · Jul 11, 2021 · N412AW · Cndair CL6002B19 · Nose/Tail Landing Gear Strut/Axle
  > AFTER TAKEOFF RECVD GEAR DISAGREE & NLG DOOR WARN MESSAGE, C/W QRH MSG CLEARED WHEN GEAR SELECTED DOWN. AIRCRAFT DIVERTED, AIRCRAFT REMOVED FROM SERVICE. REPLACED NLG ASSY IAW AWAC SUP 12-072. ALL OPS CHECK NORMAL.
- [SDR A6WA202105257785](https://openairdocs.org/sdr/A6WA202105257785.md): Warning Message · illuminated · May 24, 2021 · N412AW · Cndair CL6002B19 · Landing Gear Position and Warning
  > NOSE DOOR OPEN WARNING MESSAGE AFTER GEAR RETRACTION. CW QRH MESSAGE CLEARED WHEN GEAR WAS DOWN AND LOCKED. ***AIRCRAFT REMOVED FROM SERVICE*** INSPECTED AND FOUND NOSE GEAR DOORS CLOSED AT GATE, C/W AMM TASK 10-11-00-400-801 INSTALLED GEAR PINS. REF 326996/
- [SDR A6WA202012157460](https://openairdocs.org/sdr/A6WA202012157460.md): Thermal Switch · failed · Dec 11, 2020 · N412AW · Cndair CL6002B19 · Airfoil Anti/De-ice System
  > DURING ARRIVAL AND ENTERING ICING CONDITION RECEIVED ANTI-ICE DUCT WARNING MESSAGE. DECLARED EMERGENCY AND DIVERTED TO SB. SYNOPTIC PAGE SHOWS LEADING EDGE LEFT WING RED, EVEN WITH ALL BLEED AIR TURNED OFF AND ON THE GROUND. C/W QRH. AIRCRAFT REMOVED FROM
- [SDR A6WA202012027449](https://openairdocs.org/sdr/A6WA202012027449.md): Seat Track · corroded · Nov 21, 2020 · N412AW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > FOUND CORROSION AT SEAT TRACK AT LBL 27 FS 559+88. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED SEAT TRACK, PER REO 601R-53-00-764.
- [SDR A6WA202012027447](https://openairdocs.org/sdr/A6WA202012027447.md): Seat Track · corroded · Nov 21, 2020 · N412AW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK LOCATED ON RBL 9 FROM FS 394 TO FS 559+80 FOUND TO HAVE CORROSION OUT OF LIMITS. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED SEAT TRACK, PER REO 601R-53-00-764.
- [SDR A6WA202012027446](https://openairdocs.org/sdr/A6WA202012027446.md): Seat Track · corroded · Nov 21, 2020 · N412AW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > FOUND CORROSION ON SEAT TRACK FROM FS 364 TO 559+16. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED SEAT TRACK ON LBL 9 FROM FS 364 TO 559+16, PER SRM 51-42-02 AND REO 601R-53-00-764.
- [SDR A6WA2019020546358](https://openairdocs.org/sdr/A6WA2019020546358.md): Warning Message · multiple fail · Jan 24, 2019 · N412AW · Cndair CL6002B19 · Landing Gear Position and Warning
  > ON CLIMBOUT SELECTING GEAR UP, RECIEVED NOSE DOOR OPEN WARNING, GEAR DISAGREE WARNING, WOW INPUT CAUTION, STEERING INOP CAUTION, AND WOW OUTPUT FAIL STATUS, MESSAGES CLEARED AFTER LANDING. TAKEOFF WAS IN ICING CONDITIONS AND ALL HYDRAULICS NORMAL
- [SDR A6WA201946272](https://openairdocs.org/sdr/A6WA201946272.md): Hinge · unserviceable · Jan 3, 2019 · N412AW · Cndair CL6002B19 · Fuselage, Door Hinge
  > PAX DOOR HINGE ON FUSELAGE SIDE HAS FOUR GOUGED LUGS ON AFT END. REMOVED AND REPLACED PAX DOOR HINGE.
- [SDR A6WA2019010346270](https://openairdocs.org/sdr/A6WA2019010346270.md): Door Sill · corroded · Jan 2, 2019 · N412AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > RT FLOOR SILL FROM FS 589 TO FS 619 NUT PLATE LOCATIONS HAVE CORROSION. REPAIRED.
- [SDR A6WA2019010346271](https://openairdocs.org/sdr/A6WA2019010346271.md): Plug · defective · Jan 2, 2019 · N412AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > RT FWD PRESSURE PANEL 132AL HAS 2 BAD FREEZE PLUGS. REPLACED.
- [SDR A6WA2018010146259](https://openairdocs.org/sdr/A6WA2018010146259.md): Landing · cracked · Dec 28, 2018 · N412AW · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > LT TRU DOOR LAND CRACKED AT LATCH CUTOUT. REPLACED.
- [SDR A6WA2019010146258](https://openairdocs.org/sdr/A6WA2019010146258.md): Skin · chafed · Dec 27, 2018 · N412AW · Cndair CL6002B19 · Ailerons
  > RT AILERON LEADING EDGE UPPER SKIN CHAFFED. REPLACED.
- [SDR A6WA2018122646251](https://openairdocs.org/sdr/A6WA2018122646251.md): Floor Panel · cracked · Dec 22, 2018 · N412AW · Cndair CL6002B19 · Fuselage Floor Panel
  > FS193.00, LBL30 ELECTRICAL BAY FLOOR IS CRACKED AT INSIDE CORNER. REPAIRED FS193.00 LBL30 ELECTRICAL BAY FLOOR IAW REO 601R-53-11-111 REV -NC.
- [SDR A6WA2018122646250](https://openairdocs.org/sdr/A6WA2018122646250.md): Bracket · cracked · Dec 21, 2018 · N412AW · Cndair CL6002B19 · Fuselage Main, Attach Fittings
  > CARGO DOOR BEAM MEMBER BRACKET CRACKED ON 621 BULKHEAD. REPLACED CARGO DOOR BEAM MEMBER BRACKET IAW CRJ200 SRM 51-42-21.
- [SDR A6WA2018122646252](https://openairdocs.org/sdr/A6WA2018122646252.md): Beam · corroded · Dec 21, 2018 · N412AW · Cndair CL6002B19 · Fuselage Main, Structure
  > DURING INCORPORATION OF E.O. E17/005/425 STEP 7, LBL FLOOR BEAM CAP CORRODED AT FS569.00-621.00, LBL27, WL73. REPLACED CAP IAW CRJ200 SRM 51-40-11, 51-42-21, 51-42-22.
- [SDR A6WA2018122046245](https://openairdocs.org/sdr/A6WA2018122046245.md): Bracket · cracked · Dec 18, 2018 · N412AW · Cndair CL6002B19 · Fuselage Main, Attach Fittings
  > LEFT MLG WHEEL WELL VOLUMETRIC FUSE TRANSDUCER BRACKET IS CRACKED. REPLACED BRACKET IAW CRJ 200 SRM 51-42-06.
- [SDR A6WA2018121746244](https://openairdocs.org/sdr/A6WA2018121746244.md): Skin · gouged · Dec 16, 2018 · N412AW · Cndair CL6002B19 · Trailing Edge Flaps
  > RH FLAP IB LOWER SKIN HAS NUMEROUS SMALL GOUGES. REPLACED
- [SDR A6WA2018121746236](https://openairdocs.org/sdr/A6WA2018121746236.md): Attach Bracket · cracked · Dec 12, 2018 · N412AW · Cndair CL6002B19 · Fuselage Main, Attach Fittings
  > FS461.00 R/H FAIRING ATTACH BRACKET CRACKED. REPLACED BRACKET IAW CRJ200 SRM 51-42-06,
- [SDR A6WA2018121746238](https://openairdocs.org/sdr/A6WA2018121746238.md): Attach Bracket · cracked · Dec 12, 2018 · N412AW · Cndair CL6002B19 · Fuselage Main, Attach Fittings
  > FS449.85 R/H FAIRING ATTACH BRACKET CRACKED. REPLACED BRACKET IAW CRJ200 SRM 51-42-06.
- [SDR A6WA2018121746235](https://openairdocs.org/sdr/A6WA2018121746235.md): Attach Bracket · cracked · Dec 12, 2018 · N412AW · Cndair CL6002B19 · Fuselage Main, Attach Fittings
  > FS468 R/H FAIRING ATTACH BRACKET CRACKED. REPLACED BRACKET IAW CRJ200 SRM 51-42-06, 51-42-21.
- [SDR A6WA2018121746234](https://openairdocs.org/sdr/A6WA2018121746234.md): Attach Bracket · cracked · Dec 12, 2018 · N412AW · Cndair CL6002B19 · Fuselage Main, Attach Fittings
  > FS461 L/H FAIRING ATTACH BRACKET IS CRACKED. REPLACED BRACKET IAW CRJ200 SRM 51-42-06.
- [SDR A6WA2018121746237](https://openairdocs.org/sdr/A6WA2018121746237.md): Attach Bracket · cracked · Dec 12, 2018 · N412AW · Cndair CL6002B19 · Fuselage Main, Attach Fittings
  > FS449.85 L/H FAIRING ATTACH BRACKET CRACKED. REPLACED BRACKET IAW CRJ 200 SRM 51-42-06.
- [SDR A6WA2018121446231](https://openairdocs.org/sdr/A6WA2018121446231.md): Bulkhead · cracked · Dec 11, 2018 · N412AW · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > AFT PRESSURE BULKHEAD CRACKED AT LBL27, WL 130, TAIL END OF CARGO DOOR TRACK. BULKHEAD CRACK REPAIR ACCOMPLISHED ON AAR WORK ORDER 1016496-2000-0034 SN:67813 95.
- [SDR A6WA2018121446233](https://openairdocs.org/sdr/A6WA2018121446233.md): Skin · dented · Dec 11, 2018 · N412AW · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > EXTERIOR LOWER SKIN PANEL REPAIR DOUBLER FROM FS 700-718 STGR 23R TO 24R DENTED. REPAIRED
- [SDR A6WA2018121446230](https://openairdocs.org/sdr/A6WA2018121446230.md): Bulkhead · cracked · Dec 11, 2018 · N412AW · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > AFT PRESSURE BULKHEAD CRACKED AT LBL27, WL 106. REPAIR ACCOMPLISHED ON AAR WORK ORDER 1016496-2000-0043 SN:6781395 ITEM #6.
- [SDR A6WA2018121446232](https://openairdocs.org/sdr/A6WA2018121446232.md): Bulkhead · cracked · Dec 11, 2018 · N412AW · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > AFT PRESSURE BULKHEAD CRACKED AT LBL36, WL78. BULKHEAD CRACK REPAIR ACCOMPLISHED ON AAR WORK ORDER 1016496-2000-0043 SN:6781395.
- [SDR A6WA2018121446228](https://openairdocs.org/sdr/A6WA2018121446228.md): Attach Angle · cracked · Dec 9, 2018 · N412AW · Cndair CL6002B19 · Fuselage Main, Attach Fittings
  > FLIGHT DECK LEFT WINDSHIELD POST O/B ATTACH CLIP CRACKED. REPLACED CLIP IAW CRJ200 SRM 51-42-21.
- [SDR A6WA2018121446227](https://openairdocs.org/sdr/A6WA2018121446227.md): Attach Angle · cracked · Dec 9, 2018 · N412AW · Cndair CL6002B19 · Fuselage Main, Attach Fittings
  > FLIGHT DECK WINDSHIELD RIGHT O/B LOWER POST ATTACH CLIP IS CRACKED. REPLACED CLIP IAW CRJ 200 SRM 51-42-21.
- [SDR A6WA2018120946220](https://openairdocs.org/sdr/A6WA2018120946220.md): Angle · cracked · Dec 6, 2018 · N412AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > STR 14L OBLIQUE ANGLE IS CRACKED IN THE AEB. REPLACED STR14L OBLIQUE ANGLE IAW SRM 51-42-21, 51-25-16.
- [SDR A6WA2018120946221](https://openairdocs.org/sdr/A6WA2018120946221.md): Angle · cracked · Dec 6, 2018 · N412AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > STR 14R OBLIQUE ANGLE IS CRACKED IN AEB. REPLACED STR14R OBLIQUE ANGLE IAW SRM 51-42-21, 51-25-16.
- [SDR A6WA2018120946215](https://openairdocs.org/sdr/A6WA2018120946215.md): Fitting · cracked · Dec 3, 2018 · N412AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FS 193.00 LBL9 POST O/B CLIP CRACKED. REPLACES CLIP IAW CRJ200 SRM 51-42-06.
- [SDR A6WA2018120946214](https://openairdocs.org/sdr/A6WA2018120946214.md): Fitting · cracked · Dec 3, 2018 · N412AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FS193.00, RBL9 VERTICAL POST TOP O/B CLIP IS CRACKED. REPLACED CLIP IAW SRM 51-42-06.
- [SDR A6WA2018412036212](https://openairdocs.org/sdr/A6WA2018412036212.md): Structure · cracked · Dec 2, 2018 · N412AW · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR EDGE MEMBER CRACKED. REPAIRED EDGE MEMBER IAW REO 601R-52-11-279 REV-NC.
- [SDR A6WA2018120346211](https://openairdocs.org/sdr/A6WA2018120346211.md): Bracket · cracked · Dec 2, 2018 · N412AW · Cndair CL6002B19 · Fuselage, Equipment Attach Fittings
  > RIGHT MLG WHEEL WELL Z ANGLE FWD OF TRANSDUCER BRACKET IS CRACKED. REPLACED Z BRACKET IAW SRM 51-42-06.
- [SDR A6WA2018120346210](https://openairdocs.org/sdr/A6WA2018120346210.md): Bracket · cracked · Dec 2, 2018 · N412AW · Cndair CL6002B19 · Fuselage, Equipment Attach Fittings
  > RIGHT MLG WHEEL WELL VOLUMETRIC FUSE TRANSDUCER MOUNT IS CRACKED. REPLACED MOUNT IAW SRM 51-42-06.
- [SDR A6WA2018070345912](https://openairdocs.org/sdr/A6WA2018070345912.md): Drag Angle · cracked · Jul 2, 2018 · N412AW · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR AFT INNER SKIN DAMAGE. (DRAG ANGLE) REPAIRED PAX DOOR INNER SKIN (DRAG ANGLE) IAW REO601R-52-11-513 REV-B.
- [SDR A6WA2017101145334](https://openairdocs.org/sdr/A6WA2017101145334.md): Wire Harness · damaged · Oct 3, 2017 · N412AW · Cndair CL6002B19 · Landing Gear System Wiring
  > INFLIGHT, RECIEVED NWS INOPERATIVE AND WOW INPUT CAS MESSAGES AND WOW OUTPUT STATUS MESSAGE, COMPLIED WITH QRH, MESSAGE PERSISTED. MESSAGES CLEARED WITH GEAR DOWN. REMOVED AND REPLACED THE NOSE LANDING GEAR WOW HARNESS NR 1 IAW 12-029D. OPS CHECKED GOO
- [SDR A6WA20170908264](https://openairdocs.org/sdr/A6WA20170908264.md): Skin · punctured · Sep 7, 2017 · N412AW · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > MAINTENANCE FOUND A PUNCTURE IN THE FUSELAGE SKIN BETWEEN FS672.20/FS682.00 AND STR1L/STR2L. DAMAGE MEASURES 1.0" X 0.4". CAN BE REPAIRED WITH A GENERIC SRM REPAIR.
- [SDR A6WA201744920](https://openairdocs.org/sdr/A6WA201744920.md): Unknown · unknown · Apr 11, 2017 · N412AW · Cndair CL6002B19 · Flight Control System
  > UNCOMMANDED YAW DURING DECENT THRU 11,000 FT WITH AUTOPILOT ON AND WITH AUTOPILOT OFF ON APPROACH. YD CAUTION, HAD TO ENGAGE YD.
- [SDR A6WA201644691](https://openairdocs.org/sdr/A6WA201644691.md): Web · cracked · Dec 22, 2016 · N412AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > WEB CRACKED ON INBD SIDE OF LBL 27 BETWEEN BS 589 AND 605.
- [SDR A6WA2016122844690](https://openairdocs.org/sdr/A6WA2016122844690.md): Web · cracked · Dec 22, 2016 · N412AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > WEB CRACKED ON INBD SIDE OF LBL 27 BETWEEN BS 574 AND 589.
- [SDR A6WA2016122844692](https://openairdocs.org/sdr/A6WA2016122844692.md): Web · cracked · Dec 22, 2016 · N412AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > WEB CRACKED ON OTBD SIDE OF LBL 27 BETWEEN BS 574 AND 589.
- [SDR A6WA2016122844685](https://openairdocs.org/sdr/A6WA2016122844685.md): Angle · cracked · Dec 22, 2016 · N412AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > CARGO DOOR SILL TO STUB FRAME ANGLE CRACKED AT BS 605.
- [SDR A6WA2016122844693](https://openairdocs.org/sdr/A6WA2016122844693.md): Web · cracked · Dec 22, 2016 · N412AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > WEB CRACKED ON O/B SIDE OF LBL 27 BETWEEN BS 589 AND 605
- [SDR A6WA2016122844694](https://openairdocs.org/sdr/A6WA2016122844694.md): Plate · corroded · Dec 22, 2016 · N412AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > SERVICE DOOR STEP PLATE IS CORRODED & BENT AT BOTTOM.
- [SDR A6WA2016122844696](https://openairdocs.org/sdr/A6WA2016122844696.md): Frame · cracked · Dec 22, 2016 · N412AW · Cndair CL6002B19 · Fuselage Main, Frame
  > STUB FRAME AT BS 605 CRACKED AT STRINGER 18L
- [SDR A6WA201644689](https://openairdocs.org/sdr/A6WA201644689.md): Seat Track · corroded · Dec 22, 2016 · N412AW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > IN AFT CARGO SEAT TRACK BEAM IS CORRODED BS 621-559+80 LBL 26
- [SDR A6WA2016122844695](https://openairdocs.org/sdr/A6WA2016122844695.md): Frame · corroded · Dec 22, 2016 · N412AW · Cndair CL6002B19 · Fuselage Main, Frame
  > FRAME BS 605 IN CARGO BAY IS CORRODED BETWEEN STRINGERS 24R AND 24L
- [SDR A6WA2016122244682](https://openairdocs.org/sdr/A6WA2016122244682.md): Skin · dented · Dec 21, 2016 · N412AW · Cndair CL6002B19 · Ailerons
  > RIGHT AILERON HAS A SMALL DENT IN UPPER SKIN.
- [SDR A6WA201644683](https://openairdocs.org/sdr/A6WA201644683.md): Cargo Track · corroded · Dec 21, 2016 · N412AW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > AFT CARGO TRACK IS CORRODED BS 621 - 559+80 AT LBL 10.

Next page: https://openairdocs.org/aircraft/N412AW/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 = 'N412AW' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N412AW/reports

---
OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.