# Service difficulty reports: N419AW

A list on [N419AW](https://openairdocs.org/aircraft/N419AW.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 · 178 reports

- [SDR A6WA202110297944](https://openairdocs.org/sdr/A6WA202110297944.md): None · none · Oct 29, 2021 · N419AW · Cndair CL6002B19 · Steering Unit
  > WHILE ENROUTE TO KORD THE FLIGHT CREW RECEIVED A NOSE WHEEL STEERING INOP CAUTION MESSAGE. THE CREW FOLLOWED THE QRH AND THE MESSAGE REMAINED. CREW COORDINATED WITH DISPATCH AND ALSO DECLARED AN EMERGENCY WITH ATC. THE CREW CONTINUED TO KORD, LANDED, CONFER
- [SDR A6WA202106087800](https://openairdocs.org/sdr/A6WA202106087800.md): Seat Track · corroded · Jun 6, 2021 · N419AW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK AT LBL9 FS 349-409+96 CORRODED, R & R SEAT TRACK IAW CRJ-200 AMM 53-01-11 ***AIRCRAFT REMOVED FROM SERVICE*** R & R SEAT TRACK IAW CRJ-200 AMM 53-01-11
- [SDR A6WA202106087799](https://openairdocs.org/sdr/A6WA202106087799.md): Seat Track · corroded · Jun 6, 2021 · N419AW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK RBL9 FS 349-409+96 CORRODED, REQUIRES REPLACEMENT, R & R SEAT TRACK IAW CRJ -200 AMM 53-01-11 ***AIRCRAFT REMOVED FROM SERVICE*** R & R SEAT TRACK IAW CRJ -200 AMM 53-01-11
- [SDR A6WA202102127629](https://openairdocs.org/sdr/A6WA202102127629.md): Modulating Valve · malfunctioned · Feb 11, 2021 · N419AW · Cndair CL6002B19 · Airfoil Anti/De-ice System
  > WHILE CLIMBING FROM SDF TO INITIAL 10000 FT ALTITUDE RECEIVED WING OVERHEAT WARNING. LFT SIDE. PER QRH TURN WING SWITCH OFF AFTER 40 SEC MESSAGE REMAINED. (MESSAGE IN NORMAL AND STBY. STBY MODE WORKED NORMAL AFTER SECOND ATTEMPT) ***AIRCRAFT REMOVED FROM SER
- [SDR A6WA202011167414](https://openairdocs.org/sdr/A6WA202011167414.md): Detector · malfunctioned · Nov 12, 2020 · N419AW · Cndair CL6002B19 · Fire Protection System
  > LT 10TH DUCT WARNING MESSAGE ILLUMINATED IN FLIGHT. C/W QRH, MESSAGE PERSISTS. DUCT (10TH) SHOWS RED BETWEEN LT 10TH SOV, PACK NR 1, 10TH ISOL VALVE, AND APU LCV ON ECS SYNOPTIC PAGE. AIRCRAFT REMOVED FROM SERVICE. R & R 10TH STAGE DUCTING LOOP B BLEED AIR
- [SDR A6WA202021247160](https://openairdocs.org/sdr/A6WA202021247160.md): Controller · malfunctioned · Feb 9, 2020 · N419AW · Cndair CL6002B19 · AC Generation System
  > SHORTLY AFTER TAKE OFF, THE AIRCRAFT'S AIR DRIVEN GENERATOR DEPLOYED WITHOUT INPUT FROM THE CREW. THE FLIGHT AIR RETURNED TO RIC AS A RESULT. AIRCRAFT REMOVED FROM SERVICE C/W ALT INSP AFTER ADG DEPLOYMENT DURING UNSCHEDULE MX CHECK IAW AWAC SUP 16-172.
- [SDR A6WA2020011447105](https://openairdocs.org/sdr/A6WA2020011447105.md): Pdu · malfunctioned · Jan 12, 2020 · N419AW · Cndair CL6002B19 · Trailing Edge Flap Actuator
  > RECEIVED FLAP FAIL CAUTION MESSAGE AT 0 DEGREES WHEN SELECTING 0 TO 8 DEGREES. FOLLOWING LANDING THE FLAPS WERE RESET AND THE SYSTEM WAS PLACED ON MEL FOR 10 DAYS AS REQUIRED BY SUPPLEMENT 98-018G AIRCRAFT REMOVED FROM SERVICE. R/R FLAP PDU IAW AMM 27-52-01 O
- [SDR A6WA2019080946786](https://openairdocs.org/sdr/A6WA2019080946786.md): Bulkhead Web · cracked · Aug 9, 2019 · N419AW · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > AFT PRESSURE BULKHEAD HAS CRACK AT LBL9.5, WL75 AT THE BOTTOM OF THE LINER SUPPORT. REPAIRED AFT PRESSURE BULKHEAD IAW REO 601R-53-61-7076 REV--.
- [SDR A6WA201908146788](https://openairdocs.org/sdr/A6WA201908146788.md): Beam · damaged · Aug 8, 2019 · N419AW · Cndair CL6002B19 · Fuselage Main, Structure
  > BEAM 601R35050-64 HAS MARKS FROM DOOR CABLE ASSIST. REPLACED
- [SDR A6WA2019080946785](https://openairdocs.org/sdr/A6WA2019080946785.md): Bracket · cracked · Aug 6, 2019 · N419AW · Cndair CL6002B19 · Wing, Attach Fittings
  > RIGHT WING I/B LEADING EDGE ATTACH BRACKET IS CRACKED. REPLACED BRACKET IAW SRM 51-41-02.
- [SDR A6WA2019080546781](https://openairdocs.org/sdr/A6WA2019080546781.md): Skin · cracked · Aug 3, 2019 · N419AW · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > LEFT TRU SKIN LANDING CRACKED NEAR LATCH. REPAIRED SKIN IAW SUPP. 19-016B.
- [SDR A6WA2019080546778](https://openairdocs.org/sdr/A6WA2019080546778.md): Angle · cracked · Aug 3, 2019 · N419AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > AFB ANGLE CLIP AT RBL 36.20 CRACKED. REPLACED.
- [SDR A6WA2019080546782](https://openairdocs.org/sdr/A6WA2019080546782.md): Angle · cracked · Aug 3, 2019 · N419AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > AFT PRESSURE BULKHEAD HAS A CRACKED ANGLE CLIP ST LBL36.20 BY THE 4TH INTERCOSTAL FROM THE FLOOR. REPLACED CLIP IAW CRJ200 SRM 51-42-21.
- [SDR A6WA2019080546779](https://openairdocs.org/sdr/A6WA2019080546779.md): Bracket · cracked · Aug 2, 2019 · N419AW · Cndair CL6002B19 · Fuselage Main, Attach Fittings
  > POWER REC PLUG BOX LOWER BRACKET CRACKED. REPLACED.
- [SDR A6WA201904156559](https://openairdocs.org/sdr/A6WA201904156559.md): Warning Message · illuminated · Apr 14, 2019 · N419AW · Cndair CL6002B19 · Ice/Rain Protection System
  > WHEN DE-SELECTING COWL A/ICE AT FL280, LH COWL A/ICE CAUTION WHEN SWITCH IN OFF POSITION. C/W QRH. DIVERTED TO BNA
- [SDR A6WA2018121746243](https://openairdocs.org/sdr/A6WA2018121746243.md): Unknown · odor · Dec 16, 2018 · N419AW · Cndair CL6002B19 · Air Distribution System
  > CHEMICAL SCENT/LIGHTLY ACRID SMELL OBSERVED IN FLIGHT. ALL OTHER INDICATIONS NORMAL. ONLY OBSERVABLE IN COCKPIT. USING ENGINE AIR.
- [SDR A6WA201745154](https://openairdocs.org/sdr/A6WA201745154.md): Floor Support · corroded · Aug 3, 2017 · N419AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FLOOR SUPPORT BETWEEN LBL27 AND LBL9 HAS CORROSION AT FS621.
- [SDR A6WA2017080445156](https://openairdocs.org/sdr/A6WA2017080445156.md): Rib · cracked · Aug 3, 2017 · N419AW · Cndair CL6002B19 · Nacelle/Pylon, Frame/Spar/Rib
  > RIGHT PYLON RIB FOWARD LOWER SUPPORT FLANGE CRACKED UNDER PANEL 421AL
- [SDR A6WA201745153](https://openairdocs.org/sdr/A6WA201745153.md): Frame · corroded · Aug 3, 2017 · N419AW · Cndair CL6002B19 · Fuselage Main, Frame
  > FRAME AT BS 605 IS CORRODED BETWEEN STRINGERS 20L AND 24L.
- [SDR A6WA201745155](https://openairdocs.org/sdr/A6WA201745155.md): Skin · dented · Aug 3, 2017 · N419AW · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > SKIN DENTED BS 295 - 310, STRINGER 12R - 16R
- [SDR A6WA201745152](https://openairdocs.org/sdr/A6WA201745152.md): Door Sill · cracked · Aug 2, 2017 · N419AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > BAGGAGE LT SILL IS CRACKED AT PREVIOUS CUTOUT AT FS 605.
- [SDR A6WA2017080345149](https://openairdocs.org/sdr/A6WA2017080345149.md): Floor Support · corroded · Aug 1, 2017 · N419AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > RBL27 FLOOR SUPPORT HAS CORROSION FROM BS 559+80 TO 564 AROUND SCREW HOLES
- [SDR A6WA201745147](https://openairdocs.org/sdr/A6WA201745147.md): Floor Support · corroded · Jul 31, 2017 · N419AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > LEFT CARGO FLOOR SUPPORT FROM BS 568 TO 621 CORRODED.
- [SDR A6WA201745148](https://openairdocs.org/sdr/A6WA201745148.md): Floor Support · corroded · Jul 31, 2017 · N419AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > RBL 27 FLOOR SUPPORT BTW BS 574 TO 621 HAS CORROSION AROUND SCREW HOLES.
- [SDR A6WA2017073145145](https://openairdocs.org/sdr/A6WA2017073145145.md): Floor Support · corroded · Jul 30, 2017 · N419AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > RIGHT FLOOR SUPPORT CORRODED BETWEEN BS 349 AND 364.
- [SDR A6WA2017073145146](https://openairdocs.org/sdr/A6WA2017073145146.md): Crossbeam · corroded · Jul 30, 2017 · N419AW · Cndair CL6002B19 · Fuselage Main, Structure
  > CROSSBEAM BS 349 IS CORRODED AT RBL 42
- [SDR A6WA2017073145143](https://openairdocs.org/sdr/A6WA2017073145143.md): Bulkhead · cracked · Jul 28, 2017 · N419AW · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > AFT PRESSURE BULKHEAD CRACKED AT LBL 18 AND WL 131.
- [SDR A6WA2017073145137](https://openairdocs.org/sdr/A6WA2017073145137.md): Seat Track · corroded · Jul 21, 2017 · N419AW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > LEFT SEAT TRACK CORRODED FROM BS 409+126 TO 559+4, LBL 9.
- [SDR A6WA2017073145136](https://openairdocs.org/sdr/A6WA2017073145136.md): Seat Track · corroded · Jul 21, 2017 · N419AW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > RIGHT FLOOR SEAT TRACK CORRODED FROM BS 409+128 TO 559+16, STRINGER 17L.
- [SDR A6WA2017072545126](https://openairdocs.org/sdr/A6WA2017072545126.md): Attach Bracket · cracked · Jul 21, 2017 · N419AW · Cndair CL6002B19 · Fuselage Main, Attach Fittings
  > LEFT SIDE OVERWING ACCESS PANEL ATTACH BRACKET CRACKED AT BS 449. REPLACED ATTACH BRACKET IAW SRM 51-42-06, AND 51-42-13.
- [SDR A6WA2017072545128](https://openairdocs.org/sdr/A6WA2017072545128.md): Attach Bracket · cracked · Jul 21, 2017 · N419AW · Cndair CL6002B19 · Fuselage Main, Attach Fittings
  > RIGHT OVERWING ACCESS PANEL ATTACH BRACKET CRACKED AT BS 449. REPLACED THE ATTACH BRACKET IAW SRM 51-42-06, AND 51-42-13.
- [SDR A6WA2017072545127](https://openairdocs.org/sdr/A6WA2017072545127.md): Attach Bracket · cracked · Jul 21, 2017 · N419AW · Cndair CL6002B19 · Fuselage Main, Attach Fittings
  > RIGHT SIDE OVERWING EXIT ACCESS PANEL ATTACH BRACKET CRACKED, BS 468. REPLACED BRACKET IAW SRM 51-41-02, 51-42-06, AND 51-42-13.
- [SDR A6WA2017073145144](https://openairdocs.org/sdr/A6WA2017073145144.md): Bulkhead · cracked · Jul 20, 2017 · N419AW · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > AFT PRESSURE BULKHEAD CRACKED AT RBL18 AND WL119.
- [SDR A6WA2017071945105](https://openairdocs.org/sdr/A6WA2017071945105.md): Stiffener · cracked · Jul 15, 2017 · N419AW · Cndair CL6002B19 · Engine Collector/Tailpipe/Nozzle
  > LEFT EXHAUST FAIRING CRACKED ON FWD STIFFENER. REPAIRED THE FAIRING IAW CMM 78-11-00-300-810-A01, REPAIR SRS042.
- [SDR A6WA2017073145138](https://openairdocs.org/sdr/A6WA2017073145138.md): Frame Splice · corroded · Jul 14, 2017 · N419AW · Cndair CL6002B19 · Fuselage Main, Frame
  > CIRCUMFERENTIAL SPLICE JOINT CORRODED BETWEEN STRINGER 26L AND 26R AFT OF FRAME BS 409. REPLACED CIRCUMFERENTIAL JOINT SPLICE IAW SRM 51-40-11, AND 53-21-15.
- [SDR A6WA201745028](https://openairdocs.org/sdr/A6WA201745028.md): Battery Pack · discharged · May 17, 2017 · N419AW · Bombdr CL6002D15 · Emergency Lighting
  > EMER FLOOR LIGHTING AT ROW 9 AND AFT INOP. R&R BATTERY PACK POSITION 4 IAW AMM 33-51-04. OPS CHECKED GOOD.
- [SDR A6WA2017021344792](https://openairdocs.org/sdr/A6WA2017021344792.md): Frame · corroded · Feb 10, 2017 · N419AW · Cndair CL6002B19 · Fuselage Main, Frame
  > FRAME BS 310 IS CORRODED BETWEEN STRINGERA 23R AND 23L
- [SDR A6WA201744793](https://openairdocs.org/sdr/A6WA201744793.md): Angle · corroded · Feb 10, 2017 · N419AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > REINFORCEMENT ANGLE 600-32002-113 IS CORRODED AT BS 310, STRINGERS 23 AND 24R
- [SDR A6WA201744794](https://openairdocs.org/sdr/A6WA201744794.md): Frame · corroded · Feb 10, 2017 · N419AW · Cndair CL6002B19 · Fuselage Main, Frame
  > FRAME BS 319 CORRODED AT STRINGER 23R
- [SDR A6WA2017021344791](https://openairdocs.org/sdr/A6WA2017021344791.md): Stringer · corroded · Feb 10, 2017 · N419AW · Cndair CL6002B19 · Fuselage Main, Longeron/Stringer
  > 1014036-2000-0004 - STRINGER 23R IS CORRODED BETWEEN FS 304 AND FS 327
- [SDR A6WA2017021344795](https://openairdocs.org/sdr/A6WA2017021344795.md): Strap · corroded · Feb 10, 2017 · N419AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > 1014036-2000-0012 - SPLICE STRAP UNDER STGR 23R BETWEEN FS 310 AND FS 319 IS CORRODED
- [SDR A6WA201744796](https://openairdocs.org/sdr/A6WA201744796.md): Frame · corroded · Feb 10, 2017 · N419AW · Cndair CL6002B19 · Fuselage Main, Frame
  > FRAME BS 310 CORRODED, STRINGER 22, AND 23R
- [SDR A6WA2017010944734](https://openairdocs.org/sdr/A6WA2017010944734.md): Altimeter · reads high · Jan 8, 2017 · N419AW · Cndair CL6002B19 · Altimeter, Barometric/Encoder
  > AT 32,000FT AND 300 KNOTS, CAPTAIN'S ALTIMETER WAS 100FT HIGH, STANDBY WAS 600FT HIGH AND FO'S READ 32,000FT. STANDBY ALTIMETER WAS NOT CLICKING.
- [SDR A6WA201744724](https://openairdocs.org/sdr/A6WA201744724.md): Light · broken · Jan 3, 2017 · N419AW · Cndair CL6002B19 · Emergency Lighting
  > IN CABIN, THE FWD EMERGENCY LIGHT NOT WORKING AND PLASTIC COVER BROKEN ORANGE STRIP LIGHT STICKING UP AND EXPOSED. REMOVED AND REPLACED EMERGENCY LIGHT IAW AMM 33-51-01.
- [SDR A6WA201643482](https://openairdocs.org/sdr/A6WA201643482.md): Unknown · malfunctioned · Jan 20, 2016 · N419AW · Cndair CL6002B19 · Autopilot System
  > SHORT ERRATIC UNCOMMANDED YAW MOTION, FOLLOWED BY YAW DAMPER 2 INOPERATIVE STATUS MSG. RE-ENGAGED YAW DAMPER 2 & UNCOMMANDED YAW PERSISTED. DISENGAGED BOTH YAW DAMPERS, THE RE-ENGAGED YAW DAMPER 1 ONLY. NO FURTHER UNCOMMANDED YAW.
- [SDR A6WA201543108](https://openairdocs.org/sdr/A6WA201543108.md): Handle · damaged · Oct 6, 2015 · N419AW · Cndair CL6002B19 · Service Doors
  > SERVICE DOOR WILL NOT OPEN FROM OUTSIDE. REMOVED SERVICE DOOR OUTER HANDLE IAW AMM 52-41-03, FOUND DAMAGE ON HANDLE & HOUSING. REINSTALLED ORIGINAL HANDLE, PLACED ON MEL. REMOVED HANDLE ASSEMBLY & INSPECTED HOUSING IAW AMM 52-41-03 & SUPP 11-029B, NO DEFECT
- [SDR A6WA201542920](https://openairdocs.org/sdr/A6WA201542920.md): Beam · corroded · Jul 10, 2015 · N419AW · Cndair CL6002B19 · Fuselage Main, Structure
  > LBL 27 AT FS 621 - 559+112 HAS CORROSION.
- [SDR A6WA201542917](https://openairdocs.org/sdr/A6WA201542917.md): Skin · chafed · Jul 10, 2015 · N419AW · Cndair CL6002B19 · Trailing Edge Flaps
  > LEFT OTBD FLAP VANE HAS CHAFE.
- [SDR A6WA201542914](https://openairdocs.org/sdr/A6WA201542914.md): Mount · cracked · Jul 9, 2015 · N419AW · Cndair CL6002B19 · Fuselage Main, Attach Fittings
  > AEB NR 2 HYD SYS RETURN FILTER MOUNT PLATE HAS CRACK IN AFT LOWER CORNER.
- [SDR A6WA201542913](https://openairdocs.org/sdr/A6WA201542913.md): Attach Fitting · chafed · Jul 9, 2015 · N419AW · Cndair CL6002B19 · Horizontal Stabilizer Structure
  > RIGHT HORIZONTAL STAB SCREW JACK ATTACH FITTING HAS CHAFES & GOUGES ON THE OTBD UPPER FWD & LOWER EDGES.

Next page: https://openairdocs.org/aircraft/N419AW/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 = 'N419AW' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N419AW/reports

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