# Service difficulty reports: N416AW

A list on [N416AW](https://openairdocs.org/aircraft/N416AW.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 · 183 reports

- [SDR A6WA202512038873](https://openairdocs.org/sdr/A6WA202512038873.md): Actuator · malfunctioned · Jan 22, 2026 · N416AW · Cndair CL6002B19 · Trailing Edge Flap Control System
  > RECEIVED FLAPS FAIL WHEN SELECTING FLAPS FROM 8 TO 20. IT FAILED AT 8. C/W QRH. AIRSPEED 180 KNOTS WHEN FAILED. PERFORMED FLAP RESET PROCEDURE IAW AWAC SUPP 98-018I BOX 12. FLAPS RESET. REF 357078-1 FOR MEL REF 357077-4 PERFORMED FLAP FAIL RESET PROCEDURE. P
- [SDR A6WA202409058806](https://openairdocs.org/sdr/A6WA202409058806.md): Control Unit · faulted · Sep 5, 2024 · N416AW · Cndair CL6002B19 · Trailing Edge Flap Control System
  > FLAPS FAIL CAUT MESSAGE FLAPS FAILED AT 16K FT 250 KNOTS FAILED IN THE ZERO DEGREE POSITION. AIRCRAFT REMOVED FROM SERVICE R&R THE FECU IAW AMM 27-51-05. OPS CHECK GOOD. REMOVED PLACARD AND REMOVED FROM MEL.
- [SDR A6WA202409058804](https://openairdocs.org/sdr/A6WA202409058804.md): Control Unit · failed · Sep 5, 2024 · N416AW · Cndair CL6002B19 · Trailing Edge Flap Control System
  > FLAPS FAIL CAUT MESSAGE FLAPS FAILED AT 16K FT 250 KNOTS FAILED IN THE ZERO DEGREE POSITION. PERFORMED FLAP RESET PROCEDURE IAW AWAC SUPPLEMENT 98-18I BOX 12. FLAPS RESET. PLACARDED AND PLACED ON MEL ***** AIRCRAFT REMOVED FROM SERVICE ***** R&R THE FECU IAW
- [SDR A6WA202401198702](https://openairdocs.org/sdr/A6WA202401198702.md): Landing Gear · warning message · Jan 19, 2024 · N416AW · Cndair CL6002B19 · Nose/Tail Landing Gear
  > AFTER T/O RECEIVED NOSE DOOR OPEN AND GEAR DISAGREE. RAN QRH PROCEDURE MSG'S WENT AWAY. LANDING WIGHT 44, 600LBS, SMOOTH NORMAL LANDING. MSG APPEARED AFTER 2 SECONDS SELECTING GEAR. AIRCRAFT REMOVED FROM SERVICE PERFORMED GEAR SWING IAW AMM 32-30-00 OPS CH
- [SDR A6WA202310208661](https://openairdocs.org/sdr/A6WA202310208661.md): Sensor · unknown · Oct 20, 2023 · N416AW · Cndair CL6002B19 · Pneumatic Distribution System
  > PERSISTENT ANTI-ICE DUCT WARNING MESSAGE. RH FUSELAGE SHOWED RED ON THE SYNOPTIC PAGE. C/W QRH AND RETURNED TO YUL. *********AIRCRAFT REMOVED FROM SERVICE********* T/S PER MTCM 19-149. REPLACED LOOP A46WK PER AMM 36-21-04. OPS CHECK GOOD.
- [SDR A6WA202310208660](https://openairdocs.org/sdr/A6WA202310208660.md): Sensor · unknown · Oct 20, 2023 · N416AW · Cndair CL6002B19 · Airfoil Anti/De-ice System
  > ANTI ICE DUCT WARN MSG ******AIRCRAFT REMOVED FROM SERVICE******** T/S PER MTCM 19-149. REPLACED LOOP A46WK PER AMM 36-21-04. OPS CHECK GOOD.
- [SDR A6WA202212138409](https://openairdocs.org/sdr/A6WA202212138409.md): Strap · out of position · Dec 13, 2022 · N416AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > PREVIOUS REPAIR ON PASSENGER DOOR FRAME 310.0 DAMAGE FROM INPROPER DOOR CLOSING. AIRCRAFT REMOVED FROM SERVICE. INSTALLED NEW REPAIR STRAP 601R-53-22-033-1 IAW REO 601R-53-22-033 REV -D DATE 2014/02/17 REPAIR TYPE 1 FOR FASTENER CALL OUT
- [SDR A6WA202212138410](https://openairdocs.org/sdr/A6WA202212138410.md): Skin · none · Dec 13, 2022 · N416AW · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > TEMPORARY REPAIR TO FUSELAGE SKIN AT BS 257.75, S15L. DENT MEASURES 0.55" X 0.4" X 0.004" DEPTH - HAS BEEN COMPLIED WITH IAW EA AWAC-CRJ253-01543. PERFORMED PERMANENT REPAIR AS REQUIRED ****AIRCRAFT REMOVED FROM SERVICE**** COMPLIED WITH REO 601R-53-11-3811
- [SDR A6WA202212098403](https://openairdocs.org/sdr/A6WA202212098403.md): Floor Support · corroded · Dec 9, 2022 · N416AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > R/H PRESSURE FLOOR SILL HAS CORROSION FROM FS 513 TO FS 559. AIRCRAFT REMOVED FROM SERVICE. REPAIRED PRESSURE FLOOR SILL REF REO 601R-53-41-3104 REV -.
- [SDR A6WA202212088398](https://openairdocs.org/sdr/A6WA202212088398.md): Floor Support · corroded · Dec 8, 2022 · N416AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > L/H PRESSURE FLOOR SILL CORRODED FROM FS 439 TO 529. AIRCRAFT REMOVED FROM SERVICE. REPAIRED CORRODED AREA IAW REO 601R-53-41-3103 REV -.
- [SDR A6WA202212078397](https://openairdocs.org/sdr/A6WA202212078397.md): Skin · dented · Dec 7, 2022 · N416AW · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > FUSELAGE DENTED AT BS 605 S21L-22L. AIRCRAFT REMOVED FROM SERVICE. REPAIRED THE SKIN IAW REO 601R-53-61-7913, REV -.
- [SDR A6WA202212068396](https://openairdocs.org/sdr/A6WA202212068396.md): Rib · cracked · Dec 6, 2022 · N416AW · Cndair CL6002B19 · Trailing Edge Flap Control System
  > UPON REMOVAL OF THE INBOARD FLAP SEAL ON THE L/H INBOARD FLAP, A CRACK WAS FOUND ON THE FWD CHERRYMAX HOLE. ***AIRCRAFT REMOVED FROM SERVICE ***** REMOVED AND INSTALLED NEW RIB AT L/H INBOARD FLAP AS PER REO 601R-57-52-2472 REV -- DATED 2022-11-29
- [SDR A6WA202212028395](https://openairdocs.org/sdr/A6WA202212028395.md): Seat Track · corroded · Dec 2, 2022 · N416AW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > 9EA LH PASSENGER SEATS THE STRUCTURE HAS EVIDENCE OF CORROSION (MARKED) ****AIRCRAFT REMOVED FROM SERVICE ***** REPLACED PASSENGER SEAT STRUCTURE REF CRJ200 B/E AEROSPACE, 926-DH124A & 926-DH224A SERIES, CMM 25-26-95
- [SDR A6WA202212028394](https://openairdocs.org/sdr/A6WA202212028394.md): Seat · corroded · Dec 2, 2022 · N416AW · Cndair CL6002B19 · Passenger Compartment Equipment
  > RIGHT PASSENGER SEATS THE STRUCTURE HAS EVIDENCE OF CORROSION. AIRCRAFT REMOVED FROM SERVICE. REPLACED THE SEAT STRUCTURE IAW 926-DH124A & 926-DH224A SERIES, CMM 25-26-95.
- [SDR A6WA202211298392](https://openairdocs.org/sdr/A6WA202211298392.md): Skin · dented · Nov 29, 2022 · N416AW · Cndair CL6002B19 · Trailing Edge Flaps
  > LEFT WING INBD FLAP HAS A DENT INBD BOTTOM SIDE. ACFT REMOVED FROM SERVICE. REPAIRED THE LT INBOARD FLAP LOWER SKIN IAW SRM 57-52-00, REPAIR -3, AND SRM 51-23-00.
- [SDR A6WA202211268391](https://openairdocs.org/sdr/A6WA202211268391.md): Vane · chafed · Nov 26, 2022 · N416AW · Cndair CL6002B19 · Trailing Edge Flaps
  > RIGHT WING INBOARD FLAP THE FLAP VANE CHAFING ON THE TOP INBOAD TRAILING EDGE. ACFT REMOVED FROM SERVICE. REPAIRED THE RT WING INBOARD FLAP VANE REF REO 601R-57-52-2469 REV-.
- [SDR A6WA202211268388](https://openairdocs.org/sdr/A6WA202211268388.md): Vane · chafed · Nov 26, 2022 · N416AW · Cndair CL6002B19 · Trailing Edge Flaps
  > LEFT WING INBOARD FLAP THE FLAP VANE IS CHAFFED ON THE TOP INBOARD TRAILING EDGE. ACFT REMOVED FROM SERVICE. REPAIRED THE LT WING INBOARD FLAP VANE IAW REO 601R-57-52-2469 REV-.
- [SDR A6WA202211258387](https://openairdocs.org/sdr/A6WA202211258387.md): Strap · corroded · Nov 25, 2022 · N416AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > LEFT FLOOR STRAP A BS 559 BETWEEN LBL 47 AND LBL 27 HAD CORROSION. ACFT REMOVED FROM SERVICE. REPLACE THE STRAP.
- [SDR A6WA202201228079](https://openairdocs.org/sdr/A6WA202201228079.md): Idg · faulted · Jan 22, 2022 · N416AW · Cndair CL6002B19 · AC Generator-Alternator
  > IN FLIGHT RECEIVED GEN 1 CAUTION MESSAGE (APU WAS ON MEL), F/O SMELLED BURNED PLASTIC MOMENTARILY C/W QRH GEN 1 MESSAGE PERSISTED. TURNED GEN 1 TO OFF/RESET. MESSAGES RECEIVED: L WINDSHIELD & L WINDOW CAUTION, CW QRH MESSAGES CLEARED. ***AIRCRAFT REMOVED FR
- [SDR A6WA202103127712](https://openairdocs.org/sdr/A6WA202103127712.md): Reservoir · malfunctioned · Mar 11, 2021 · N416AW · Cndair CL6002B19 · Hydraulic Reservoir, Main
  > OPEN WARNING MESSAGE. CW QRH. ON HYD SYNOPTIC PAGE, #3 SYS SHOWED 300PSI, 70% QUANTITY AND BOTH HYD PUMP OFF. SYS 3 HYD SWITCHES SET FOR TAKEOFF. WITH FLAPS SET TO 8D DEGREES. PUMP CB'S WERE IN. AT GATE, QUANTITY SHOWS 70%. NO OBVIOUS SIGNS OF LEAKS NOTE
- [SDR A6WA202101047509](https://openairdocs.org/sdr/A6WA202101047509.md): Skin · cracked · Dec 31, 2020 · N416AW · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > FS 220 RIGHT SIDE EXTERNAL SKIN CRACKED AFT OF NOSE GEAR CUT OUT RADIUS. AIRCRAFT REMOVED FROM SERVICE. REPAIRED FUSELAGE EXTERNAL SKIN FS 220.00 RIGHT SIDE AFT OF NOSE GEAR CUT OUT, IAW MHI RJ AVIATION REO 601R-53-11-3647.
- [SDR A6WA202012237495](https://openairdocs.org/sdr/A6WA202012237495.md): Structure · corroded · Dec 22, 2020 · N416AW · Cndair CL6002B19 · Fuselage Main, Structure
  > T-CAP EXTRUSION ON LBL 27, FS 559+118 TO FS 621 IS CORRODED BEYOND LIMITS. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED T-CAP EXTRUSION ON LBL 27, FS 559+118 TO FS 621.
- [SDR A6WA202012187467](https://openairdocs.org/sdr/A6WA202012187467.md): Seat Track · corroded · Dec 17, 2020 · N416AW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > RT SIDEWALL SEAT TRACK FROM FS 559 TO FS 559+64 CORRODED. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED RT SIDEWALL SEAT TRACK FROM FS 559 TO FS 559+64.
- [SDR A6WA202012187469](https://openairdocs.org/sdr/A6WA202012187469.md): Seat Track · corroded · Dec 17, 2020 · N416AW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > LBL 9, FLOOR SEAT TRACK FS 364 THRU FS 409 CORRODED BEYOND LIMITS. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED SEAT TRACK AT LBL 9, FS 364 THRU FS 409.
- [SDR A6WA202012187466](https://openairdocs.org/sdr/A6WA202012187466.md): Seat Track · corroded · Dec 17, 2020 · N416AW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK CORROSION AT RBL 9, FS 559+64. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED SEAT TRACK AT RBL 9, FS 559+64.
- [SDR A6WA202012187468](https://openairdocs.org/sdr/A6WA202012187468.md): Seat Track · corroded · Dec 17, 2020 · N416AW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > RBL 9, FLOOR SEAT TRACK FS 364 THRU FS 409 CORRODED BEYOND LIMITS. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED FLOOR SEAT TRACK AT RBL 9, FS 364 THRU FS 409.
- [SDR A6WA20190416562](https://openairdocs.org/sdr/A6WA20190416562.md): Display · failed · Apr 15, 2019 · N416AW · Cndair CL6002B19 · Central Display
  > ON ARRIVAL, BOTH MFD'S FAILED, ONCE SHUTDOWN AT GATE, MFD #2 CAME BACK. (INFLIGHT AT 10000FT FAILURE OCCURRED).
- [SDR A6WA2019030546451](https://openairdocs.org/sdr/A6WA2019030546451.md): Flap · failed · Mar 3, 2019 · N416AW · Cndair CL6002B19 · Trailing Edge Flap Control System
  > RECEIVED FLAP FAIL CAUTION MESSAGE ON APPROACH WHILE SELECTING FLAPS 45. FLAPS FAILED AT 33 DEGREES.
- [SDR A6WA2019020246355](https://openairdocs.org/sdr/A6WA2019020246355.md): Drag Angle · cracked · Feb 1, 2019 · N416AW · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR AFT DRAG ANGLE CRACKED.
- [SDR A6WA2019013146349](https://openairdocs.org/sdr/A6WA2019013146349.md): Stringer · corroded · Jan 30, 2019 · N416AW · Cndair CL6002B19 · Fuselage Main, Longeron/Stringer
  > STRINGER 26R IS CORRODED BETWEEN F.S.319 AND F.S.349.
- [SDR A6WA2019013146350](https://openairdocs.org/sdr/A6WA2019013146350.md): Structure · gouged · Jan 30, 2019 · N416AW · Cndair CL6002B19 · Trailing Edge Flaps
  > R/H INBD FLAP, OUTBD HINGE BOX IS GOUGED ON INBD SIDE OF OUTBD LUG WHERE FLAP ATTACHES TO HINGE BOX.
- [SDR A6WA2019012946342](https://openairdocs.org/sdr/A6WA2019012946342.md): Frame · corroded · Jan 28, 2019 · N416AW · Cndair CL6002B19 · Fuselage Main, Frame
  > FS 319 IS CORRODED AT STR 26R.
- [SDR A6WA2019012846340](https://openairdocs.org/sdr/A6WA2019012846340.md): Frame · corroded · Jan 27, 2019 · N416AW · Cndair CL6002B19 · Fuselage Main, Frame
  > FS 310.00 LOWER FRAME SEGMENT IS CORRODED AT STRINGER 26R.
- [SDR A6WA2019012846329](https://openairdocs.org/sdr/A6WA2019012846329.md): Bulkhead · cracked · Jan 24, 2019 · N416AW · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > INDICATIONS NOTED AT FS 621 REAR PRESSURE BULKHEAD FWD FACE AT LBL18 WL131.9.9" IN LENGTH AND 55% FSH. AT LBL27.5 WL131 2.9" LONG AND 100% FSH. AT LBL 27.5 WL 105 1.25" LONG AND 78% FSH. ALL FAIL NDT.
- [SDR A6WA2019012446325](https://openairdocs.org/sdr/A6WA2019012446325.md): Skin · dented · Jan 24, 2019 · N416AW · Cndair CL6002B19 · Trailing Edge Flaps
  > LEFT WING I/B FLAP LOWER SKIN DENTED WITH CREASE THROUGH DENT WS 70.00 DENT APPROX..300" X.250" X.025" DEEP.
- [SDR A6WA2019020646370](https://openairdocs.org/sdr/A6WA2019020646370.md): Former · corroded · Jan 22, 2019 · N416AW · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR FWD FORMER IS CORRODED UNDER PANEL 832HL.
- [SDR A6WA2019012146314](https://openairdocs.org/sdr/A6WA2019012146314.md): Support Angle · cracked · Jan 20, 2019 · N416AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > LT WINDSHIELD SUPPORT ANGLE IS CRACKED BETWEEN FS 220.00 AND FS 235.00 BETWEEN STGR 11L TO 14L.
- [SDR A6WA2018102546123](https://openairdocs.org/sdr/A6WA2018102546123.md): Bulkhead · cracked · Oct 13, 2018 · N416AW · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > DURING SCHEDULED INSP OF AFT PRESS BULKHEAD FS621. FOUR CRACKS WERE DISCOVERED DURING EDDY CURRENT, 8 DAMAGED RIVETS DURING VISUAL, AND 7 TOOLING MARKS DURING VISUAL.
- [SDR A6WA201845541](https://openairdocs.org/sdr/A6WA201845541.md): Windshield · cracked · Jan 4, 2018 · N416AW · Cndair CL6002B19 · Flight Compartment Windows
  > FO WINDSHIELD CRACKED AT 21,200'. C/W QRH. RETURNED TO CAE, LANDING OVERWEIGHT AT 48,240 LBS. LANDING WAS SMOOTH.
- [SDR A6WA201745078](https://openairdocs.org/sdr/A6WA201745078.md): Apu · shutdown · Jul 1, 2017 · N416AW · Cndair CL6002B19 · APU Cowling/Containment
  > 4108 APU AUTO SHUT DOWN ON GROUND WITH ASSOCIATED FUEL SMELL. REPLACED THE APU.
- [SDR A6WA2017010444725](https://openairdocs.org/sdr/A6WA2017010444725.md): Floor Support · corroded · Jan 3, 2017 · N416AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FLOOR SUPPORT HAS LIGHT CORROSION SPOTS ON THE TOP AND BOTTOM SIDE BETWEEN BS 574 - 601.00 IN THE CARGO BAY. REPAIRED IAW EA AWAC-CRJ253-00609 REV-IR.
- [SDR A6WA201744726](https://openairdocs.org/sdr/A6WA201744726.md): Doubler · cracked · Jan 3, 2017 · N416AW · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > INTERNAL DOUBLER COMMON TO UPPER BEACON LIGHT INSTALLATION IS CRACKED
- [SDR A6WA2017010444723](https://openairdocs.org/sdr/A6WA2017010444723.md): Pulley Bracket · damaged · Jan 3, 2017 · N416AW · Cndair CL6002B19 · Fuselage Main, Structure
  > TWO INBD BOLT HOLES FOR LANDING GEAR ALTERNATE EXTENTION PULLEY BRACKET ARE ELONGATED AT LBL 12 POST BS 280.00. REPAIRED IAW REO 601R-53-11-300- REV --.
- [SDR A6WA2017010344721](https://openairdocs.org/sdr/A6WA2017010344721.md): Floorbeam · corroded · Jan 2, 2017 · N416AW · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > 1013785-1000-0065 - FLOORBEAM AT FS 280 IS CORRODED BTW RBL 9 AND LBL 9
- [SDR A6WA2017010344720](https://openairdocs.org/sdr/A6WA2017010344720.md): Floor Support · corroded · Jan 2, 2017 · N416AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > MAIN CABIN FLOOR SUPPORT CORRODED LBL43 BS 349-408.
- [SDR A6WA2017010344717](https://openairdocs.org/sdr/A6WA2017010344717.md): Fitting · corroded · Dec 31, 2016 · N416AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > SERVICE DOOR LOWER SILL FITTING IS CORRODED
- [SDR A6WA2017010344716](https://openairdocs.org/sdr/A6WA2017010344716.md): Angle · corroded · Dec 31, 2016 · N416AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > SERVICE DOOR CUT-OUT SILL HAS AREAS OF CORROSION FROM BS 319 - 349
- [SDR A6WA2016123044712](https://openairdocs.org/sdr/A6WA2016123044712.md): Bulkhead · gouged · Dec 30, 2016 · N416AW · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > FORWARD FACE OF THE AFT PRESSURE BULKHEAD HAS SEVEN AREAS THAT ARE GOUGED. REPAIRED THE PRESSURE BULKHEAD IAW GREO 601R-53-61-2155 REV-A AND REO 601R-53-61-5895.
- [SDR A6WA2016010344713](https://openairdocs.org/sdr/A6WA2016010344713.md): Frame · corroded · Dec 30, 2016 · N416AW · Cndair CL6002B19 · Fuselage Main, Frame
  > FRAME BS 605 HAS CORROSION ON THE FWD AND AFT SIDE, BETWEEN STRINGER 20 AND 23L.
- [SDR A6WA2016123044711](https://openairdocs.org/sdr/A6WA2016123044711.md): Skin · dented · Dec 30, 2016 · N416AW · Cndair CL6002B19 · Trailing Edge Flaps
  > LEFT INBOARD FLAP LOWER SKIN HAS MULTIPLE DENTS BELOW INBD LOWER ACCESS PANEL. REPAIRED THE LT WING TE FLAP LOWER SKIN IAW REO 601R-57-52-1544.

Next page: https://openairdocs.org/aircraft/N416AW/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 = 'N416AW' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N416AW/reports

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