# Service difficulty reports: N446AW

A list on [N446AW](https://openairdocs.org/aircraft/N446AW.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 · 186 reports

- [SDR A6WA202203088120](https://openairdocs.org/sdr/A6WA202203088120.md): None · none · Mar 8, 2022 · N446AW · Cndair CL6002B19 · Stabilizer Position Indicating
  > DURING CLIMB OUT RECEIVED STAB TRIM AND MACH TRIM CAUTION MESSAGES. ALSO RECEIVED AP PITCH TRIM CAUTION MSG. DISCONNECTED AP. C/W QRH. MESSAGES REMAINED. AIR RETURN TO DAY. LANDED UNDER 47000 LBS. ***AIRCRAFT REMOVED FROM SERVICE **** R&R CA PITCH T
- [SDR A6WA202111167972](https://openairdocs.org/sdr/A6WA202111167972.md): None · none · Nov 15, 2021 · N446AW · Cndair CL6002B19 · Steering Unit
  > ON TAKE OFF RECEIVED STEERING INOP AND WOW INPUT CAUTION MESSAGES CYCLED NOSE WHEEL STEERING MESSAGE REMAINS. AFTER GEAR DEPLOY WOW INPUT MESSAGE CLEARED. ***AIRCRAFT REMOVED FROM SERVICE*** MX IN PROGRESS AFTER GEAR RETRACTION RECIEVED NWS INOP CAUTION MS
- [SDR A6WA202107207833](https://openairdocs.org/sdr/A6WA202107207833.md): Wire · broken · Jul 19, 2021 · N446AW · Cndair CL6002B19 · Equipment/Furnishings Wiring
  > 20 MINUTES INTO FLT, AT FL 250. NOTED RT PACK AT MINUS 31 DEG C. A MINUTE LATER GOT A SMOKE TOILET CAUTION MSG. CW QRH, SMOKE MSG WENT OUT. CONTINUED WITH THE FLT. FA REPORTED THAT THE HAZE SEEMED CENTERED IN LAV. HAZE CLEARED AFTER QRH, BREAKERS PULLED. LA
- [SDR A6WA202102197660](https://openairdocs.org/sdr/A6WA202102197660.md): Warning Message · false activation · Feb 17, 2021 · N446AW · Cndair CL6002B19 · Central Warning
  > WHILE AT CRUISE AT 10,000 FT, RECEIVED DISPLAY COOL CAUTION MESSAGE, COMPLIED WITH QRH, MESSAGE DID NOT CLEAR. ON DESCENT, CLEARED AT 8,000 FT. AIRCRAFT REMOVED FROM SERVICE. PERFORMED OPS CHECK OF PILOT DISPLAY REVISION SWITCH PANEL AND CO-PILOT IAW CRJ
- [SDR A6WA202010147323](https://openairdocs.org/sdr/A6WA202010147323.md): Tee Fitting · corroded · Oct 14, 2020 · N446AW · Cndair CL6002B19 · Fuselage Main, Attach Fittings
  > LBL 27 T-CAP EXTRUSION HAS CORROSION ON THE NUT PLATES AND SURROUNDING AREA. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED T-CAP LBL 27.
- [SDR A6WA202010147321](https://openairdocs.org/sdr/A6WA202010147321.md): Seat Track · corroded · Oct 14, 2020 · N446AW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > RBL 9, FS 484 TO FS 559 HAS CORROSION ON SEAT TRACK. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED SEAT TRACK RBL 9, FS 484 TO FS 559 +80.
- [SDR A6WA202010147322](https://openairdocs.org/sdr/A6WA202010147322.md): Seat Track · corroded · Oct 14, 2020 · N446AW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > RBL 9, FS 559+80 TO FS 559+88 HAS CORROSION ON SEAT TRACK. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED SEAT TRACK AT RBL 9 FS 559+80 TO FS 559+88.
- [SDR A6WA202010147320](https://openairdocs.org/sdr/A6WA202010147320.md): Seat Track · corroded · Oct 14, 2020 · N446AW · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > RIGHT INBOARD SEAT TRACK CORRODED AT FS 474 AND FS 551, RBL 9. AIRCRAFT REMOVED FROM SERVICE. REMOVED CORRODED SEAT TRACK AND REPLACED WITH NEW SEAT TRACK AT FS 474 AND 551, IAW REO 601R-53-00-764.
- [SDR A6WA202010307376](https://openairdocs.org/sdr/A6WA202010307376.md): Bulkhead Web · dented · Oct 12, 2020 · N446AW · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > MULTIPLE SCRIBE AND DENTS FOUND OF AFT PRESSURE BULKHEAD LBL 27.5+25 TO OUTBOARD OF CARGO DOOR ENTRANCE WL 93.5 TO WL 132.43 BEHIND CARGO DOOR TRACK. AIRCRAFT REMOVED FROM SERVICE. ACCOMPLISHED REPAIR AT BULKHEAD LBL 27.5+25 OUTBOARD CARGO DOOR ENTRANCE WL 9
- [SDR A6WA202010307374](https://openairdocs.org/sdr/A6WA202010307374.md): Bulkhead Web · cracked · Oct 12, 2020 · N446AW · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > CRACK DETECTED ON AFT PRESSURE BULKHEAD WEB FWD FACE AT BL 0.0, 36" ABOVE FLOOR. CRACK IS 2". AIRCRAFT REMOVED FROM SERVICE. REMOVED DAMAGE AND INSTALLED REPAIR AT BL 0.0, IAW REO 601R-53-61-1285.
- [SDR A6WA202010307375](https://openairdocs.org/sdr/A6WA202010307375.md): Bulkhead Web · cracked · Oct 12, 2020 · N446AW · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > CRACK DETECTED ON AFT PRESSURE BULKHEAD WEB FWD FACE AT LBL 27.50 DIRECTLY ABOVE THE UPPER DOOR TRACK, L SHAPED CRACK 0.5"X0.5". AIRCRAFT REMOVED FROM SERVICE. ACCOMPLISHED REPAIR AT BULKHEAD LBL 27.50 ABOVE UPPER DOOR TRACK, IAW REO 601R-53-61-7467 601R-53-
- [SDR A6WA2019122347079](https://openairdocs.org/sdr/A6WA2019122347079.md): Amplifier · malfunctioned · Dec 21, 2019 · N446AW · Cndair CL6002B19 · Fuel Control/Turbine Engines
  > AFTER DEPARTING IAD THE CREW ADVISED DISPATCH THEY WERE RETURNING TO IAD WITH AN ENGINE ISSUE. NO OTHER INFORMATION AVAILABLE AT THIS TIME. LOSS OF POWER UP TO 3% ON TAKE OFF ROLL AND INITIAL CLIMB- AT 10K POWER LOS(N1) EXCEEDED 10% RIGHT ENGINE. AIRCRAFT RE
- [SDR A6WA2019060446644](https://openairdocs.org/sdr/A6WA2019060446644.md): Warning System · false activation · May 10, 2019 · N446AW · Cndair CL6002B19 · Landing Gear Position and Warning
  > AFTER LANDING GEAR SELECTED UP, RECEIVED A/SKID I/B CAUTION, GEAR DISAGREE WARNING LMLG/NLG & PARK BRAKE SOV CAUTION. R MLG GREEN INDICATION ONLY. SELECTED GEAR DOWN, RECEIVED ALL GREEN LIGHTS. ALL MESSAGES CLEARED ON GEAR DOWN SELECTION. PERFORMED AIR RETURN
- [SDR A6WA2019031146459](https://openairdocs.org/sdr/A6WA2019031146459.md): Web · cracked · Mar 8, 2019 · N446AW · Cndair CL6002B19 · Passenger/Crew Doors
  > PASSENGER DOOR AFT WEB IS BUCKLED AND CRACKED.
- [SDR A6WA2019031146461](https://openairdocs.org/sdr/A6WA2019031146461.md): Step · bent · Mar 8, 2019 · N446AW · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR LOWER MID STEP IS BENT/BUCKLED.
- [SDR A6WA2019031146460](https://openairdocs.org/sdr/A6WA2019031146460.md): Drag Angle · cracked · Mar 8, 2019 · N446AW · Cndair CL6002B19 · Passenger/Crew Doors
  > PASSENGER DOOR AFT DRAG ANGLE IS CRACKED AT POWER ASSIST MOTOR PULLEY BRACKET.
- [SDR A6WA2019020846374](https://openairdocs.org/sdr/A6WA2019020846374.md): Flap System · malfunctioned · Feb 7, 2019 · N446AW · Cndair CL6002B19 · Trailing Edge Flap Control System
  > AT FLIGHT LEVEL 27,000 RECEIVE FLAP FAIL CAUTION WITH FLAPS AT ZERO DEGREES. NO FLAP SELECTIONS WERE MADE. CREW DECLARED AN EMERGENCY LANDING WITH IAD TOWER. ONCE AT THE GATE THE CREW CALLED MAINTENANCE CONTROL. THE FLAPS WERE SUCCESSFULLY RESET PER FIM SUPPLE
- [SDR A6WA2018072445948](https://openairdocs.org/sdr/A6WA2018072445948.md): Sensing Element · shorted · Jul 22, 2018 · N446AW · Cndair CL6002B19 · Pneumatic Indicating System
  > IN CLIMB RECEIVED LT 10TH STAGE DUCT WARNING. COMPLIED WITH QRH MSG REMAINS WITH POWER SETTING AT IDLE MSG WAS INTERMITTENT THE REMAINING FLIGHT 10TH STAGE DUCT BETWEEN LT 10TH SOV, LT PACK AND ISOL VALVE IND RED. TROUBLESHOT AND FOUND LEFT 10TH STAGE B LOOP S
- [SDR A6WA2018060545857](https://openairdocs.org/sdr/A6WA2018060545857.md): Cargo Track · corroded · May 29, 2018 · N446AW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > CARGO TRACK CORRODED, BS 614 TO 620, LBL 35. REPLACED THE CARGO TRACK IAE SRM 51-42-06.
- [SDR A6WA2018060545864](https://openairdocs.org/sdr/A6WA2018060545864.md): Fitting · cracked · May 27, 2018 · N446AW · Cndair CL6002B19 · Fuselage Main, Attach Fittings
  > BS 461 FLOOR SUPPORT FITTING WAS CRACKED. REPLACED FITTING IAW SRM 51-41-06, AND 51-42-21.
- [SDR A6WA2018052945852](https://openairdocs.org/sdr/A6WA2018052945852.md): Door Sill · cracked · May 27, 2018 · N446AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > CARGO DOOR SILL CRACKED AT FS 589.00, LBL45. REPAIRED CARGO DOOR SILL AT FS 589.00, LBL45 IAW REO 601R-53-61-433 REV-C.
- [SDR A6WA2018060545856](https://openairdocs.org/sdr/A6WA2018060545856.md): Frame · corroded · May 25, 2018 · N446AW · Cndair CL6002B19 · Fuselage Main, Frame
  > FRAME BS 589 CORRODED BETWEEN STRINGERS 23L AND 23R. REPLACED THE FRAME IAW SRM 53-61-15, 51-42-06, 51-42-21, AND 51-21-11.
- [SDR A6WA2018052945850](https://openairdocs.org/sdr/A6WA2018052945850.md): Retainer · cracked · May 25, 2018 · N446AW · Cndair CL6002B19 · Nacelle/Pylon Miscellaneous Structure
  > PYLON PNL 422BT SEAL RETAINER CRACKED. REPLACED SEAL RETAINER IAW SRM 51-42-06.
- [SDR A6WA2018060545867](https://openairdocs.org/sdr/A6WA2018060545867.md): Skin · cracked · May 24, 2018 · N446AW · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > LEFT TRU DOOR AFT LATCH CUTOUT ON PANEL LANDING WAS CRACKED. REPLACED THE SKIN IAW SRM 51-42-06.
- [SDR A6WA2018060545861](https://openairdocs.org/sdr/A6WA2018060545861.md): Cap · damaged · May 24, 2018 · N446AW · Cndair CL6002B19 · Trailing Edge Flaps
  > RIGHT INBD FLAP VANE INBD END CAP HAD ELONGATED FASTENER HOLES. REPLACED THE END CAP IAW SRM 51-42-13.
- [SDR A6WA2018052945851](https://openairdocs.org/sdr/A6WA2018052945851.md): Fitting · cracked · May 24, 2018 · N446AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FLOOR SUPPORT BATHTUB FITTING AT FS 461.00, LBL9 CRACKED. REPLACED FITTING IAW SRM 51-42-06, 51-42-21, 51-40-11.
- [SDR A6WA2018060545866](https://openairdocs.org/sdr/A6WA2018060545866.md): Skin · damaged · May 22, 2018 · N446AW · Cndair CL6002B19 · Trailing Edge Flaps
  > LEFT INBD FLAP, LOWER INBD SKIN DENTED AND PITTED. REPLACED THE SKIN IAW SRM 51-42-13.
- [SDR A6WA2018060545865](https://openairdocs.org/sdr/A6WA2018060545865.md): Skin · damaged · May 22, 2018 · N446AW · Cndair CL6002B19 · Trailing Edge Flaps
  > RIGHT INBD FLAP LOWER INBD SKIN DENTED AND PITTED. REPLACED THE SKIN IAW SRM 51-42-13.
- [SDR A6WA2018060545863](https://openairdocs.org/sdr/A6WA2018060545863.md): Skin · gouged · May 21, 2018 · N446AW · Cndair CL6002B19 · Trailing Edge Flaps
  > LEFT OTBD FLAP VANE OTBD LE SKIN WAS GOUGED. REPLACED THE VANE SKIN IAW SRM 51-42-13.
- [SDR A6WA2018060545858](https://openairdocs.org/sdr/A6WA2018060545858.md): Doubler · corroded · May 21, 2018 · N446AW · Cndair CL6002B19 · Fuselage Structure (General)
  > BS 280 TO 310, LBL 36 AND RBL 36 TWO DOUBLERS WERE CORRODED. REPLACED DOUBLERS IAW SRM 51-42-13.
- [SDR A6WA2018060545862](https://openairdocs.org/sdr/A6WA2018060545862.md): Doubler · corroded · May 21, 2018 · N446AW · Cndair CL6002B19 · Fuselage Floor Panel
  > BS 310, LBL 18 DOUBLER CORRODED. REPLACED THE DOUBLER IAW SRM 51-42-13.
- [SDR A6WA2018060545859](https://openairdocs.org/sdr/A6WA2018060545859.md): Frame · corroded · May 19, 2018 · N446AW · Cndair CL6002B19 · Fuselage Main, Frame
  > FRAME BS 605 WAS CORRODED FROM STRINGERS 23L TO 23R. REPLACED THE FRAME IAW SRM 53-61-15, 51-42-06, AND 51-42-21.
- [SDR A6WA2018060545860](https://openairdocs.org/sdr/A6WA2018060545860.md): Skin · chafed · May 19, 2018 · N446AW · Cndair CL6002B19 · Trailing Edge Flaps
  > RIGHT INBD FLAP VANE SKIN CHAFED. REPLACED THE SKIN IAW SRM 51-42-13.
- [SDR A6WA201644271](https://openairdocs.org/sdr/A6WA201644271.md): Connector · loose · Aug 28, 2016 · N446AW · Cndair CL6002B19 · Light System Wiring
  > EMERGENCY FLOOR TRACK LIGHTS INOPERATIVE ROW 9-12. INSPECTED EMERGENCY LIGHTS AND FOUND LOOSE CONNECTOR. RESECURED CONNECTOR BY THE LAV AND ADDED SECURITY TAPE TO THAT CONNECTOR REF SUP 13-022. OPS CHECK GOOD.
- [SDR A6WA201644264](https://openairdocs.org/sdr/A6WA201644264.md): Light · inoperative · Aug 26, 2016 · N446AW · Cndair CL6002B19 · Emergency Lighting
  > EMERGENCY FLOOR TRACK LIGHTING ROWS 9-12 WILL NOT ILLUMINATE.
- [SDR A6WA201644255](https://openairdocs.org/sdr/A6WA201644255.md): Light · inoperative · Aug 22, 2016 · N446AW · Cndair CL6002B19 · Emergency Lighting
  > EMERGENCY LIGHTS INOPERATIVE IN CABIN ROW 9-12.
- [SDR A6WA2016080144122](https://openairdocs.org/sdr/A6WA2016080144122.md): Door · binding · Jul 18, 2016 · N446AW · Cndair CL6002B19 · Passenger/Crew Doors
  > PASSENGER DOOR WILL NOT OPEN FROM INSIDE OR OUTSIDE.
- [SDR A6WA2016071944122](https://openairdocs.org/sdr/A6WA2016071944122.md): Seal · lack of lube · Jul 18, 2016 · N446AW · Cndair CL6002B19 · Passenger/Crew Doors
  > PASSENGER DOOR WILL NOT OPEN FROM INSIDE OR OUTSIDE. LUBRICATED PAX DOOR SEAL AS REQUIRED IAW AMM 15-053, OPS CHECKED GOOD.
- [SDR A6WA201643918](https://openairdocs.org/sdr/A6WA201643918.md): Panel · chafed · May 21, 2016 · N446AW · Cndair CL6002B19 · Nacelle/Pylon, Plate/Skin
  > PANEL 422DB HAS THREE EACH CHAFES ON OUTER SURFACE. REPAIRED PANEL 422DB IAW SUPPLEMENT 16-155.
- [SDR A6WA201643917](https://openairdocs.org/sdr/A6WA201643917.md): Cotter Pin · out of position · May 21, 2016 · N446AW · Cndair CL6002B19 · Ailerons
  > LEFT AILERON NR 2 HINGE BOLT COTTER PIN HEAD IS CHAFING ON LE SKIN OF AILERON. REPLACED LE SKIN IAW SRM 51-42-06, 51-42-21. RE-POSITIONED HINGE BOLT COTTER PIN TO PREVENT CONTACT IAW AMM 27-15-01.
- [SDR A6WA201643914](https://openairdocs.org/sdr/A6WA201643914.md): Skin · cracked · May 20, 2016 · N446AW · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > NLG WW CUT OUT AFT LT CORNER IS CRACKED. REPAIRED NLG WW CUT OUT AFT LT CORNER IAW REO 601R-53-11-048 REV D DATED 2015 06 10 & REO 601R-53-11-2906 REV DATED 2016 05 16.
- [SDR A6WA201643899](https://openairdocs.org/sdr/A6WA201643899.md): Floor Support · corroded · May 18, 2016 · N446AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > LBL 9 INBD FLOORBOARD SUPPORT HAS CORROSION FROM FS 589.0 - 608.0.
- [SDR A6WA201643900](https://openairdocs.org/sdr/A6WA201643900.md): Bracket · chafed · May 18, 2016 · N446AW · Cndair CL6002B19 · Wing Miscellaneous Structure
  > LEFT WING LE BRACKET BEHIND LE ACCESS PANEL 530BL IS CHAFED ON INBD & OTBD FLANGES.
- [SDR A6WA201643898](https://openairdocs.org/sdr/A6WA201643898.md): Angle · cracked · May 18, 2016 · N446AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FLOOR SUPPORT ANGLE AT FS 621 CRACKED AT LBL 36.
- [SDR A6WA201643890](https://openairdocs.org/sdr/A6WA201643890.md): Skin · dented · May 14, 2016 · N446AW · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > PERFORM PERMANENT REPAIR TO FUSELAGE SKIN, 2 OFF DENTS BETWEEN LT FS 409+64 - 409+80, STRINGER 18L - 19L. REPAIRED SKIN IAW SRM 53-00-31 REPAIR NR 1 & SRM 53-00-15.
- [SDR A6WA201643888](https://openairdocs.org/sdr/A6WA201643888.md): Intercostal · cracked · May 14, 2016 · N446AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > LEFT SIDE INTERCOSTAL MEMBER AT FS 621.00 - 625.00, STRINGER 13L IS CRACKED. REPLACED INTERCOSTAL IAW SRM 51-42-06 & 51-42-21.
- [SDR A6WA201643889](https://openairdocs.org/sdr/A6WA201643889.md): Intercostal · cracked · May 14, 2016 · N446AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > LEFT SIDE INTERCOSTAL MEMBER AT FS 621.00 - 625.00, STRINGER 14L IS CRACKED. REPLACED INTERCOSTAL IAW SRM 51-42-21, 51-40-11, 53-61-17, 51-42-06 & 51-42-21.
- [SDR A6WA201643885](https://openairdocs.org/sdr/A6WA201643885.md): Frame · cracked · May 13, 2016 · N446AW · Cndair CL6002B19 · Fuselage Main, Frame
  > PASSENGER CABIN FRAME FS 333.000 CRACKED AT TOOLING HOLE, BETWEEN STRINGER 0 & 1L. REPLACED FRAME IAW SRM 51-42-02.
- [SDR A6WA201643887](https://openairdocs.org/sdr/A6WA201643887.md): Seat Track · corroded · May 13, 2016 · N446AW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > RIGHT SIDE WALL SEAT TRACK STICK NR 4 HAS CORROSION, BETWEEN FS 409+112 & 449.85 IN CABIN. REPLACED SEAT TRACK IAW REO 601R-53-00-485, SRM 51-42-02 & SUPPLEMENT 13-074.
- [SDR A6WA201643886](https://openairdocs.org/sdr/A6WA201643886.md): Bracket · cracked · May 13, 2016 · N446AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > RIGHT LOWER CTR WINDSHIELD POST BRACKET CRACKED. REPLACED BRACKET IAW SRM 51-42-21.

Next page: https://openairdocs.org/aircraft/N446AW/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 = 'N446AW' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N446AW/reports

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