# N406AW: Bombardier CL-600-2B19, registration cancelled 2019-06-25

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: June 25, 2019
- Status when cancelled: Valid registration
- Airframe: [Bombardier CL-600-2B19](https://openairdocs.org/model/bombardier-cl-600-2b19) (registry code 1390008)
- Data sheets: [TCDS A21EA-1](https://openairdocs.org/tcds/A21EA-1) (OpenAirDocs)
- Serial number: 7402
- Type of aircraft: Fixed wing multi engine
- Last registry action: June 25, 2019
- Mode S code: A4C300
- Owner when cancelled: [Air Wisconsin Airlines LLC](https://openairdocs.org/faa-owner/AIR%20WISCONSIN%20AIRLINES%20LLC)
- Location: [Appleton, WI](https://openairdocs.org/faa-place/WI/Appleton)
- Owner type: LLC
- Owner's area on the map: 44.2676° N, 88.4990° W: Placed by OpenAirDocs at the center of ZIP code 54914, within about 2 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N406AW
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=406AW
- Page: https://openairdocs.org/deregistered/N406AW-2019-06-25

From the FAA registry file of October 29, 2026, cancelled registrations. Owners' street addresses are left out. The Mode S code belongs to the N-number, not the airframe.

ADs and bulletins for the Bombardier CL-600-2B19: https://openairdocs.org/model/bombardier-cl-600-2b19.md

## Service difficulty reports (161, newest 50)

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.

- [SDR A6WA201543414](https://openairdocs.org/sdr/A6WA201543414), Dec 28, 2015: WIRE HARNESS. DEFECTIVE. STEERING INOPERATIVE CAUTION IN FLIGHT. COMPLIED WITH QRH, MSG PERSISTED. R & R NLG HARNESS & LT ROTARY VOLTAGE DIFFERENTIAL TRANSDUCER. OPERATIONS CHECKED GOOD
- [SDR A6WA201543368](https://openairdocs.org/sdr/A6WA201543368), Dec 16, 2015: WARNING SYSTEM. ACTIVATED. RECEIVED GEAR DISAGREE WARNING ALONG WITH WOW INPUT CAUTION ON CLIMB OUT. TRIED TO RECYCLE GEAR WITH NO CHANGE. LEFT THE GEAR IN DOWN POSITION. GEAR SHOWED DOWN
- [SDR A6WA201543149](https://openairdocs.org/sdr/A6WA201543149), Oct 19, 2015: HANDLE. LACK OF LUBE. PASSENGER DOOR WILL NOT OPEN FROM OUTSIDE. INSPECTED PAX DOOR OUTER HANDLE & CLEARANCES IAW AMM 52-11-03, NO VISUAL DEFECTS NOTED. DOOR WILL NOT OPEN FROM OUTSI
- [SDR A6WA201543048](https://openairdocs.org/sdr/A6WA201543048), Sep 10, 2015: LIGHT. INOPERATIVE. FORWARD FACING EMER EXIT SIGN AT ROW 8, LIGHTS BURNED OUT.
- [SDR A6WA201543042](https://openairdocs.org/sdr/A6WA201543042), Sep 7, 2015: APU. UNKNOWN. FLIGHT 3945, APU WILL NOT START IN THE AIR. HEAVY FUEL ODOR OCCURS AFTER START ON THE GND WITH BOTH PACKS ON. COMPLIED WITH CM ACTION PLACARDED & PLACED ON MEL.
- [SDR A6WA201542620](https://openairdocs.org/sdr/A6WA201542620), Apr 11, 2015: SEAL. FAILED. AT 30,000 FT RECEIVED LOUD NOISE COMING FROM SERVICE DOOR. PRESSURIZATION WAS NORMAL, NO DOOR WARNING INDICATIONS. NOISE COMES FROM LOWER RT SIDE. FLIGHT ATTEND
- [SDR A6WA201341324](https://openairdocs.org/sdr/A6WA201341324), Feb 8, 2015: UNKNOWN. ODOR. WITH PACKS ON THERE IS A STRONG FUEL SMELL IN THE AIRPLANE WITH APU ON.
- [SDR A6WA201442091](https://openairdocs.org/sdr/A6WA201442091), Oct 27, 2014: LIGHT. INOPERATIVE. EMERGENCY FLOOR TRACK LIGHTS ROW 8 - 12 INOPERATIVE.
- [SDR A6WA201442048](https://openairdocs.org/sdr/A6WA201442048), Oct 12, 2014: WARNING SYSTEM. ACTIVATED. DESCENDING THROUGH 20,000' ALL CRTS EXCEPT ED1 & 2 WENT BLANK. FMS WENT BLANK. FMS, FD MAP CAUTION, FMS NOT AVAILABLE. G/S WARNING APPEARED. THROUGH 10,000' APU
- [SDR A6WA201441978](https://openairdocs.org/sdr/A6WA201441978), Sep 17, 2014: LIGHT. INOPERATIVE. FLOOR TRACK EMER LIGHTS 2 - 5 WILL NOT ILLUMINATE.
- [SDR A6WA201441902](https://openairdocs.org/sdr/A6WA201441902), Aug 27, 2014: TRIM SYSTEM. OUT OF ADJUST. ON DEPARTURE LEVELING OFF AT 8,000 FT UNCOMMANDED FULL RT RUDDER TRIM. AUTO PILOT HAD BEEN ENGAGED FOR 2 MINUTES. COMPLIED WITH QRH DISCONNECTED AUTO PILOT & YA
- [SDR A6WA201441592](https://openairdocs.org/sdr/A6WA201441592), May 26, 2014: MOUNT BRACKET. CRACKED. FWD LT NOSE HYD COMPARTMENT BRAKE ACCUMULATOR FWD OTBD MOUNT BRACKET CRACKED. R & R WITH SERVICEABLE PART, PN 601R75250-55 IAW SRM 51-40-11 & 51-42-21.
- [SDR A6WA201441590](https://openairdocs.org/sdr/A6WA201441590), May 25, 2014: FLOOR SUPPORT. CORRODED. LBL 27 FLOORBEAM CAP CORRODED AROUND NUTPLATE HOLES, FS 574 TO 621. R & R FLOORBEAM CAP WITH SERVICEABLE SECTION IAW SRM 51-40-11 & 51-42-21.
- [SDR A6WA201441571](https://openairdocs.org/sdr/A6WA201441571), May 23, 2014: DOOR SILL. CORRODED. PAX DOOR LWR SILL IS CORRODED BETWEEN FS 315 TO FS 344. R & R WITH NEW SERVICEABLE SILL ANGLE IAW SRM 51-41-02, 51-42-06 & 51-42-13.
- [SDR A6WA201441572](https://openairdocs.org/sdr/A6WA201441572), May 23, 2014: SKIN. CHAFED. LEFT INBD FLAP VANE LE SKIN IS CHAFED AT 3 LOCATIONS. REMOVED & REPLACED INBD & CTR FLAP VANE LE SKIN IAW SRM 51-42-13 & 51-40-11.
- [SDR A6WA201441573](https://openairdocs.org/sdr/A6WA201441573), May 22, 2014: DOOR FRAME. CRACKED. PAX DOOR AFT FRAME AT FS 338 IS CRACKED UNDER PREVIOUS REPAIR. REMOVED CRACKED FRAME & REPLACED WITH NEW SERVICEABLE FRAME IAW REO 601R-52-11-402 REV H.
- [SDR A6WA201441588](https://openairdocs.org/sdr/A6WA201441588), May 20, 2014: MOUNT BRACKET. CRACKED. EXTERNAL SERVICES PANEL ASSEMBLY UPPER MOUNT BRACKET CRACKED. R & R EXTERNAL SERVICES PANEL UPPER MOUNT BRACKET WITH SERVICEABLE PART, PN 601R51590-13 IAW SRM 5
- [SDR A6WA201441560](https://openairdocs.org/sdr/A6WA201441560), May 18, 2014: FITTING. CORRODED. RIGHT WINDSCREEN LWR FITTINGS HAVE CORROSION ON LWR SIDE. R & R UNSERVICEABLE FITTINGS & INSTALLED NEW SERVICEABLE FITTINGS IAW SRM 51-41-02.
- [SDR A6WA201441587](https://openairdocs.org/sdr/A6WA201441587), May 17, 2014: SKIN. DAMAGED. COMPLIED WITH CARD 4DMI16358 REPAIR LT ELEVATOR DAMAGE NR 12 & 13 601R-51-00-293. PERFORMED PERMANENT REPAIR IAW SRM 55-20-00 FIG 204.
- [SDR A6WA201441565](https://openairdocs.org/sdr/A6WA201441565), May 17, 2014: CLEAT. CORRODED. PAX DOOR LWR SILL FWD & AFT CLEATS ARE CORRODED. REMOVED FWD & AFT CLEATS ON LWR PAX DOOR SILL & INSTALLED NEW SERVICEABLE CLEATS IAW SRM 51-42-06.
- [SDR A6WA201441574](https://openairdocs.org/sdr/A6WA201441574), May 16, 2014: SKIN. GOUGED. UPPER SURFACE OF LWR WING PLANK IS GOUGED AT WS 88.5. REPAIRED GOUGED UPPER SURFACE OF LWR WING PLANK IAW REO 601R--57-21-2192 DATED 5-21-14.
- [SDR A6WA201441589](https://openairdocs.org/sdr/A6WA201441589), May 16, 2014: FRAME. CORRODED. LOWER SECTION OF FS 605 FRAME HAS CORROSION. REPAIRED FRAME FS 605 IAW EA 15-2014-122 REV C DATED 5/24/2014.
- [SDR A6WA201441561](https://openairdocs.org/sdr/A6WA201441561), May 16, 2014: CLEAT. CORRODED. SERVICE DOOR CUT OUT THRESHOLD CLEATS HAVE CORROSION ATTACHED FASTENERS. REMOVED CORRODED FASTENERS & INSTALLED NEW SERVICEABLE FASTENERS IAW AMM 20-24-00.
- [SDR A6WA201441558](https://openairdocs.org/sdr/A6WA201441558), May 16, 2014: RIB. CRACKED. LEFT BATTERY RIB CRACKED ON FWD END. REMOVED CRACKED RIB & INSTALLED SERVICEABLE BATTERY RIB IAW REO 601R-57-51-046 REV B.
- [SDR A6WA201441591](https://openairdocs.org/sdr/A6WA201441591), May 15, 2014: HOUSING. CHAFED. SERVICE DOOR HANDLE HOUSING CHAFED. R & R HANDLE HOUSING WITH SERVICEABLE PART, PN 119935-1 IAW SRM 51-40-11 & 51-42-21.
- [SDR A6WA201441562](https://openairdocs.org/sdr/A6WA201441562), May 15, 2014: FITTING. CRACKED. CLIPS AT FS 280 & STRINGER 3L CRACKED. REMOVED UNSERVICEABLE CLIP & INSTALLED SERVICEABLE CLIP IAW SRM 51-42-06, 51-41-02, 51-42-06 & 51-42-21.
- [SDR A6WA201441559](https://openairdocs.org/sdr/A6WA201441559), May 15, 2014: FITTING. CRACKED. CLIP AT FS 280 & STRINGER 3L CRACKED. REMOVED CRACKED CLIP & INSTALLED SERVICEABLE CLIP IAW SRM51-41-11 & 51-41-02.
- [SDR A6WA201441553](https://openairdocs.org/sdr/A6WA201441553), May 14, 2014: ANGLE. CRACKED. LEFT & RIGHT OBLIQUE ANGLES IN AEB ARE CRACKED. R & R CRACKED RT OBLIQUE ANGLE WITH NEW SERVICEABLE ANGLE IAW SRM 51-40-11 & 51-42-21. SEE W C 54596-3000-0004 F
- [SDR A6WA201441549](https://openairdocs.org/sdr/A6WA201441549), May 14, 2014: DRAG ANGLE. CRACKED. LEFT DRAG ANGLE COMMON TO BATTERY RIB CRACKED AT AFT END. R & R CRACKED LT DRAG ANGLE WITH NEW SERVICEABLE DRAG ANGLE IAW SRM 51-42-21, 51-40-11 & 51-25-16.
- [SDR A6WA201441548](https://openairdocs.org/sdr/A6WA201441548), May 14, 2014: DRAG ANGLE. CRACKED. PAX DOOR DRAG ANGLE FWD OF POWER ASSIST PULLEY BRACKET IS CRACKED. REPAIRED PAX DOOR DRAG ANGLE IAW REO 601R-52-11-513 REV A.
- [SDR A6WA201441547](https://openairdocs.org/sdr/A6WA201441547), May 14, 2014: SKIN. CRACKED. EXTERNAL LWR FUSELAGE SKIN AT AFT NLG CUT OUT ON BOTH LT & RT CORNERS ARE CRACKED. REPAIRED NLG WW CUT OUT IAW REO 601R-53-11-048 REV C 10-1-08.
- [SDR A6WA201441554](https://openairdocs.org/sdr/A6WA201441554), May 13, 2014: ATTACH FITTING. CORRODED. SERVICE DOOR FWD SILL ATTACH AT FRAME IS CORRODED. R & R WITH NEW SERVICEABLE PART IAW SRM 51-42-21.
- [SDR A6WA201441552](https://openairdocs.org/sdr/A6WA201441552), May 13, 2014: ANGLE. CRACKED. LEFT LWR OBLIQUE ANGLE CRACKED ON AFT SIDE OF 621 BULKHEAD. R & R LWR OBLIQUE ANGLE WITH NEW SERVICEABLE ANGLE IAW SRM 51-42-21.
- [SDR A6WA201441551](https://openairdocs.org/sdr/A6WA201441551), May 13, 2014: DRAG ANGLE. CRACKED. RIGHT DRAG ANGLE COMMON TO BATTERY RIB IS CRACKED. R & R RT DRAG ANGLE IAW SRM 51-42-21.
- [SDR A6WA201441550](https://openairdocs.org/sdr/A6WA201441550), May 13, 2014: MOUNT BRACKET. CRACKED. EXTERNAL SERVICE PANEL 122CR CUT OUT LWR MOUNT BRACKET FOR SERVICE BOX CRACKED. REMOVED CRACKED MOUNT BRACKET & INSTALLED NEW BRACKET IAW SRM 51-42-13 & 51-40-1
- [SDR A6WA201441600](https://openairdocs.org/sdr/A6WA201441600), May 11, 2014: POST. CRACKED. VERTICAL POST AT RBL 18 ON FS 409+128 BULKHEAD IS CRACKED AT LOWER END, OTBD AFT FLANGE. REPAIRED RBL 18 OTBD POST AT FS 409+128 IAW REO 601R-53-41-056 REV F DA
- [SDR A6WA201441586](https://openairdocs.org/sdr/A6WA201441586), May 11, 2014: SKIN. DENTED. LEFT ELEVATOR HAS 4 DENTS ON LOWER SURFACE. REPAIRED 2 DENTS IAW SRM 55-20-00 FIG 204 & FOUND 2 DENTS TO BE IN LIMITS IAW SRM 55-20-00 FIG 101.
- [SDR A6WA201441543](https://openairdocs.org/sdr/A6WA201441543), May 11, 2014: SEAT TRACK. CORRODED. CABIN NR 1 FLOOR SEAT TRACK CORRODED AT FWD END OF LBL 9 FS 364.00. REMOVED CORRODED SEAT TRACK & REPLACED WITH NEW SERVICEABLE SEAT TRACK IAW AMM 53-01-11.
- [SDR A6WA201441542](https://openairdocs.org/sdr/A6WA201441542), May 11, 2014: SEAT TRACK. CORRODED. CABIN NR 1 FLOOR SEAT TRACK CORRODED AT FWD END RBL 9 AT FS 364.00. REMOVED CORRODED FLOOR SEAT TRACK & REPLACED WITH NEW SERVICEABLE FLOOR SEAT TRACK IAW SRM 5
- [SDR A6WA201441544](https://openairdocs.org/sdr/A6WA201441544), May 10, 2014: SEAT TRACK. CORRODED. SEAT TRACK AFT OF 9G TIE DOWN AT FS 559+112 HAS CORROSION AROUND FASTENERS HOLES. REMOVED UNSERVICEABLE SEAT TRACK & INSTALLED A NEW SERVICEABLE TRACK IAW SRM 5
- [SDR A6WA201441541](https://openairdocs.org/sdr/A6WA201441541), May 10, 2014: ANGLE. CORRODED. FS 280.00 FLOOR ANGLES CORRODED & RBL 9 OTBD CLIP CRACKED. REPAIRED FWD 7 AFT FLOOR ANGLES AT FS 280 RBL 9 - LBL9. R & R OTBD CLIP AT FS 280 & RBL 9 IAW SRM 51-
- [SDR A6WA201441113](https://openairdocs.org/sdr/A6WA201441113), Feb 6, 2014: APU. SHUTDOWN. TURNED APU GENERATOR ON, APU AUTO SHUTDOWN. HEAVY SMELL OF JET FUEL & SMOKE FROM EXHAUST. ACTION TAKEN IN PROGRESS. 
- [SDR A6WA201312104046](https://openairdocs.org/sdr/A6WA201312104046), Dec 8, 2013: FUEL SYS. LEAKING. 3847 WITH PACKS ON THERE IS A STRONG FUEL SMELL IN THE AIRPLANE WITH APU ON. FOUND FUEL LEAK BY FUEL CONTROL. R, OPERATIONS & LEAK CHECKED GOOD AT THIS TIME NO 
- [SDR A6WA201303014018](https://openairdocs.org/sdr/A6WA201303014018), Mar 1, 2013: WARNING SYSTEM. ACTIVATED. FLAPS FAIL CAUTION MSG DURING RETRACTION AFTER LANDING. PERFORMED FLAP RESET PROCEDURE IAW AWAC SUP 98-18E BOX 12. FLAPS RESET. PLACARD AND PLACED ON MEL.
- [SDR A6WA201301234011](https://openairdocs.org/sdr/A6WA201301234011), Jan 23, 2013: WINDSHIELD. DAMAGED. IN FLIGHT SAW SPARKING AND MELTING ON LEFT WINDSHIELD. COMPLIED WITH QRH. TURNED WINDSHIELD HEAT OFF, SPARKS STOPPED. COORDINATED WITH DISPATCH AND ATC, RETURNE
- [SDR A6WA201240805](https://openairdocs.org/sdr/A6WA201240805), Aug 15, 2012: BPSU. FAILED. FLAPS FAILED WHEN SELECTED 20-30. FLAPS STAYED AT 20 DEGREES. REPLACED RT BPSU PER 27 51 OPS CK GOOD.
- [SDR A6WA201240772](https://openairdocs.org/sdr/A6WA201240772), Aug 14, 2012: BPSU. FAILED. FLAPS FAILED IN FLT AT 20 DEGREES WHEN 30 DEGREES WAS SELECTED. PERFORMED FLAP RESET PROCEDURE IAW SUPPLEMENT 98-18E BOX 12, FLAPS RESET. FOUND REPEAT BPSU FAUL
- [SDR A6WA201240645](https://openairdocs.org/sdr/A6WA201240645), Jun 30, 2012: WARNING MESSAGE. FALSE ACTIVATION. CARGO BOTTLE LOW CAUTION MESSAGE IN FLIGHT, NO INDICATION OF FIRE/SMOKE. INSPECTED CARGO BAY, NO EVIDENCE OF FIRE/SMOKE. NO BOTTLE DISCHARGE.
- [SDR A6WA201240535](https://openairdocs.org/sdr/A6WA201240535), May 11, 2012: PANEL. CRACKED. RT ENGINE PYLON PANEL 422AB HAS CRACKED SEAL RETAINER. REMOVED UNSERVICEABLE RT ENG PYLON PANEL 422AB SEAL RETAINER AND INSTALLED SERVICEABLE SEAT RETAINER IAW 
- [SDR A6WA201240534](https://openairdocs.org/sdr/A6WA201240534), May 4, 2012: BRACKET. BROKEN. T2 SENSE LINE BRACKET BROKEN, SUPPORT BRACKET FOR THE T2 SENSE LINE ON TOP OF THE ENGINE. REMOVED ENG INLET AND INSTALLED A NEW SERVICEABLE BRACKET.

All 161: https://openairdocs.org/deregistered/N406AW-2019-06-25/reports.md

## FAA accident and incident reports (2)

From the FAA Accident/Incident Data System. Reports are matched to registry aircraft by N-number and event date, checked against the reported make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [Incident 20140826017419I](https://openairdocs.org/incident/20140826017419I), Aug 26, 2014: Bombardier Inc CL-600-2B19 (N406AW), Arlington, VA, No damage. On departure from dca leveling off at 8000 feet the crew experienced full right rudder trim. Autopilot was engaged for 2 minutes. Qrh c/w. crew disconnected…
- [Incident 20081127853559I](https://openairdocs.org/incident/20081127853559I), Nov 27, 2008: Cndair CL6002B19 (N406AW), Pittsburgh, PA, No damage. Loss of oil pressure indication in flight at FL340, complied with quick reference handbook for shut down of left engine, oil temp remained in green/normal…

## Other aircraft with N406AW

- [Registered now](https://openairdocs.org/aircraft/N406AW): Cirrus Design SF50, S/N 0655, built 2025

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