# N401AW: 1999 Bombardier CL-600-2B19, registration cancelled 2017-03-28

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: March 28, 2017
- Status when cancelled: Valid registration
- Airframe: [Bombardier CL-600-2B19](https://openairdocs.org/model/bombardier-cl-600-2b19) (registry code 1390008)
- Engine: [GE CF34 series](https://openairdocs.org/engine/ge-cf34-series) (registry code 30015)
- Data sheets: [TCDS A21EA-1](https://openairdocs.org/tcds/A21EA-1) (OpenAirDocs)
- Serial number: 7280
- Year built: 1999
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: December 21, 1998
- Certificate issued: June 22, 2015
- Last registry action: June 22, 2015
- Mode S code: A4B06D
- Owner when cancelled: [Air Wisconsin Airlines Corp](https://openairdocs.org/faa-owner/AIR%20WISCONSIN%20AIRLINES%20CORP)
- Location: [Appleton, WI](https://openairdocs.org/faa-place/WI/Appleton)
- Owner type: Corporation
- 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/N401AW
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=401AW
- Page: https://openairdocs.org/deregistered/N401AW-2017-03-28

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 (175, newest 50)

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

- [SDR A6WA201644339](https://openairdocs.org/sdr/A6WA201644339), Sep 15, 2016: FITTING. CRACKED. BATH TUB FITTING AT FS 461 AND RBL 9 IS CRACKED, REPLACED.
- [SDR A6WA201643523](https://openairdocs.org/sdr/A6WA201643523), Feb 1, 2016: FLAP. MALFUNCTIONED. FLAP FAIL CAUTION MSG WITH FLAPS AT 35 DEGREES ON APPROACH. COMPLIED WITH FIM RESET, RESET FAILED IAW SUPP 97-018G.
- [SDR A6WA201543133](https://openairdocs.org/sdr/A6WA201543133), Oct 13, 2015: SIGN. MISSING. PASSENGER DOOR EMER EXIT SIGN MISSING.
- [SDR A6WA201542936](https://openairdocs.org/sdr/A6WA201542936), Jul 17, 2015: SKIN. CHAFED. THE RT INBD FLAP VANE LE CHAFED BEYOND LIMITS AT CTR STOP.
- [SDR A6WA201542934](https://openairdocs.org/sdr/A6WA201542934), Jul 17, 2015: BUSHING. SCORED. RIGHT MLG FWD FACE OF MAIN FITTING BUSHING SCORED.
- [SDR A6WA201542652](https://openairdocs.org/sdr/A6WA201542652), Apr 20, 2015: AUTOPILOT SYS. MALFUNCTIONED. FLIGHT NUMBER 3753. AUTOPILOT ENGAGED RECEIVED A LT WING DOWN CAUTION, DISCONNECTED AUTOPILOT. AILERON CONTROL WAS HEAVY IN BOTH DIRECTIONS. COMPLIED WITH AUTO 
- [SDR A6WA201442217](https://openairdocs.org/sdr/A6WA201442217), Dec 3, 2014: WARNING SYSTEM. ACTIVATED. AFTER TAKEOFF, SELECTED GEAR UP RECEIVED GEAR DISAGREE WARNING MSG WITHIN 6 SECONDS. AFTER MSG PERSISTED FOR ONE MINUTE, BEGAN GEAR DISAGREE QRH.
- [SDR A6WA201441090](https://openairdocs.org/sdr/A6WA201441090), Jan 30, 2014: HOUSING. CRACKED. CARGO DOOR HANDLE HOUSING CRACKED. R & R WITH SERVICEABLE HANDLE HOUSING IAW CRJ 200 SRM 51-40-11 & 51-42-21.
- [SDR A6WA201441083](https://openairdocs.org/sdr/A6WA201441083), Jan 30, 2014: FITTING. WORN. RIGHT WING TE, OTBD FLAP ALIGNMENT FITTING WORN BEYOND LIMITS. R & R FITTING PN 601R10156-4 IAW CRJ 200 SRM 51-40-11 & 51-42-06.
- [SDR A6WA201441087](https://openairdocs.org/sdr/A6WA201441087), Jan 29, 2014: SEAL DEPRESSOR. CORRODED. SERVICE DOOR SILL AREA, FWD & AFT SPIGOT STOP BOLT FITTINGS & LOWER SILL AREA, SEAL DEPRESSOR CORRODED. R & R LOWER SILL SUPPORT ANGLE & DEPRESSOR WITH SERVICEA
- [SDR A6WA201441085](https://openairdocs.org/sdr/A6WA201441085), Jan 29, 2014: PLATE. CRACKED. LEFT EXHAUST FAIRING INBD NUTPLATE MOUNT PLATE CRACKED. R & R PN 228-50181-833 IAW CMM 20-42-06.
- [SDR A6WA201441084](https://openairdocs.org/sdr/A6WA201441084), Jan 29, 2014: SKIN. DENTED. COMPLIED WITH JOB CARD 4DMI16050 PERFORM PERMANENT REPAIR OF FUSELAGE AT FS 265 IAW REO 601R-53-11-2301. COMPLIED WITH PERMANENT REPAIR OF FUSELAGE SKIN AT FS 2
- [SDR A6WA201441091](https://openairdocs.org/sdr/A6WA201441091), Jan 27, 2014: BRACKET. CORRODED. PASSENGER DOOR LOWER SILL HAND RAIL RELIEF BRACKETS CORRODED. R & R TWO EACH BRACKETS PN 601R31527-149 IAW CRJ 200 SRM 51-40-11 & 51-42-06.
- [SDR A6WA201441086](https://openairdocs.org/sdr/A6WA201441086), Jan 27, 2014: ANGLE. CORRODED. PASSENGER DOOR LOWER SILL ANGLE CORRODED. R & R WITH SERVICEABLE PART IAW CRJ 200 SRM 51-40-11, 51-42-21 & 51-24-21.
- [SDR A6WA201441092](https://openairdocs.org/sdr/A6WA201441092), Jan 25, 2014: STIFFENER. CRACKED. LEFT EXHAUST FAIRING STIFFENER IS CRACKED, 2ND FROM FRONT. REPAIRED STIFFENER IAW CMM 78-11-00-300-810-A01.
- [SDR A6WA201441074](https://openairdocs.org/sdr/A6WA201441074), Jan 24, 2014: FRAME. CORRODED. FRAME AT FS 319 CORRODED ON AFT SIDE BETWEEN STRINGER 26L & 26R. R & R LOWER FRAME SECTOR PN 601R32003-61 IAW CRJ 200 SRM 51-42-06, 51-42-21 & 51-40-11.
- [SDR A6WA201441082](https://openairdocs.org/sdr/A6WA201441082), Jan 23, 2014: MOUNT BRACKET. CRACKED. EXTERNAL SERVICE PANEL LOWER MOUNT BRACKET CRACKED. R & R WITH SERVICEABLE PN 601R33003-19 IAW CRJ 200 SRM 51-40-11 & 51-42-06.
- [SDR A6WA201441078](https://openairdocs.org/sdr/A6WA201441078), Jan 23, 2014: DRAG ANGLE. CRACKED. DRAG ANGLE IN RT MLG WW UPPER APRON CRACKED. R & R ANGLE PN 600-10389-2 IAW CRJ 200 SRM 51-40-11 & 51-42-21.
- [SDR A6WA201441077](https://openairdocs.org/sdr/A6WA201441077), Jan 23, 2014: STRINGER CLIP. CRACKED. STRINGER ATTACH CLIP AFT OF FS 280 AT STRINGER 3L CRACKED. R & R WITH SERVICEABLE CLIP IAW CRJ 200 SRM 51-24-21,51-40-11, 51-42-06 & 51-42-21.
- [SDR A6WA201441076](https://openairdocs.org/sdr/A6WA201441076), Jan 23, 2014: ATTACH ANGLE. CRACKED. RIGHT WING INBD LE, OTBD ATTACH ANGLE CRACKED. R & R WITH SERVICEABLE ANGLE PN 600-12025-8 IAW CRJ 200 SRM 51-40-11 & 51-41-02.
- [SDR A6WA201441075](https://openairdocs.org/sdr/A6WA201441075), Jan 23, 2014: SUPPORT ANGLE. CRACKED. CARGO DOOR FWD SUPPORT UPPER ANGLE CRACKED. R & R WITH SERVICEABLE ANGLE IAW CRJ 200 SRM 51-24-16, 51-40-11 & 51-42-21.
- [SDR A6WA201441089](https://openairdocs.org/sdr/A6WA201441089), Jan 21, 2014: SEAT TRACK. CORRODED. FLOOR SUPPORT SEAT RAIL AT LBL 9 FROM FS 409 TO 409+128 IS CORRODED. R & R SEAT TRACK AT LBL 9 WITH SERVICEABLE PART IAW CRJ 200 SRM 51-40-11 & AMM 53-01-11.
- [SDR A6WA201441088](https://openairdocs.org/sdr/A6WA201441088), Jan 21, 2014: SEAT TRACK. CORRODED. FLOOR SUPPORT SEAT RAIL AT RBL 9 FROM FS 409 TO 409+128 HAS CORROSION & GOUGES. R & R FLOOR SEAT TRACK WITH SERVICEABLE TRACK IAW CRJ 200 SRM 51-40-11 & AMM 53-
- [SDR A6WA201441081](https://openairdocs.org/sdr/A6WA201441081), Jan 21, 2014: CARGO TRACK. CORRODED. CARGO FLOOR TIE DOWN TRACK AT RBL 27 & FS 559+80 IS CORRODED. R & R WITH SERVICEABLE TRACK IAW CRJ 200 SRM 51-40-11 & AMM 53-01-11.
- [SDR A6WA201441080](https://openairdocs.org/sdr/A6WA201441080), Jan 21, 2014: CARGO TRACK. CORRODED. CARGO FLOOR TIE DOWN TRACK AT LBL 27 & FS 559+96 IS CORRODED. R & R WITH SERVICEABLE TRACK IAW CRJ 200 SRM 51-40-11 & AMM 53-01-11.
- [SDR A6WA201441079](https://openairdocs.org/sdr/A6WA201441079), Jan 21, 2014: CARGO TRACK. CORRODED. CARGO FLOOR, TIE DOWN TRACK AT LBL 9 & FS 559+112 CORRODED. R & R WITH SERVICEABLE TRACK IAW CRJ 200SRM 51-40-11 & 53-01-11.
- [SDR A6WA201441063](https://openairdocs.org/sdr/A6WA201441063), Jan 16, 2014: ATTACH FITTING. CRACKED. THE INTERCOSTAL REPAIR ATTACH CLIP AT 484 & RBL 36 ABOVE THE PRESS FLOOR IS CRACKED. R & R REPAIR ATTACH CLIP IAW 601R-53-41-059 REV B DATED 2009-09-16.
- [SDR A6WA201441062](https://openairdocs.org/sdr/A6WA201441062), Jan 16, 2014: ATTACH FITTING. CRACKED. THE INTERCOSTAL ATTACH CLIP AT FS 484 & LBL 27 ABOVE THE PRESS FLOOR IS CRACKED. R & R ATTACH CLIP IAW CRJ 200 SRM 51-40-11, 51-42-06 & 601R-53-41-059 REV B DAT
- [SDR A6WA201441061](https://openairdocs.org/sdr/A6WA201441061), Jan 16, 2014: ATTACH ANGLE. CRACKED. THE RBL 9 FLOOR BEAM OTBD ATTACH ANGLE AT FS 280 IS CRACKED. R & R ANGLE IAW 601R-53-11-171 REV D.
- [SDR A6WA2013090740025](https://openairdocs.org/sdr/A6WA2013090740025), Sep 7, 2013: CLAMP. DAMAGED. WHILE CLIMBING, RECEIVED LT 10TH DUCT WARNING MESSAGE. PERFORMED QRH, MESSAGE CAME BACK SEVERAL TIMES WHILE PERFORMING QRH. ONCE LT ENGINE AT IDLE POWER, MESSAG
- [SDR A6WA20130114009](https://openairdocs.org/sdr/A6WA20130114009), Jan 14, 2013: PROXIMITY SWITCH. OUT OF ADJUST. DURING CLIMB THRU 30,000FT RECEIVED PAX DOOR OUTER HANDLE CAUTION MESSAGE. RAN QRH, MESSAGE PERSISTED. CREW DECLARED AN EMERGENCY AND DIVERTED TO CVG IAW QRH. C
- [SDR A6WA201212114000](https://openairdocs.org/sdr/A6WA201212114000), Dec 7, 2012: ANTI-ICE VALVE. FAULTY. LEFT COWL ANTI-ICE CAUTION IN FLT, WOULD NOT EXTINGUISH. COMPLIED WITH QRH. WITH SWITCH OFF MSG CLEARED. AIR RETURN DCA. REMOVED AND REPLACED LEFT COWL ANTI-ICE
- [SDR A6WA201240316](https://openairdocs.org/sdr/A6WA201240316), Feb 7, 2012: DOUBLER. CRACKED. FWD PRESSURE BULKHEAD STRIP, DOUBLER, 2ND RT OTBD FROM BL0.00 IS CRACKED, UPPERFWD INBD RADIUS BY WIPER MOTOR BRACKET. REPAIRED IAW REO 601R-53-11-2271, REV A.
- [SDR A6WA201240309](https://openairdocs.org/sdr/A6WA201240309), Feb 5, 2012: STRINGER. CRACKED. STRINGER 6R IS CRACKED AFT SIDE OF FS 439.
- [SDR A6WA201240284](https://openairdocs.org/sdr/A6WA201240284), Feb 3, 2012: SKIN. CRACKED. PAX DOOR INTERIOR SKIN CRACKED ON AFT FRAME AT FS 338.00 AND INTERCOSTAL. REPAIRED INNER SKIN CRACK AT FS 338.00 IAW REO 601R-52-11-2009.
- [SDR A6WA201240285](https://openairdocs.org/sdr/A6WA201240285), Feb 3, 2012: INTERCOSTAL. CRACKED. INTERCOSTAL UNDER PAX DOOR PANEL 832BR CRACKED. REMOVED CRACKED INTERCOSTAL THEN INSTALLED NEW SERVICEABLE INTERCOSTAL.
- [SDR A6WA201240326](https://openairdocs.org/sdr/A6WA201240326), Feb 3, 2012: SEAT TRACK. CORRODED. SEAT TRACK CORRODED AT LBL9, FS 364. R & R SEAT TRACK.
- [SDR A6WA201240283](https://openairdocs.org/sdr/A6WA201240283), Feb 3, 2012: DOOR FRAME. CRACKED. PAX DOOR FRAME AT FS 338.00 IS CRACKED 4" FROM BOTTOM OF FRAME. REMOVED CRACKED SECTION WHEN INSTALLED NEW SECTION IAW REO 601R-52-11-402, REV H.
- [SDR A6WA201240198](https://openairdocs.org/sdr/A6WA201240198), Feb 2, 2012: SKIN. WORN. LEFT EXTERIOR FUSELAGE SKIN WHERE STUB FAIRING MAKES CONTACT IS GOUGED AND WORN, APPROX FS 544. CUT AWAY DAMAGED PORTION OF SKIN PANEL AND INSTALLED NEW SKIN SE
- [SDR A6WA201240297](https://openairdocs.org/sdr/A6WA201240297), Feb 2, 2012: SKIN. GOUGED. LEFT EXTERIOR FUSELAGE SKIN & WHERE STUB FAIRING MAKES CONTACT IS GOUGED AND WORN. APPROXIMATELY FS 544.0 - 559.0. C UT AWAY DAMAGED PORTION OF SKIN PANEL AND I
- [SDR A6WA201240321](https://openairdocs.org/sdr/A6WA201240321), Feb 2, 2012: SKIN. MISINSTALLED. SKIN MISREPAIRED. REPAIRED IAW REO 601R-53-41-1535, REV A.
- [SDR A6WA201240289](https://openairdocs.org/sdr/A6WA201240289), Jan 31, 2012: FITTING. CHAFED. RT OTBD FLAP ROLLER FITTING CHAFED, COMPIED WITH REO 601R-57-53-915.
- [SDR A6WA201240302](https://openairdocs.org/sdr/A6WA201240302), Jan 31, 2012: SKIN. CRACKED. A CRACK IN RT (FWD) CORE COWL DOOR OUTER SKIN. REMOVED DAMAGE FROM OUTER SKIN. FABRICATED DOUBLER AND SPIGOT IAW REO 601R-71-12-4095 AND CMM 71-12-01. REPAIR SR
- [SDR A6WA201240320](https://openairdocs.org/sdr/A6WA201240320), Jan 28, 2012: STRUCTURE. CRACKED. BOTH CORNERS ON MLG WW CUT CRACKED. REPAIRED CRACKS IAW REO 601R-53-11-048.
- [SDR A6WA201240286](https://openairdocs.org/sdr/A6WA201240286), Jan 27, 2012: STRUCTURE. CHAFED. LEFT MLG DOOR CHAFED NEAR BRUSH, COMPLIED WITH REO 601R-52-82-330.
- [SDR A6WA201240306](https://openairdocs.org/sdr/A6WA201240306), Jan 27, 2012: FLOOR SUPPORT. CORRODED. RT FS 349 CORRODED AND SILL IS SEPARATING. REMOVED UNSERVICEABLE ANGLE SUPPORT ANGLE AND UNSERVICEABLE SILL AND INSTALLED SERVICEABLE ANGLE SUPPORT AND SILL IAW
- [SDR A6WA201240322](https://openairdocs.org/sdr/A6WA201240322), Jan 27, 2012: SKIN. DAMAGED. FUSELAGE SKIN AT FS 295.00 AND S26L. ONE LIGHTNING STRIKE 0.018" DEEP X 0.125" WIDE ON THE FUSELAGE SKIN LOCATED 3/00" AFT OF FS 295.00 + 0.156" FROM STRINGER 2
- [SDR A6WA201240317](https://openairdocs.org/sdr/A6WA201240317), Jan 26, 2012: STRIKER. GOUGED. PAX DOOR AFT SEAL STRIKER GOUGED. REPAIRED IAW REO 601R53-22-033, REV C.
- [SDR A6WA201240299](https://openairdocs.org/sdr/A6WA201240299), Jan 26, 2012: FITTING. CHAFED. CHAFING AT LEFT OTBD FLAP ROLLER FITTING. OPEN
- [SDR A6WA201240305](https://openairdocs.org/sdr/A6WA201240305), Jan 26, 2012: FITTING. CORRODED. FITTING CORRODED AT FS 349, JUST AFT OF THE SERVICE DOOR. BLENDED CORROSION IAW SRM 53-00-00 AND SRM 51-21-06. REMAINING MATERIAL IS WITHIN SERVICEABLE LIMITS I

All 175: https://openairdocs.org/deregistered/N401AW-2017-03-28/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 20040205001099I](https://openairdocs.org/incident/20040205001099I), Feb 5, 2004: Cndair CL6002B19 (N401AW), Kansas City, MO. (-23) Air Wisconsin flight 5764, aircraft N401AW, a CL-600-2B19, landed at mci from den at approximately 12:00L. The weather at the time of the incident was…
- [Incident 20040104000049I](https://openairdocs.org/incident/20040104000049I), Jan 4, 2004: Cndair CL6002B19 (N401AW), Columbia, MO. (-23) On January 4, 2004 air Wisconsin flt. 5452 a CL-600 diverted to Columbia MO. Due to a left engine 14th stage duct warning fail message. A/c landed…

## Other aircraft with N401AW

- [Registered now](https://openairdocs.org/aircraft/N401AW): Xag P150, S/N 1863FPEG8223443Y077Q
- [Cancelled 1993-04-08](https://openairdocs.org/deregistered/N401AW-1993-04-08): Boeing 737-33A, S/N 25603. Exported to China. Owner: [Wilmington Trust Company Trustee](https://openairdocs.org/faa-owner/WILMINGTON%20TRUST%20COMPANY%20TRUSTEE), [Wilmington, DE](https://openairdocs.org/faa-place/DE/Wilmington)

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