# N407AW: 2000 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) - 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: 7424 - Year built: 2000 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: October 11, 2000 - Certificate issued: April 29, 2010 - Last registry action: December 15, 2016 - Mode S code: A4C6B7 - Owner when cancelled: [Southshore Aircraft III LLC](https://openairdocs.org/faa-owner/SOUTHSHORE%20AIRCRAFT%20III%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/N407AW - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=407AW - Page: https://openairdocs.org/deregistered/N407AW-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 (119, newest 50) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR A6WA201643865](https://openairdocs.org/sdr/A6WA201643865), May 10, 2016: LIGHT. INOPERATIVE. EMERGENCY LIGHTS, BETWEEN ROW 1- 5 WILL NOT LIGHT. - [SDR A6WA201643730](https://openairdocs.org/sdr/A6WA201643730), Mar 25, 2016: LIGHT. INOPERATIVE. FORWARD EMER LIGHT CEILING LIGHT IS INOPERATIVE. - [SDR A6WA201643597](https://openairdocs.org/sdr/A6WA201643597), Feb 17, 2016: SHAFT. DAMAGED. UNABLE TO OPEN SERVICE DOOR FROM OUTSIDE. DISASSEMBLED OUTER SERVICE DOOR HANDLE & INSPECTED IAW SUP 11-029B. MINOR DAMAGE ADDRESSED ON OUTER HANDLE SHAFT & ASS - [SDR A6WA201543102](https://openairdocs.org/sdr/A6WA201543102), Oct 2, 2015: HANDLE. LACK OF LUBE. SERVICE DOOR UNABLE TO BE OPENED FROM OUTSIDE. LUBED OUTER HANDLE & HANDLE RELEASE PIN AS REQUIRED. OPERATIONS CHECKED GOOD AT THIS TIME. - [SDR A6WA201543095](https://openairdocs.org/sdr/A6WA201543095), Sep 30, 2015: STRIP. MISSING. EMERGENCY FLOOR TRACK LIGHTING MISSING AMBER STRIP AT SEAT 1DF & MISSING END CAP. - [SDR A6WA201542942](https://openairdocs.org/sdr/A6WA201542942), Jul 25, 2015: DIMMER. DEFECTIVE. FLIGHT 3825, ODOR OF ELEC BURNING IN CABIN AREA MID TO FWD. R & R BOTH POWER UNIT DIMMERS AT ROW 2D - F IAW AMM 33-21-04. OPS CHECKED GOOD. INSPECTED WIRING FOR - [SDR A6WA201542937](https://openairdocs.org/sdr/A6WA201542937), Jul 21, 2015: DIMMER. FAULTY. FLIGHT 3961STRONG ELECT BURNING SMELL AT ROW 3 IN CABIN. PER CREW, LIGHTING IS SUFFICIENT FOR DAY TIME FLIGHTS. ON CALL IDENTIFIED BALLAST ROW 3. PLACARDED & PL - [SDR A6WA201542521](https://openairdocs.org/sdr/A6WA201542521), Mar 14, 2015: FLAP SYSTEM. MALFUNCTIONED. FLAP FAIL AT 30 DEGREES IN FLIGHT. PERFORMED FLAP RESET PROCEDURE IAW AWAC, FLAPS RESET. PLACARD & PLACED ON MEL. TROUBLE SHOT IAW FIM 27-50-00 & AWAC SUP 98-01 - [SDR A6WA201441986](https://openairdocs.org/sdr/A6WA201441986), Sep 20, 2014: FRAME. CORRODED. FORWARD & AFT FACE FRAME 295 IS CORRODED. - [SDR A6WA201441985](https://openairdocs.org/sdr/A6WA201441985), Sep 20, 2014: FRAME. CORRODED. FORWARD AFT FACE OF FRAME 333 IS CORRODED. - [SDR A6WA201441980](https://openairdocs.org/sdr/A6WA201441980), Sep 19, 2014: SKIN. DENTED. RIGHT INBD FLAP LOWER OTBD EXTERIOR SKIN DENTED. - [SDR A6WA201441982](https://openairdocs.org/sdr/A6WA201441982), Sep 19, 2014: FLOORBEAM. CORRODED. CARGO BAY FLOORBEAM LBL 27 AT FS 589 TO FS 621 IS CORRODED AROUND SCREW HOLES. - [SDR A6WA201441981](https://openairdocs.org/sdr/A6WA201441981), Sep 19, 2014: ATTACH FITTING. CRACKED. WIND SHIELD CTR POST ON RT LOWER ATTACH FITTING CRACKED. - [SDR A6WA201441958](https://openairdocs.org/sdr/A6WA201441958), Sep 13, 2014: BRACKET. CRACKED. LEFT MLG DOOR ROLLER BRACKET CRACKED. - [SDR A6WA201441959](https://openairdocs.org/sdr/A6WA201441959), Sep 13, 2014: ATTACH BRACKET. CRACKED. LEFT WING LE ATTACH BRACKETS ARE CRACKED AT WS 139 & WS 149. - [SDR A6WA201441963](https://openairdocs.org/sdr/A6WA201441963), Sep 13, 2014: SEAT TRACK. CORRODED. LEFT NR 2 SEAT TRACK HAS FOUR EACH AREAS OF CORROSION FS 394 - 409+128. - [SDR A6WA201441962](https://openairdocs.org/sdr/A6WA201441962), Sep 13, 2014: MOUNT BRACKET. CRACKED. NUMBER 3 HYD BRAKE ACCUMULATOR FWD MOUNTING BRACKET CRACKED. - [SDR A6WA201441961](https://openairdocs.org/sdr/A6WA201441961), Sep 13, 2014: SEAT TRACK. CORRODED. LEFT NR 3 FLOOR SEAT TRACK GOUGED & CORRODED. - [SDR A6WA201441955](https://openairdocs.org/sdr/A6WA201441955), Sep 13, 2014: FITTING. CRACKED. LEFT FS 484 CLIP CRACKED. - [SDR A6WA201441956](https://openairdocs.org/sdr/A6WA201441956), Sep 13, 2014: SKIN PANEL. CORRODED. EXTERIOR LOWER SKIN PANEL HAS CORROSION ON LOWER SURFACE AT FS 599+116 STRINGER 26L. - [SDR A6WA201441964](https://openairdocs.org/sdr/A6WA201441964), Sep 13, 2014: FITTING. CRACKED. FLOOR SUPPORT BEAM HAS CRACKED CLIP AT FS 280, RBL 9 INBD CLIP. - [SDR A6WA201441957](https://openairdocs.org/sdr/A6WA201441957), Sep 13, 2014: FITTING. CRACKED. CLIP CRACKED FS 280 FLOORBEAM RBL10. - [SDR A6WA201441954](https://openairdocs.org/sdr/A6WA201441954), Sep 13, 2014: MOUNT BRACKET. CRACKED. CARGO DOOR LOWER FWD TRACK MOUNT BRACKET CRACKED. - [SDR A6WA201441960](https://openairdocs.org/sdr/A6WA201441960), Sep 13, 2014: SKIN. CORRODED. FUSELAGE SKIN UNDER LOWER T CAS ANTENNA IS CORRODED. - [SDR A6WA201441996](https://openairdocs.org/sdr/A6WA201441996), Sep 12, 2014: HANDLE. CRACKED. PASSENGER DOOR INNER HANDLE CRACKED. - [SDR A6WA201441994](https://openairdocs.org/sdr/A6WA201441994), Sep 11, 2014: BEAM. CRACKED. FS 409+128 VERTICAL BEAM AT RBL 18 IS CRACKED ON LOWER END. - [SDR A6WA201441970](https://openairdocs.org/sdr/A6WA201441970), Sep 11, 2014: TIE CLIP. CRACKED. INBOARD & OUTBOARD TIE CLIPS AT STRINGER 3L & FS 280 ARE CRACKED. - [SDR A6WA201441987](https://openairdocs.org/sdr/A6WA201441987), Sep 9, 2014: FLOOR PANEL. CRACKED. FORWARD EQUIPMENT COMPARTMENT FLOOR SKIN CRACKED ON LT SIDE AT FS 193. - [SDR A6WA201441947](https://openairdocs.org/sdr/A6WA201441947), Sep 9, 2014: BULKHEAD. CHAFED. AFT SIDE OF FS 280 BULKHEAD CHAFED AT RBL 9 AT WL 86.L. - [SDR A6WA201441946](https://openairdocs.org/sdr/A6WA201441946), Sep 9, 2014: SEAT TRACK. CORRODED. RIGHT SEAT TRACK CORRODED BETWEEN FS 394 - FS 409+128. - [SDR A6WA201441945](https://openairdocs.org/sdr/A6WA201441945), Sep 9, 2014: SEAT TRACK. CORRODED. RIGHT SEAT TRACK CORRODED BETWEEN FS 364 - FS 394. - [SDR A6WA201441949](https://openairdocs.org/sdr/A6WA201441949), Sep 9, 2014: DRAG ANGLE. CRACKED. RIGHT DRAG ANGLE COMMON TO BATTERY RIB CRACKED. - [SDR A6WA201441944](https://openairdocs.org/sdr/A6WA201441944), Sep 9, 2014: SKIN. CRACKED. FUSELAGE SKIN CRACKED AT AFT RT CORNER OF NLG WW. - [SDR A6WA201441948](https://openairdocs.org/sdr/A6WA201441948), Sep 9, 2014: SEAT TRACK. CORRODED. RIGHT FLOOR SEAT TRACK CORRODED FROM FS 424 - FS 559. - [SDR A6WA201441989](https://openairdocs.org/sdr/A6WA201441989), Sep 7, 2014: CROSSBEAM. CORRODED. FLOOR SUPPORT CROSSBEAM AT FRAME FS 349 CORRODED. - [SDR A6WA201441974](https://openairdocs.org/sdr/A6WA201441974), Sep 7, 2014: FITTING. CORRODED. FLOOR SUPPORT FITTING AT FS 319 BELOW SERVICE DOOR IS CORRODED. - [SDR A6WA201441969](https://openairdocs.org/sdr/A6WA201441969), Sep 7, 2014: FLOORBEAM. CRACKED. FLOORBEAM WEB CRACKED AT LBL 10 OTBD & FS 280 FROM LOWER OTBD PULLEY BRACKET ATTACHMENT BOLT HOLE. - [SDR A6WA201441971](https://openairdocs.org/sdr/A6WA201441971), Sep 7, 2014: CARGO TRACK. CORRODED. CARGO BAY TIE DOWN TRACK CORRODED, RBL 9 FROM FS 559+80 TO 559+112. - [SDR A6WA201441988](https://openairdocs.org/sdr/A6WA201441988), Sep 6, 2014: SKIN. DENTED. COMPLIED WITH CARD 4DMI17806 REPAIR DENTS FS 179 STRINGER 26 & 24. - [SDR A6WA201441972](https://openairdocs.org/sdr/A6WA201441972), Sep 6, 2014: SEAT TRACK. CORRODED. LEFT FLOOR SEAT TRACK CORRODED FS 364 - 394. - [SDR A6WA201441992](https://openairdocs.org/sdr/A6WA201441992), Sep 5, 2014: FITTING. CRACKED. CARGO DOOR SUPPORT BEAM LOWER CLIP AT FS 621 BULKHEAD CRACKED. - [SDR A6WA201441993](https://openairdocs.org/sdr/A6WA201441993), Sep 3, 2014: SEAL. CRACKED. LEFT SPOILERON CTR SPRING SEAL CRACKED. - [SDR A6WA201441995](https://openairdocs.org/sdr/A6WA201441995), Sep 3, 2014: FRAME. CORRODED. FRAME CORRODED AT FS 349 BETWEEN STRINGERS 25L & 25R. - [SDR A6WA201441973](https://openairdocs.org/sdr/A6WA201441973), Sep 3, 2014: TIE CLIP. CRACKED. AFT TIE CLIP STRINGER 3L TO FS 280 CRACKED. - [SDR A6WA201441114](https://openairdocs.org/sdr/A6WA201441114), Feb 7, 2014: ACTUATOR. FAULTY. DURING CLIMB ACFT YAWED UNCOMMANDED. COMPLIED WITH QRH, DISCONNECTED YAW DAMPERS & YAWING PERSISTED. FD NR 2 WAS ENGAGED. ACFT RETURNED TO PHL, EMERGENCY DECLAR - [SDR A6WA201240826](https://openairdocs.org/sdr/A6WA201240826), Aug 28, 2012: SILL. CORRODED. PAX DOOR SILL HAS CORROSION. FOUND CORROSION TO BE 100 PERCENT MATERIAL LOSS. REMOVED, FABRICATED, AND INSTALLED NEW SERVICEABLE SILL IAW SRM 51-42-06, 51-42-13 - [SDR A6WA201240814](https://openairdocs.org/sdr/A6WA201240814), Aug 28, 2012: RIB. GOUGED. LOWER CORE COWL 445AB HAS 1 EA GOUGE ON 2 INNER RIBS AND NUMEROUS SMALL GOUGES AND DENTS ON INNER SKIN. C/W REO 601R-71-12-4129 BY HAND BLENDING MINOR CHAFING C - [SDR A6WA201240828](https://openairdocs.org/sdr/A6WA201240828), Aug 25, 2012: ROLLER. CHAFED. LEFT OTBD FLAP ROLLER FITTING CHAFED. PERFORMED REPAIR OF LT OTBD FLAP INBD ROLLER FITTING IAW REO 601R-57-53-943. - [SDR A6WA201240818](https://openairdocs.org/sdr/A6WA201240818), Aug 25, 2012: LEVER. CHAFED. PAX DOOR FWD PULL IN LEVER IS CHAFING THE PAX DOOR STRUCTURE. REPAIRED STRUCTURE IAW REO 601R-52-2058. - [SDR A6WA201240827](https://openairdocs.org/sdr/A6WA201240827), Aug 23, 2012: CARGO TRACK. CORRODED. THREE CARGO TRACKS ON LBL AND RBL 9 HAS CORROSION IN CARGO AREA. REMOVED AND INSTALLED SERVICEABLE CARGO TRACKS IAW AMM 53-01-11. All 119: https://openairdocs.org/deregistered/N407AW-2019-06-25/reports.md ## NTSB investigations (1) From the NTSB's public API. Aircraft are matched to registry aircraft by N-number and event date, checked against the reported serial number, make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model. - [NTSB DCA09IA017](https://openairdocs.org/ntsb/DCA09IA017), Dec 14, 2008: Bombardier CL-600-2B19 (N407AW), Philadelphia, PA, incident, minor damage. Probable cause: the failure of the maintenance personnel to properly complete the installation, and the inspection personnel to conduct the proper functional test, of the left main landing gear uplock assembly. ## 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 20081214855989I](https://openairdocs.org/incident/20081214855989I), Dec 14, 2008: Cndair CL6002B19 (N407AW), Philadelphia, PA, Minor damage. (-23) 1-PHL int'l airport, a CRJ2(mobardier CL-600-2B19) landed onr runway 27L with the left main gear retracted. Phl ARFF responded and foamed the aircraft… - [Incident 20080414832029I](https://openairdocs.org/incident/20080414832029I), Apr 14, 2008: Cndair CL6002B19 (N407AW), Buffalo, NY, No damage. (-23) On April 14, 2008, 0945EDT, a Bombardier CL-600-B19, N407AW, flight 3908, operated by air Wisconsin airlines, departed from philadelphia, Pennsylvania to… --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.