# N402AW: 1998 Bombardier CL-600-2B19, registration cancelled 2017-01-03

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: January 3, 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: 7281
- Year built: 1998
- 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: A4B424
- 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/N402AW
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=402AW
- Page: https://openairdocs.org/deregistered/N402AW-2017-01-03

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 (168, newest 50)

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

- [SDR A6WA201643736](https://openairdocs.org/sdr/A6WA201643736), Mar 31, 2016: LIGHT. INOPERATIVE. EMERGENCY EXIT LIGHT BY PAX & SERVICE DOOR WILL NOT ILLUMINATE.
- [SDR A6WA201643737](https://openairdocs.org/sdr/A6WA201643737), Mar 29, 2016: LIGHT. INOPERATIVE. EMERGENCY EXIT LIGHT AT PAX DOOR & SERVICE DOOR WILL NOT ILLUMINATE.
- [SDR A6WA201643701](https://openairdocs.org/sdr/A6WA201643701), Mar 15, 2016: ENGINE. MALFUNCTIONED. DESCENDING THROUGH 5,000 FT, FLIGHT ATTENDANT REPORTED SMOKE IN CABIN, MOVING FROM BACK TO FRONT. AT THE TIME THE APU WAS OFF. SMK CASS MSG WAS NOT DISPLAYED. S
- [SDR A6WA201643682](https://openairdocs.org/sdr/A6WA201643682), Mar 6, 2016: LINE. LEAKING. REQUEST INSPECTION OF RT PACK FOR ODD SMELL & HAZE IN CABIN, OCCURRED AT 8,000 FT, IMC CONDITIONS. INSPECTED RT PACK & FOUND OIL LEAKING ONTO RT DUCT, OIL COMIN
- [SDR A6WA201643683](https://openairdocs.org/sdr/A6WA201643683), Mar 5, 2016: A/C PACK. CONTAMINATED. UNBEARABLE ORANGE SMELL IN CABIN, STARTED WHEN PACK TURNED ON. PERFORMED PACK BURN OUT IAW AMM 09-037A FOR RT PACK, NO FURTHER ORANGE SMELL IN CABIN OR COCKPIT.
- [SDR A6WA201643654](https://openairdocs.org/sdr/A6WA201643654), Mar 5, 2016: WATER SEPARATOR. FAULTY. ON SHORT FINAL, NOTICED SMELL & IT CONTINUED ON GND. FLIGHT ATTENDANT REPORTED MIST IN CABIN. MIST DISSIPATED WHEN RT PACK WAS TURNED OFF. REPLACED WATER SEPARA
- [SDR A6WA201643646](https://openairdocs.org/sdr/A6WA201643646), Mar 5, 2016: ACM. MALFUNCTIONED. LEFT PACK TEMP 118, SHUTDOWN PACK. RECEIVED SMOKE IN COCKPIT. INSPECTED LT PACK & DUCT WORK IN AFT EQUIPMENT BAY. NO DAMAGE NOTED. VERIFIED NO SMOKE IN COCKPIT.
- [SDR A6WA201643604](https://openairdocs.org/sdr/A6WA201643604), Feb 21, 2016: LIGHT. INOPERATIVE. EMERGENCY FLOOR TRACK LIGHTING AT ROW 1 INOPERATIVE, GREEN EMER LIGHTS AT PAX & SERV DOOR INOPERATIVE.
- [SDR A6WA201543289](https://openairdocs.org/sdr/A6WA201543289), Nov 27, 2015: LIGHT. INOPERATIVE. EMERGENCY FLOOR LIGHTING ROWS 2 - 6 INOPERATIVE. EMER EXIT SIGN AT ROW 8A INOPERATIVE.
- [SDR A6WA201543131](https://openairdocs.org/sdr/A6WA201543131), Oct 12, 2015: SHOULDER BELT. DEFECTIVE. FIRST OFFICER SHOULDER HARNESS WILL NOT LOCK INTO RETAINER.
- [SDR A6WA201543128](https://openairdocs.org/sdr/A6WA201543128), Oct 11, 2015: SHOULDER BELT. DEFECTIVE. ON APPROACH FIRST OFFICER WAS NOT ABLE TO LOCK SHOULDER HARNESS.
- [SDR A6WA201542997](https://openairdocs.org/sdr/A6WA201542997), Aug 20, 2015: ENGINE. BIRD INGESTION. BIRD STRIKE RT ENG AFTER TAKEOFF, ROTATION VIB FELT IN ACFT, N1 FAN BLADES. ENG VIB WENT FROM .3 TO 2.1, LANDED UNDERWEIGHT. VIBE FELT IN FEET & YOKE.
- [SDR A6WA201542965](https://openairdocs.org/sdr/A6WA201542965), Aug 1, 2015: CONNECTOR. DIRTY. IN FLIGHT RECEIVED APU OIL TEMP CAUTION. RAN QRH, DIVERTED BACK. MSG DID NOT CLEAR. ON GND MANUALLY SHUTDOWN APU. CLEANED APU OIL TEMP CONNECTOR P13 & COMPLIED 
- [SDR A6WA201542765](https://openairdocs.org/sdr/A6WA201542765), May 19, 2015: LIGHT. INOPERATIVE. FLOOR LEVEL EMER LIGHTS ROW 2 - 5 INOPERATIVE.
- [SDR A6WA201542720](https://openairdocs.org/sdr/A6WA201542720), May 9, 2015: WARNING LIGHT. FALSE ACTIVATION. FLIGHT 3812 WHEN EXTENDING GEAR ON APPROACH, RECEIVED ANTI-SKID INBD & OTBD. WHEN GEAR UP, CAUTION GOES AWAY & WHEN PARKING BRAKE SET. PERFORMED ANTI-SKID SYS B
- [SDR A6WA201542552](https://openairdocs.org/sdr/A6WA201542552), Mar 22, 2015: INVERTER. INOPERATIVE. EMERGENCY LIGHTS FROM ROW 5D TO 8F INOPERATIVE WITH SWITCH IN ON POSITION. INSPECTED & FOUND EMERGENCY LIGHTS AT 5F & 8D NOT WORKING. R & R NR 3 INVERTOR IAW AM
- [SDR A6WA201542482](https://openairdocs.org/sdr/A6WA201542482), Mar 7, 2015: SIGN. INOPERATIVE. WHITE EMER EXIT SIGN BY SERVICE DOOR INOPERATIVE.
- [SDR A6WA201442178](https://openairdocs.org/sdr/A6WA201442178), Nov 15, 2014: LIGHT. INOPERATIVE. EMERGENCY LIGHT ROWS 6 - 8 & SIDE WALL LIGHT AT ROW 8 RT INOPERATIVE.
- [SDR A6WA201442077](https://openairdocs.org/sdr/A6WA201442077), Oct 19, 2014: UNKNOWN. MALFUNCTIONED. AFTER STARTING TAKEOFF ROLL ALL SCREENS, MFD, PFD, RTU, ED 1 & 2 & FMS, WENT BLACK & STARTED TO FLASH ON & OFF. DISPATCH REPORTS 120 KTS AT ABORT. BTMS READS 64
- [SDR A6WA201442070](https://openairdocs.org/sdr/A6WA201442070), Oct 18, 2014: ADG. DEPLOYED. IMMEDIATELY AFTER ROTATION ADG AUTO DEPLOYED. FOLLOWED BY ALL CTR PEDESTAL LIGHTS, EICAS & RTU LIGHTS FLASHING ON & OFF. NO MSG'S POSTED ADG SHOWED DEPLOYED ON 
- [SDR A6WA201441746](https://openairdocs.org/sdr/A6WA201441746), Jul 8, 2014: HINGE FITTING. GOUGED. LT FLT SPOILER CTR INBD HINGE FITTING GOUGED.
- [SDR A6WA201441728](https://openairdocs.org/sdr/A6WA201441728), Jul 3, 2014: COVER. CRACKED. LEFT THRUST REVERSER LOWER PYLON COVER IS CRACKED.
- [SDR A6WA201441727](https://openairdocs.org/sdr/A6WA201441727), Jul 2, 2014: SEAL. CRACKED. RIGHT THRUST REVERSER TORQUE BOX METAL SEAL CRACKED.
- [SDR A6WA201441734](https://openairdocs.org/sdr/A6WA201441734), Jul 2, 2014: DOOR SILL. CORRODED. SERVICE DOOR SILL IS CORRODED IN FWD & AFT CORNERS.
- [SDR A6WA201441729](https://openairdocs.org/sdr/A6WA201441729), Jul 2, 2014: BRACKET. CRACKED. LIGHTNING PROTECTION RETAINING BRACKET IS CRACKED.
- [SDR A6WA201441723](https://openairdocs.org/sdr/A6WA201441723), Jul 1, 2014: SEAL. CRACKED. LT THRUST REVERSER LOWER TORQUE BOX METAL SEAL IS CRACKED.
- [SDR A6WA201441715](https://openairdocs.org/sdr/A6WA201441715), Jul 1, 2014: MOUNT BRACKET. CRACKED. RT WING CTR LE MOUNT BRACKET IS CRACKED NEAR WS 150.
- [SDR A6WA201441713](https://openairdocs.org/sdr/A6WA201441713), Jun 28, 2014: SUPPORT. CRACKED. CARGO BAY DOOR FWD RAIL LOWER SUPPORT HAS A CRACK PN 601R35050-25.
- [SDR A6WA201441740](https://openairdocs.org/sdr/A6WA201441740), Jun 27, 2014: SUPPORT. CRACKED. PAX DOOR SUPPORT STRUCTURE UNDER UPPER STEP CRACKED.
- [SDR A6WA201441714](https://openairdocs.org/sdr/A6WA201441714), Jun 27, 2014: BRACKET. CRACKED. EXTERNAL SERVICE PANEL LOWER BRACKET IS CRACKED ON FWD SIDE.
- [SDR A6WA201441704](https://openairdocs.org/sdr/A6WA201441704), Jun 27, 2014: FITTING. CRACKED. FS 280 RBL 9 INBD & OTBD CLIPS CRACKED.
- [SDR A6WA201441701](https://openairdocs.org/sdr/A6WA201441701), Jun 26, 2014: SEAT TRACK. CORRODED. LEFT MID NR 3 SEAT RAIL HAS CORROSION.
- [SDR A6WA201441708](https://openairdocs.org/sdr/A6WA201441708), Jun 26, 2014: DRAG ANGLE. CRACKED. LEFT MLG WHEEL DRAG ANGLE COMMON TO BATTERY RIB IS CRACKED.
- [SDR A6WA201441706](https://openairdocs.org/sdr/A6WA201441706), Jun 26, 2014: TIE DOWN. CORRODED. LEFT 9G TIE DOWN HAS CORROSION AT 559 + 96 TO 559 + 80.
- [SDR A6WA201441705](https://openairdocs.org/sdr/A6WA201441705), Jun 26, 2014: TIE DOWN. CORRODED. LBL 27 AT 574 THRU 559+96 TIE DOWNS HAVE CORROSION.
- [SDR A6WA201441707](https://openairdocs.org/sdr/A6WA201441707), Jun 26, 2014: TIE DOWN. CORRODED. LBL 9 IN CARGO BAY 2 EACH TIE DOWNS HAS CORROSION.
- [SDR A6WA201441709](https://openairdocs.org/sdr/A6WA201441709), Jun 26, 2014: DRAG ANGLE. CRACKED. RIGHT MLG WW DRAG ANGLE COMMON TO BATTERY RIB IS CRACKED.
- [SDR A6WA201441702](https://openairdocs.org/sdr/A6WA201441702), Jun 26, 2014: ISOLATOR. CRACKED. 621 BULKHEAD AT RBL 27 HAS CRACKED ISOLATOR.
- [SDR A6WA201441742](https://openairdocs.org/sdr/A6WA201441742), Jun 25, 2014: HINGE FITTING. CHAFED. RUDDER HINGE FITTINGS CHAFED FROM MISSING RUDDER HAT BUSHINGS.
- [SDR A6WA201441716](https://openairdocs.org/sdr/A6WA201441716), Jun 25, 2014: SUPPORT ANGLE. CRACKED. AFT OTBD SIDE OF RT MLG WW HAS A CRACKED SUPPORT ANGLE.
- [SDR A6WA201441735](https://openairdocs.org/sdr/A6WA201441735), Jun 24, 2014: SKIN. CHAFED. LOWER WING PLANK CHAFED AT RBL 45, .500" X .650" X .048"D. LOWER WING PLANK CHAFED AT LBL 45, 475" X .750" X .044"D.
- [SDR A6WA201441703](https://openairdocs.org/sdr/A6WA201441703), Jun 24, 2014: CLEAT. CORRODED. FWD & AFT PAX DOOR CLEATS HAVE CORROSION.
- [SDR A6WA201441722](https://openairdocs.org/sdr/A6WA201441722), Jun 22, 2014: CROSSBEAM. CORRODED. FS 349 FLOOR SUPPORT CROSSBEAM AT PAX DOOR HAS CORROSION BETWEEN LBL 36 - LBL45.
- [SDR A6WA201441743](https://openairdocs.org/sdr/A6WA201441743), Jun 21, 2014: FRAME. CORRODED. FRAME AT FS 319 HAS CORROSION ON FWD & AFT SIDES BETWEEN STRINGER 25L & 25R.
- [SDR A6WA201441741](https://openairdocs.org/sdr/A6WA201441741), Jun 20, 2014: INTERCOSTAL. CRACKED. PAX DOOR INTERCOSTAL CRACKED UNDER PANEL 832BR.
- [SDR A6WA201441068](https://openairdocs.org/sdr/A6WA201441068), Jan 24, 2014: ACTUATOR. MALFUNCTIONED. UPON GEAR RETRACTION, RECEIVED THREE MESSAGES, GEAR DISAGREE W, ANTI-SKID INBD C & PARK BRAKE SOV C. COMPLIED WITH QRH, GEAR EXTENDED MANUALLY. LANDED IN PHL AT
- [SDR A6WA201441067](https://openairdocs.org/sdr/A6WA201441067), Jan 23, 2014: WARNING SYSTEM. FALSE ACTIVATION. UPON GEAR RETRACTION, RECEIVED ANTI-SKID INBD CAUTION, GEAR DISAGREE MESSAGE, LT MLG SHOWED DOWN & GREEN WHILE REST SHOWED UP WHITE, WITH HANDLE UP. STAB TRIM C
- [SDR A6WA201311134041](https://openairdocs.org/sdr/A6WA201311134041), Nov 12, 2013: UNKNOWN. ODOR. F/A REPORTS FUEL ODOR IN ROUTE, FUEL ODOR REMAINS AFTER LANDING, APU OFF, NO LEAKS NOTED ON OUTSIDE OF ACFT. INSPECTED ACFT FOR FUEL LEAKS NO LEAKS NOTED, RAN A
- [SDR A6WA201306104201](https://openairdocs.org/sdr/A6WA201306104201), Jun 8, 2013: PUMP. FAILED. FLT LEVEL 250, RECEIVED HYD NR 1 LOW PRESSURE CAUTION. COMPLIED WITH QRH HYD PUMP NR 1 B DIDN'T PROVIDE PRESSURE QTY READS DASHES. REMOVED AND REPLACED EDP 1 HY
- [SDR A6WA201240664](https://openairdocs.org/sdr/A6WA201240664), Jun 16, 2012: HINGE FITTING. GOUGED. LT OTBD FLAP, OTBD HINGE ARM IS GOUGED. REPAIRED HINGE FITTING ASSY AT WS 264 IAW REO 601R-57-54-222.

All 168: https://openairdocs.org/deregistered/N402AW-2017-01-03/reports.md

## Other aircraft with N402AW

- [Cancelled 1993-04-20](https://openairdocs.org/deregistered/N402AW-1993-04-20): Boeing 737-33A, S/N 25505. Exported to China. Owner: [Wilmington Trust Company Trustee](https://openairdocs.org/faa-owner/WILMINGTON%20TRUST%20COMPANY%20TRUSTEE), [Wimington, DE](https://openairdocs.org/faa-place/DE/Wimington)

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