# N422AW: 1999 Bombardier CL-600-2B19, registration cancelled 2018-11-07

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: November 7, 2018
- Exported to: Mexico
- 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: 7341
- Year built: 1999
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: November 17, 1999
- Certificate issued: June 28, 2017
- Last registry action: June 28, 2017
- Mode S code: A50322
- Owner when cancelled: [Frontera Flight Holdings Inc](https://openairdocs.org/faa-owner/FRONTERA%20FLIGHT%20HOLDINGS%20INC)
- Location: [Dover, DE](https://openairdocs.org/faa-place/DE/Dover)
- Owner type: Corporation
- Owner's area on the map: 39.1815° N, 75.4736° W: Placed by OpenAirDocs at the center of ZIP code 19901, within about 5 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N422AW
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=422AW
- Page: https://openairdocs.org/deregistered/N422AW-2018-11-07

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 (196, newest 50)

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

- [SDR A6WA201744762](https://openairdocs.org/sdr/A6WA201744762), Jan 20, 2017: ACTUATOR. MALFUNCTIONED. INFLIGHT, AFTER SELECTING GEAR LEVER UP, NOSE GEAR LOCK AND DOOR CYCLED FOR 1 MINUTE THEN LOCKED IN UP POSITION. GEAR EXTENDED NORMALLY AND LOCKED AFTER GEAR LE
- [SDR A6WA201644263](https://openairdocs.org/sdr/A6WA201644263), Aug 26, 2016: LIGHT. INOPERATIVE. DURING FIRST FLIGHT ACCEPTANCE INSPECTION CREW REPORTED THE EMERGENCY FLOOR TRACK LIGHTING WAS INOPERATIVE FROM ROW 1-5.
- [SDR A6WA201644257](https://openairdocs.org/sdr/A6WA201644257), Aug 22, 2016: DOWNLOCK SENSOR. FAILED. AFTER CLIMB OUT REC GEAR DISAGREE WARNING, NLG RED HASHES RAN QRH MSGS CLEARED RETURNED TO DEPARTURE IAW QRH. MESSAGES RECEIVED AT AROUND 7,000 FT AND 250 KTS G
- [SDR A6WA2016080144127](https://openairdocs.org/sdr/A6WA2016080144127), Jul 18, 2016: DOOR. LACK OF LUBE. PAX DOOR WILL NOT OPEN FROM THE OUTSIDE. LUBRICATED PAX DOOR IAW SUP 15-053. OPS CHECKED GOOD.
- [SDR A6WA2016071944127](https://openairdocs.org/sdr/A6WA2016071944127), Jul 18, 2016: DOOR. LACK OF LUBE. PAX DOOR WILL NOT OPEN FROM OUTSIDE. LUBRICATED PAX DOOR PER 15-053. OPS CHECKED GOOD.
- [SDR A6WA201643862](https://openairdocs.org/sdr/A6WA201643862), May 8, 2016: ROLLER. DAMAGED. NUMBER 1 PAX DOOR VERY DIFFICULT TO MOVE TO THE OPEN POSITION FROM THE OUTSIDE. FOUND INSIDE HANDLE ROLLER DAMAGED, ROLLER HAS MULTIPLE FLAT SPOTS CAUSING ROLLE
- [SDR A6WA201643847](https://openairdocs.org/sdr/A6WA201643847), May 5, 2016: FUEL. LEAKING. FLIGHT 3914, 3930 STRONG FUEL ODOR COMING FROM THE PACKS. NOTED FUEL LEAK AROUND APU FUEL MANIFOLD & FILTER AREA. WIPED EXCESS FUEL IAW 299136 4 FOR MEL. DID NO
- [SDR A6WA201643623](https://openairdocs.org/sdr/A6WA201643623), Feb 28, 2016: LIGHT. INOPERATIVE. FLIGHT 3791 EMER LIGHTS ROW 1 INOPERATIVE & UNSECURE. R & R EMER LIGHT COVER IAW AMM 33-51-01. OPERATIONS CHECKED GOOD AT THIS TIME.
- [SDR A6WA201643458](https://openairdocs.org/sdr/A6WA201643458), Jan 15, 2016: LIGHT. INOPERATIVE. EMERGENCY FLOOR TRACK LIGHT ROW 5 - 7 ARE NOT WORKING;.
- [SDR A6WA201543415](https://openairdocs.org/sdr/A6WA201543415), Dec 29, 2015: ROD. OUT OF ADJUST. GALLEY SERVICE DOOR DIFFICULT TO OPEN FROM INSIDE & OUTSIDE. ADJUSTED UPPER STABILIZER ROD IAW AMM 52-41. OPERATIONS CHECKED GOOD. REMOVED PLACARD & FROM MEL.
- [SDR A6WA201543413](https://openairdocs.org/sdr/A6WA201543413), Dec 27, 2015: ROD. OUT OF ADJUST. CREW REPORTED SERVICE DOOR DIFFICULT TO OPEN AFTER UNLATCHING HANDLE INSIDE & OUTSIDE OF ACFT. INSPECTED DOOR FOR SAFETY & SECURITY. PLACED SERVICE DOOR ON MEL 
- [SDR A6WA201543394](https://openairdocs.org/sdr/A6WA201543394), Dec 21, 2015: SEAL. TORN. GALLEY SERVICE DOOR DIFFICULT TO OPEN & CLOSE. INSPECTED GALLEY SERVICE DOOR & FOUND LOWER AFT SECTION TORN IN TWO PLACES APPROX 1" LONG. R & R SERVICE DOOR SEA
- [SDR A6WA201543288](https://openairdocs.org/sdr/A6WA201543288), Nov 25, 2015: MOUNT BRACKET. CRACKED. EXTERNAL SERVICE INSTRUMENT PANEL, LOWER ANGLE MOUNTING BRACKET IS CRACKED, REPLACED.
- [SDR A6WA201543285](https://openairdocs.org/sdr/A6WA201543285), Nov 24, 2015: SUPPORT. CRACKED. SPOILER ADAPTER OTBD SUPPORT CRACKED, REPLACED.
- [SDR A6WA201543284](https://openairdocs.org/sdr/A6WA201543284), Nov 24, 2015: MOUNT BRACKET. CRACKED. AC POWER RECEPTACLE MOUNT BRACKET IS CRACKED AT THE FWD FASTENER HOLE, REPLACED.
- [SDR A6WA201543280](https://openairdocs.org/sdr/A6WA201543280), Nov 22, 2015: BRACKET. CHAFED. BRACKET FOR RT BRAIDED HYD LINE RUNNING THRU INTERCOSTAL AT STRINGER 9R, BETWEEN FRAMES 645 & 672 IN THE AFT EQUIPMENT BAY IS CHAFED, REPAIRED.
- [SDR A6WA201543281](https://openairdocs.org/sdr/A6WA201543281), Nov 22, 2015: INTERCOSTAL. CRACKED. PASSENGER DOOR AFT UPPER INTERCOSTAL CRACKED, REPLACED.
- [SDR A6WA201543270](https://openairdocs.org/sdr/A6WA201543270), Nov 21, 2015: SUPPORT BRACKET. CRACKED. RIGHT DUEL HEAT EXCHANGER, SUPPORT BRACKET CLIP IS CRACKED. R & R CRACKED BRACKET ON RT DUEL HEAT EXCHANGER SUPPORT WITH SERVICEABLE FABRICATED BRACKET IAW SRM 
- [SDR A6WA201543277](https://openairdocs.org/sdr/A6WA201543277), Nov 21, 2015: SKIN. CRACKED. LOWER FWD FUSELAGE SKIN AT NLG AFT DOOR CUT OUT, AFT RT RADIUS IS CRACKED. REPAIRED DAMAGED FUSELAGE SKIN CRACK AT NLG CUT OUT, AFT RADIUS RT SIDE IAW REO 601R-
- [SDR A6WA201543276](https://openairdocs.org/sdr/A6WA201543276), Nov 21, 2015: FLOORBEAM. CORRODED. ON RBL 27, THE OTBD FLOOR LANDING HAS CORROSION, BETWEEN FS 605.0 & FS 621.0, IN THE CARGO BAY. REMOVED CORRODED FLOORBEAM CAP & REPLACED WITH NEW SERVICEABLE B
- [SDR A6WA201543272](https://openairdocs.org/sdr/A6WA201543272), Nov 21, 2015: WEB. CRACKED. RIGHT WING OTBD LE WEB IS CRACKED, BETWEEN ACCESS PANELS 630KZ & 630LZ. R & R RT OTBD LE WEB, BETWEEN ACCESS PANELS 630KZ & 630LZ IAW SRM 51-42-13.
- [SDR A6WA201543268](https://openairdocs.org/sdr/A6WA201543268), Nov 21, 2015: INTERCOSTAL. CRACKED. CARGO DOOR LOWER AFT VERTICAL MEMBER IS CRACKED FROM TOP TO BOTTOM, CRACK 6" LONG. R & R CARGO DOOR LOWER AFT VERTICAL MEMBER, INTERCOSTAL, IAW SRM 51-42-06 & 5
- [SDR A6WA201543265](https://openairdocs.org/sdr/A6WA201543265), Nov 21, 2015: SEAT TRACK. CORRODED. SMALL SEAT TRACK ON LBL9, JUST FWD OF THE AFT PRESS BULKHEAD HAS CORROSION, IN THE CARGO BAY. R & R SMALL SEAT TRACK, PN 601R31032-51 ON LBL 9, JUST FWD OF THE 
- [SDR A6WA201543271](https://openairdocs.org/sdr/A6WA201543271), Nov 21, 2015: ATTACH ANGLE. CRACKED. APU ENCLOSURE SUPPORT STRUCTURE, RT FWD VERTICAL POST AFT ATTACH ANGLE CRACKED. R & R CRACKED ANGLE FROM RT VERTICAL POST AFT SIDE OF FWD POST OF APU ENCLOSURE 
- [SDR A6WA201543266](https://openairdocs.org/sdr/A6WA201543266), Nov 21, 2015: SEAT TRACK. CORRODED. SEAT TRACK ON LBL 9, BETWEEN FS 559+112 & 574.00 HAS CORROSION, IN THE CARGO BAY. R & R SEAT TRACK, PN 601R38779-5, ON LBL 9, BETWEEN FS 559+112 & 574.00 IAW AM
- [SDR A6WA201543269](https://openairdocs.org/sdr/A6WA201543269), Nov 21, 2015: SKIN. CHAFED. FUSELAGE SKIN IS CHAFED NEXT TO PREVIOUS REPAIR CUT OUT, JUST FWD OF PAX DOOR OPENING & JUST ABOVE WL 79.50. REPAIRED FUSELAGE SKIN JUST FWD OF PAX DOOR OPENING
- [SDR A6WA201543267](https://openairdocs.org/sdr/A6WA201543267), Nov 21, 2015: SEAT TRACK. CORRODED. SEAT TRACK ON RBL 9 HAS CORROSION, BETWEEN FS 559+80 & FS 559+96 IN THE CARGO BAY. R & R SEAT TRACK IAW AMM 53-01-11.
- [SDR A6WA201543274](https://openairdocs.org/sdr/A6WA201543274), Nov 21, 2015: DRAG ANGLE. CRACKED. LEFT MLG WW DRAG ANGLE FWD MOUNT STRUCTURE IS CRACKED. R & R LT MLG WW DRAG ANGLE FWD MOUNT STRUCTURE IAW EA 30-2015-523 & SUP 15-287.
- [SDR A6WA201543275](https://openairdocs.org/sdr/A6WA201543275), Nov 21, 2015: DRAG ANGLE. CRACKED. RIGHT MLG WW DRAG ANGLE COMMON TO BAT RIB IS CRACKED IN THE AFT RADIUS. R & R RT MLG DRAG ANGLE COMMON TO BAT RIB IAW SRM 51-42-21.
- [SDR A6WA201543273](https://openairdocs.org/sdr/A6WA201543273), Nov 21, 2015: DRAG ANGLE. CRACKED. RIGHT MLG WW DRAG ANGLE FWD MOUNT STRUCTURE IS CRACKED. R & R RT MLG WW DRAG ANGLE FWD MOUNT STRUCTURE IAW EA 30-2015-523 & AWAC SUPPLEMENT 15-287.
- [SDR A6WA201543264](https://openairdocs.org/sdr/A6WA201543264), Nov 20, 2015: ATTACH ANGLE. CRACKED. APU ENCLOSURE SUPPORT STRUCTURE, RT AFT ATTACH ANGLE SUPPORT BRACKET CRACKED. REMOVED CRACKED ATTACH ANGLE ON APU SUPPORT STRUCTURE, RT AFT SIDE & REPLACED WITH
- [SDR A6WA201543258](https://openairdocs.org/sdr/A6WA201543258), Nov 17, 2015: FRAME SPLICE. BENT. FRAME SPLICE AT FS 736.00, STRINGER 6L - 7L BENT.
- [SDR A6WA201543248](https://openairdocs.org/sdr/A6WA201543248), Nov 15, 2015: SEAT TRACK. CORRODED. RIGHT AISLE SEAT TRACK STICK NR 1 HAS CORROSION, BETWEEN FS 364 & 394, REPLACED.
- [SDR A6WA201543249](https://openairdocs.org/sdr/A6WA201543249), Nov 15, 2015: SEAT TRACK. CORRODED. RIGHT AISLE SEAT TRACK STICK NR 4 HAS CORROSION, BETWEEN FS 559 & 559+96, REPLACED.
- [SDR A6WA201543251](https://openairdocs.org/sdr/A6WA201543251), Nov 15, 2015: FLOORBEAM. CORRODED. FLOORBEAM 589 CAP HAS CORROSION ON THE TOP SIDE, BETWEEN RBL 27 & THE RT FLOOR SILL, REPLACED.
- [SDR A6WA201543250](https://openairdocs.org/sdr/A6WA201543250), Nov 15, 2015: FLOORBEAM. CORRODED. FLOORBEAM 559+80 CAP HAS CORROSION ON THE TOP SIDE, BETWEEN LBL 9 & RBL 9, REPLACED.
- [SDR A6WA201543247](https://openairdocs.org/sdr/A6WA201543247), Nov 15, 2015: SEAT TRACK. CORRODED. RIGHT AISLE SEAT TRACK STICK NR 3 HAS CORROSION, BETWEEN 409+128 & 559, REPLACED.
- [SDR A6WA201543252](https://openairdocs.org/sdr/A6WA201543252), Nov 15, 2015: STRUCTURE. CRACKED. PLATFORM SKIN IS CRACKED NEXT TO ADG RETRACTION PUMP, OTBD SIDE AT FRAME CUT OUT, REPAIRED.
- [SDR A6WA201543234](https://openairdocs.org/sdr/A6WA201543234), Nov 10, 2015: FITTING. CRACKED. OUTBOARD CLIP ON STRINGER 3L CRACKED AT FS 280, IN CABIN.
- [SDR A6WA201543233](https://openairdocs.org/sdr/A6WA201543233), Nov 10, 2015: FITTING. CRACKED. INBOARD CLIP ON STRINGER 3L CRACKED AT FS 280, IN CABIN.
- [SDR A6WA201542972](https://openairdocs.org/sdr/A6WA201542972), Aug 9, 2015: STRIP. MISINSTALLED. FLIGHT 3737, 3884 EMER FLOOR TRACK LIGHTING ARROWS POINT BACKWARDS, LAST SECTION. FOUND EMER FLOOR AFT STRIP BY LAVATORY INSTALLED INCORRECTLY. REINSTALLED EMER
- [SDR A6WA201542727](https://openairdocs.org/sdr/A6WA201542727), May 12, 2015: LIGHT. INOPERATIVE. FLIGHT 3862, STRIP OF EMERGENCY FLOOR LIGHT NOT WORKING ROW 12. REPLACED ROW 12 FLOOR TRACK EMERGENCY STRIP IAW AMM 33-50. OPERATIONS CHECKED GOOD.
- [SDR A6WA201542592](https://openairdocs.org/sdr/A6WA201542592), Apr 6, 2015: ACTUATOR. FAILED. WHEN SELECTING FLAPS FROM 8 DEG TO 20 DEG, AT 17 LT & 15 RT INDICATED, FLAPS FAILED. COMPLIED WITH FLAP CIRCUIT BREAKER RESET. ON 3RD RETRACTION FLAPS FAILED WH
- [SDR A6WA201542522](https://openairdocs.org/sdr/A6WA201542522), Mar 15, 2015: CONNECTOR. MISSING. REQUIRES INSPECTION OF FLOOR TRACK LIGHTING AT ROW 1D-F, PULLED FROM FLOOR BY PAX. INSPECTED FLOOR TRACK LIGHTING AT ROW 1 D & F, FOUND TRACK PULLED UP FROM FLO
- [SDR A6WA201442081](https://openairdocs.org/sdr/A6WA201442081), Oct 23, 2014: WARNING SYSTEM. FALSE ACTIVATION. ON TAKEOFF SELECTED GEAR UP & RECEIVED GEAR DISAGREE WARNING. COMPLIED WITH QRH & MSG CLEARED. GEAR EXTENDED NORMALLY ON EXTENSION.
- [SDR A6WA201310214288](https://openairdocs.org/sdr/A6WA201310214288), Oct 21, 2013: DRAG ANGLE. CRACKED. LEFT MLG DRAG ANGLE IS CRACKED, COMMON TO UPPER SKIN. R & R ANGLE IAW SRM 51-46-11 & 51-42-21.
- [SDR A6WA201310214267](https://openairdocs.org/sdr/A6WA201310214267), Oct 21, 2013: FRAME. CORRODED. FS 319 FRAME CORRODED. R & R LWR FRAME SEGMENT.
- [SDR A6WA201310214266](https://openairdocs.org/sdr/A6WA201310214266), Oct 21, 2013: FRAME. CORRODED. FS 333 FRAME CORRODED. R & R FRAME SEGMENT.
- [SDR A6WA201310214265](https://openairdocs.org/sdr/A6WA201310214265), Oct 21, 2013: FRAME. CORRODED. FS 349 FRAME CORRODED. R & R FRAME SEGMENT.
- [SDR A6WA201310214264](https://openairdocs.org/sdr/A6WA201310214264), Oct 21, 2013: FRAME. CORRODED. FS 310 FRAME HAS CORROSION. R & R FRAME SEGMENT.

All 196: https://openairdocs.org/deregistered/N422AW-2018-11-07/reports.md

## FAA accident and incident reports (1)

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 20050512007369I](https://openairdocs.org/incident/20050512007369I), May 12, 2005: Cndair CL6002B19 (N422AW), Harrisburg, PA. (-23) Crew experienced master caution illumination followed by illumination of DC essential bus caution message. Captain elected to divert to MDT and completed…

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