# N976EV: 2001 Bombardier CL-600-2B19, registration cancelled 2024-09-09

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: September 9, 2024
- 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: 7601
- Year built: 2001
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: January 31, 2002
- Certificate issued: September 27, 2019
- Last registry action: September 2, 2023
- Mode S code: AD9A67
- 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/N976EV
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=976EV
- Page: https://openairdocs.org/deregistered/N976EV-2024-09-09

From the FAA registry file of November 4, 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 (72, newest 50)

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

- [SDR ASOA2014021109967](https://openairdocs.org/sdr/ASOA2014021109967), Feb 3, 2014: FLOOR SUPPORT. CORRODED. THE LT FLOOR SUPPORT BETWEN BS 559+48 - 559+80 CORRODED AROUND NUT PLATES AND IN OPEN AREAS. BLENDED CORROSION IAW REO 601R-53-00-526.
- [SDR ASOA2014021109966](https://openairdocs.org/sdr/ASOA2014021109966), Feb 3, 2014: SEAT TRACK. CORRODED. SEAT TRACK AT LBL 9 BETWEEN BS 409 - 409+128 CORRODED. R & R SEAT TRACK IAW AMM 53-01-11.
- [SDR ASOA2014021109965](https://openairdocs.org/sdr/ASOA2014021109965), Feb 3, 2014: SEAT TRACK. CORRODED. SEAT TRACK AT RBL 9 BETWEEN BS 409-409+128 CORRODED. R & R SEAT TRACK IAW AMM 53-01-11 & 53-01-11-400-802.
- [SDR ASOA2014021109964](https://openairdocs.org/sdr/ASOA2014021109964), Feb 3, 2014: SEAT TRACK. CORRODED. SEAT TRACK AT RBL 9 BETWEEN BS 364 - 394 CORRODED. R & R SEAT TRACK IAW AMM 53-01-11-000-802 AND 53-01-11-400-802.
- [SDR ASOA2014021109963](https://openairdocs.org/sdr/ASOA2014021109963), Feb 3, 2014: SEAT TRACK. CORRODED. SEAT TRACK AT LBL 9 BETWEEN BS 364 - 394 CORRODED. R & R SEAT TRACK IAW AMM 53-01-11-000-802 AND 53-01-11-400-802.
- [SDR ASOA2014021109962](https://openairdocs.org/sdr/ASOA2014021109962), Feb 3, 2014: FRAME. CORRODED. FRAME BS 589 CORRODED AT S25R. REMOVED CORROSION IAW SRM 51-21-06-00.
- [SDR ASOA2014021109961](https://openairdocs.org/sdr/ASOA2014021109961), Feb 3, 2014: FRAME. CORRODED. FRAME BS 605, CORRODED FROM S25LT, 25RT. REMOVED CORROSION IAW SRM 51-21-06 AND 53-27-00. MAJOR REPAIR.
- [SDR ASOA2013121809656](https://openairdocs.org/sdr/ASOA2013121809656), Nov 27, 2013: WINDSHIELD. CRACKED. PILOT'S WINDSHIELD CRACKED ENROUTE, ACFT DIVERTED. R & R WINDSHIELD IAW AMM 56-11-01. OPS & LEAK CHECKED GOOD.
- [SDR ASOA2013060703797](https://openairdocs.org/sdr/ASOA2013060703797), May 15, 2013: BULKHEAD. CRACKED. FS 621, BULKHEAD FAILS NDT WITH AN INDICATION AT CARGO TRACK LBL 27.5 WL 130.0 GREATER THAN 50 PERCENT SCREEN HEIGHT. REPAIRED IAW EC/TC REO 601R-53-61-1541 AND
- [SDR ASOA2013060303743](https://openairdocs.org/sdr/ASOA2013060303743), May 15, 2013: BULKHEAD. CRACKED. FS 621 BULKHEAD FAILS NDT WITH AN INDICATION AT CARGO TRACK LBL 27.5 WL 130.0 GREATER THAN 50 PERCENT SCREEN HEIGHT. COMPLIED WITH EC/TC REO 601R-53-61-1541 AND
- [SDR ASOA2013060303742](https://openairdocs.org/sdr/ASOA2013060303742), May 14, 2013: ISOLATOR. BROKEN. FS 621 PRESSURE BULKHEAD FWD FACE HAS 8 BROKEN ISOLATORS AS MARKED WITH ORANGE TAPE. REMOVED 8 BROKEN ISOLATORS AND REPLACED WITH SERVICEABLE PARTS IAW SRM 51-4
- [SDR ASOA2013020102946](https://openairdocs.org/sdr/ASOA2013020102946), Jan 28, 2013: DOOR. BINDING. SERVICE DOOR DIFFICULT TO OPEN FROM THE OUTSIDE. CLEANED EXCESSIVE LUBRICATION FROM OUTER HANDLE. COMPLIED WITH OPS TEST OF THE SERVICE DOOR. OPS CHECK GOOD. AC
- [SDR ASOA2013013102930](https://openairdocs.org/sdr/ASOA2013013102930), Jan 27, 2013: HANDLE. UNKNOWN. SERVICE DOOR HANDLE DIFFICULT TO OPEN. PERFORMED OPS CHECK AT SERVICE DOOR IAW AMM 52-11-00. OPS CHECKED GOOD, NO DEFECT NOTED.
- [SDR ASOA2012091702225](https://openairdocs.org/sdr/ASOA2012091702225), Sep 13, 2012: SENSOR. OUT OF ADJUST. RT GEAR DISAGREE MESSAGE AFTER TAKE OFF. RAN QRH PROCEDURE AND LANDED WITHOUT ISSUE WITH 3 GREEN INDICATED. ACFT RETURNED TO DEPARTURE, EMERGENCY DECLARED. ADJU
- [SDR ASOA2012080302033](https://openairdocs.org/sdr/ASOA2012080302033), Jul 31, 2012: BPSU. FAILED. AFTER TAKEOFF, FLAPS FAILED AT 8 DEGREES. COMPLIED WITH QRH. EMERGENCY DECLARED, ACFT RETURNED TO DEPARTURE. R & R RT BPSU IAW AMM 27-51-10. R & R FECU IAW AMM 
- [SDR ASOA2012080302029](https://openairdocs.org/sdr/ASOA2012080302029), Jul 30, 2012: CONTROL UNIT. FAILED. FLAPS FAILED AT 0 ON APPROACH, SKEW DETECTION SYS DEACTIVATED. EMERGENCY DECLARED. REMOVED AND REPLACED RT BPSU AND FECU. OPS CHECKED GOOD.
- [SDR ASOA201102397](https://openairdocs.org/sdr/ASOA201102397), Dec 19, 2011: LAMP. BURNED OUT. PAX DOOR EMERGENCY INOPERATIVE. RELAMPED PAX DOOR OUTER EMERGENCY LIGHT IAW AMM 33-51-21. OPS CHECKED GOOD.
- [SDR ASOA201101116](https://openairdocs.org/sdr/ASOA201101116), Jun 2, 2011: LAMP. BURNED OUT. EXTERIOR RT AFT EMERGENCY LIGHT IS INOP. R & R EXTERIOR RT AFT EMERGENCY LIGHT LAMP IAW MM 33-51-21-000-810 AND 33-51-21-400-801. OPS CHECKED GOOD.
- [SDR ASOA201101067](https://openairdocs.org/sdr/ASOA201101067), May 19, 2011: FLOORBEAM. CORRODED. FLIGHT DECK FLOOR SUPPORT ANGLE AT FS 280 IS CORRODED. LOCATED AND DRILLED NEW FLOOR SUPPORT FOR FLIGHT DECK FS 280 ANGLE IAW SRM 51-42-06. INSTALLED ANGLE. THI
- [SDR ASOA201101055](https://openairdocs.org/sdr/ASOA201101055), May 19, 2011: FLOORBEAM. CORRODED. CORROSION AROUND FASTENER HOLES IN CARGO BAY ON FLOORBEAM. REMOVED CORROSION ON FLOORBEAM IAW SRM 51-21-06. FOUND OUT OF LIMITS IAW SRM 53-00-00. REMOVED FLOORB
- [SDR ASOA201101054](https://openairdocs.org/sdr/ASOA201101054), May 19, 2011: CARGO TRACK. CORRODED. CORROSION AROUND FASTENER HOLES IN CARGO BAY ON RBL 27 FROM FS 605 TO FS 621. FINAL DRILLED, SEALED AND INSTALLED NEW SEAT RAIL IAW SRM 51-42-21, 51-45-06, 51-4
- [SDR ASOA201101053](https://openairdocs.org/sdr/ASOA201101053), May 19, 2011: CARGO TRACK. CORRODED. CORROSION ON 1 CARGO BAY SEAT RAIL AND 3 ANCHOR PLATES AND ATTACHING HARDWARE AT LBL 27. REMOVED SEVERELY CORRODED FASTENERS & 1 EA SEAT TRACK, 3 EA ANCHOR PLAT
- [SDR ASOA201101035](https://openairdocs.org/sdr/ASOA201101035), May 19, 2011: SEAT TRACK. CORRODED. CORROSION ON CARGO BAY SEAT RAIL AND 2 ANCHOR PLATES AT LBL 18 AND ATTACHING HARDWARE. REMOVED SEVERELY CORRODED SCREWS & TRACKS, ANCHOR PLATES. INSTALLED NEW P
- [SDR ASOA201101034](https://openairdocs.org/sdr/ASOA201101034), May 19, 2011: FLOOR SUPPORT. CORRODED. CORROSION IN CARGO BAY ON RT FLOOR SUPPORT FROM FS 559+80 - 621. REPAIRED IAW REO 601R-53-61-4074, REV.
- [SDR ASOA201101033](https://openairdocs.org/sdr/ASOA201101033), May 19, 2011: SEAT TRACK. CORRODED. CORROSION ON 1 CARGO BAY SEAT RAIL AT RBL 27 AND ATTACHMENT HARDWARE. REMOVED CORRODED SCREWS & CORRODED SEAT RAIL, INSTALLED NEW SEAT RAIL & NEW HARDWARE IAW S
- [SDR ASOA201101032](https://openairdocs.org/sdr/ASOA201101032), May 19, 2011: SEAT TRACK. CORRODED. CORROSION ON 2 CARGO BAY SEAT RAILS AT RBL 18 AND ATTACHING HARDWARE. REMOVED CORRODED SCREWS & TRACK SEGMENT. INSTALL NEW TRACK WITH NEW HARDWARE IAW SRM 51-41
- [SDR ASOA201100990](https://openairdocs.org/sdr/ASOA201100990), May 16, 2011: POST. CRACKED. FS 409+128 VERT POST BL 0 FAILS NDT WITH AN INDICATION IN LT AFT CHANNEL ON UPPER END. GREATER THAN 50 PERCENT SCREEN HEIGHT APPROX .1 LONG. REMOVED POST, LOCAT
- [SDR ASOA201100989](https://openairdocs.org/sdr/ASOA201100989), May 16, 2011: POST. CRACKED. FS 409+128 VERTICAL POST, RBL 18 FAILS NDT WITH AN INDICATION IN OTBD AFT CHANNEL ON UPPER END. GREATER THEN 50 PERCENT SCREEN HEIGHT APPROX 1" LONG. REMOVED PO
- [SDR ASOA201100988](https://openairdocs.org/sdr/ASOA201100988), May 16, 2011: ANGLE. CRACKED. CARGO DOOR SUPPORT BEAM AFT LOWER ANGLE IS CRACKED APPROX .3" IN LENGTH. REMOVED CRACKED ANGLE AND REPLACED WITH NEW. INSTALLED NEW ANGLE IAW SRM 51-42-21. MINO
- [SDR ASOA201100987](https://openairdocs.org/sdr/ASOA201100987), May 16, 2011: FLOOR SUPPORT. CORRODED. CORROSION ON FLOOR SUPPORT AROUND NUTPLATES LBL 27, FS 574.00-621.00. REMOVED FLOOR SUPPORT AND MATCHED DRILL NEW FLOOR SUPPORT IAW SRM 51-42-06, 51-42-21. INST
- [SDR ASOA201100986](https://openairdocs.org/sdr/ASOA201100986), May 16, 2011: ISOLATOR. CRACKED. FS 621.0 BULKHEAD CARGO PANEL NUTPLATE ISOLATORS MISSING OR BROKEN 3 EA, 1 AT LBL 9, 2ND FROM FLOOR, 1 AT RBL 9 2ND FROM FLOOR, AND 1 AT LBL 27, 4TH UP FROM FLO
- [SDR ASOA201100985](https://openairdocs.org/sdr/ASOA201100985), May 16, 2011: FLOORBEAM. CORRODED. RIGHT FS 349 FLOORBEAM CORRODED ON OTBD END AT SERVICE DOOR ENTRANCE. REPAIRED IAW REO 601R-53-21-1286.
- [SDR ASOA201100984](https://openairdocs.org/sdr/ASOA201100984), May 16, 2011: ANGLE. CRACKED. FS 484, ANGLE AT OBS OF LBL 27 IS CRACKED. LOCATED, DRILLED AND INSTALLED NEW SERVICEABLE CLIP (PN 601R31171-17) AT FS 484 OTBD SIDE OF LBL 27 WITH 8 EA NEW HI-
- [SDR ASOA201100983](https://openairdocs.org/sdr/ASOA201100983), May 16, 2011: ANGLE. CRACKED. FS 484, ANGLE AT OBS OF RBL 27 IS CRACKED. LOCATED, DRILLED AND INSTALLED NEW SERVICEABLE CLIP (PN 601R31171-9) AT FS 484 OTBD SIDE OF RBL 27 WITH 8 EA NEW HI-L
- [SDR ASOA201100964](https://openairdocs.org/sdr/ASOA201100964), May 13, 2011: WEB. CRACKED. FS 280.0 WEB IS CRACKED OTBD OF LBL 9, RBL 9. REPAIRED IAW REO 601R-53-11-926, REV B.
- [SDR ASOA201100960](https://openairdocs.org/sdr/ASOA201100960), May 11, 2011: INTERCOSTAL. CRACKED. RIGHT FS 621.00-625.30 INTERCOSTAL AT S14R IS CRACKED NEAR RADIUS APPROX .7" LONG. R & R CRACKED INTERCOSTAL IAW SRM 51-42-21. CLASSIFIED AS A MINOR REPAIR.
- [SDR ASOA201001318](https://openairdocs.org/sdr/ASOA201001318), Sep 12, 2010: CONTROL UNIT. FAILED. "SPOILERONS" MESSAGE IN FLIGHT(EMERGENCY DECLARED). R & R NR 2 SECU IAW AMM 27-61-05. OPS CHECK GOOD, NO DEFECT NOTED AT THIS TIME. (CLOSED)
- [SDR ASOA20100001](https://openairdocs.org/sdr/ASOA20100001), Dec 26, 2009: ECU. FAILED. IAW FIM 32-50-00 R & R NWS ECU IAW AMM 32-51-10. OPS CHECK GOOD. (CLOSED)
- [SDR ASOA201000001](https://openairdocs.org/sdr/ASOA201000001), Dec 26, 2009: STEERING SYS. INOPERATIVE. AFTER T/O RECEIVED "STEERING INOP" CAUTION MESSAGE. RETURNED TO DEPARTURE. STEERING RESET ON GROUND. (EMERGENCY DECLARED -- ACFT RETURNED TO DEPARTURE AFTER T/O
- [SDR ASOA200901338](https://openairdocs.org/sdr/ASOA200901338), Dec 1, 2009: LIGHT. INOPERATIVE. LT EXTERIOR NR 4 EMERGENCY LIGHT INOP.
- [SDR ASOA200901337](https://openairdocs.org/sdr/ASOA200901337), Dec 1, 2009: LIGHT. INOPERATIVE. RT EXTERIOR NR 2 EMERGENCY LIGHT INOP.
- [SDR ASOA200901336](https://openairdocs.org/sdr/ASOA200901336), Dec 1, 2009: LIGHT. INOPERATIVE. NR 4 CEILING EMERGENCY LIGHT INOP.
- [SDR ASOA200900746](https://openairdocs.org/sdr/ASOA200900746), Jul 5, 2009: LIGHT. INOPERATIVE. FWD OVERWING EMERGENCY LIGHT INOP.
- [SDR ASOA200900654](https://openairdocs.org/sdr/ASOA200900654), Jun 11, 2009: WIRE. BROKEN. WARDROBE LOWER EMERGENCY LIGHT WIRE HAS END BROKEN OFF.
- [SDR ASOA200900626](https://openairdocs.org/sdr/ASOA200900626), May 29, 2009: POST. DAMAGED. LT FS 409.0+128 O/B VERTICAL POST LBL 18.0 HAS AN INDICATION NOTED APPROX .2 INCHES IN LENGTH 50 PERCENT FSH AT WL 69.0. FAILED NDT INSPECTION. REMOVED LBL 18 P
- [SDR ASOA200900593](https://openairdocs.org/sdr/ASOA200900593), May 27, 2009: BULKHEAD. DAMAGED. JOB 8760125 OPERATION 198 REAR PRESSURE BULKHEAD WEB THAT SURROUNDS THE LINTEL FITTING HAS AN INDICATION NOTED APPROX .2" IN LENGTH 70% FSH. FAILED NDT INSPECTI
- [SDR ASOA200900590](https://openairdocs.org/sdr/ASOA200900590), May 26, 2009: SEAT TRACK. CORRODED. FLOOR SEAT TRACK RBL 9, FS 399.5 HAS CORROSION AROUND SCREW HOLES. REMOVED SEAT TRACK AND INSTALLED NEW SEAT TRACK IAW SRM 51-40-11 AND AMM 53-01-11-420-001B.
- [SDR ASOA200900589](https://openairdocs.org/sdr/ASOA200900589), May 26, 2009: SEAT TRACK. CORRODED. FLOOR SEAT TRACK RBL 9, FS 364 HAS CORROSION AROUND SCREW HOLES. REMOVED SEAT TRACK & INSTALLED NEW FLOOR SEAT TRACK IAW AMM 53-01-11.
- [SDR ASOA200900580](https://openairdocs.org/sdr/ASOA200900580), May 23, 2009: BULKHEAD. DAMAGED. RT FS 559 BULKHEAD WEB HAS AN INDICATION NOTED AT WL 59.10 I/B OF RBL 18.0 APPROX .3" IN LENGTH 70% FSH. FAILED NDT INSPECTION. COMPLIED WITH REPAIR AT FS 559 B
- [SDR ASOA200900578](https://openairdocs.org/sdr/ASOA200900578), May 23, 2009: DRAG ANGLE. CRACKED. JOB 8760121 OPERATION 139 PAX DOOR AFT DRAG ANGLE IS CRACKED 1.25"L JUST ABOVE THE DOOR ASSIST CABLE PULLEY. REPAIRED PAX DOOR CRACKED AFT DRAG ANGLE PRE-EXISTI

All 72: https://openairdocs.org/deregistered/N976EV-2024-09-09/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 20091226053589I](https://openairdocs.org/incident/20091226053589I), Dec 26, 2009: Bombardier CL-600-2B19 (N976EV), Atlanta, GA, No damage. On December 26, 2009, atlantic southeast airlines (asoa) flight 5050, operating from Atlanta, Georgia to savannah, Georgia with CRJ-200 aircraft N976EV,…

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