# N684BR: 2002 Bombardier CL-600-2B19, registration cancelled 2022-01-03

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: January 3, 2022
- 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: 7708
- Year built: 2002
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: November 13, 2002
- Certificate issued: February 14, 2020
- Last registry action: February 14, 2020
- Mode S code: A9123C
- 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/N684BR
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=684BR
- Page: https://openairdocs.org/deregistered/N684BR-2022-01-03

From the FAA registry file of November 5, 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 (47)

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

- [SDR ASOA201201013](https://openairdocs.org/sdr/ASOA201201013), Mar 26, 2012: BULB. BURNED OUT. LEFT EXTERNAL AFT EMERGENCY LIGHT INOPERATIVE. REMOVED AND INSTALLED A NEW BULB IAW AMM 33-51-21. OPS CHECKED GOOD.
- [SDR ASOA201200433](https://openairdocs.org/sdr/ASOA201200433), Feb 8, 2012: GROUND WIRE. DISCONNECTED. SERVICE DOOR LIGHTED EXIT SIGN INOPERATIVE. CONNECTOR GROUND TERMINAL END TO GROUNDING STUD IAW ESPM 20-20-00. OPS CHECKED GOOD. C
- [SDR ASOA201101982](https://openairdocs.org/sdr/ASOA201101982), Oct 17, 2011: LAMP. BURNED OUT. FLOOR EMERGENCY EXIT LIGHT BY ASD DIM. RELAMPED IAW AMM 33-50-19, OPS CHECKED GOOD.
- [SDR ASOA201001439](https://openairdocs.org/sdr/ASOA201001439), Sep 24, 2010: LAMP. BROKEN. RT EXTERIOR NR 2 EMERGENCY LIGHT INOP. RELAMPED RT EXTERIOR NR2 EMERGENCY LIGHT IAW AMM 33-51-21. OPS CHECK GOOD. RELAMPED RT EXTERIOR NR2 EMERGENCY LIGHT IAW A
- [SDR ASOA201000962](https://openairdocs.org/sdr/ASOA201000962), Jun 27, 2010: DOOR. MISINSTALLED. RT OVERWING EMERGENCY EXIT DOOR IS DIFFICULT TO OPEN. UPON INVESTIGATION FOUND THE OVERWING EMERGENCY EXITS TO BE INSTALLED IN THE INCORRECT POSITION. INSTALLED
- [SDR ASOA201000935](https://openairdocs.org/sdr/ASOA201000935), Jun 23, 2010: FLOOR SUPPORT. CORRODED. CARGO COMPARTMENT FLOORBEAM CAP IS CORRODED BEYOND REPAIR AT LBL 27 FROM FS 569.00 TO FS 621.00. EC/TC REQUIRED FOR REO 601R-53-61-3400 REV.H. COMPLIED WITH EC/
- [SDR ASOA201000920](https://openairdocs.org/sdr/ASOA201000920), Jun 17, 2010: FRAME. CORRODED. LEFT FRAME 513.00 HAS CORROSION AT PRESSURE FLOOR. COMPLIED WITH STEP 2 OF REO 601R-53-41-1241. PERFORMED EDDY CURRENT OF LT FRAME 513 AT PRESSURE FLOOR REPAIR 
- [SDR ASOA201000919](https://openairdocs.org/sdr/ASOA201000919), Jun 17, 2010: PRESSURE PANEL. CORRODED. LEFT PRESSURE FLOOR SKIN OTBD OF LBL 36 HAS AREAS OF CORROSION. C/W REO 601R-53-41-666, REV A.
- [SDR ASOA201000917](https://openairdocs.org/sdr/ASOA201000917), Jun 17, 2010: SILL. CRACKED. SUPPORT ANGLE AT FS 589.00, LBL 36 UNDER CARGO DOOR FLOOR SILL IS CRACKED. LOCATED & INSTALLED NEW SUPPORT ANGLE IAW SRM 51-42-06 & 51-42-21.
- [SDR ASOA201000916](https://openairdocs.org/sdr/ASOA201000916), Jun 17, 2010: SEAT TRACK. CORRODED. LEFT WALL SEAT TRACK AT FS 559+75 IS CORRODED. REMOVED CORRODED SEAT RAIL SECTION ON LT WALL IAW AMM 53-01-11-000-802. INSTALLED NEW RAIL SECTION IAW AMM 53-01-
- [SDR ASOA201000898](https://openairdocs.org/sdr/ASOA201000898), Jun 11, 2010: FLOOR SUPPORT. CORRODED. CARGO COMPARTMENT FLOOR SUPPORT CAP IS CORRODED BEYOND REPAIR AT LBL 27 FROM FS 569.00 TO FS 621.00. REMOVED CARGO COMPARTMENT FLOOR SUPPORT CAP IAW SRM 51-42-2
- [SDR ASOA201000897](https://openairdocs.org/sdr/ASOA201000897), Jun 11, 2010: SEAT TRACK. CORRODED. CARGO COMPARTMENT SEAT RAILS AT RBL 9 BETWEEN FS 559.00+80 AND FS 569.00 ARE CORRODED. REPLACED SEAT RAILS IAW SRM 51-41-02. FOUND FITTING BROKEN ON SEAT TRACK 
- [SDR ASOA201000896](https://openairdocs.org/sdr/ASOA201000896), Jun 11, 2010: SEAT TRACK. CORRODED. CARGO COMPARTMENT SEAT RAILS AT LBL 9 BETWEEN FS 559+91 AND FS 617.00 ARE CORRODED. R & R SEAT RAILS AND ANCHOR PLATES IAW SRM 51-41-02.
- [SDR ASOA201000895](https://openairdocs.org/sdr/ASOA201000895), Jun 11, 2010: SEAT TRACK. CORRODED. CARGO COMPARTMENT SEAT RAILS AT LBL 27 BETWEEN FS 559+80 AND 567.00 ARE CORRODED. R & R SEAT RAILS IAW SRM 51-41-02.
- [SDR ASOA201000894](https://openairdocs.org/sdr/ASOA201000894), Jun 11, 2010: SEAT TRACK. CORRODED. CARGO COMPARTMENT SEAT RAIL AT RBL 27 FS 559.00+80 TO 559.00+96 IS CORRODED. R & R SEAT RAIL IAW SRM 51-41-02.
- [SDR ASOA201000893](https://openairdocs.org/sdr/ASOA201000893), Jun 11, 2010: ANGLE. CRACKED. FOUND FS 559 LT CAP ANGLE HAS INDICATION NOTED, APPROX .3" IN LENGTH 60 PERCENT FSH AT LBL 18.0 AND FS 559 RT. BULKHEAD WEB HAS INDICATIONS NOTED APPROX .3" IN 
- [SDR ASOA201000909](https://openairdocs.org/sdr/ASOA201000909), Jun 10, 2010: DRAG ANGLE. CRACKED. PAX DOOR AFT DRAG ANGLE IS CRACKED IN PREVIOUS REPAIR. COMPLIED WITH EC/TC REO 601R-52-11-513 IAW REO 601R-52-11-513.
- [SDR ASOA201000887](https://openairdocs.org/sdr/ASOA201000887), Jun 10, 2010: CHANNEL. CRACKED. INDICATION NOTES AT FS 409+128 RBL 18 WL 69.0 IN RADIUS OF OTBD U CHANNEL OF THE BULKHEAD BEAM APPROX .30" LONG 50 PERCENT FULL SCREEN HEIGHT. REMOVED RBL 18 VE
- [SDR ASOA201000877](https://openairdocs.org/sdr/ASOA201000877), Jun 9, 2010: SEAT TRACK. CORRODED. LEFT AND RT FWD FLOOR SEAT TRACK SEGMENT IN CABIN ARE CORRODED AT THE FWD ENDS. REMOVED LT AND RT FWD SEAT TRACKS IAW AMM 53-01-11-000-802. INSTALLED NEW SEAT T
- [SDR ASOA201000489](https://openairdocs.org/sdr/ASOA201000489), Apr 4, 2010: LIGHT. BROKEN. LOWER EMERGENCY LIGHT ON F/A WARDROBE BASE BROKEN. R & R FLOOR LEVEL EMERGENCY FLOOD LIGHT ON WARDROBE IAW AMM 33-51-19. OPS CHECK GOOD. R & R FLOOR LEVEL EMERG
- [SDR ASOA200801708](https://openairdocs.org/sdr/ASOA200801708), Dec 12, 2008: FLAP. FAILED. FLAPS FAILED AT 8 WHEN SELECTING 20 ON APPROACH.
- [SDR TRAX200800767](https://openairdocs.org/sdr/TRAX200800767), Jun 6, 2008: SUPPORT BEAM. CRACKED. CARGO DOOR SUPPORT BEAM LOWER ANGLE IS CRACKED .3" IN LENGTH. REMOVED CRACKED SUPPORT BEAM. INSTALLED NEW SERVICEABLE IAW SRM 51-42-21. (B)
- [SDR TRAX200800765](https://openairdocs.org/sdr/TRAX200800765), Jun 5, 2008: ATTACH FITTING. CRACKED. BULKHEAD FS 280.00 LBL 9.0 HAS A CLIP CRACKED .5 INCH. REMOVED OLD CRACKED CLIP AT FS 280.00 LBL 9.0, INSTALLED NEW SERVICEABLE CLIP P/N 601R-31113-57 IAW CRJ 2
- [SDR TRAX200800764](https://openairdocs.org/sdr/TRAX200800764), Jun 5, 2008: INTERCOSTAL. CRACKED. RIGHT FS 484 INTERCOSTAL AT RBL 27.00 AND RBL 36.00 IS CRACKED .25 INCH. REMOVED CLIP FROM FS 484.00, RBL 27.00 AND INSTALLED NEW SERVICEABLE CLIP ON INTERCOSTA
- [SDR TRAX200800742](https://openairdocs.org/sdr/TRAX200800742), Jun 3, 2008: DRAG ANGLE. CRACKED. PASSENGER DOOR STAIR AFT DRAG ANGLE IS CRACKED 1/2" REPAIRED PAX DOOR STAIR AFT DRAG ANGLE IAW REO 601R-52-11-513 AND ET/CT 601R-52-11-513. (B)
- [SDR TRAX200800771](https://openairdocs.org/sdr/TRAX200800771), Jun 3, 2008: PLACARD. WORN. CREW ESCAPE HATCH EXTERNAL PLACARDS ARE UNREADABLE. REAPPLIED SILKSCREENS ON CREW ESCAPE HATCH IAW MM 11-10-03-400-801.
- [SDR TRAX200800727](https://openairdocs.org/sdr/TRAX200800727), Jun 2, 2008: BULKHEAD. CRACKED. FS 202.75 BULKHEAD HAS A .50 INCH CRACK WHERE PARKING BRAKE CABLE GOES THROUGH. REPAIRED FS 202 BULKHEAD IAW ASA EO 600-53-217 IN ITS ENTIRETY. (B)
- [SDR TRAX200800772](https://openairdocs.org/sdr/TRAX200800772), Jun 2, 2008: HINGE FITTING. CRACKED. JOB 8770831 OPERATION 152 CREW ESCAPE HATCH RIGHT HINGE ARM IS CRACKED. RESOLVED ON W/O: 91780 TASKCARD: N/R-00192. REMOVED AND REPLACED RT HINGE ARM ON CREW ES
- [SDR TRAX200800057](https://openairdocs.org/sdr/TRAX200800057), Jan 7, 2008: LIGHT. INOPERATIVE. WHITE EMERGENCY EXIT LIGHT BY PAX DOOR INOP.
- [SDR TRAX200701270](https://openairdocs.org/sdr/TRAX200701270), Sep 1, 2007: SIGN. INOPERATIVE. EMERGENCY EXIT SIGN AT ASD IS INOP.
- [SDR TRAX200701143](https://openairdocs.org/sdr/TRAX200701143), Aug 8, 2007: STEP. CRACKED. ASD BOTTOM STEP CRACKED.
- [SDR TRAX200700718](https://openairdocs.org/sdr/TRAX200700718), May 23, 2007: BRACKET. CRACKED. PAX DOOR AFT CABLE COUNTER BALANCE ANCHOR BRACKET CRACKED.
- [SDR TRAX200700419](https://openairdocs.org/sdr/TRAX200700419), Mar 21, 2007: LIGHT. INOPERATIVE. RIGHT FWD EMERGENCY LIGHT OUT.
- [SDR TRAX200700177](https://openairdocs.org/sdr/TRAX200700177), Feb 5, 2007: FLAP SYSTEM. MALFUNCTIONED. WHEN ATTEMPTING TO EXTEND FLAPS TO 8 DEG, FAILED AT 0 DEG. EN ROUTE TO ERI A/C DIVERTED TO CLE DUE TO MTC. EMERGENCY DECLARED. FLT 4266 CX & ON 02/0607 FLTS 463
- [SDR TRAX200700049](https://openairdocs.org/sdr/TRAX200700049), Jan 7, 2007: LIGHT. INOPERATIVE. RT EMERG EXTERIOR OVERWING FWD LIGHT IS INOP.
- [SDR TRAX200601065](https://openairdocs.org/sdr/TRAX200601065), Nov 28, 2006: BEAM. CRACKED. SUSPECT CRACK ON RT SIDE OF ENGINE SUPPORT BEAM. REPAIRED IAW ALL PERTINENT REPAIR INSTRUCTIONS.
- [SDR TRAX200601064](https://openairdocs.org/sdr/TRAX200601064), Nov 28, 2006: FRAME. CRACKED. SUSPECT CRACK ON FS 640 FRAME PER INSPECTION OF TASK CARD E0600-53-69-0002. FLT 4256 CX.
- [SDR TRAX200601063](https://openairdocs.org/sdr/TRAX200601063), Nov 28, 2006: ANCHOR FITTING. CRACKED. A/S/D AFT CABLE COUNTER BALANCE ANCHOR BRACKET CRACKED.
- [SDR TRAX200600991](https://openairdocs.org/sdr/TRAX200600991), Nov 5, 2006: MASTER CAUTION. ILLUMINATED. NOSE GEAR DISAGREE MASTER CAUTION AFTER TAKEOFF AND GEAR UNSAFE CAUTION WARNING. A/C RETURNED TO SHV AFTER T/O. EMERGENCY DECLARED. FLT 4884 CX.
- [SDR TRAX200600952](https://openairdocs.org/sdr/TRAX200600952), Oct 27, 2006: LANDING GEAR. INOPERATIVE. NLG DID NOT RETRACT AFTER TAKEOFF, C/W QRH AND RETURNED TO OMA. FLT 4418 CX - EMERGENCY DECLARED.
- [SDR TRAX200600401](https://openairdocs.org/sdr/TRAX200600401), Jun 20, 2006: ANGLE. CRACKED. ETNRC 100-1 ANGLE CRACK AT FS260 RBL 11 UNDER FLOOR BEAM.
- [SDR VTZA200500213](https://openairdocs.org/sdr/VTZA200500213), Oct 19, 2005: SWITCH. FAULTY. STABILIZER TRIM/MACH TRIM CAUTION MESSAGE. FOUND PILOT STAB DISCONNECT SWITCH FAULTED. REMOVED AND REPLACED SWITCH.
- [SDR 04317684](https://openairdocs.org/sdr/04317684), Nov 12, 2004: ENGINE. SHUTDOWN. EVENT SUMMARY STATED RIGHT ENG SHUT DOWN IN FLT DUE TO LOW OIL PRESSURE. REMOVED AND REPLACED AGB CARBON SEALS FOR IDG, ATS AND HYDRAULIC PUMP IAW AMM 72-60-00.
- [SDR 04311684](https://openairdocs.org/sdr/04311684), Nov 6, 2004: WARNING LIGHT. ILLUMINATED. EVENT SUMMARY STATED THRUST REVERSER UNLOCK MESSAGE IN FLIGHT. OPENED DM 3114105-1 MEL 78-30-01 CAT B. RIGHT THRUST REVERSER UNLOCK MESSAGE ON ROTATION, (M) PRO
- [SDR 04021684](https://openairdocs.org/sdr/04021684), Jan 21, 2004: BULB. BURNED OUT. DURING INSPECTION THE LEFT HAND FUSELAGE EMERGENCY LIGHT WAS FOUND INOPERATIVE. THE BULB WAS REPLACED AND A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED. AIRCRA
- [SDR 03273684](https://openairdocs.org/sdr/03273684), Sep 30, 2003: BULB. BURNED OUT. DURING INSPECTION THE FORWARD OVERHEAD EMERGENCY LIGHT WAS FOUND INOPERATIVE. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE EMERGENCY LIGHT. A SATISFACTORY OPE
- [SDR 02347684](https://openairdocs.org/sdr/02347684), Feb 13, 2002: CONNECTOR. NOT SEATED. DURING OVERNIGHT MAINTENANCE IT WAS DISCOVERED THAT THE FLIGHT ATTENDANT EMERGENCY LIGHT SWITCH WAS INOPERATIVE. MAINTENANCE PERSONNEL RESEATED THE CONNECTOR PL

## 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 20061027022469I](https://openairdocs.org/incident/20061027022469I), Oct 27, 2006: Cndair CL6002B19 (N684BR), Omaha, NE. (-23) N684BR, CL-600-2B1, was being operated by atlantic southeast airlines as delta connection flight 4418, from oma to atl. The crew reported that the nose…

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