# N849AS: 1999 Bombardier CL-600-2B19, registration cancelled 2025-12-09

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: December 9, 2025
- 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: 7347
- Year built: 1999
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: November 17, 1999
- Certificate issued: April 22, 2019
- Last registry action: July 28, 2023
- Mode S code: ABA159
- Owner when cancelled: [Frontera Flight Holdings Inc](https://openairdocs.org/faa-owner/FRONTERA%20FLIGHT%20HOLDINGS%20INC)
- Location: [Laredo, TX](https://openairdocs.org/faa-place/TX/Laredo)
- Owner type: Corporation
- Owner's area on the map: 27.8338° N, 99.6814° W: Placed by OpenAirDocs at the center of ZIP code 78045, within about 15 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N849AS
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=849AS
- Page: https://openairdocs.org/deregistered/N849AS-2025-12-09

From the FAA registry file of October 31, 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 (162, newest 50)

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

- [SDR ASOA2016081615271](https://openairdocs.org/sdr/ASOA2016081615271), Aug 16, 2016: BATTERY. DISCHARGED. FWD CABIN EMERGENCY LIGHTS ARE NOT ILLUMINATING IN THE CEILING AND AT THE FWD EXITS AND GALLEY. CHARGED & OPS CHECKED OK IAW AMM 33-51-04.
- [SDR ASOA2016041214701](https://openairdocs.org/sdr/ASOA2016041214701), Apr 12, 2016: ROLLER. STUCK. PASSENGER DOOR WOULD NOT OPEN FROM THE OUTSIDE. FREED ROLLER ON INNER HANDLE AND PERFORMED OPS CHECK. NO FURTHER DEFECTS NOTED AMM 52-11-00.
- [SDR ASOA2016040714695](https://openairdocs.org/sdr/ASOA2016040714695), Apr 7, 2016: ROLLER. FAILED. PASSENGER DOOR WILL NOT OPEN FROM OUTSIDE. R & R PASSENGER DOOR ROLLER ASSY IAW AMM 52-11-02. LUBED AND PERFORMED OPS CHECK OF PASSENGER DOOR OUTER HANDLE ASSY 
- [SDR ASOA2016040314683](https://openairdocs.org/sdr/ASOA2016040314683), Apr 3, 2016: HANDLE. LACK OF LUBE. COULD NOT OPEN PAX DOOR FROM OUTSIDE ACFT. HAD TO ENTER ACFT FROM SERVICE DOOR. WAS ABLE TO OPEN FROM INSIDE. TESTED DOOR AGAIN FROM OUTSIDE W/ NO SUCCESS. FOUN
- [SDR ASOA2016012114374](https://openairdocs.org/sdr/ASOA2016012114374), Jan 21, 2016: LENS. MISSING. MISSING LENS ON OVERHEAD EMERGENCY EXIT LIGHT. INSTALLED MISSING LENS ON OVERHEAD EMERGENCY EXIT LIGHT IAW AMM 33-51-14.
- [SDR ASOA2015102313949](https://openairdocs.org/sdr/ASOA2015102313949), Oct 23, 2015: APU. ODOR. DURING APPROACH STRONG AROMA OF FUEL/OIL FILLED CABIN COMING FROM APU IN AFT EQUIPMENT BAY. AUXILIARY POWER UNIT, APU, DOOR POSITION VERIFIED CLOSED. DEFER CLEA
- [SDR ASOA2015081313480](https://openairdocs.org/sdr/ASOA2015081313480), Aug 13, 2015: ACTUATOR. FAILED. UNCOMMENDED YAW DAMPER IN MOTION WAS DETECTED IN THE CLIMB AROUND 290 KNOTS WITH AP OFF C/W QRH AND IN DESCENT MOTION WAS DETECTED 2 TIMES AT 250 KNOTS SEVERAL 
- [SDR ASOA2015071013315](https://openairdocs.org/sdr/ASOA2015071013315), Jul 6, 2015: STRUCTURE. DAMAGED. RIGHT WING L/E NR 1 AND NR 2 HAS 1 EACH SHEAR RIVET LOCATED AT TRANSITION PANEL. COMPLIED WITH EC/TC REO 601R-57-41-001, PERMANENT REPAIR.
- [SDR ASOA2015041012600](https://openairdocs.org/sdr/ASOA2015041012600), Mar 20, 2015: SEAT TRACK. CORRODED. FLOOR BEAM CORRODED INBD SIDE OF SEAT RAIL AT FS94.00-409.00+112. RECEIVED REO 601R-53-31-841, DATED 2015-03-24. REMOVED EXTRUDED FLOORBEAM CAP FS394.00-409.00+
- [SDR ASOA2015041012599](https://openairdocs.org/sdr/ASOA2015041012599), Mar 19, 2015: FLOOR SUPPORT. CORRODED. RIGHT FLOOR SILL AFT OF THE SERVICE DOOR AT FS 349-364 CORRODED. REMOVED CORROSION IAW EC/TC REO 601R-53-00-530 DAMAGE OUT OF LIMITS IAW REO 601R-53-00-530. COM
- [SDR ASOA2015041012598](https://openairdocs.org/sdr/ASOA2015041012598), Mar 19, 2015: SEAT TRACK. CORRODED. FLOOR SEAT RAIL CORRODED AT FS 559.00 TO 559.00 + 80, RBL 9. SEAT RAIL AT RBL 9.0, FS 559.00 TO 559+80 HAS EXFOLIATING CORROSION AROUND SEVERAL FASTENER HEADS O
- [SDR ASOA2015041012597](https://openairdocs.org/sdr/ASOA2015041012597), Mar 19, 2015: DOOR FRAME. CORRODED. FWD OF AVIONICS BAY DOOR ACCESS AT FS 364.00 FWD SIDE CORRODED, BETWEEN STR 25L-25R. REMOVED CORROSION ON FS 364 BETWEEN 26L & 27 STR IAW SRM 51-21-01-00 UPON F
- [SDR ASOA2015041012596](https://openairdocs.org/sdr/ASOA2015041012596), Mar 19, 2015: SEAT TRACK. CORRODED. FLOOR SEAT RAIL AT FS 694.00- 409.00+12 AND RBL 27 CORRODED. FLOOR SEAT RAIL RBL9, FS 394.00 TO 409+112 FOUND TO BE OUT OF LIMITS IAW SRM 53-21-49, FIG 101. REM
- [SDR ASOA2015041012595](https://openairdocs.org/sdr/ASOA2015041012595), Mar 19, 2015: FLOOR SUPPORT. CORRODED. RIGHT OVERWING PRESSURE FLOOR SILL CORRODED BETWEEN FS 484.00 - FS 559.00+21. COMPLIED WITH ECTC REO 601R-53 -41-666, REV C.
- [SDR ASOA2015041012594](https://openairdocs.org/sdr/ASOA2015041012594), Mar 19, 2015: FLOOR SUPPORT. CORRODED. LEFT OVERWING PRESSURE FLOOR SILL CORRODED BETWEEN FS 484.00 - FS 559+21. COMPLIED WITH ECTC REO 601R-53 -41-666-01.
- [SDR ASOA2015041012593](https://openairdocs.org/sdr/ASOA2015041012593), Mar 19, 2015: FLOOR SUPPORT. CORRODED. RIGHT OVERWING PRESSURE FLOOR SUPPORT CORRODED BETWEEN FS 409+128-484.00. COMPLIED WITH EC/TC REO 601R-53-41-666 01, REO 601R 53-41-666, REV C.
- [SDR ASOA2015041012592](https://openairdocs.org/sdr/ASOA2015041012592), Mar 19, 2015: FLOOR SUPPORT. CORRODED. LEFT OVERWING PRESSURE FLOOR SILL CORRODED BETWEEN FS 409+128-FS 484.00. COMPLIED WITH EC/TC REO 601R-53-41-666-01 AND REO 601R-53-41-666, REV C, DATED 11/06/20
- [SDR ASOA2015041012591](https://openairdocs.org/sdr/ASOA2015041012591), Mar 18, 2015: SKIN. CRACKED. RIGHT SIDE WING, AT 148.019 IS CRACKED ON AFT PLANK, PROXIMITY .102. COMPLIED WITH ECTC REO 601R-57-21-130-01 AND REO 601R-57-21-130-01, REV K DATED 11/27/2013 
- [SDR ASOA2015041012590](https://openairdocs.org/sdr/ASOA2015041012590), Mar 16, 2015: DOOR. LACK OF LUBE. LEFT OVERWING EMERGENCY EXIT EXCEEDS MAX FORCE TO OPERATE HANDLE. LUBED LT OVERWING EMERGENCY EXIT DOOR AND PERFORMED FUNCTIONAL CHECK IAW AMM 52-21-00-710-801 
- [SDR ASOA2015041012589](https://openairdocs.org/sdr/ASOA2015041012589), Mar 16, 2015: DOOR. LACK OF LUBE. RIGHT OVERWING EMERGENCY EXIT EXCEEDS MAX FORCE TO OPERATE HANDLE. LUBED RT OVERWING EMERGENCY EXIT DOOR AND PERFORMED FUNCTIONAL CHECK IAW AMM 52-21-00-710-801
- [SDR ASOA2015041012588](https://openairdocs.org/sdr/ASOA2015041012588), Mar 16, 2015: LIGHT. WEAK. EMERGENCY EXITS AND SERVICE DOOR BETA LIGHTS WEAK. R & R EMERGENCY EXIT BETA LIGHTS.
- [SDR ASOA2014121111860](https://openairdocs.org/sdr/ASOA2014121111860), Dec 7, 2014: LIGHT. INOPERATIVE. EMERGENCY LIGHT IN GALLEY AND MAIN PASSENGER ENTRY ARE INOPERATIVE. REPLACED LIGHT IAW AMM 33-51-19.
- [SDR ASOA2014121011859](https://openairdocs.org/sdr/ASOA2014121011859), Dec 6, 2014: LIGHT. INOPERATIVE. EMERGENCY LIGHT AT PASSENGER DOOR INOPERATIVE. R & R THE LIGHT IAW AMM 33-51-19. OPS CHECKED GOOD.
- [SDR ASOA2014100811387](https://openairdocs.org/sdr/ASOA2014100811387), Sep 4, 2014: SKIN. CRACKED. WING SKIN FOUND TO HAVE CRACK INDICATION WHILE PERFORMING LOW FREQUENCY INSPECTION AT WS 65.75 SECOND ROW OF FASTENERS BETWEEN STR8 AND STR9, SECOND FASTENER IN
- [SDR ASOA2014081511069](https://openairdocs.org/sdr/ASOA2014081511069), Aug 11, 2014: BLANKING PLATE. LEAKING. SLOWLY LOST OIL PRESSURE DURING FLIGHT, SHUTDOWN NR 1 ENGINE, OIL PULL NEVER GOT BELOW 25 PSI, EMERGENCY DECLARED. FOUND OIL LEAK AT BLANKING PLATE FOR EDP.
- [SDR ASOA2014042810392](https://openairdocs.org/sdr/ASOA2014042810392), Apr 23, 2014: SKIN. BURNED. BURNS ON LT WINGLET TIP FAIRING. REMOVED DAMAGED LT WINGLET TIP IAW SRM 51-42-13. REMOVED AND REPLACED.
- [SDR ASOA2013110809372](https://openairdocs.org/sdr/ASOA2013110809372), Nov 4, 2013: LAMP. BURNED OUT. NR 7 EXTERIOR EMERGENCY LIGHT INOPERATIVE. REPLACED LAMP IAW AMM 33-51-21, OPS CHECKED GOOD.
- [SDR ASOA2013100209142](https://openairdocs.org/sdr/ASOA2013100209142), Oct 1, 2013: LENS. MISSING. NR 1 CEILING EMERGENCY LIGHT COVER MISSING. INSTALLED NEW COVER IAW AMM 35-51-16, OPS CHECKED GOOD.
- [SDR ASOA2013042203418](https://openairdocs.org/sdr/ASOA2013042203418), Apr 16, 2013: LIGHT. BROKEN. EMERGENCY LIGHT AT LOWER BULKHEAD PAX DOOR BROKEN. R & R FLOOR LEVEL EMERGENCY LIGHT OPS CHECKED GOOD REF MM 33-51-10.
- [SDR ASOA2013041003344](https://openairdocs.org/sdr/ASOA2013041003344), Mar 26, 2013: ACCESS PANEL. CRACKED. RT BOOST PUMP HOLE FAILS NDT WITH AN INDICATION ON AFT SIDE OF HOLE WITH MULTIPLE INDICATING, SOME 50 PERCENT SCREEN HEIGHT (ON LANDING). REPAIRED IAW REO 601R-
- [SDR ASOA2013041003338](https://openairdocs.org/sdr/ASOA2013041003338), Mar 22, 2013: POST. CRACKED. FOUND FS 409+128 VERTICAL POSTS AT LBL18.0 INBD SIDES HAS INDICATION NOTED AT AFT FLANGE RADIUS WL 69.0 APPROX .2" IN LENGTH 50 PERCENT FSH. FAILED NDT INSPECTI
- [SDR ASOA2013041003337](https://openairdocs.org/sdr/ASOA2013041003337), Mar 22, 2013: POST. CRACKED. FOUND FS 409+128 VERTICAL POSTS AT BL0.0 LT & RT SIDES HAVE INDICATIONS NOTED AT AFT FLANGE RADIUS WL 69.0 BOTH APPROX .3" IN LENGTH 70 PERCENT AND 80 PERCENT F
- [SDR ASOA2013041003343](https://openairdocs.org/sdr/ASOA2013041003343), Mar 21, 2013: HINGE. GOUGED. PAX DOOR PIANO HINGE ON PAX DOOR SIDE 1ST AND 6TH LUG FROM AFT SIDE CHAFED. DEEPEST APPROX .015. REMOVED PASSENGER DOOR IAW AMM 52-11-000-801. INSTALLED PASSENG
- [SDR ASOA2013041003342](https://openairdocs.org/sdr/ASOA2013041003342), Mar 21, 2013: ACCESS PANEL. DAMAGED. RT FWD FUSELAGE ACCESS PANEL 132AL DOOR SURROUND FASTENER HOLE DAMAGED AT 7 0'CLOCK POSITION. REPAIRED IAW REO 601R-53-11-2477. MAJOR REPAIR.
- [SDR ASOA2013041003341](https://openairdocs.org/sdr/ASOA2013041003341), Mar 21, 2013: FITTING. CHAFED. RT WING T/E OTBD FLAP ALIGNMENT RECEPTACLE IS CHAFED. REPAIRED IAW REO 601R-57-51-143. MAJOR REPAIR.
- [SDR ASOA2013041003340](https://openairdocs.org/sdr/ASOA2013041003340), Mar 21, 2013: FITTING. CHAFED. LT WING T/E FLAP ALIGNMENT RECEPTACLE IS CHAFED. REPAIRED IAW REO 601R-57-51-143. MAJOR REPAIR.
- [SDR ASOA2013041003339](https://openairdocs.org/sdr/ASOA2013041003339), Mar 21, 2013: SKIN. CHAFED. TOP CENTER OF CARGO DOOR EXTERIOR SKIN IS CHAFED 1.5" LONG, .350" WIDE, .018" DEEP. REPAIRED CARGO DOOR IAW REO 601R-52-31-198 REV A, MAJOR REPAIR.
- [SDR ASOA2013041003336](https://openairdocs.org/sdr/ASOA2013041003336), Mar 21, 2013: BULKHEAD. CRACKED. FOUND FS 621 REAR PRESSURE BULKHEAD TO HAVE AN INDICATION NOTED AT LBL 27.50 AND WL 130 (TOP OF CARGO DOOR TRACK) APPROX .500" LONG X 70 PERCENT FSH. FAILED NDT
- [SDR ASOA2013041003335](https://openairdocs.org/sdr/ASOA2013041003335), Mar 21, 2013: BULKHEAD. CRACKED. FOUND FS 621 REAR PRESS BULKHEAD TO HAVE AN INDICATION NOTED AT LBL 36.2 AND APPROX WL 80 APPROX .500" LONG X 50 PERCENT FSH. FAILED NDT INSPECTION. R & R APU F
- [SDR ASOA2013041003334](https://openairdocs.org/sdr/ASOA2013041003334), Mar 21, 2013: STRUCTURE. CRACKED. CARGO DOOR AFT VERTICAL MEMBER IS CRACKED INSIDE OF DOOR AT LOWER AFT DOOR STOP FITTING. INSTALLED NEW SERVICEABLE AFT VERTICAL MEMBER, IAW SRM 51-42-06.
- [SDR ASOA2013041003333](https://openairdocs.org/sdr/ASOA2013041003333), Mar 21, 2013: SEAT TRACK. CORRODED. FS 349, RBL 9 SEAT TRACK HAS CORROSION. R & R SEAT TRACK SEGMENT FS 349 TO FS 395.0 IAW AMM 53-01-11-000-802 AND AMM 53-01-11-400-802.
- [SDR ASOA2013041003332](https://openairdocs.org/sdr/ASOA2013041003332), Mar 21, 2013: SUPPORT ANGLE. CRACKED. FS 280 INBD SIDE OF RBL 9.0 1 EA SUPPORT ANGLE CRACKED. INSTALLED NEW ANGLE IAW SRM 51-42-21 AND REO 601R-53-11-926, STEP 11 AND 12.
- [SDR ASOA2013041003331](https://openairdocs.org/sdr/ASOA2013041003331), Mar 21, 2013: FITTING. CRACKED. CO-PILOT'S WINDSHIELD SIDE POST LOWER AFT FITTING CRACKED. R & R WITH NEW FITTING PN 601R33245-45 IAW SRM 51-42-21.
- [SDR ASOA2013041003330](https://openairdocs.org/sdr/ASOA2013041003330), Mar 21, 2013: ISOLATOR. CRACKED. FORWARD FACE OF THE FS 621 REAR PRESSURE BULKHEAD BETWEEN WL 74.00 AND WL 110.00 HAS 9 ISOLATORS EITHER CRACKED OR MISSING. 4 AT RBL 45, 1 AT RBL 36.2, 1 AT RBL
- [SDR ASOA2013041003329](https://openairdocs.org/sdr/ASOA2013041003329), Mar 21, 2013: ANGLE. CRACKED. FS 280.0 INBD SIDE OF LBL 9.0 1 EA SUPPORT ANGLE CRACKED. INSTALLED NEW ANGLE IAW SRM 51-42-21 AND REO 601R-53-11-926 STEP 11 AND 12.
- [SDR ASOA2013041003328](https://openairdocs.org/sdr/ASOA2013041003328), Mar 21, 2013: ANGLE. CRACKED. FS 484.0 TWO SUPPORT ANGLES CRACKED AT LBL 27.0 AND LBL 36.0. INSTALLED NEW SUPPORT ANGLES IAW SRM 51-42-21.
- [SDR ASOA2013041003327](https://openairdocs.org/sdr/ASOA2013041003327), Mar 21, 2013: ANGLE. CRACKED. FS 484.00 TWO SUPPORT ANGLES CRACKED AT RBL 27.0 AND RBL 36.0. R & R ANGLES IAW SRM 51-42-21.
- [SDR ASOA2013041003326](https://openairdocs.org/sdr/ASOA2013041003326), Mar 21, 2013: ATTACH ANGLE. CRACKED. RT WING CENTER LEADING EDGE INBD ATTACHING ANGLE CRACKED IN RADIUS. INSTALLED NEW ANGLE IAW AMM 20-21-00-910-801.
- [SDR ASOA2013041003325](https://openairdocs.org/sdr/ASOA2013041003325), Mar 21, 2013: DRAG ANGLE. CRACKED. PAX DOOR AFT DRAG ANGLE CRACKED AT PREVIOUS REPAIR. REPAIRED AFT DRAG ANGLE IAW REO 601R-52-11-517.
- [SDR ASOA201201060](https://openairdocs.org/sdr/ASOA201201060), Mar 27, 2012: IDG. FAILED. NR 1 GENERATOR FAILED ENROUTE, ACFT DIVERTED. R & R NR 1 IDG ASSY IAW AMM 24-11-01, PERFORMED IDG ENGINE RUN LEAK AND OPS CHECK, OPS CHECKED GOOD. ACFT OK FOR S

All 162: https://openairdocs.org/deregistered/N849AS-2025-12-09/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 ATL02FA113](https://openairdocs.org/ntsb/ATL02FA113), Jun 3, 2002: Bombardier CL600-2B19 (N849AS), Atlanta, GA, substantial damage. Probable cause: Failure of the left main landing gear fitting due to a fatigue crack that emanated from multiple origins at the external surface of the wall at the shock strut radius run out area for undetermined…

## 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.

- [Accident 20020602010469A](https://openairdocs.org/incident/20020602010469A), Jun 2, 2002: Cndair CL6002B19 (N849AS), Atlanta, GA, No damage. (-23) During landing roll-out the LH m/l/g fitting sheared off. At this time the cause is unknown. The aircraft was carrying 50 passengers and bags. Everyone…

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