# N843AS: 1999 Bombardier CL-600-2B19, registration cancelled 2017-06-01 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: June 1, 2017 - Status when cancelled: Sale reported - 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: 7310 - Year built: 1999 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: May 7, 1999 - Last registry action: June 1, 2017 - Mode S code: AB8B0F - Location: [Plano, TX](https://openairdocs.org/faa-place/TX/Plano) - Owner type: Individual - Owner's area on the map: 33.0779° N, 96.8110° W: Placed by OpenAirDocs at the center of ZIP code 75024, within about 2 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N843AS - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=843AS - Page: https://openairdocs.org/deregistered/N843AS-2017-06-01 From the FAA registry file of October 28, 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 (148, newest 50) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR ASOA2016021014503](https://openairdocs.org/sdr/ASOA2016021014503), Feb 10, 2016: FLOORBEAM. CORRODED. CORROSION ON PRESSURE FLOORBEAM AT FS430.00 AND LBL9. BLENDED CORROSION IAW SRM 51-21-06. BLENDED AREA IS OUT OF ALLOWABLE LIMITS IAW SRM 53-00-00. COMPLIED WIT - [SDR ASOA2016021014502](https://openairdocs.org/sdr/ASOA2016021014502), Feb 10, 2016: FLOORBEAM. CORRODED. CORROSION ON PRESSURE FLOORBEAM FS 461.00 AND LBL9. BLENDED CORROSION IAW SRM 51-21-06. BLENDED AREA IS OUT OF ALLOWABLE LIMITS IAW SRM 53-00-00. COMPLIED WITH - [SDR ASOA2016021014501](https://openairdocs.org/sdr/ASOA2016021014501), Feb 10, 2016: FLOOR SUPPORT. CORRODED. CORROSION ON PRESSURE FLOOR SUPPORT BEAM IN MULTIPLE LOCATIONS BETWEEN FS409.00+128 AND FS559.00 AT RBL9. BLENDED CORROSION IAW SRM 51-21-06. BLENDED AREA IS OU - [SDR ASOA2016020914511](https://openairdocs.org/sdr/ASOA2016020914511), Feb 9, 2016: SKIN. DENTED. ASD SURROUNDING STRUCTURE LOWER FWD CORNER HAS DAMAGE, DENT. REMOVED DAMAGE AT ASD SURROUNDING STRUCTURE LOWER FWD CORNER IAW REO 601R-53-21-160. BLENDED AREA I - [SDR ASOA2016020614500](https://openairdocs.org/sdr/ASOA2016020614500), Feb 6, 2016: FLOOR PANEL. CORRODED. CORROSION FOUND ON PRESSURE FLOOR JUST FWD OF FS 559 ON RT SIDE. BLENDED CORROSION FWD OF FS 559 ON CROSSBEAM ABOVE PRESSURE FLOOR IAW SRM 51-21-06-00. EVALUATE - [SDR ASOA2016020514499](https://openairdocs.org/sdr/ASOA2016020514499), Feb 5, 2016: DOOR SILL. GOUGED. PAX DOOR SILL IS GOUGED CAUSED BY ANTI-MIGRATION PIN. EC/TC REO 601R-53-21-814 FOUND TO BE OUT OF LIMITS. DAMAGE MEASURED BY MECHANICAL MEANS .063" FOUND TO BE - [SDR ASOA2016020214510](https://openairdocs.org/sdr/ASOA2016020214510), Feb 2, 2016: INLET. ERODED. LEFT ENGINE INLET ERODED. COMPLIED WITH PERMANENT REPAIR OF LT ENGINE INLET IAW CMM 71-61-01. REPAIRED LT ING INLET EROSION IAW CMM TASK 71-61-01-300-822-A01. - [SDR ASOA2014102711491](https://openairdocs.org/sdr/ASOA2014102711491), Oct 20, 2014: ISOLATOR. CRACKED. BS 621 FWD FACE OF BULKHEAD NUMEROUS ISOLATOR MOUNTS CRACKED AND/OR BROKEN. REPLACED ISOLATORS WITH NEW IAW SRM 51-42-06. - [SDR ASOA2014102711490](https://openairdocs.org/sdr/ASOA2014102711490), Oct 20, 2014: SUPPORT ANGLE. CRACKED. BS 621 BULKHEAD, CARGO DOOR SUPPORT MEMBER. LOWER ATTACHMENT ANGLE IS CRACKED. R & R SUPPORT ANGLE WITH NEW SERVICEABLE PART IAW SRM 51-42-21. - [SDR ASOA2014082211133](https://openairdocs.org/sdr/ASOA2014082211133), Aug 21, 2014: LIGHT. DAMAGED. PAX ENTRY FLOOR LEVEL EMERGENCY FLOOD LIGHT ASSY DAMAGED. R & R PAX ENTRY FLOOR LEVEL EMERGENCY LIGHT ASSY IAW AMM 33-51-19. OPS CHECK GOOD NO FURTHER DEFECTS N - [SDR ASOA2014021909989](https://openairdocs.org/sdr/ASOA2014021909989), Jan 31, 2014: TRUNNION. CRACKED. LEFT MLG TRUNNION HAS ONE CRACKED FASTENER HOLE. RECEIVED AND COMPLIED WITH REO 601R-57-21-2099 AND EC/TC REO 601R-57-21-2099. REPAIR CLASSIFIED AS MAJOR. - [SDR ASOA2014021909988](https://openairdocs.org/sdr/ASOA2014021909988), Jan 30, 2014: SKIN. CORRODED. ACCESS PANEL 540BB HAS PITTING AROUND THE FLANGE. COMPLIED WITH REO 601R-57-21-030 AND EC/TC EO 600-57-81. REPAIR CLASSIFIED AS MAJOR. - [SDR ASOA2014021909987](https://openairdocs.org/sdr/ASOA2014021909987), Jan 30, 2014: SKIN. CORRODED. ACCESS PANEL RT WING 640BB HAS CORROSION AROUND LAND. COMPLIED WITH REO 601R-57-21-030 AND ECTC EO 600-57-81. REPAIR CLASSIFIED AS MAJOR. - [SDR ASOA2014021909986](https://openairdocs.org/sdr/ASOA2014021909986), Jan 30, 2014: ACCESS PANEL. CORRODED. ACCESS PANEL 650CB CORRODED. COMPLIED WITH REO 601R-57-21-030 AND ECTC EO 600-57-81. REPAIR CLASSIFIED AS MAJOR. - [SDR ASOA2014021909985](https://openairdocs.org/sdr/ASOA2014021909985), Jan 28, 2014: BULKHEAD. CRACKED. CRACK INDICATION ON REAR PRESSURE BULKHEAD FORWARD FACE BELOW WL 120.43 AT BL 0. COMPLIED WITH ECTC REO601R-53-61-1285 AND MET ALL THE REQUIREMENTS OF REO 601R- - [SDR ASOA2014021909984](https://openairdocs.org/sdr/ASOA2014021909984), Jan 25, 2014: CARGO TRACK. CORRODED. CARGO TRACK CORRODED FS 559+80, LBL 27.5. REMOVED AND REPLACED CARGO TRACK IAW AMM 53-01-11, TASK 53-01-11-000-802, & 53-01-11-400-802. - [SDR ASOA2014021909983](https://openairdocs.org/sdr/ASOA2014021909983), Jan 25, 2014: SEAT TRACK. CORRODED. SEAT TRACK CORRODED FS 409+128-559, RBL 9. COMPLIED WITH REO 601R-53-00-485, REMOVED AND REPLACED SEAT TRACK IAW AMM 53-01-11, TASK 53-01-11-000-802 AND AMM 53- - [SDR ASOA2014021909982](https://openairdocs.org/sdr/ASOA2014021909982), Jan 25, 2014: SEAT TRACK. CORRODED. SEAT TRACK CORRODED FS 394-409+128, RBL 9. REMOVED AND REPLACED SEAT TRACK IAW AMM 53-01-11, TASK 53-01-11-000-802 AND 53-01-11-400-802. - [SDR ASOA2014021909981](https://openairdocs.org/sdr/ASOA2014021909981), Jan 25, 2014: SEAT TRACK. CORRODED. SEAT TRACK CORRODED FS 394-409+128, LBL 9. R & R SEAT TRACK IAW AMM 53-01-11-000-802 & 01-11-400-802. - [SDR ASOA2014021909980](https://openairdocs.org/sdr/ASOA2014021909980), Jan 25, 2014: SEAT TRACK. CORRODED. SEAT TRACK CORRODED FS 364-394, RBL 9. R & R SEAT TRACK IAW AMM 53-01-11-000-802, & 53-01-11-400-802. - [SDR ASOA2014021909979](https://openairdocs.org/sdr/ASOA2014021909979), Jan 25, 2014: SEAT TRACK. CORRODED. SEAT TRACK CORRODED, FS 364-394, LBL 9.0. R & R SEAT TRACK IAW AMM 53-01-11-000-802 & 53-01-11-400-802. - [SDR ASOA2014021909978](https://openairdocs.org/sdr/ASOA2014021909978), Jan 25, 2014: ATTACH ANGLE. CRACKED. BS 280 BULKHEAD TO LBL 9 FLOOR ATTACH ANGLE CRACKED OTBD SIDE. REMOVED ATTACH ANGLE IAW SRM 51-42-20. INSTALLED FABRICATED NEW ATTACH ANGLE IAW REO 601R-53-11-9 - [SDR ASOA2014021909977](https://openairdocs.org/sdr/ASOA2014021909977), Jan 24, 2014: HINGE. DENTED. PASSENGER DOOR HINGE HALF DENTED BETWEEN RIVET 7 AND 11 AND INCLUDE DOOR FRAME UNDER SEAL RETAINER. REPAIRED IAW SRM 52-00-00 AND SRM 51-42-06. REPAIR CLASSIFIE - [SDR ASOA2014021909976](https://openairdocs.org/sdr/ASOA2014021909976), Jan 23, 2014: HINGE. GOUGED. HINGE SEGEMENT, PASSENGER DOOR LUGS HAS GOUGE DAMAGE. R & R HINGE IAW SUPPLEMENT ASA 52-11-26. COMPLIED WITH ECTC EO600-52-0146. REPAIR CLASSIFIED AS MAJOR. - [SDR ASOA2014021909975](https://openairdocs.org/sdr/ASOA2014021909975), Jan 23, 2014: HINGE. GOUGED. HINGE SEGEMENT HALF ON FUSELAGE SIDE HAS GOUGED LUGS. REPAIRED IAW REO 601R-53-21-814. REPAIR CLASSIFIED AS MAJOR. - [SDR ASOA2014021909974](https://openairdocs.org/sdr/ASOA2014021909974), Jan 23, 2014: INTERCOSTAL. CRACKED. CARGO DOOR LOWER AFT CORNER INTERCOSTAL CRACKED. REMOVED INTERCOSTAL IAW SRM 51-42-06-000. INSTALLED INTERCOSTAL & FASTENERS IAW SRM DWG 601R3507. REPAIR CLASSI - [SDR ASOA2013101409213](https://openairdocs.org/sdr/ASOA2013101409213), Oct 8, 2013: LIGHT. WRONG PART. CABIN FLOOR EMERGENCY LIGHT INCORRECT FOR THIS ACFT. R & R PAX CABIN EMERGENCY LIGHT IAW AMM 33-51-01 01. - [SDR ASOA2013092509099](https://openairdocs.org/sdr/ASOA2013092509099), Sep 24, 2013: SKIN. DENTED. DENT ON FUSELAGE AT FS 310 AND STGR 16L CAUSED BY CONTACT WITH FWD LOWER PAX DOOR LATCH PIN. REPAIRED IAW GREO 601R-53-21-160, REV B. CLASSIFIED AS MAJOR REPAIR - [SDR ASOA2012122102698](https://openairdocs.org/sdr/ASOA2012122102698), Dec 19, 2012: SIGN. INOPERATIVE. LIGHTED EMERGENCY EXIT SIGN ON THE LOWER WARDROBE INOPERATIVE. R & R THE LIGHTED EMERGENCY EXIT SIGN IAW AMM 33-51-10. OPS CHECKED GOOD. - [SDR ASOA2012102902405](https://openairdocs.org/sdr/ASOA2012102902405), Oct 25, 2012: PUSHROD. OUT OF ADJUST. PAX DOOR SOMETIMES WILL NOT OPEN. ADJUSTED PUSH ROD ON LATCH CAM TORQUE-TUBE MECHANISM IAW AMM 52-11-23. SDR CLOSED. - [SDR ASOA2012102602399](https://openairdocs.org/sdr/ASOA2012102602399), Oct 22, 2012: WIRE. MISROUTED. ON GATE RETURN, COULD NOT OPEN PAX DOOR. WIRING ON P55MB AND P56MB WAS FOUND HOOKED OVER THE CAM ON PAX DOOR TORQUE TUBE . REPAIRED. PERFORMED OPS TEST OF PAX D - [SDR ASOA201200539](https://openairdocs.org/sdr/ASOA201200539), Feb 20, 2012: FRAME. CORRODED. FS 333.00 FRAME CORRODED AT LOWER SIDE NEAR STRINGER 26L. REPAIRED IAW REO 601R-53-21-2264. - [SDR ASOA201200510](https://openairdocs.org/sdr/ASOA201200510), Feb 17, 2012: SKIN. CRACKED. RT WING PLANK CRACKED OTBD OF RT JACK PAD. REWORKED AREA IAW REO 601R-57-21-130 REV J. - [SDR ASOA201200492](https://openairdocs.org/sdr/ASOA201200492), Feb 13, 2012: ANGLE. CORRODED. SERVICE DOOR AFT LOWER CORNER AND TEE CAP AT FS 349.50 CORRODED. REMOVED DAMAGE IAW REO 601R-53-21-2263. COMPLIED NDTM PART 1, 51-20-06. NO INDICATIONS NOTED. I - [SDR ASOA201200552](https://openairdocs.org/sdr/ASOA201200552), Feb 9, 2012: SILL. CORRODED. SERVICE DOOR SILL CORRODED AROUND BOTH FWD AND AFT STOP FITTINGS. REMOVED SERVICE DOOR SILL DUE TO CORROSION BE BEYOND LIMITS IAW SRM 31-42-21 AND 51-42-06. INS - [SDR ASOA201200455](https://openairdocs.org/sdr/ASOA201200455), Feb 9, 2012: STRUCTURE. CORRODED. SERVICE DOOR AFT LOWER CORNER AND TEE CAP AT FS 349.50 ON CORRODED. REMOVED CORROSION IAW SRM 51-21-06 FOUND TO BE BEYOND LIMITS. REMOVED FITTING AND ANGLE, IAW - [SDR ASOA201200443](https://openairdocs.org/sdr/ASOA201200443), Feb 9, 2012: FRAME. CORRODED. BS 333 FRAME CORRODED AT LOWER SIDE NEAR STRINGER 26L. REMOVED CORROSION IAW SRM 51-21-06-00. PERFORMED UT THICKINESS INSPECTION IAW MAC NDT PROCEDURES UT-3. MI - [SDR ASOA201200550](https://openairdocs.org/sdr/ASOA201200550), Feb 8, 2012: BUSHING. CORRODED. LEFT SIDE HORIZONTAL TO VERTICAL ATTACHMENT POINT BUSHING CORRODED ON VERTICAL. REMOVED THE HORISONTAL STABLIZER IAW AMM 55-10-00-000-801. REPAIRED BUSHING, INS - [SDR ASOA201200439](https://openairdocs.org/sdr/ASOA201200439), Feb 8, 2012: RIB. CRACKED. RIGHT WING AFT SPAR SUPPORT RIB AT WS 149.58 CRACKED. PERFORMED EDDY CURRENT INSPECTION IAW MAC NDT INSPECTION PROCEDURE ET-2 AREA IS CONFIRMED CRACKED. REPAIRE - [SDR ASOA201200437](https://openairdocs.org/sdr/ASOA201200437), Feb 8, 2012: HOUSING. BROKEN. CEILING EMERGENCY LIGHT HOUSING BROKEN AT FLOOD LIGHT 1, FS 405.00. R & R EMERGENCY LIGHT ASSY WITH NEW LIGHT ASSY IAW AMM 33-51-16-000-801 & 33-51-16-400-801. - [SDR ASOA201200548](https://openairdocs.org/sdr/ASOA201200548), Feb 6, 2012: SEAT BELT. UNSERVICEABLE. SEATS 1A AND 1B SEAT BELT TAGS UNREADABLE. R & R SEAT BELTS FOR PAX SEATS 1A&1B IAW CMM 25-25-82. - [SDR ASOA201200414](https://openairdocs.org/sdr/ASOA201200414), Feb 6, 2012: LIGHT. DAMAGED. EMERGENCY LIGHT STAINED BEYOND 10 PERCENT OF 48 INCH LENGTH. (4.75) AT SEATS 1&2 ABCD. R & R LIGHT IAW AMM SUPPLEMENT 33-51-00 AND 33-51-01-000-806, 33-51-01-40 - [SDR ASOA201101500](https://openairdocs.org/sdr/ASOA201101500), Aug 13, 2011: FITTING. CRACKED. LT MLG MAIN FITTING HAS A CRACK INDICATION ON OTBD SIDE OF AFT BOLT HOLE AREA. REMOVED LT MLG ASSY IAW AMM 32-11-00. R & R MAIN FITTING ASSY IAW CMM 32-10-15. R - [SDR ASOA201001831](https://openairdocs.org/sdr/ASOA201001831), Nov 24, 2010: BATTERY. DISCHARGED. CAPTAIN'S FLASHLIGHT INOP. REPLACED BATTERIES IN FLASHLIGHT, OPS TEST GOOD IAW CRJ 200 AMM 25-61-00. - [SDR ASOA201001511](https://openairdocs.org/sdr/ASOA201001511), Oct 7, 2010: THRUST REVERSER. UNKNOWN. LT ENGINE THRUST REVERSER ECAIS MESSAGE AND REV N1 WARNING INFLIGHT. COMPLIED WITH QRH 1-12 NO OTHER ABNORMALITIES NOTED. (ACFT RETURNED TO DEPARTURE AFTER T/O - [SDR ASOA201001145](https://openairdocs.org/sdr/ASOA201001145), Aug 18, 2010: DOOR. BINDING. PAX DOOR HARD TO OPEN, OUTER HANDLE HARD TO DEPLOY. COMPLIED WITH OPS CHECK OF PAX DOOR IAW AMM 52-11-00. OPS CHECKED GOOD IAW AMM. OK FOR SERVICE. - [SDR ASOA201000160](https://openairdocs.org/sdr/ASOA201000160), Feb 3, 2010: SKIN. CRACKED. RT WING FUEL DRAIN HOLE AT APPROX WS 50.00 HAS A 60 PERCENT FSH HFEC INDICATION NOTED 0.100" LONG APPROX 0125" OTBD OF DRAIN HOLE. INDICATION MARKED ON ACFT. FA - [SDR ASOA201000152](https://openairdocs.org/sdr/ASOA201000152), Feb 3, 2010: SILL. CORRODED. CARGO DOOR SILL PLATE HAS CORROSION AROUND NUTPLATE HOLES FROM FS 574.00 TO FS 621.00. REMOVED 5 OLD DAMAGED INSERTS. INSTALLED 5 NEW SERVICEABLE INSERTS FROM L - [SDR ASOA201000151](https://openairdocs.org/sdr/ASOA201000151), Feb 3, 2010: PLATE. CRACKED. CARGO FLOOR LANDING PLATE IS CRACKED AT FS 589 AT INBD FLOORBEAM RIVET. C/W EC/TC REO 601R-53-61-433 AND MET ALL THE REQUIREMENTS OF REO 601R-53-61-433. - [SDR ASOA201000141](https://openairdocs.org/sdr/ASOA201000141), Feb 1, 2010: BEAM. CRACKED. FS 409+128 BULKHEAD LBL 18.00 VERTICAL BEAM CRACKED ON C/B SIDE BY LOWER ATTACH FASTENER. REMOVED VERT BEAM IAW SRM 51-42-06 ST 1 AND 11. INSTALLED NEW SERVICEA All 148: https://openairdocs.org/deregistered/N843AS-2017-06-01/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 20020520011009I](https://openairdocs.org/incident/20020520011009I), May 20, 2002: Cndair CL6002B19 (N843AS), Fayetteville, AR. (-23) Candler 502, N843AS, departed xna for atl experienced smoke and fire alarm in lav, returned to xna landed without incident. Contacted asa pmi, hurley… ## Other aircraft with N843AS - [Registered now](https://openairdocs.org/aircraft/N843AS): Ea Vision EA J100, S/N EAVUAV502585857 --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.