# N841AS: 1999 Bombardier CL-600-2B19, registration cancelled 2021-08-11

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: August 11, 2021
- Exported to: Mexico
- 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: 7300
- Year built: 1999
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: March 26, 1999
- Last registry action: August 4, 2021
- Mode S code: AB83A1
- Location: [Xxx, OK](https://openairdocs.org/faa-place/OK/Xxx)
- Owner type: Individual
- The mark today: https://openairdocs.org/aircraft/N841AS
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=841AS
- Page: https://openairdocs.org/deregistered/N841AS-2021-08-11

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 (133, newest 50)

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

- [SDR ASOA2015111714089](https://openairdocs.org/sdr/ASOA2015111714089), Nov 17, 2015: SMOKE DETECTOR. FALSE INDICATION. "SMOKE TOILET" CAUTION ON TAKEOFF, MESSAGE WENT AWAY ON FINAL APPROCH. R & R LAV SMOKE DETECTOR REF AMM 26-16-01. OPS CHECK GOOD, NO OTHER DEFECTS NOTED.
- [SDR ASOA2015012812105](https://openairdocs.org/sdr/ASOA2015012812105), Jan 20, 2015: ISOLATOR. BROKEN. BROKEN ISOLATOR ON FS 621 BULKHEAD. R & R ISOLATOR IAW SRM 51-42-13.
- [SDR ASOA2015012612092](https://openairdocs.org/sdr/ASOA2015012612092), Jan 20, 2015: ANGLE. CRACKED. BS 621 ANGLE CRACKED. R & R THE ANGLE IAW SRM 51-42-21 & TR 51-32.
- [SDR ASOA2015012812104](https://openairdocs.org/sdr/ASOA2015012812104), Jan 13, 2015: FLOOR SUPPORT. CORRODED. LT CABIN FLOOR SUPPORT CORRODED BEYOND LIMITS OF REO 601R-53-41-666 BS 426 - 519. CUT OUT DAMAGE IAW REO 601R-53-41-1871, REV P1. FABRICATED REPAIR IAW REO 601R
- [SDR ASOA2015012812103](https://openairdocs.org/sdr/ASOA2015012812103), Jan 13, 2015: SKIN. CRACKED. RT LOWER WING PLANK/TRUNNION HAS AN INDICATION NOTED IN BORE OF THE 4TH FASTENER GOING AFT FROM FWD END NOTED IN SB 601R-57-046, REV C. INDICATION IS ON INBD SI
- [SDR ASOA2015012812102](https://openairdocs.org/sdr/ASOA2015012812102), Jan 12, 2015: SKIN. CORRODED. CORROSION FOUND ON LOWER WING PLANK LANDING AFT/INBD EDGE UNDER PANEL 650BB. COMPLIED WITH EC/TC EO 600-57-81. C/W IAW REO 601R-57-21-030, REV L.
- [SDR ASOA2015012612091](https://openairdocs.org/sdr/ASOA2015012612091), Jan 12, 2015: ANGLE. CRACKED. BS 621, UPPER LT AND RT OBLIQUE ANGLES ARE CRACKED. R & R THE ANGLES IAW SRM 51-42-21.
- [SDR ASOA2015012612090](https://openairdocs.org/sdr/ASOA2015012612090), Jan 9, 2015: STRINGER. CRACKED. STRINGER 3L AT BS 280 BULKHEAD CRACKED. REPAIRED IAW SRM 51-42-06 AND SRM 51-40-11-00.
- [SDR ASOA2015012812101](https://openairdocs.org/sdr/ASOA2015012812101), Jan 8, 2015: BULKHEAD WEB. CRACKED. FOUND REAR PRESSURE BULKHEAD WEB HAS A CRACK INDICATION. LBL 18.00, WL 140 REMOVED FS 621.00 BULKHEAD STIFFENING ANGLE IAW SRM 51-42-06. INSTALLED SERVICEABLE F
- [SDR ASOA2015012812100](https://openairdocs.org/sdr/ASOA2015012812100), Jan 8, 2015: BULKHEAD WEB. CRACKED. FOUND REAR PRESSURE BULKHEAD WEB HAS A CRACK INDICATION AT BL 0.0, WL 102 . REPAIRED IAW EC/TC REO 601R-53-61-1285 AND GREO 601R-53-61-1285, REV D.
- [SDR ASOA2015012812099](https://openairdocs.org/sdr/ASOA2015012812099), Jan 8, 2015: FLOOR SUPPORT. CORRODED. PRESSURE FLOOR SUPPORT HAS MINOR CORROSION BETWEEN BS 409+128 - 559. FOUND TO BE WITHIN LIMITS OF REO 601R-53-41-666.
- [SDR ASOA2015012812098](https://openairdocs.org/sdr/ASOA2015012812098), Jan 8, 2015: SKIN. CRACKED. LOWER WING PLANK ACCESS HOLE HAS AN INDICATION NOTED ON LANDING, FOR PANEL 650DB AT AFT INBD EDGE APPROXIMATELY .250" X .250" X 50 PERCENT FSH. FAILED NDT. COMP
- [SDR ASOA2015012812097](https://openairdocs.org/sdr/ASOA2015012812097), Jan 8, 2015: SKIN. CRACKED. LOWER WING PLANK ACCESS HOLE HAS MULTIPLE INDICATIONS NOTED, ON LANDING FOR PANEL 610AB AT FWD OUTBD EDGE, APPROXIMATELY 1.0" X .250" X 50 PERCENT FSH, FAILED N
- [SDR ASOA2015012812096](https://openairdocs.org/sdr/ASOA2015012812096), Jan 8, 2015: SKIN. CRACKED. LOWER WING PLANK ACCESS HOLE HAS MULTIPLE INDICATIONS NOTED ON LANDING FOR PANEL 650FB AT FWD AND OTBD EDGE, APPROXIMATELY .250" X .250" X 50 PERCENT FSH. COMPL
- [SDR ASOA2015012612089](https://openairdocs.org/sdr/ASOA2015012612089), Jan 8, 2015: BULKHEAD WEB. CRACKED. FOUND REAR PRESSURE BULKHEAD WEB HAS A CRACK INDICATION NOTED AT LBL 36.20, WL 76.0. REPAIRED IAW REO 601R-53-61-5417, REV.
- [SDR ASOA2015012612088](https://openairdocs.org/sdr/ASOA2015012612088), Jan 8, 2015: BULKHEAD WEB. CRACKED. FOUND REAR PRESSURE BULKHEAD WEB HAS A CRACK INDICATION NOTED AT RBL 18.00, WL 108. REPAIRED IAW EC/TC REO 601R-53-61-1285 & GREO 601R-53-61-1285.
- [SDR ASOA2015012612087](https://openairdocs.org/sdr/ASOA2015012612087), Jan 8, 2015: FLOOR SUPPORT. CORRODED. PRESSURE FLOOR SUPPORT HAS MINOR CORROSION BETWEEN BS 409+128 - 559. REPAIRED IAW EC/TC REO 601R-53-41-666-01 AND REO 601R-53-41-666, REV C.
- [SDR ASOA2015012612086](https://openairdocs.org/sdr/ASOA2015012612086), Jan 8, 2015: INTERCOSTAL. CRACKED. INTERCOSTAL AT STRINGER 13L BS 621 IS CRACKED. REMOVED AND REPLACED TEH INTERCOSTAL IAW SRM 51-42-06 AND 51-42-21.
- [SDR ASOA2015012612085](https://openairdocs.org/sdr/ASOA2015012612085), Jan 8, 2015: ANGLE. CRACKED. INTERCOSTAL AT BS 484, LBL 27 HAS A CRACKED ANGLE. R & R THE ANGLE IAW SRM 51-40-11 AND 51-42-21.
- [SDR ASOA2015012612084](https://openairdocs.org/sdr/ASOA2015012612084), Jan 7, 2015: ANGLE. CRACKED. INTERCOSTAL AT FS 484, LBL 36 HAS A CRACKED ANGLE. REPAIRED IAW REO 601R-53-41-1870 AND REO 601R-53-41-059.
- [SDR ASOA2015012612083](https://openairdocs.org/sdr/ASOA2015012612083), Jan 7, 2015: ANGLE. CRACKED. INTERCOSTAL AT BS 484, RBL 27 HAS A CRACKED ANGLE. R & R THE ANGLE IAW SRM 51-40-11 AND 51-42-21.
- [SDR ASOA2015012612082](https://openairdocs.org/sdr/ASOA2015012612082), Jan 7, 2015: ANGLE. CRACKED. INTERCOSTAL AT FS 484, RBL 36.00 HAS A CRACKED ANGLE. REPAIRED IAW REO 601R-53-41-1870 AND REO 601R-53-41-059.
- [SDR ASOA2015012612081](https://openairdocs.org/sdr/ASOA2015012612081), Jan 6, 2015: SKIN. CRACKED. RT BOOST PUMP CUTOUT HAS MULTIPLE INDICATIONS ALL AROUND THE VERTICAL AND HORIZONTAL LANDING 60 PERCENT FSH FAIL NDT. COMPLIED WITH EA 32-2015-004.
- [SDR ASOA2015012812095](https://openairdocs.org/sdr/ASOA2015012812095), Jan 3, 2015: DOOR. DELAMINATED. LEFT NLG DOOR L/E DELAMINATED. REPAIRED LT NLG DOOR IAW REO 601R-52-81-020, REV NC DATED 99-09-17. PAINTED REPAIRED AREA ON LT NLG DOOR L/E IAW SRM 51-25-01. AP
- [SDR ASOA2015010512002](https://openairdocs.org/sdr/ASOA2015010512002), Dec 28, 2014: LANDING GEAR. MALFUNCTIONED. NOSE GEAR DID NOT RETRACT AFTER TAKEOFF. ACFT RETURNED TO DEPARTURE. GEAR EXTENDED MANUALLY.
- [SDR ASOA2014122211893](https://openairdocs.org/sdr/ASOA2014122211893), Dec 18, 2014: ROD. BROKEN. PAX DOOR WILL NOT OPEN. FOUND PRESSURE RELIEF VENT FLAP ROD BROKEN. REPLACED PAX DOOR VENT FLAP ROD IAW AMM 52-11-15. OPS CHECK GOOD. ACFT OK FOR SERVICE.
- [SDR ASOA2014013109816](https://openairdocs.org/sdr/ASOA2014013109816), Jan 26, 2014: SUPPORT BRACKET. CRACKED. FWD SUPPORT BRACKET IN AFT CARGO DOOR IS CRACKED. R & R FWD SUPPORT BRACKET IAW SRM 51-42-06.
- [SDR ASOA2013062708511](https://openairdocs.org/sdr/ASOA2013062708511), Jun 23, 2013: SKIN. DAMAGED. FUSELAGE SKIN DAMAGED AT FS 310 NEAR STR 16L AT SKIN EDGE. REPAIRED IAW GREO 601R-53-21-160, REO 601R-53-21-2447.
- [SDR ASOA2013020702969](https://openairdocs.org/sdr/ASOA2013020702969), Jan 23, 2013: FLOOR SUPPORT. CORRODED. RT FLOOR SUPPORT FWD OF SERVICE DOOR CUTOUT IS CORRODED FROM FS 310 TO FS 319. R & R FLOOR SUPPORT ANGLE IAW SRM 51-42-06. LOCATED, DRILLED NEW FLOOR SUPPORT IA
- [SDR ASOA2013020502958](https://openairdocs.org/sdr/ASOA2013020502958), Jan 21, 2013: RIB. CRACKED. RT WING L/E RIB AT WS 167.46 IS CRACKED AT EDGE OF PICCOLO TUBE CUTOUT. REMOVED CRACKED RIB AT WS 167.46 IAW SRM 51-42-06. INSTALLED NEW RIB, PN 601R12047-4 IAW
- [SDR ASOA2013020502957](https://openairdocs.org/sdr/ASOA2013020502957), Jan 21, 2013: ANGLE. CRACKED. WHILE REPLACING FWD J ANGLE ON FS 280, FOUND INBD CLIPS AT LBL 9 & RBL 9 TO BE CRACKED. REMOVED CLIPS IAW SRM 51-42-21. FABRICATED & INSTALLED INBD CLIPS AT LBL
- [SDR ASOA2013020702968](https://openairdocs.org/sdr/ASOA2013020702968), Jan 17, 2013: POST. CRACKED. FOUND FS 409.00+128 VERTICAL POST BL 0.0 LT & RT SIDE HAVE INDICATIONS NOTED APPROX .2" IN LENGTH 50 PERCENT FSH AT AFT FLANGE RADIUS FAILED NDT INSPECTION. REM
- [SDR ASOA2013020702967](https://openairdocs.org/sdr/ASOA2013020702967), Jan 16, 2013: ANGLE. CORRODED. PAX DOOR LOWER SILL ANGLE IS CORRODED. REMOVED PAX DOOR LOWER SILL ANGLE IAW SRM 51-42-21, 51-42-13 & 51-42-06. LOCATED & DRILLED NEW SERVICEABLE PAX DOOR LOWER
- [SDR ASOA2013020602964](https://openairdocs.org/sdr/ASOA2013020602964), Jan 16, 2013: BEAM. CORRODED. CORROSION FOUND ON END OF TRANSVERSE BEAM AT FS 349 RT SIDE. REPAIRED IAW REO 601R-53-21-2401.
- [SDR ASOA2013020602963](https://openairdocs.org/sdr/ASOA2013020602963), Jan 16, 2013: SILL. CORRODED. CORROSION FOUND ON LOWER SERVICE DOOR SILL ANGLE BETWEEN FS 319 AND FS 349. REMOVED CORRODED SILL FOR REPLACEMENT IAW SRM 51-42-06, 51-42-13 AND 51-42-21. INSTA
- [SDR ASOA2013020602962](https://openairdocs.org/sdr/ASOA2013020602962), Jan 16, 2013: FITTING. CRACKED. CO-PILOT SIDE POST LOWER AFT FITTING IS CRACKED (FITTING IS FOR WINDOWS). R & R LOWER AFT FITTING ON THE CO-PILOT'S SIDE POST WITH A NEW SERVICEABLE FITTING IAW
- [SDR ASOA2013020502956](https://openairdocs.org/sdr/ASOA2013020502956), Jan 16, 2013: FRAME. CORRODED. FRAME 605 IS CORRODED AT STRINGER 27. PERFORMED FRAME REPAIR NR 2 FRAME OUTER FLANGE REPAIR TO FS 605 BETWEEN STR 26-27 IAW SRM 53-00-15, REPAIR NR 2. COMPLIED 
- [SDR ASOA2013020502955](https://openairdocs.org/sdr/ASOA2013020502955), Jan 16, 2013: ANGLE. CORRODED. CORROSION ON FS 280.00 J-ANGLE. R & R WITH NEW SERVICEABLE J-ANGLE IAW SRM 51-42-06 AND SRM 51-42-21.
- [SDR ASOA2013020602961](https://openairdocs.org/sdr/ASOA2013020602961), Jan 15, 2013: SEAT TRACK. CORRODED. CORROSION ON LT AND RT AISLE SEAT TRACKS FROM FS 364.00 TO FS 559.00+32. REMOVED LT NR 1 SEAT TRACK IAW AMM 53-01-11-000-802. LOCATED & DRILLED NR 1 LT SEAT TRA
- [SDR ASOA2013020602960](https://openairdocs.org/sdr/ASOA2013020602960), Jan 15, 2013: SKIN. CORRODED. EXTERIOR SKIN PANELS BETWEEN FS 559.00+96 AND 559.00+112 CENTERLINE OF BELLY HAS CORROSION AROUND BUTTON HEAD RIVETS. BETWEEN FS 559+96 AND FS 559+112 BETWEEN S
- [SDR ASOA2013020502954](https://openairdocs.org/sdr/ASOA2013020502954), Jan 15, 2013: RIB. CRACKED. RT BATT RIB ASSY CRACKED AT WS 53.60 APPROX 1" LONG. REPAIRED IAW REO 601R-57-51-046.
- [SDR ASOA2013020102951](https://openairdocs.org/sdr/ASOA2013020102951), Jan 15, 2013: BRACKET. CRACKED. REAR PRESSURE BULKHEAD AT FS 621.00 HAS 4 ISOLATOR BRACKET ASSY CRACKED AT RBL 45, 1 BRACKET AT RBL 9, 1 BRACKET AT LBL 9, 1 BRACKET AT LBL 27 AND 1 BRACKET AT 
- [SDR ASOA2013020102950](https://openairdocs.org/sdr/ASOA2013020102950), Jan 14, 2013: ANGLE. CRACKED. RT FS 621-625 INTERCOSTAL ANGLE CRACKED AT S14R. LOCATED FASTENER HOLES IN NEW ANGLE IAW SRM 51-40-11 AND INSTALLED NEW ANGLE IAW SRM 51-42-21.
- [SDR ASOA2012071301899](https://openairdocs.org/sdr/ASOA2012071301899), Jul 9, 2012: LAMP. BURNED OUT. FWD WARDROBE FLOOR FLOOD EMERGENCY LIGHT HAS SEVERAL BULBS INOPERATIVE. RELAMPED FLOOR LEVEL EMERGENCY FLOOD LIGHT ON WARDROBE. OPS CHECKED GOOD.
- [SDR ASOA201100845](https://openairdocs.org/sdr/ASOA201100845), Apr 25, 2011: LATCH. BINDING. UNABLE TO UNLATCH PAX DOOR FROM OUTSIDE. PERFORMED OPS CHECK OF PAX DOOR HANDLE IAW AMM 52-11-02.
- [SDR ASOA201100218](https://openairdocs.org/sdr/ASOA201100218), Feb 4, 2011: LIGHT. BROKEN. EMERGENCY LIGHT FLOOR LEVEL FLOODLIGHT AT PASSENGER DOOR BROKEN. R & R FLOOR LEVEL EMERGENCY FLOOD LIGHT IAW CRJ 200 33-51-19-000-801 & -400-801. EMERGENCY LIGH
- [SDR ASOA201100208](https://openairdocs.org/sdr/ASOA201100208), Jan 25, 2011: WIRE. BROKEN. PANEL 232BZ HAS A BROKEN WIRE ON THE EXIT LIGHT PANEL. R & R EXIT LIGHT ON PANEL 232BZ IAW AMM 33-51-10-000-801 AND 33-51-10-400-801. OPS CHECK DUE. PERFORMED O
- [SDR ASOA201100184](https://openairdocs.org/sdr/ASOA201100184), Jan 24, 2011: ISOLATOR. BROKEN. AFT BULKHEAD 621 ISOLATOR IS BROKEN. INSTALLED A NEW SERVICEABLE ISOLATOR ON THE 621 BULKHEAD IAW SRM 51-42-13. THIS REPAIR IS CLASSIFIED AS A MINOR REPAIR IAW 
- [SDR ASOA201100161](https://openairdocs.org/sdr/ASOA201100161), Jan 24, 2011: WEB. CRACKED. PAX DOOR AFT WEB IS CRACKED AT FWD EDGE OF STEP 832AT. REPAIRED DAMAGE IAW REO NR: 601R-52-11-1901.
- [SDR ASOA201100160](https://openairdocs.org/sdr/ASOA201100160), Jan 24, 2011: FLOOR SUPPORT. CORRODED. CORROSION ON NUTPLATES OF FLOOR SUPPORT FS 585 - 600 LBL 27.

All 133: https://openairdocs.org/deregistered/N841AS-2021-08-11/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 20030504008839I](https://openairdocs.org/incident/20030504008839I), May 4, 2003: Cndair CL6002B19 (N841AS), Jacksonville, FL, Minor damage. (-23) After atlantic southeast air lines flight 4284 began taxiing from the gate and had rolled about two feet, the leading edge of the left wingtip struck the…

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