# N851AS: 1999 Bombardier CL-600-2B19, registration cancelled 2018-07-30

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: July 30, 2018
- 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: 7360
- Year built: 1999
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: January 26, 2000
- Certificate issued: February 13, 2017
- Last registry action: February 13, 2017
- Mode S code: ABAB20
- Owner when cancelled: [Delta Materal Services LLC](https://openairdocs.org/faa-owner/DELTA%20MATERAL%20SERVICES%20LLC)
- Location: [Atlanta, GA](https://openairdocs.org/faa-place/GA/Atlanta)
- Owner type: Corporation
- Owner's area on the map: 33.6604° N, 84.3865° W: Placed by OpenAirDocs at the center of ZIP code 30354, within about 2 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N851AS
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=851AS
- Page: https://openairdocs.org/deregistered/N851AS-2018-07-30

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 (154, newest 50)

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

- [SDR ASOA2016080315154](https://openairdocs.org/sdr/ASOA2016080315154), Jul 30, 2016: SENSOR. OUT OF ADJUST. DURING DEPARTURE, SELECTED GEAR HANDLE UP AND RECEIVED GEAR DISAGREE FOLLOWED BY NOSE DOOR WARNING MESSAGE. NOSE GEAR WAS NOT UP. FOLLOWED QRH AND PULL EMERGENC
- [SDR ASOA2016071715113](https://openairdocs.org/sdr/ASOA2016071715113), Jul 17, 2016: DOOR. UNKNOWN. PAX DOOR WOULD NOT OPEN FROM INSIDE. PERFORMED OPERATIONAL TEST OF THE MAIN PAX DOOR IAW AMM 52-11-02, OPS CHECK NORMAL, NO DEFECTS NOTED. OK FOR SERIVCE.
- [SDR ASOA2016040514693](https://openairdocs.org/sdr/ASOA2016040514693), Apr 5, 2016: BATTERY PACK. DISCHARGED. F/A FLASHLIGHT IS DEAD. REPLACED BATTERIES IN F/A`S FLASHLIGHT.
- [SDR ASOA2016010214302](https://openairdocs.org/sdr/ASOA2016010214302), Jan 2, 2016: SEAT TRACK. CORRODED. SEAT RAIL FROM FS559.00-FS559.00+80 AT LBL9 IS CORRODED AS REPORTED BY MAINTENANCE. REMOVED CORROSION IAW SRM 51-21-06-00, SEAT TRACK OUT OF LIMITS IAW SRM 53-5
- [SDR ASOA2015123014325](https://openairdocs.org/sdr/ASOA2015123014325), Dec 30, 2015: SKIN. CRACKED. DURING FASTENER HOLE INSPECTION OF RT LOWER WING PLANK 1EA HOLE HAS CRACK INDICATION. RECEIVED & COMPLIED WITH ADR JLEB-15-3626196, REF SRM 51-40-11. RECEIVED &
- [SDR ASOA2015123014301](https://openairdocs.org/sdr/ASOA2015123014301), Dec 30, 2015: SEAT TRACK. CORRODED. FLOOR SEAT RAIL BETWEEN FS 409.00+128 AND FS559.00 AT RBL 9 IS CORRODED. EVALUATED AND FOUND DAMAGE TO BE OUT OF LIMITS REF SRM 53-41-49. R & R SEAT RAIL BETWEE
- [SDR ASOA2015123014300](https://openairdocs.org/sdr/ASOA2015123014300), Dec 30, 2015: SEAT TRACK. CORRODED. SEAT RAIL BETWEEN FS 409.00+128 AND FS 559.00 AT LBL9 IS CORRODED. REMOVED SEAT RAIL BETWEEN FS 409 + 128 & FS 559.00, LBL 9 IAW AMM 53-01-11-000-802. INSTALLED
- [SDR ASOA2015122814320](https://openairdocs.org/sdr/ASOA2015122814320), Dec 28, 2015: FLOOR SUPPORT. CORRODED. CORROSION FOUND ON FLOORBEAM, OTBD SIDE, FS 589.00-605.00 AND LBL9. REMOVED DAMAGE AND FOUND NOT WITHIN LIMITS IAW SRM 53-00-00. REMOVED FLOOR SUPPORT BEAM CAP 
- [SDR ASOA2015122814319](https://openairdocs.org/sdr/ASOA2015122814319), Dec 28, 2015: STRUCTURE. CORRODED. CORROSION FOUND RBL4.0 SILL AT 559+80-559.00+96. BLENDED CORROSION IAW SRM 51-21-06. COMPLIED WITH EC/TC REO 601R-53-00-526 01 AND GREO 601R-53-00-526, REC, DAT
- [SDR ASOA2015122814318](https://openairdocs.org/sdr/ASOA2015122814318), Dec 28, 2015: FRAME. CORRODED. CORROSION FOUND AROUND SCREW HOLES AT FS 559.00+69 AND 559.00+80 RBL9 ON OTBD SIDE. REMOVED DAMAGE AND FOUND NOT WITHIN LIMITS IAW SRM 53-00-00 AT FS 559+69 AND
- [SDR ASOA2015122814310](https://openairdocs.org/sdr/ASOA2015122814310), Dec 28, 2015: SEAT TRACK. CORRODED. CORROSION FOUND ON SEAT TRACK AT 559.00+ 559.00+96 AND RBL 27. EVLAUATED AND FOUND DAMAGE TO BE OUT OF LIMITS IAW SRM 53-51-49. R & R SEAT RAIL BETWEEN FS 559.0
- [SDR ASOA2015122814309](https://openairdocs.org/sdr/ASOA2015122814309), Dec 28, 2015: SEAT TRACK. CORRODED. CORROSION FOUND ON SEAT TRACK BETWEEN 559.00+80 TO 559.00+98 AND RBL 9. REMOVED SEAT TRACK FROM FS 559.+87 TO 559+96 RBL9 IAW AMM 53-01-11-000-802. INSTALLED NE
- [SDR ASOA2015122814299](https://openairdocs.org/sdr/ASOA2015122814299), Dec 28, 2015: SEAT TRACK. CORRODED. CORROSION FOUND FOUND ON SEAT TRACK AT FS559.00+112-574.00, LBL9. REMOVED CORROSION IAW SRM 51-21-06-00. SEAT TRACK OUT OF LIMITS IAW SRM 53-61-49. REMOVED SEAT
- [SDR ASOA2015122814291](https://openairdocs.org/sdr/ASOA2015122814291), Dec 28, 2015: PLATE. CORRODED. CORROSION FOUND TIE DOWN BLOCK AT BS 574 - 589 AND LBL9. R & R ANCHOR PLATE IAW SRM 51-41-02.
- [SDR ASOA2015122814290](https://openairdocs.org/sdr/ASOA2015122814290), Dec 28, 2015: PLATE. CORRODED. CORROSION FOUND TIE DOWN BLOCK AT BS 589 - 605 AND LBL9. R & R ANCHOR PLATE IAW SRM 51-41-02.
- [SDR ASOA2015122814289](https://openairdocs.org/sdr/ASOA2015122814289), Dec 28, 2015: PLATE. CORRODED. CORROSION FOUND ON TIE DOWN LOCK AT FS559+96-559-.00+112 AND F, LBL27. R & R ANCHOR PLATE AT 559.00+96-559.00+112 AND LBL27 IAW SRM 51-41-02. UPON REPLACMENT OF
- [SDR ASOA2015122814288](https://openairdocs.org/sdr/ASOA2015122814288), Dec 28, 2015: DOOR SILL. CRACKED. CRACKS FOUND ON CARGO DOOR SILL AT FS589.00 AND 605.00 AND LBL 4.0. COMPLIED WITH EC/TC REO 601R-53-61-433 AND REO 601R-53-61-433, REV B, DATED 10/9/2009 AS WRI
- [SDR ASOA2015122114308](https://openairdocs.org/sdr/ASOA2015122114308), Dec 21, 2015: SKIN. CRACKED. RT WING PLANK CRACKED AT WS 148.019. REMOVED RT INBD LOWER T/E INBD OF "PIE PANEL" IAW SRM 51-42-21, 51-42-06. INSTALLED INBD LOWER T/E INBD OF "PIE PANEL", REF
- [SDR ASOA2015121214212](https://openairdocs.org/sdr/ASOA2015121214212), Dec 12, 2015: LAMP. BURNED OUT. RIGHT EXTERIOR EMERGENCY LIGHT NR 2 INOPERATIVE. RELAMPED RT EXTERIOR EMERGENCY LIGHT NR 2 IAW AMM 33-51-21. OPS CHECK GOOD.
- [SDR ASOA2015050412744](https://openairdocs.org/sdr/ASOA2015050412744), May 1, 2015: BATTERY PACK. INOPERATIVE. AFT CENTER CEILING EMERGENCY LIGHTS INOPERATIVE. REPLACED NR 2 EMERGENCY LIGHT BATTERY IAW AMM 33-51-24-400-801. OPS CHECK GOOD IAW AMM 33-51-00-710-801. VERIFI
- [SDR ASOA2015050412743](https://openairdocs.org/sdr/ASOA2015050412743), Apr 26, 2015: BULKHEAD. CRACKED. 2 INDICATIONS NOTED AT 621 REAR PRESSURE BULKHEAD FWD FACE AT BL 0.0, WL 110 APPROXIMATELY 1.350" IN LENGTH VERTICALLY AND 90 PERCENT FULL SCREEN HEIGHT INDICAT
- [SDR ASOA2015050412742](https://openairdocs.org/sdr/ASOA2015050412742), Apr 25, 2015: STIFFENER. CRACKED. CARGO DOOR AFT VERTICAL MEMBER, PN:601R35027-31, CRACKED APPROXIMATELY 5" LONG INSIDE OF DOOR FS 605. REMOVED AFT VERTICAL MEMBER IAW SRM 51-42-06. INSTALLED NE
- [SDR ASOA2014101711438](https://openairdocs.org/sdr/ASOA2014101711438), Oct 14, 2014: SKIN. BURNED. ONE BURNED FASTENER ON BS 265 STRINGER 16L. FOUND DAMAGE CONTAINED TO FASTENER HEAD ONLY. REMOVED FASTENER IAW SRM 51-42-06. COMPLED WITH EC/TC REO 601R-53-00-1
- [SDR ASOA2014101711437](https://openairdocs.org/sdr/ASOA2014101711437), Oct 14, 2014: SKIN. DAMAGED. ONE BURN LOCATED 1 INCH AFT OF BS 235 AND ON STRINGER 16L. FOUND DAMAGE CONTAINED TO FASTENER HEAD ONLY. REMOVED FASTENER IAW SRM 51-42-06. COMPLED WITH EC/TC R
- [SDR ASOA2014091811257](https://openairdocs.org/sdr/ASOA2014091811257), Sep 14, 2014: FLASHLIGHT. INOPERATIVE. F/A FLASHLIGHT INOPERATIVE. R & R FLASHLIGHT IAW AMM 25-61-04. OPS CHECKED GOOD.
- [SDR ASOA2014091211217](https://openairdocs.org/sdr/ASOA2014091211217), Sep 11, 2014: SKIN. DAMAGED. DENT AND HOLE IN FUSELAGE SKIN BETWEEN BS 654-672 AND STRINGERS 26 - 27R. FOUND DAMAGE TO BE IN A NON-REPAIRABLE LOCATION IAW SRM 53-00-31. SUBMITTED DAMAGE REP
- [SDR ASOA2013122409687](https://openairdocs.org/sdr/ASOA2013122409687), Dec 21, 2013: CABLE. LOOSE. MAIN PAX DOOR IS JAMMED, WILL ONLY OPEN ABOUT 1 FOOT. FOUND CABLE OFF OF PULLEY INSTALLED PAX DOOR ASSIST CABLE IAW AMM 52-11-08, OPS CHECK GOOD.
- [SDR ASOA2013080608834](https://openairdocs.org/sdr/ASOA2013080608834), Aug 4, 2013: BULB. BURNED OUT. EMERGENCY LIGHT AT SERVICE DOOR INOPERATIVE. R & R BULB IAW AMM 33-51-21, OPS CHECKED GOOD.
- [SDR ASOA2013071708716](https://openairdocs.org/sdr/ASOA2013071708716), Jul 1, 2013: WIRE. BROKEN. WIRE BROKEN AT CONNECTOR FOR EMERGENCY LIGHT ON SERVICE DOOR SURROUND PANEL 232BZ. REPAIRED WIRE IAW ECSPM 20-17-00. OPS CHECKED GOOD IAW AMM 31-51-00-710-801.
- [SDR ASOA2013071708715](https://openairdocs.org/sdr/ASOA2013071708715), Jun 21, 2013: STRUCTURE. MISREPAIRED. WHILE WORKING SB 601R-25-187, FOUND REPAIR AT LBL 27 TO HAVE BEEN DONE INCORRECTLY. REPAIRED IAW SRM 51-42-21 AND REO 601R-53-61-4939.
- [SDR ASOA2013071708714](https://openairdocs.org/sdr/ASOA2013071708714), Jun 9, 2013: ANGLE. CRACKED. VERTICAL ANGLE AT LBL 27.50 ON FWD SIDE OF THE ENG BEAM IS CRACKED AT THE BOTTOM OF THE ANGLE APPROX 1"L. REMOVED CRACKED ANGLE AT LBL 27.50 IAW SRM 51-42-06 AN
- [SDR ASOA2013071708713](https://openairdocs.org/sdr/ASOA2013071708713), Jun 5, 2013: SKIN. CRACKED. LT FUEL ACCESS HOLE 540EB FAILS NDT WITH AN INDICATION ON INBD SIDE OF HOLE GREATER THAN 50 PERCENT SCREEN HEIGHT. REPAIRED IAW REO 601R-57-21-030, REV J.
- [SDR ASOA2013071708712](https://openairdocs.org/sdr/ASOA2013071708712), Jun 5, 2013: SKIN. CRACKED. RT FUEL ACCESS HOLE 650CB FAILS NDT WITH INDICATIONS GREATER THAN 50 PERCENT SCREEN HEIGHT ON FWD SIDE OF HOLE. REPAIRED IAW REO 601R-57-21-030, REV J.
- [SDR ASOA2013071708711](https://openairdocs.org/sdr/ASOA2013071708711), Jun 5, 2013: SKIN. CRACKED. RT FUEL ACCESS HOLE 650DB FAILS NDT WITH INDICATIONS ON FWD SIDE OF HOLE GREATER THAN 50 PERCENT SCREEN HEIGHT. REPAIRED IAW REO 601R-57-21-030, REV J.
- [SDR ASOA2013071708710](https://openairdocs.org/sdr/ASOA2013071708710), Jun 5, 2013: SKIN. CRACKED. RT FUEL ACCESS HOLE 640DB FAILS NDT WITH AN INDICATION ON INBD SIDE OF HOLE GREATER THAN 50 PERCENT SCREEN HEIGHT. REPAIRED IAW REO 601R-57-21-030, REV J.
- [SDR ASOA2013071708709](https://openairdocs.org/sdr/ASOA2013071708709), Jun 5, 2013: SKIN. CRACKED. RT FUEL ACCESS HOLE 650BB FAILS NDT WITH AN INDICATION ON FWD SIDE OF HOLE GREATER THAN 50 PERCENT SCREEN HEIGHT. REPAIRED IAW REO 601R-57-21-030, REV J.
- [SDR ASOA2013071708708](https://openairdocs.org/sdr/ASOA2013071708708), Jun 5, 2013: SKIN. CRACKED. RT FUEL ACCESS HOLE 650AB FAILS NDT WITH AN INDICATION ON FWD INBD SIDE OF HOLE GREATER THAN 50 PERCENT SCREEN HEIGHT. REPAIRED IAW REO 601R-57-21-030, REV J.
- [SDR ASOA2013071708707](https://openairdocs.org/sdr/ASOA2013071708707), Jun 3, 2013: SKIN. CORRODED. LEFT WING LOWER WING PLANK ACCESS HOLE AT WS 54.897, HOLE NR 1 AT PANEL LOCATION 540BB HAS PITTING CORROSION AT FORWARD AND AFT ENDS IN THE CRITICAL REGIONS. DE
- [SDR ASOA2013071708706](https://openairdocs.org/sdr/ASOA2013071708706), Jun 3, 2013: SILL. CORRODED. SERVICE DOOR LOWER SILL IS CORRODED. REPAIRED IAW SRM 51-42-21, 51-40-11, 51-42-21, 51-42-10, 52-142-00.
- [SDR ASOA2013071708705](https://openairdocs.org/sdr/ASOA2013071708705), Jun 3, 2013: MOUNT. CORRODED. GALLEY FWD INBD AND AFT INBD FLOOR STRUCTURE MOUNT PLATES AT FS 295 AND 315 RBL 5 CORRODED AND FWD OTBD MOUNT PLATE AT FS 285 RBL 36 CORRODED. REPAIRED IAW EO 6
- [SDR ASOA2013071708704](https://openairdocs.org/sdr/ASOA2013071708704), Jun 3, 2013: INTERCOSTAL. CORRODED. PASSENGER COMPARTMENT INTERCOSTAL AT FS 349 RBL 36.45 CORRODED. REPAIRED IAW REO 601R-53-21-2439.
- [SDR ASOA2013071708703](https://openairdocs.org/sdr/ASOA2013071708703), Jun 3, 2013: ANGLE. CORRODED. PASSENGER COMPARTMENT FLOOR SILL CORRODED AT RBL 45 FROM BS 310 - 364 TO INCLUDE SERVICE DOOR SILL ANGLE. REPAIRED IAW SRM 51-40-11, 51-42-06.
- [SDR ASOA2013071708702](https://openairdocs.org/sdr/ASOA2013071708702), Jun 3, 2013: SEAT TRACK. CORRODED. PASSENGER COMPARTMENT SEAT TRACK AT RBL 9 CORRODED FROM FS 364 THRU 409+128. R & R SEAT TRACK IAW SRM 51-41-00/51-40-11.
- [SDR ASOA2013071708701](https://openairdocs.org/sdr/ASOA2013071708701), Jun 3, 2013: SEAT TRACK. CORRODED. PASSENGER COMPARTMENT SEAT TRACK AT LBL 9 CORRODED FROM FS 364 THRU 409+128. REMOVED SEAT TRACK IAW AMM 53-01-11-946-003. INSTALLED SEAT TRACK IAW AMM 53-01-11-
- [SDR ASOA2013071708700](https://openairdocs.org/sdr/ASOA2013071708700), Jun 3, 2013: FRAME. CORRODED. FUSELAGE FRAME BS 333 CORRODED ON FWD AND AFT SIDES BETWEEN STR 26L AND STR 26R. INSTALLED NEW FRAME SEGMENT IAW SRM 51-42-06 AND 51-42-21.
- [SDR ASOA2013071708699](https://openairdocs.org/sdr/ASOA2013071708699), Jun 3, 2013: FRAME. CORRODED. FUSELAGE FRAME BS 319.7 CORRODED ON FWD AND AFT SIDES BETWEEN S26L AND 26R. REMOVED CORRODED FRAME SECTOR IAW SRM 51-42-06, 51-42-21. DRILL & LOCATED 319.70 FRA
- [SDR ASOA2013071708698](https://openairdocs.org/sdr/ASOA2013071708698), Jun 3, 2013: FRAME. CORRODED. FUSELAGE FRAME BS 310 CORRODED ON THE FWD AND AFT SIDES BETWEEN S26L AND 26R. REMOVED CORRODED FRAME IAW SRM 51-42-06, 51-42-21. LOCATED, DRILLED AND INSTALLED 
- [SDR ASOA2013071708697](https://openairdocs.org/sdr/ASOA2013071708697), Jun 3, 2013: INTERCOSTAL. CRACKED. INTERCOSTAL CRACKED FROM FS 621-625 AT S13L. REMOVED INTERCOSTAL IAW SRM 51-42-06 AND 51-42-21. LOCATED AND DRILLED NEW INTERCOSTAL IAW SRM 521-40-06 AND 51-40-
- [SDR ASOA2013071708696](https://openairdocs.org/sdr/ASOA2013071708696), Jun 3, 2013: ANGLE. CRACKED. OBLIQUE ANGLE CRACKED AT FS 621-626 AT S14L. REMOVED OBLIQUE ANGLE IAW SRM 51-42-21. DRILLED AND INSTALLED NEW ANGLE IAW SRM 51-40-11 & 51-42-21.
- [SDR ASOA2013071708695](https://openairdocs.org/sdr/ASOA2013071708695), Jun 3, 2013: STRINGER. CRACKED. PAX DOOR STRINGER 3L IS CRACKED AT FS 280. R & R ONE STRINGER IAW 51-42-21-00 AND 51-42-06-00.

All 154: https://openairdocs.org/deregistered/N851AS-2018-07-30/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 20040425008089I](https://openairdocs.org/incident/20040425008089I), Apr 25, 2004: Cndair CL6002B19 (N851AS), Roanoke, VA, Minor damage. (-23) The #4 main tire tread separated during landing, causing both #4 and #3 main tires to fail. Rubber tread debris caused damage to the flap, gear door, and…

## Other aircraft with N851AS

- [Registered now](https://openairdocs.org/aircraft/N851AS): Airbus A321-211, S/N 1185

---
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.