# N847AS: 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: 7335
- Year built: 1999
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: September 17, 1999
- Certificate issued: February 13, 2017
- Last registry action: February 13, 2017
- Mode S code: AB99EB
- Owner when cancelled: [Delta Material Services LLC](https://openairdocs.org/faa-owner/DELTA%20MATERIAL%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/N847AS
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=847AS
- Page: https://openairdocs.org/deregistered/N847AS-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 (150, newest 50)

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

- [SDR ASOA2015111614061](https://openairdocs.org/sdr/ASOA2015111614061), Nov 16, 2015: DOOR FRAME. DAMAGED. AC EXTERIOR POWER RECEPTACLE DOOR LANDING DAMAGED. CUT AWAY THE DAMAGED PORTION OF THE DOOR LANDING, PN:600-33042-145 AS SHOWN ON SHEET 2 IAW GREO 601R-53-11-00
- [SDR ASOA2015072813444](https://openairdocs.org/sdr/ASOA2015072813444), Jul 28, 2015: DOOR FRAME. CRACKED. PAX DOOR FRAME IS CRACKED . REPLACED THE DOOR FRAME IAW SRM TR 51-32, AND DWG 601R31902.
- [SDR ASOA2015072413443](https://openairdocs.org/sdr/ASOA2015072413443), Jul 24, 2015: FRAME. CORRODED. FOUND WEB OF FRAME AT FS 559+96 TO HAVE MAJOR CORROSION BETWEEN STR 26L AND 26R. CUTOUT SECTION OF FRAME BETWEEN STR 25L AND 25R IAW SRM 53-00-15, REPAIR NR 1, 
- [SDR ASOA2015072013442](https://openairdocs.org/sdr/ASOA2015072013442), Jul 20, 2015: FLOOR SUPPORT. CRACKED. LEFT SIDE CARGO FLOOR LANDING PLATE HAS CRACKS AT FS 589.00 AND FS 605.00 ORIGINATING FROM RIVET HOLE. COMPLIED WITH EC/TC REO 601R-53-61-433 AND REO 601R-53-61
- [SDR ASOA2015071613441](https://openairdocs.org/sdr/ASOA2015071613441), Jul 16, 2015: INTERCOSTAL. CRACKED. BS 621 - 625 INTERCOSTAL ANGLE AT STRINGER 14R IS CRACKED. REMOVED THE INTERCOSTAL ANGLE AND INSTALLED A NEW ANGLE IAW SRM 51-40-11 AND 51-42-21.
- [SDR ASOA2015071613440](https://openairdocs.org/sdr/ASOA2015071613440), Jul 16, 2015: BULKHEAD WEB. CRACKED. FOUND THE BS 621 REAR PRESSURE BULKHEAD WEB HAS MULTIPLE CRACK INDICATIONS NOTED AT LBL 9.5, WL 127. COMPLIED WITH EC/TC REO 601R-53-61-1285 AND GREO 601R-53-61
- [SDR ASOA2015071613439](https://openairdocs.org/sdr/ASOA2015071613439), Jul 16, 2015: BULKHEAD WEB. CRACKED. FOUND BS 6210REAR PRESSURE BULKHEAD WEB HAS MULTIPLE CRACK INDICATIONS NOTED AT RBL 27.5, WL 85, APPROXIMATELY 5 INCHES IN LENGTH. INSTALLED ISOLATION BRACKETS 
- [SDR ASOA2015071513438](https://openairdocs.org/sdr/ASOA2015071513438), Jul 15, 2015: ANGLE. CORRODED. LOWER PAX DOOR SILL BS 310 - 349 FOUND CORRODED OUT OF LIMITS IAW SRM 53-00-00. REMOVED THE DOOR SILL ANGLE IAW SRM 51-42-06, 51-42-13 AND 51-42-21. LOCATED AND
- [SDR ASOA2015071513437](https://openairdocs.org/sdr/ASOA2015071513437), Jul 15, 2015: BRACKET. CRACKED. LEFT AILERON, ANGLE BRACKET BETWEEN BOTH CENTER HINGE ATTACHMENTS IS CRACKED. INSTALLED A FABRICATED ANGLE IAW SNIEO 601R3035S03.
- [SDR ASOA2015071413436](https://openairdocs.org/sdr/ASOA2015071413436), Jul 14, 2015: FLOORBEAM. CORRODED. FLOORBEAM ANGLE BS 349 IS CORRODED. CORROSION REMOVED AND FOUND OUT OF LIMITS. REPAIRED IAW REO 601R-53-21-2642, REV.
- [SDR ASOA2015071413435](https://openairdocs.org/sdr/ASOA2015071413435), Jul 14, 2015: FLOOR SUPPORT. CORRODED. LEFT FLOOR SUPPORT IS CORRODED AT BS 310. REPAIRED IAW REO:601R53-00-530, REV A.
- [SDR ASOA2015071313434](https://openairdocs.org/sdr/ASOA2015071313434), Jul 13, 2015: INTERCOSTAL. CORRODED. INTERCOSTAL BS 349 - 364, STRINGER 27R CORRODED. REMOVED THE INTERCOSTAL IAW SRM 51-42-06. REPAIRED IAW EA 32-2015-307.
- [SDR ASOA2015071313433](https://openairdocs.org/sdr/ASOA2015071313433), Jul 13, 2015: INTERCOSTAL. CORRODED. INTERCOSTAL BS 364 - 349 STR 27L CORRODED. REMOVED THE INTERCOSTAL IAW SRM 51-42-06. LOCATED AND DRILLED A NEW INTERCOSTAL IAW SRM 51-40-11. INSTALLED THE NEW I
- [SDR ASOA2015071313432](https://openairdocs.org/sdr/ASOA2015071313432), Jul 13, 2015: SKIN. CORRODED. CORROSION FORMING ON EXTERNAL SKIN ALONG STRINGER 27, BS 559+80 - 559+112. COMPLIED WITH EA 32-2015-293.
- [SDR ASOA2015071313429](https://openairdocs.org/sdr/ASOA2015071313429), Jul 13, 2015: FRAME. CORRODED. FS 319 FRAME IS CORRODED FROM STR 25L TO 25R. REMOVED CORRODED LOWER FRAME SECTOR FS 319 IAW SRM 51-42-06, 51-42-21. PN 601R32003-61. LOCATED AND DRILLED UP NEW
- [SDR ASOA2015071313428](https://openairdocs.org/sdr/ASOA2015071313428), Jul 13, 2015: FRAME. CORRODED. FS 364 FRAME IS CORRODED FROM STR 25L TO 25R. REMOVED FS 364 LOWER FRAME SECTOR IAW SRM 51-42-06. INSTALLED REPAIRED LOWER FS 364 FRAME IAW SRM 51-42-06.
- [SDR ASOA2015071313427](https://openairdocs.org/sdr/ASOA2015071313427), Jul 13, 2015: FRAME. CORRODED. FS 333 FRAME IS CORRODED FROM STR 25L TO 25R. REMVOED CORRODED LOWER FRAME SECTOR, FS 333 IAW SRM 51-42-06, 1-42-21 PN 601R32004-55. LOCATED AND DRILLED UP NEW 
- [SDR ASOA2015071313426](https://openairdocs.org/sdr/ASOA2015071313426), Jul 13, 2015: FRAME. CORRODED. FS 349 FRAME IS CORRODED FROM STR 25L TO 26R. REMOVED LOWER FRAME SECTOR PN 601R32005-69 IAW SRM 51-42-06, 51-42-21. INSTALLED NEW SERVICEABLE 601R32005-69 IAW 
- [SDR ASOA2015071313425](https://openairdocs.org/sdr/ASOA2015071313425), Jul 13, 2015: INTERCOSTAL. CORRODED. INTERCOSTAL AT FS 394 JUST TO THE LT OF STR 27 IS CORRODED. REMOVED CORRODED INTERCOSTAL PN 601R31049-11 IAW SRM 51-42-06. FOUND TO BE OUT OF LIMITS. CORROSION 
- [SDR ASOA2015071313424](https://openairdocs.org/sdr/ASOA2015071313424), Jul 13, 2015: FLOOR SUPPORT. CORRODED. RT SIDE CABIN FLOOR SILL HAS 3 AREAS OF CORROSION AROUND NUTPLATE HOLES FROM FS 559+16 TO FS 559+32. COMPLIED WITH REO 601R-53-00-526, REV DATED 5/22/13. COMPLI
- [SDR ASOA2015071313423](https://openairdocs.org/sdr/ASOA2015071313423), Jul 13, 2015: FLOOR SUPPORT. CORRODED. LT SIDE PRESSURE FLOOR SILL IS CORRODED AT 6 SPOTS AROUND NUTPLATE HOLES FROM FS 439 TO FS 559. COMPLIED WITH REO 601R-53-41-666. COMPLIED WITH REPAIR FOR CORRO
- [SDR ASOA2015071313422](https://openairdocs.org/sdr/ASOA2015071313422), Jul 13, 2015: FLOOR SUPPORT. CORRODED. RIGHT SIDE CABIN SIDE SILL IS CORRODED AT 8 NUTPLATE HOLES FROM FS 349 TO FS 394. COMPLIED WITH REO 601R-53-00-530, REV A DATED 10/7/14. REPAIRED FLOOR SILL BET
- [SDR ASOA2015071313421](https://openairdocs.org/sdr/ASOA2015071313421), Jul 13, 2015: FLOOR SUPPORT. CORRODED. LEFT CABIN SIDE SILL IS CORRODED AROUND 5 NUTPLATE HOLES FROM FS 349 TO FS 394. COMPLIED WITH REO 601R-53-00-530. ONE AREA AT FS 353 FOUND TO BE OUT OF LIMITS, 
- [SDR ASOA2015071313420](https://openairdocs.org/sdr/ASOA2015071313420), Jul 13, 2015: DOOR SILL. CORRODED. CARGO DOOR SILL PLATE IS CORRODED AROUND NUTPLATE HOLES FROM FS 574 TO FS 621. COMPLIED WITH REO 601R-53-00-526, REV. COMPLIED WITH EC/TC REO 601R-53-00-526 AND
- [SDR ASOA2015071313419](https://openairdocs.org/sdr/ASOA2015071313419), Jul 13, 2015: PLATE. CORRODED. SERVICE DOOR STEP PLATE HAS CORROSION ALL ALONG THE BOTTOM INBD EDGE. REMOVED AND LOCATED NEW SERVICEABLE STEP PLATE. DRILLED AND INSTALLED NUTPLATES IAW SRM 51
- [SDR ASOA2015071313418](https://openairdocs.org/sdr/ASOA2015071313418), Jul 13, 2015: ANGLE. CRACKED. FS 625, LT UPPER OBLIQUE ANGLE IS CRACKED. REMOVED IAW SRM 51-42-21. INSTALLEDIAW SRM 51-42-21 AND PAINTED SRM 51-21-16.
- [SDR ASOA2014090511185](https://openairdocs.org/sdr/ASOA2014090511185), Sep 3, 2014: SEAT TRACK. CORRODED. EVIDENCE OF CORROSION ON SEAT TRACK BS 349- 559. REMOVED AND REPLACED THE SEAT TRACKS IAW AMM 53-01-11, AND SRM 51-40-11.
- [SDR ASOA2014090511184](https://openairdocs.org/sdr/ASOA2014090511184), Sep 3, 2014: SEAT TRACK. CORRODED. EVIDENCE OF CORROSION ON SEAT TRACKS. REMOVED AND REPLACED THE SEAT TRACKS IAW AMM 53-01-11, AND SRM 51-40-11.
- [SDR ASOA2013012902923](https://openairdocs.org/sdr/ASOA2013012902923), Jan 13, 2013: FLOOR SUPPORT. CORRODED. FLOOR SUPPORT AND DOUBLER CORRODED AT FS 319.70, RBL 42. REMOVED RT FLOOR SUPPORT FS 310.00 TO FS 319.70 IAW SRM 51-42-06 FOR REPAIR OR REPLACEMENT. LOCATED & D
- [SDR ASOA2013012902922](https://openairdocs.org/sdr/ASOA2013012902922), Jan 11, 2013: BULKHEAD. CRACKED. INDICATION NOTED AT FS 621 REAR PRESSURE BULKHEAD AT LBL 36, WL 78 APPROX .300 IN LENGTH AT 100/5 FULL SCREEN HEIGHT. REPAIRED FS 631 BULKHEAD AT LBL 36 & WL 78
- [SDR ASOA2013012902921](https://openairdocs.org/sdr/ASOA2013012902921), Jan 11, 2013: BULKHEAD. CRACKED. INDICATION NOTED AT FS 621 REAR PRESSURE BULKHEAD AT LBL 27.50, WL 141 APRROX .150 IN LENGTH AND 55 PERCENT FULL SCREEN HEIGHT. COMPLIED REO 601R-53-61-1546 AND
- [SDR ASOA2013012902920](https://openairdocs.org/sdr/ASOA2013012902920), Jan 10, 2013: DRAG ANGLE. CRACKED. PAX DOOR AFT DRAG ANGLE CRACKED. COMPLIED WITH W/O 276849 AND REO 601R-52-11-513.
- [SDR ASOA2013012902919](https://openairdocs.org/sdr/ASOA2013012902919), Jan 9, 2013: ANGLE. CRACKED. FS 484.00, ANGLE AT RBL 27 IS CRACKED. REPAIRED ANGLE IAW REO 601R-53-41-059.
- [SDR ASOA2013012902918](https://openairdocs.org/sdr/ASOA2013012902918), Jan 9, 2013: ANGLE. CRACKED. FS 484.00 ANGLE AT LBL 9 IS CRACKED. R & R ANGLE IAW SRM 51-40-11, 51-42-06 AND 51-42-21.
- [SDR ASOA2013012902917](https://openairdocs.org/sdr/ASOA2013012902917), Jan 9, 2013: ANGLE. CRACKED. FS 484.00, ANGLE AT LBL 27 IS CRACKED. REPAIRED IAW REO 601R-53-41-059.
- [SDR ASOA2013012902915](https://openairdocs.org/sdr/ASOA2013012902915), Jan 9, 2013: BRACKET. CORRODED. SERVICE DOOR CUTOUT TEE BRACKET IS SEVERELY CORRODED AT FS 319.70, WL 70.60. REMOVED FITTING IAW SRM 51-42-21 FOR REPLACEMENT. LOCATED & DRILLED NEW SERVICEABLE
- [SDR ASOA2013012902914](https://openairdocs.org/sdr/ASOA2013012902914), Jan 9, 2013: FLOORBEAM. CRACKED. FLOORBEAM ANGLE CRACKED AT FS 280, LBL 9 INBD AND OTBD. R & R CRACKED FLOORBEAM ANGLE AT FS 280, LBL 9 INBD AND OTBD IAW SRM 51-42-21. FABRICATED NEW FS 280, LB
- [SDR ASOA2013012902913](https://openairdocs.org/sdr/ASOA2013012902913), Jan 9, 2013: FLOORBEAM. CORRODED. CARGO FLOORBEAM HAS CORROSION AROUND FASTENER HOLES AT FS 589, BETWEEN LBL 9 AND LBL 27. REMOVED CAP STRIP BETWEEN LBL 9 AND LBL 27 IAW SRM 51-42-06 AND 51-42-2
- [SDR ASOA2013012902912](https://openairdocs.org/sdr/ASOA2013012902912), Jan 9, 2013: FLOOR SUPPORT. CORRODED. RT FLOOR SILL HAS CORROSION AROUND FASTENER HOLDS BETWEEN FS 559+80 AND FS 589. BLENDED CORROSION IAW SRM 51-21-00. SRM HAS NO ALLOWABLE LIMITS. AMOUNT OF CORRO
- [SDR ASOA2013012902911](https://openairdocs.org/sdr/ASOA2013012902911), Jan 9, 2013: FLOOR SUPPORT. CORRODED. LT FLOOR SILL HAS CORROSION AROUND FASTENER HOLES BETWEEN FS 559+96 AND 559+112. BLENDED CORROSION IAW SRM 51-21-06, SRM HAS NO ALLOWABLE LIMITS SUBMITTED FOR R
- [SDR ASOA2013012902910](https://openairdocs.org/sdr/ASOA2013012902910), Jan 9, 2013: FRAME. CORRODED. FS 605, FRAME CORRODED BETWEEN STRINGERS 26L AND 26R. R & R FS 605 FRAME FROM STR 25L TO STR 22R IAW REO 601R-53-61-4763 USING SRM 53-00-15, SHEET 2 REPAIR NR 1
- [SDR ASOA2013012902909](https://openairdocs.org/sdr/ASOA2013012902909), Jan 9, 2013: FITTING. CRACKED. CO-PILOTS WINDSHIELD SIDE POST LOWER AFT, OTBD FITTING IS CRACKED. REMOVED CRACKED LOWER AFT OTBD FITTING FROM CO-PILOTS WINDSHIELD SIDE POST IAW SRM 51-42-21. 
- [SDR ASOA2013012902908](https://openairdocs.org/sdr/ASOA2013012902908), Jan 9, 2013: FITTING. CRACKED. PILOTS WINDSHIELD SIDE POST LOWER AFT OTBD FITTING IS CRACKED. REMOVED CRACKED LOWER AFT OTBD FITTING FROM PILOTS WINDSHIELD SIDE POST IAW SRM CH 51-42-21. LOCA
- [SDR ASOA2013012902907](https://openairdocs.org/sdr/ASOA2013012902907), Jan 7, 2013: DOOR. MISINSTALLED. RT OVERWING EMERGENCY EXIT EXCEEDED FORCE TO OPEN. ON FURTHER INVESTIGATION, FOUND LT AND RT EMERGENCY EXIT DOORS INSTALLED IN WRONG LOCATION. FUNCTION TEST GOO
- [SDR ASOA2012101602353](https://openairdocs.org/sdr/ASOA2012101602353), Oct 12, 2012: LAMP. BURNED OUT. CEILING AFT EMERGENCY FLOOD LIGHT INOPERATIVE. LAMPED CEILING EMERGENCYH AFT FLOOD LIGHT IAW AMM 33-51-16.
- [SDR ASOA201201677](https://openairdocs.org/sdr/ASOA201201677), May 23, 2012: COALESCER BAG. ODOR. ACFT HAS STRONG FUEL ODOR DURING DESCENT. R & R WATER SEPARATOR COLESCER ON LT AND RT PACKS IAW AMM 21-51-13, OPS CHECKED GOOD, NO FURTHER DEFECTS NOTED. ACFT O
- [SDR ASOA201201229](https://openairdocs.org/sdr/ASOA201201229), Apr 7, 2012: BULKHEAD. CRACKED. BULKHEAD CRACKED AT FS 202 BY PARKING BRAKE CABLE. WORK COMPLETED IAW EC/TC REO 601R-53-11-563 AND STARTED DRILLING OUT FASTENERS FOR REPAIR NR 1 IAW EC/TC REO 
- [SDR ASOA201200877](https://openairdocs.org/sdr/ASOA201200877), Feb 23, 2012: LATCH. LACK OF LUBE. ON PASSENGER DOOR, TEE HANDLE INDICATOR SHOWS LOCKED WHEN DOOR IS OPEN AND F/A IS HAVING DIFFICULTY OPENING AND CLOSING THE DOOR. LUBRICATED PASSENGER DOOR LATC
- [SDR ASOA201102169](https://openairdocs.org/sdr/ASOA201102169), Nov 12, 2011: LAMP. BURNED OUT. AFT CENTER CEILING EMERGENCY EXIT SIGN HAS SEVERAL INOPERATIVE BULBS. REPLAMPED AFT CENTER CEILING EMERGENCY EXIT SIGN. OPS CHECKED GOOD IAW AMM 33-51-00.
- [SDR ASOA201101870](https://openairdocs.org/sdr/ASOA201101870), Oct 7, 2011: LAMP. BURNED OUT. LT OVER WING AFT EMERGENCY LIGHT INOPERATIVE. RELAMPED LT OVERWING AFT EM LIGHT W/A SERVICEABLE LAMP IAW AMM 33-51-21. OPS CHECKED GOOD.

All 150: https://openairdocs.org/deregistered/N847AS-2018-07-30/reports.md

## FAA accident and incident reports (2)

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 20050321008189I](https://openairdocs.org/incident/20050321008189I), Mar 21, 2005: Cndair CL6002B19 (N847AS), Covington/Cinci, KY, Minor damage. (-23) Ground crew tug operator stopped his tug to assist at gate A-26. Tug operator heard that a tug had hit an aircraft and noticed that his tug was missing.…
- [Incident 19991023038719I](https://openairdocs.org/incident/19991023038719I), Oct 23, 1999: Cndair CL6002B19 (N847AS), Fort Wayne, IN, Minor damage. While repositioning the aircraft from gate six to gate two, the left winglet made contact with the jetway and 17 inches of vertical wing tip was broken off…

## Other aircraft with N847AS

- [Registered now](https://openairdocs.org/aircraft/N847AS): Ea Vision EA J100, S/N EAVUAV502585747

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