# N848AS: 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: 7339 - Year built: 1999 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: November 17, 1999 - Certificate issued: February 13, 2017 - Last registry action: February 13, 2017 - Mode S code: AB9DA2 - 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/N848AS - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=848AS - Page: https://openairdocs.org/deregistered/N848AS-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 (128, newest 50) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR ASOA20160905001](https://openairdocs.org/sdr/ASOA20160905001), Sep 5, 2016: BOLT. BROKEN. CABIN WILL NOT RAISE. MX REPLACED BROKEN EYEBOLT AND OPS CHECKED PAX DOOR IAW 52-11-00. AIRCRAFT APPROVED FOR RETURN TO SERVICE. - [SDR ASOA2016071315087](https://openairdocs.org/sdr/ASOA2016071315087), Jul 13, 2016: BATTERY PACK. DISCHARGED. F/A FLASHLIGHT INOPERATIVE. REPLACED THE BATTERIES. - [SDR ASOA2016071315086](https://openairdocs.org/sdr/ASOA2016071315086), Jul 13, 2016: FLASHLIGHT. INOPERATIVE. F/O FLASHLIGHT INOPERATIVE. REPLACED THE FLASHLIGHT IAW AMM 25-61-04. - [SDR ASOA2015060513054](https://openairdocs.org/sdr/ASOA2015060513054), Jun 4, 2015: LIGHT. UNSERVICEABLE. LOWER EMERGENCY LIGHT IN GALLEY UNSERVICEABLE. R & R GALLEY EMERGENCY LIGHT IAW AMM 33-51-10. - [SDR ASOA2015020612167](https://openairdocs.org/sdr/ASOA2015020612167), Feb 5, 2015: BATTERY. DISCONNECTED. NR 3 AND 4 EXTERIOR EMERGENCY LIGHTS INOPERATIVE. FOUND NR 2 EMERGENCY BATTERY PACK NOT INSTALLED IN CHARGER UNIT. INSTALLED BATTERY PACK IAW AMM 33-51-04. OPS - [SDR ASOA2015012212071](https://openairdocs.org/sdr/ASOA2015012212071), Jan 19, 2015: CONNECTOR. BROKEN. EMERGENCY EXIT INOPERATIVE ON SIDE PANEL OF GALLEY NR 1. REPLACED BROKEN CONNECTOR J122LY BY REMOVING IT AND INSTALLING A NEW ONE IAW ESPM 20-17-31. PERFORMED O - [SDR ASOA2015012212070](https://openairdocs.org/sdr/ASOA2015012212070), Jan 18, 2015: SEAT TRACK. CORRODED. SEAT TRACK CORRODED OUT OF LIMITS IAW SRM 53-31-49 AND SRM 53-21-49. FABRICATED & INSTALLED NEW SEAT TRACK IAW REO 601R-53-00-485. - [SDR ASOA2015012212069](https://openairdocs.org/sdr/ASOA2015012212069), Dec 20, 2014: ATTACH BRACKET. CRACKED. CARGO DOOR LINTEL AFT BRACKET ATTACHED TO PRESSURE BULKHEAD CRACKED, REMOVED THE BRACKET. INSTALLED A NEW BRACKET IAW SRM 51-40-11, SRM 51-42-21. - [SDR ASOA2014122911997](https://openairdocs.org/sdr/ASOA2014122911997), Dec 20, 2014: SEAT TRACK. CORRODED. SEAT TRAC AT RBL9 BS 559-559+80 CORRODED. R & R THE SEAT TRACK IAW AMM 53-01-11-000-802, 53-01-11-400-802, AND SRM 51-40-11. - [SDR ASOA2014122911996](https://openairdocs.org/sdr/ASOA2014122911996), Dec 20, 2014: ISOLATOR. BROKEN. 5 BROKEN ISOLATORS FOUND ON THE AFT PRESSURE BULKHEAD FWD FACE. REPLACED 5 BROKEN ISOLATORS ON AFT PRESSURE BULKHEAD FWD FACE IAW SRM 51-42-13. - [SDR ASOA2014122911995](https://openairdocs.org/sdr/ASOA2014122911995), Dec 19, 2014: FRAME. CORRODED. CORROSION AROUND 2 NUTPLATES UNDER FLOORBOARD 251ALF ON RBL9 AND AT FS 409+16 AND FS 409+32. REMOVED CORROSION IAW SRM 51-21-06. REMOVED .023 MATERIAL THICKINES - [SDR ASOA2014080110987](https://openairdocs.org/sdr/ASOA2014080110987), Jul 31, 2014: LENS. MISSING. EMERGENCY EXIT SIGN COVER MISSING BETWEEN GALLEY SERVICE DOOR AND SNACK BINS. REINSTALLED EMERGENCY LIGHT COVER IAW AMM 33-51-13. - [SDR ASOA2013011502802](https://openairdocs.org/sdr/ASOA2013011502802), Jan 10, 2013: WIRE. DISCONNECTED. AFT CEILING EMERGENCY LIGHT IS INOPERATIVE. REMOVED AFT CEILING EMERGENCY LIGHT, FOUND WIRES TO BE DISCONNECTED. CONNECTED WIRES AND REINSTALLED LIGHT. OPS CHEC - [SDR ASOA2013011502801](https://openairdocs.org/sdr/ASOA2013011502801), Dec 19, 2012: FITTING. CORRODED. SERVICE DOOR FITTING IS GOUGED AND CORRODED. REMOVED SERVICE DOOR FITTING BETWEEN FS 319 AND 349 IAW SRM 51-41-02. LOCATED AND DRILLED NEW SERVICE DOOR FITTING, - [SDR ASOA2013011502800](https://openairdocs.org/sdr/ASOA2013011502800), Dec 19, 2012: FLOORBEAM. CORRODED. THE FLOORBEAM STRUCTURE MOUNT IS CORRODED AT FS 310. REMOVED FLOORBEAM SUPPORT MOUNT IAW SRM 51-42-21. LOCATED & INSTALLED FLOORBEAM JOINT ANGLE IAW SRM 51-40-1 - [SDR ASOA2013011502799](https://openairdocs.org/sdr/ASOA2013011502799), Dec 19, 2012: FLOORBEAM. CRACKED. FS 280 FLOORBEAM CRACKED AND CORRODED. REMOVED DAMAGED AND REPAIRED IAW SRM CH 51-42-06, 51-42-10 & 51-42-21, & REO 601R-53-11-926. - [SDR ASOA2013011502798](https://openairdocs.org/sdr/ASOA2013011502798), Dec 19, 2012: FLOOR SUPPORT. CORRODED. CORROSION ON FS 280.00 FLOOR SUPPORT. REMOVED DAMAGED FWD FLOOR SUPPORT IAW SRM CH 51-42-06 & 51-42-21. LOCATED & DRILLED NEW SERVICEABLE FLOOR SUPPORT, IAW SRM - [SDR ASOA2013011502797](https://openairdocs.org/sdr/ASOA2013011502797), Dec 19, 2012: SILL. CORRODED. CORROSION ON PAX DOOR LOWER SILL. REMOVED SILL ANGLE (LOWER) IAW SRM 51-42-21 & 51-42-06. LOWER SILL ANGLE FOUND TO HAVE CORROSION EXCEEDING LIMITS IAW SRM 53-0 - [SDR ASOA2013011502796](https://openairdocs.org/sdr/ASOA2013011502796), Dec 19, 2012: SILL. CORRODED. CORROSION ON PAX DOOR LOWER SILL FWD AND AFT CUPS. REPAIRED IAW SRM CH 51-42-06 & 51-42-11. - [SDR ASOA2013011502795](https://openairdocs.org/sdr/ASOA2013011502795), Dec 19, 2012: BEAM. CORRODED. CORROSION ON PAX DOOR AFT FRAME LOWER TRANSVERSE BEAM AT FS 349.00. REPAIRED IAW REO 601R-53-21-2392. THIS REPAIR IS CLASSIFIED AS A MAJOR REPAIR IAW SOP 5702. - [SDR ASOA2013011502794](https://openairdocs.org/sdr/ASOA2013011502794), Dec 19, 2012: FRAME. CORRODED. CORROSION ON FRAME AT FS 349 BETWEEN STR 26L AND 26R. REMOVED LOWER FRAME SECTION FS 349 IAW SRM 51-42-06 AND 51-42-21. LOCATED AND DRILLED NEW SERVICEABLE LWR - [SDR ASOA2013011502793](https://openairdocs.org/sdr/ASOA2013011502793), Dec 19, 2012: FRAME. CORRODED. CORROSION ON FRAME AT FS 314.7 BETWEEN STR 26L AND STR 26R. REMOVED LOWER SECTION OF FRAME AT FS 319.00, STR 24L-24R IAW SRM 51-42-06 & 51-42-21. LOCATED & DRIL - [SDR ASOA2013011502792](https://openairdocs.org/sdr/ASOA2013011502792), Dec 19, 2012: FRAME. CORRODED. CORROSION ON FRAME AT FS 310.00 BETWEEN S26L AND 26R. REPAIRED IAW SRM 51-42-06 AND 51-42-21. - [SDR ASOA2013011502791](https://openairdocs.org/sdr/ASOA2013011502791), Dec 19, 2012: FLOOR SUPPORT. CORRODED. CORROSION ON RT FLOOR SUPPORT FWD OF SERVICE DOOR FROM FS 319.70 TO FS 310.00 AND AFT OF DOOR FROM FS 349.00 TO 364.00. REPAIRED IAW SRM 51-42-06, SRM 53-00-00 - [SDR ASOA2013011502790](https://openairdocs.org/sdr/ASOA2013011502790), Dec 19, 2012: BEAM. CORRODED. CORROSION ON THE END OF THE TRANSVERSE BEAM FS 349.00, RBL 36 AT SERVICE DOOR AFT FRAME. COMPLIED WITH STEP 1 OF REO 601R-53-21-2391, REV P1 CUT AWAY DAMAGE. - [SDR ASOA2013011502789](https://openairdocs.org/sdr/ASOA2013011502789), Dec 19, 2012: SILL. CORRODED. CORROSION ON SERVICE DOOR SILL FROM FS 319.70 TO FS 349.00. REMOVED SILL IAW SRM 51-42-06 AND SRM 51-42-21 AND SRM 51-42-10. DRILLED, LOCATED AND INSTALLED NEW - [SDR ASOA2013011402788](https://openairdocs.org/sdr/ASOA2013011402788), Dec 19, 2012: SILL. CORRODED. CARGO DOOR SILL IS CORRODED AROUND ALL NUTPLATES. REMOVED CARGO DOOR SILL IAW SRM 51-42-06, 51-42-21 & 51-42-10. INSTALLED NEW SERVICEABLE SILL IAW REO 601R-53- - [SDR ASOA2013011402787](https://openairdocs.org/sdr/ASOA2013011402787), Dec 19, 2012: FLOOR SUPPORT. CORRODED. RT PRESSURE FLOOR SUPPORT IS CORRODED INBD OF EMERGENCY EXIT. REPAIRED IAW REO 601R-53-41-666, REV C. - [SDR ASOA2013011402786](https://openairdocs.org/sdr/ASOA2013011402786), Dec 19, 2012: STRINGER. CORRODED. AFT EQUIPMENT COMPARTMENT STRINGER 19R IS CORRODED BETWEEN FS 654.5 AND 672.2. STRINGER DAMAGED BEYOND REPAIR, REMOVED STRINGER IAW SRM 51-42-06. LOCATED, DRILL - [SDR ASOA2013011402785](https://openairdocs.org/sdr/ASOA2013011402785), Dec 17, 2012: POST. CRACKED. FS 409+128 VERTICAL POST LBL 18 INBOARD AFT UPPER RADIUS FAILED NDT WITH INDICATION GREATER THAN 50 PERCENT SCREEN HEIGHT APPROX .2 LONG. REMOVED INBD & OTBD VE - [SDR ASOA2013011402784](https://openairdocs.org/sdr/ASOA2013011402784), Dec 11, 2012: FLOORBEAM. CRACKED. FLOORBEAM ANGLES AT FS 484.00, LBL 27 AND LBL 36 ARE CRACKED. FABRICATED AND INSTALLED NEW ANGLES IAW REO 601R-53-41-059. - [SDR ASOA2013011402783](https://openairdocs.org/sdr/ASOA2013011402783), Dec 11, 2012: FLOORBEAM. CRACKED. FLOORBEAM AT FS 484.00, RBL 27 AND RBL 36 CRACKED. FABRICATED AND INSTALLED FLOORBEAM ANGLE IAW REO 601R-53-41-059. - [SDR ASOA2013011402782](https://openairdocs.org/sdr/ASOA2013011402782), Dec 11, 2012: ANGLE. CRACKED. INBD AND OTBD ANGLES AT FS 280.00, RBL 9 CRACKED. ANGLES REPLACED IN CONJUNCTION WITH REO 601R-53-11-926. - [SDR ASOA2013011402781](https://openairdocs.org/sdr/ASOA2013011402781), Dec 11, 2012: ANGLE. CRACKED. INBD AND OTBD ANGLES AT FS 280.00 LBL 9 CRACKED. ANGLES REPLACED IN CONJUNCTION WITH REO 601R-53-11-926. - [SDR ASOA2013011402780](https://openairdocs.org/sdr/ASOA2013011402780), Dec 11, 2012: SUPPORT BRACKET. CRACKED. RIGHT WINDSHIELD LOWER SIDE POST SUPPORT BRACKET IS CRACKED, APPROX .500" LONG. INSTALLED NEW SUPPORT BRACKET IAW SRM 51-42-21. - [SDR ASOA2013011402779](https://openairdocs.org/sdr/ASOA2013011402779), Dec 11, 2012: CONNECTOR. BROKEN. BROKEN QUICK DISCONNECT FOR EMERGENCY LIGHTS IN WARDROBE. INSTALLED QUICK DISC SPLICES FOR WARDROBE EMERGENCY LIGHT IAW ESPM 20-17-10 ON ACFT SIDE. OPS CHECKED, - [SDR ASOA2013011102778](https://openairdocs.org/sdr/ASOA2013011102778), Dec 11, 2012: BULKHEAD. CRACKED. FS 621 BULKHEAD FWD FACE FAILS NDT WITH AN INDICATION ON RBL 27.50, WL 83-93 GREATER THAN 50 PERCENT SCREEN HEIGHT. REPAIRED IAW REO 601R-53-61-1285. - [SDR ASOA2013011102777](https://openairdocs.org/sdr/ASOA2013011102777), Dec 11, 2012: BULKHEAD. CRACKED. FS 621, BULKHEAD FWD FACE FAILS NDT WITH AN INDICATION ON LBL 36.20, WL 80 GREATER THAN 50 PERCENT SCREEN HEIGHT. REPAIRED IAW REO 601R-53-61-4747. - [SDR ASOA201200065](https://openairdocs.org/sdr/ASOA201200065), Jan 6, 2012: PDU. FAILED. LEFT THRUST REVERSER UNLOCKED MESSAGE DURING CLIMB, EMERGENCY DECLARED. PERFORMED CHECKLIST AND COMPLIED WITH QRH PROCEDURE. AIR RETURN TO DEPARTURE. R & R LT E - [SDR ASOA201102315](https://openairdocs.org/sdr/ASOA201102315), Dec 4, 2011: FLASHLIGHT. INOPERATIVE. F/O FLASHLIGHT INOPERATIVE. R & R F/O FLASHLIGHT IAW AMM 25-61-04. OPS CHECKED GOOD. - [SDR ASOA201100468](https://openairdocs.org/sdr/ASOA201100468), Mar 11, 2011: BATTERY. INOPERATIVE. CA'S FLASHLIGHT INOP. REPLACED BATTERIES, CAPT FLASHLIGHT IAW AMM 25-60-00. OPS CHECK GOOD. - [SDR ASOA201001943](https://openairdocs.org/sdr/ASOA201001943), Dec 14, 2010: FLOORBEAM. CORRODED. CORROSION AROUND SEVERAL SCREW HOLES UNDER FLOORBOARD 251ALF AND ON FLOORBEAMS. BLENDED AREA AT RBL9 BETWEEN FS 409.00+48 AND FS 409.00+64 HAS A REMAINING THICK - [SDR ASOA201001905](https://openairdocs.org/sdr/ASOA201001905), Dec 9, 2010: ATTACH FITTING. CRACKED. CLIP CRACKED REAR BULKHEAD AFT FACE AT FS 621 ON 3RD INTERCOSTAL FROM BOTTOM ON RT SIDE. CLIP CRACKED REAR BULKHEAD AFT FACE AT FS 621 ON 3RD INTERCOSTAL FROM B - [SDR ASOA201001904](https://openairdocs.org/sdr/ASOA201001904), Dec 9, 2010: ATTACH FITTING. CRACKED. CLIP CRACKED REAR BULKHEAD AFT FACE AT FS 621 ON 3RD INTERCOSTAL FROM BOTTOM ON LT SIDE. CLIP CRACKED ON REAR BULKHEAD AFT FACE WAS FOUND TO BE AT FS 625 LT SID - [SDR ASOA201002015](https://openairdocs.org/sdr/ASOA201002015), Dec 8, 2010: SEAT TRACK. CORRODED. LT SIDE SEAT RAIL HAS MINOR CORROSION AT SEAT POSITION 3A (SIDE RAIL). REMOVED MINOR CORROSION ON LT SIDE SEAT RAIL AT SEAT POSITION 3A IAW SRM 51-21-06. MATERI - [SDR ASOA201002003](https://openairdocs.org/sdr/ASOA201002003), Dec 8, 2010: SEAT TRACK. CORRODED. RT SIDE SEAT RAIL HAS MINOR CORROSION AT SEAT LOCATION 12CD. REMOVED MINOR CORROSION ON RT SIDE SEAT RAIL. REMOVED .008" MATERIAL AT LOCATION 12CD. IAW SRM 51-2 - [SDR ASOA201001911](https://openairdocs.org/sdr/ASOA201001911), Dec 8, 2010: NUT PLATE. BROKEN. AFT CARGO AFT PRESSURE BULKHEAD HAS NUTPLATE BROKEN AT CTR ROW, 2ND ROW UP FROM FLOOR (ISOLATOR). REMOVED BROKEN ISOLATOR MOUNT ON AFT PRESS BULKHEAD & INSTALLE - [SDR ASOA201001892](https://openairdocs.org/sdr/ASOA201001892), Dec 8, 2010: SEAT TRACK. CORRODED. 9L SEAT TRACK SEGMENT FROM FS 559 + 32 TO 559 + 80 CORRODED BEYOND LIMITS. REMOVED CORROSION FROM SEAT TRACK. BLEND DIMENSIONS .5" WIDE X .5" LENGTH X .024" DEE - [SDR ASOA201001891](https://openairdocs.org/sdr/ASOA201001891), Dec 8, 2010: SEAT TRACK. CORRODED. 9R SEAT TRACK SEGMENT FROM FS 409 TO 559 + 32 CORRODED BEYOND LIMITS. REMOVED CORROSION FROM SEAT TRACK. BLEND DIMENSIONS .5" WIDE X .5" LONG X .022" DEEP. OUT - [SDR ASOA201001890](https://openairdocs.org/sdr/ASOA201001890), Dec 8, 2010: SEAT TRACK. CORRODED. 9L SEAT TRACK SEGMENT FROM FS 409 TO 559 + 32 CORRODED BEYOND LIMITS. REMOVED CORROSION FROM LT PASSENGER SEAT TRACK. BLEND DIMENSION .5" LONG X .5" WIDE X .025 All 128: https://openairdocs.org/deregistered/N848AS-2018-07-30/reports.md ## Other aircraft with N848AS - [Registered now](https://openairdocs.org/aircraft/N848AS): Ea Vision EA J100, S/N EAVUAV502585748 --- 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.