# N850AS: 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: 7355
- Year built: 1999
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: January 7, 2000
- Certificate issued: February 13, 2017
- Last registry action: February 13, 2017
- Mode S code: ABA769
- 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/N850AS
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=850AS
- Page: https://openairdocs.org/deregistered/N850AS-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 (178, newest 50)

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

- [SDR ASOA2015111714064](https://openairdocs.org/sdr/ASOA2015111714064), Nov 17, 2015: LAMP. BURNED OUT. EXTERNAL EMERGENCY LIGHT, NR 2 INOPERATIVE. RE-LAMPED IAW AMM 33-51-21. SYSTEM OPS CHECKED GOOD. NO FURTHER ACTION.
- [SDR ASOA2015092513833](https://openairdocs.org/sdr/ASOA2015092513833), Sep 25, 2015: BRACKET. UNSERVICEABLE. NOSE GEAR DID NOT RETRACT AFTER TAKEOFF. GEAR DISAGREE MSG AND NOSE DOOR MSG DISPLATED GEAR HANDLE PULLED AND STOWED. ACFT RETURNED TO DEPARTURE. R & R NLG LENT
- [SDR ASOA2015073013530](https://openairdocs.org/sdr/ASOA2015073013530), Jul 30, 2015: SEAT TRACK. CORRODED. LEFT SIDE SEAT TRACK HAS CORROSION AT BS 409+16 TO 409+112. CORROSION EXCEEDS THE LIMITS OF SRM 53-21-49, FIG 101. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 5
- [SDR ASOA2015072513528](https://openairdocs.org/sdr/ASOA2015072513528), Jul 25, 2015: SEAT TRACK. CORRODED. SEAT TRACK BS 544 - 559+112 CORRODED. FOUND TO BE OUT OF LIMITS IAW SRM 53-21-49-00. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-01-11-000-802, SRM 51-40-11,
- [SDR ASOA2015072513527](https://openairdocs.org/sdr/ASOA2015072513527), Jul 25, 2015: SEAT TRACK. CORRODED. SEAT TRACK BS 544 - 559+112 CORRODED. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-01-11-000-802 AND AMM 53-01-11-400-802.
- [SDR ASOA2015072513526](https://openairdocs.org/sdr/ASOA2015072513526), Jul 25, 2015: SEAT TRACK. CORRODED. SEAT TRACK BS 450 - 499 CORRODED. CORROSION FOUND OUT OF LIMITS IAW SRM 53-21-49-00, FIG 101. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-01-11-000-802 AND A
- [SDR ASOA2015072513525](https://openairdocs.org/sdr/ASOA2015072513525), Jul 25, 2015: SEAT TRACK. CORRODED. SEAT TRACK BS 409+128 - 559 CORRODED. FOUND TO BE OUT OF LIMITS IAW SRM 53-21-49-00. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-01-11-000-802 & GREO 601R 53
- [SDR ASOA2015072513524](https://openairdocs.org/sdr/ASOA2015072513524), Jul 25, 2015: SEAT TRACK. CORRODED. SEAT TRACK BS 394 - 409+128 CORRODED. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-01-11-000-802 AND AMM 53-01-11-40-802.
- [SDR ASOA2015072513523](https://openairdocs.org/sdr/ASOA2015072513523), Jul 25, 2015: SEAT TRACK. CORRODED. SEAT TRACK BS 364 - 394 FOUND CORRODED. CORROSION FOUND OUT OF LIMITS OF SRM 53-21-49, FIG 101. R & R THE SEAT TRACK IAW AMM 53-01-11-000-400-802.
- [SDR ASOA2015072513522](https://openairdocs.org/sdr/ASOA2015072513522), Jul 25, 2015: SEAT TRACK. CORRODED. SEAT TRACK BS 364-394 LT FOUND CORRODED. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-01-11-000-802 AND AMM 53-01-11-400-802.
- [SDR ASOA2015072413521](https://openairdocs.org/sdr/ASOA2015072413521), Jul 24, 2015: FLOOR SUPPORT. CORRODED. CORROSION FOUND LT SIDE PRESSURE FLOOR SUPPORT AT BS 544. REPAIRED IAW EC/TC REO 601R-53-41-666-01 AND REO 601R-53-41-666, REV C.
- [SDR ASOA2015072413520](https://openairdocs.org/sdr/ASOA2015072413520), Jul 24, 2015: FLOOR SUPPORT. CORRODED. CORROSION FOUND ON LT SIDE PRESSURE FLOOR SUPPORT AT BS 522.4. REPAIRED IAW EC/TC REO 601R-53-41-666-01 AND REO 601R-53-41-666, REV C.
- [SDR ASOA2015072413519](https://openairdocs.org/sdr/ASOA2015072413519), Jul 24, 2015: FLOOR SUPPORT. CORRODED. CORROSION FOUND LT SIDE PRESSURE FLOOR SUPPORT AT BS 513. REPAIRED IAW EC/TC REO 601R-53-41-666-01 AND REO 601R-53-41-666, REV C.
- [SDR ASOA2015072413518](https://openairdocs.org/sdr/ASOA2015072413518), Jul 24, 2015: FLOOR SUPPORT. CORRODED. CORROSION FOUND RT PRESSURE FLOOR SUPPORT AT BS 513. REPAIRED IAW ECTC REO 601R-53-41-666 01 AND REO 601R-53-41-666, REV C.
- [SDR ASOA2015072413517](https://openairdocs.org/sdr/ASOA2015072413517), Jul 24, 2015: ANGLE. CORRODED. ANGLE FOUND CORRODED, RT SIDE BS 449.85 - 473.15. REPAIRED IAW EC/TC REO 601R-53-41-666-01 AND REO 601R-53-41-666, REV C.
- [SDR ASOA2015072313516](https://openairdocs.org/sdr/ASOA2015072313516), Jul 23, 2015: FLOOR SUPPORT. CORRODED. RIGHT FLOOR SUPPORT BETWEEN BS 310 - 319.7 CORRODED. REMOVED FLOOR SUPPORT IAW SRM 51-42-00. REPLACED THE FLOOR SUPPORT IAW SR 51-42-06-00.
- [SDR ASOA2015072113515](https://openairdocs.org/sdr/ASOA2015072113515), Jul 21, 2015: ANGLE. CRACKED. CRACK FOUND ON ANGLE ATTACHED TO AFT PRESSURE BULKHEAD AT BS 625 - 621 ABOVE LOWER TRANSVERSE BEAM STRUCTURE LT SIDE. R & R THE ANGLE IAW SRM 51-42-20.
- [SDR ASOA2015072113514](https://openairdocs.org/sdr/ASOA2015072113514), Jul 21, 2015: ANGLE. CRACKED. CRACK FOUND ON ANGLE ATTACHED TO AFT PRESSURE BULKHEAD BS 625 - 621 ABOVE LOWER TRANSVERSE BEAM STRUCTURE RT SIDE. REMOVED CRACKED ANGLE AND INSTALLED IAW SRM 5
- [SDR ASOA2015072113513](https://openairdocs.org/sdr/ASOA2015072113513), Jul 21, 2015: SKIN. DENTED. DENT FOUND ON FUSELAGE AT BS 625 - 640 AND STRINGERS 25-26. REPAIRED IAW EA 32-2015-319 SECTION 1.
- [SDR ASOA2015072113512](https://openairdocs.org/sdr/ASOA2015072113512), Jul 21, 2015: BATTERY PACK. NO TEST. NR 1 EMERGENCY LIGHT BATTERY PACK FAILED OPS CHECK. R & R THE BATTERY PACK IAW AMM 33-51-04-000-801 & OPS CHECKED GOOD 35-51-04-400-801.
- [SDR ASOA2015072013531](https://openairdocs.org/sdr/ASOA2015072013531), Jul 20, 2015: STRUCTURE. DAMAGED. DURING VISUAL INSPECTION OF RT WING DAMAGE TO RT FLAP OTBD T/E. COMPLIED WITH EC/TC EO 600-57-128 02. REPAIRED DAMAGE IAW SRM 51-42-00, KJ161732 8/9/15 (PB) M/A
- [SDR ASOA2015042212627](https://openairdocs.org/sdr/ASOA2015042212627), Apr 18, 2015: SIGN. INOPERATIVE. LIGHTED FLOOR-LEVEL EXIT SIGN AT ENTRANCE BULKHEAD INOPERATIVE. R & R SIGN IAW AMM 33-51-10. SYS OPS CHECKED GOOD. NO FURTHER ACTION.
- [SDR ASOA2015020212137](https://openairdocs.org/sdr/ASOA2015020212137), Jan 28, 2015: BULKHEAD. CRACKED. AFT PRESSURE BULKHEAD CRACKED ALONG RBL 27.50 BETWEEN SECOND AND THIRD STAND OFF, FROM FLOOR WL 73.50.
- [SDR ASOA2015020212136](https://openairdocs.org/sdr/ASOA2015020212136), Jan 28, 2015: BULKHEAD. CRACKED. AFT PRESSURE BULKHEAD CRACKED ABOVE WL121.93 AND RBL9.50.
- [SDR ASOA2015020212135](https://openairdocs.org/sdr/ASOA2015020212135), Jan 28, 2015: BULKHEAD. CRACKED. AFT PRESSURE BULKHEAD CRACKED BELOW WL 120.43 AND LBL 18.00.
- [SDR ASOA2015020212134](https://openairdocs.org/sdr/ASOA2015020212134), Jan 28, 2015: ANGLE. CRACKED. CRACK ANGLE BELOW AFT END OF CARGO DOOR HORIZONTAL SUPPORT AT APPROXIMATELY WL120.43 AND LBL36.2.
- [SDR ASOA2015020212133](https://openairdocs.org/sdr/ASOA2015020212133), Jan 28, 2015: BULKHEAD. CRACKED. AFT PRESSURE BULKHEAD CRACKED AT UPPER END OF CARGO DOOR AFT TRACK AND LBL 27.5.
- [SDR ASOA2014110711616](https://openairdocs.org/sdr/ASOA2014110711616), Nov 6, 2014: LENS. MISSING. EXIT SIGN LENS IN GALLEY BY SERVICE DOOR MISSING. REPLACED THE EXIT SIGN LENS IAW AMM 33-51-13.
- [SDR ASOA2014091211215](https://openairdocs.org/sdr/ASOA2014091211215), Sep 10, 2014: LIGHT. INOPERATIVE. NR 5 EXTERIOR EMERGENCY LIGHT INOPERATIVE. R & R NR 5 EXTERIOR EMERGENCY LIGHT IAW AMM 33-51-21. OPS CHECKED GOOD.
- [SDR ASOA2013122009665](https://openairdocs.org/sdr/ASOA2013122009665), Dec 16, 2013: LENS. DETACHED. LENS DETACHED ON EMERGENCY LIGHT JUST AFT OF SERVICE DOOR. REPLACED LENS IAW CMM 33-51-21.
- [SDR ASOA2013091108985](https://openairdocs.org/sdr/ASOA2013091108985), Sep 7, 2013: LENS. MISSING. EMERGENCY LIGHT NEAR PAX BOARDING DOOR MISSING COVER. REPLACED MISSING EMERGENCY LIGHT COVER IAW AMM 33-51-19. OPS CHECKED GOOD. NO FURHTER DEFECTS NOTED.
- [SDR ASOA2013062103883](https://openairdocs.org/sdr/ASOA2013062103883), Jun 17, 2013: CONNECTOR. BROKEN. WIRING FOR GALLEY EMERGENCY EXIT LIGHT ON TRIM PANEL HAS BROKEN CONNECTOR (QUICK DISCONNECT) ON ACFT SIDE. REPLACED EMERGENCY EXIT LIGHT TRIM PANEL CONNECTOR IA
- [SDR ASOA2013062103882](https://openairdocs.org/sdr/ASOA2013062103882), Jun 12, 2013: DOOR. CORRODED. MID CAP DOOR ON SERVICE DOOR CORRODED OUT OF LIMITS. R & R MID CAP ON SERVICE DOOR.
- [SDR ASOA2013062103881](https://openairdocs.org/sdr/ASOA2013062103881), Jun 10, 2013: ATTACH ANGLE. CORRODED. ATTACH ANGLE BS 349, RT OTBD CORRODED. R & R ATTACH ANGLE IAW SRM 51-42-06 AND SRM 51-42-21.
- [SDR ASOA2013062103880](https://openairdocs.org/sdr/ASOA2013062103880), Jun 7, 2013: FLOORBEAM. CORRODED. FLOORBEAM FS 349 IS CORRODED. REPAIRED FLOORBEAM IAW REO 601R-53-21-2443. NDT PERFORMED. MAJOR REPAIR.
- [SDR ASOA2013062103879](https://openairdocs.org/sdr/ASOA2013062103879), Jun 4, 2013: SEAT TRACK. CORRODED. LEFT SEAT TRACK AT BS 559 - 559 + 80 CORRODED. INSTALLED SEAT TRACK IAW AMM 53-01-11, AMM 51-21-11, SRM 51-40-11, SRM 51-41-02, AMM 53-01-11 AND AMM 51-23-00.
- [SDR ASOA2013062103878](https://openairdocs.org/sdr/ASOA2013062103878), Jun 4, 2013: SEAT TRACK. CORRODED. LEFT SEAT TRACK AT FS 349 - 409 CORRODED. INSTALLED SEAT TRACK IAW AMM 53-01-11, SRM 51-21-11, SRM 51-41-02, SRM 51-40-11, SRM 51-23-00.
- [SDR ASOA2013062103877](https://openairdocs.org/sdr/ASOA2013062103877), Jun 4, 2013: SEAT TRACK. CORRODED. RT SEAT TRACK AT FS 349 -409 CORRODED. INSTALLED SEAT TRACK IAW AMM 53-01-11, SRM 51-41-02, SRM 51-40-11, SRM 51-21-11, SRM 51-23-00.
- [SDR ASOA2013062103876](https://openairdocs.org/sdr/ASOA2013062103876), Jun 4, 2013: SEAT TRACK. CORRODED. LEFT SEAT TRACK AT FS 409 + 96 - 559 CORRODED. R & R SEAT TRACK IAW AMM 53-01-11, CLEANED AREA IAW SRM 51-26-00.
- [SDR ASOA2013062103875](https://openairdocs.org/sdr/ASOA2013062103875), Jun 4, 2013: SEAT TRACK. CORRODED. RIGHT SIDE SEAT TRACK AT FS 409 + 96 - 559 CORRODED. R & R SEAT TRACK IAW AMM 53-01-11. CLEANED AREA IAW SRM 51-26-00.
- [SDR ASOA2013062103874](https://openairdocs.org/sdr/ASOA2013062103874), Jun 4, 2013: SEAT TRACK. CORRODED. LEFT FLOOR SEAT TRACK AT FS 409 - 409 + 96 CORRODED. BLENDED SEAT TRACK. FOUND OUT OF LIMITS IAW SRM 53-21-49 AND SRM 51-21-06. MATERIAL REMAINING 0.40" MINIMUM
- [SDR ASOA2013062103873](https://openairdocs.org/sdr/ASOA2013062103873), Jun 4, 2013: SEAT TRACK. CORRODED. RT SEAT TRACK AT FS 409 - 409 + 96 CORRODED. R & R SEAT TRACK IAW AMM 53-01-11. CLEANED AREA IAW SRM 51-26-00.
- [SDR ASOA2013062103872](https://openairdocs.org/sdr/ASOA2013062103872), Jun 3, 2013: SILL. CORRODED. SERVICE DOOR LOWER SILL HAS CORROSION ON FWD AND AFT SIDES. REMOVED FWD AND AFT CLEAT, REMOVED MID BRACKET, REMOVED KICK ANGLE AND MID CAP, DRILLED NEW KICKANGL
- [SDR ASOA2013062103871](https://openairdocs.org/sdr/ASOA2013062103871), Jun 3, 2013: ANGLE. CORRODED. PAX DOOR THRESHOLD ANGLE CORRODED. R & R THRESHOLD ANGLE IAW SRM 51-42-06, 51-42-26, 51-40-11, 51-42-21, 51-25-16.
- [SDR ASOA2013062103870](https://openairdocs.org/sdr/ASOA2013062103870), May 31, 2013: SEAT TRACK. CRACKED. LT SIDE SEAT TRACK FWD OF FS 409.0+128 CRACKED. CLEANED DAMAGE AREA, NO DEFECTS NOTED IAW SRM 53-21-49. DIMENSION AFTER REMOVAL OF DAMAGE: 19.31MM SIDE SEAT TRA
- [SDR ASOA2013062103869](https://openairdocs.org/sdr/ASOA2013062103869), May 30, 2013: SILL. CORRODED. RT SILL AFT OF SERVICE DOOR HAS CORROSION. R & R RT SILL AFT OF SERVICE DOOR IAW SRM 51-42-06 AND SRM 51-42-10. FOUND OUT OF LIMITS WITH A .010 MAT LOSS IAW SRM
- [SDR ASOA2013062103868](https://openairdocs.org/sdr/ASOA2013062103868), May 30, 2013: BRACKET. CRACKED. FS 280 L BRACKET CRACKED RT SIDE. R & R WITH SERVICEABLE PART IAW SRM 51-42-20, SRM 51-42-06, SRM 51-22-00 AND SRM 51-42-20, AMM 51-25-00, AMM 51-25-56.
- [SDR ASOA2013062103867](https://openairdocs.org/sdr/ASOA2013062103867), May 30, 2013: BRACKET. CRACKED. BS 280 BRACKET CRACKED LT SIDE. R & R WITH SERVICEABLE PART IAW SRM 51-42-20, SRM 51-42-06, SRM 51-22-00 AND SRM 51-42-20, AMM 51-25-00, AMM 51-25-56.
- [SDR ASOA2013062103866](https://openairdocs.org/sdr/ASOA2013062103866), May 23, 2013: BULB. BURNED OUT. DURING EMERGENCY LIGHTS OPS TEST, FOUND OVERHEAD EMERGENCY FLOODLIGHT INOPERATIVE AT BS 544. R & R CEILING EMERGENCY LIGHT BULB IAW AMM 33-51-16. OPS CHECKED GO
- [SDR ASOA2013030503101](https://openairdocs.org/sdr/ASOA2013030503101), Mar 2, 2013: ISOLATOR. BROKEN. FOUR ISOLATORS BROKEN ON AFT PRESSURE BULKHEAD. R & R DAMAGED ISOLATORS ON THE AFT PRESSURE BULKHEAD IAW SRM 51-42-13.

All 178: https://openairdocs.org/deregistered/N850AS-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 20140327011419I](https://openairdocs.org/incident/20140327011419I), Mar 27, 2014: Bombardier Inc CL-600-2B19 (N850AS), Cedar Rapids, IA, No damage. During number 1 engine start the APU temperature spiked then shut down. Ramp personnel reported that flames were coming from the APU exhaust, and smoke from…
- [Incident 20091203052609I](https://openairdocs.org/incident/20091203052609I), Dec 3, 2009: Bombardier CL-600-2B19 (N850AS), Atlanta, GA, No damage. Flaps failed in flight at ). Flaps were retracted after takeoff-thats when they failed at 0.[emergency declaired]performed ground maint. Test iaw fim 27-50-00…

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