# N870AS: 2001 Bombardier CL-600-2B19, registration cancelled 2023-07-30

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: July 30, 2023
- 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: 7530
- Year built: 2001
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: October 9, 2001
- Certificate issued: January 17, 2019
- Last registry action: July 7, 2023
- Mode S code: ABF667
- Owner when cancelled: [Skywest Airlines Inc](https://openairdocs.org/faa-owner/SKYWEST%20AIRLINES%20INC)
- Location: [Saint George, UT](https://openairdocs.org/faa-place/UT/Saint%20George)
- Owner type: Corporation
- Owner's area on the map: 37.0461° N, 113.5573° W: Placed by OpenAirDocs at the center of ZIP code 84790, within about 4 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N870AS
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=870AS
- Page: https://openairdocs.org/deregistered/N870AS-2023-07-30

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 (146, newest 50)

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

- [SDR SWIA2019102246555](https://openairdocs.org/sdr/SWIA2019102246555), Oct 21, 2019: WARNING MESSAGE. FALSE ACTIVATION. N2 VIB MESSAGE CAME UP ON TAKE OFF ROLL. ABORTED TAKE OFF 80 KNOTS. BTMS WITHIN LIMITS FLT # 5946 CLOSED. NO DAMAGE NOTED. PERFORMED HIGH POWER ENGINE RUNS AND 
- [SDR ASOA2019040864012](https://openairdocs.org/sdr/ASOA2019040864012), Apr 6, 2019: BATTERY PACK. DISCHARGED. IAH - FLIGHT 4306, THE CREW REPORTED EMERGENCY LIGHTS NOT WORKING. MAINTENANCE REMOVED AND REPLACED THE #3 EMERGENCY LIGHT BATTERY PACK, OPERATIONALLY TESTED WI
- [SDR ASOA2019040173021](https://openairdocs.org/sdr/ASOA2019040173021), Mar 27, 2019: SEAL. FAULTY. THE CREW REPORTED AT 35,000 FEET LOST ALL PRESSURIZATION. MAINTENANCE INSPECTED AND REPLACED SERVICE DOOR SEAL. OPERATIONAL CHECK WERE GOOD.
- [SDR ASOA2016030514551](https://openairdocs.org/sdr/ASOA2016030514551), Mar 5, 2016: BULB. MISSING. EMERGENCY RT COVER AND LIGHT BULB MISSING ON NR 1 GALLEY WALL, ENTRANCE LT SIDE. REPLACED EMERGENCY LIGHT ASSY ON IAW AMM 33-5119, GOOD. OK FOR SERVICE.
- [SDR ASOA2016012614402](https://openairdocs.org/sdr/ASOA2016012614402), Jan 26, 2016: SKIN. DAMAGED. DURING FLIGHT CONTROL TEST AFTER PUSHBACK, THE RT RUDDER PEDDAL WILL NOT REACH FULL DEFLECTION. DAMAGE TO RUDDAR, CAUSING OBSTRUCTION, SHEETMETAL REMOVED IAW RE
- [SDR ASOA2015081013475](https://openairdocs.org/sdr/ASOA2015081013475), Aug 10, 2015: SKIN. DAMAGED. FUSELAGE SKIN DAMAGE AROUND LOW PRESSURE GROUND CONNECTION DOOR. THE REPAIR HAS BEEN DETERMINED AND CLASSIFIED TO BE MAJOR REAPAIR. RECEIVED AND COMPLIED IAW EA
- [SDR ASOA2015042912729](https://openairdocs.org/sdr/ASOA2015042912729), Apr 25, 2015: ANGLE. CRACKED. CARGO DOOR CROSSMEMBER ANGLE CRACKED AT FS 621.00 BULKHEAD. R & R ANGLE AT FS 621.00 CARGO DOOR CROSSMEMBER WITH NEW SERVICEABLE PART IAW SRM 51-42-21.
- [SDR ASOA2015050412751](https://openairdocs.org/sdr/ASOA2015050412751), Apr 15, 2015: SKIN. CRACKED. FOUND RT LOWER WING PLANK FUEL ACCESS HOLE 640FB HAS MULTIPLE INDICATIONS NOTED ON AFT OTBD SIDE APPROXIMATELY 1.5" LONG, 50 PERCENT FSH. FAILED NDT INSPECTION.
- [SDR ASOA2015050412750](https://openairdocs.org/sdr/ASOA2015050412750), Apr 13, 2015: FRAME. CORRODED. CORROSION ON FRAME AT FS 605.00, STR 27. REMOVED CORROSION ON FS 605. FRAME BETWEEN STR 25L AND 25R IAW SRM 51-21-06. FS 605.00 FRAME FOPUND TO BE OUT OF LIMITS
- [SDR ASOA2015050412749](https://openairdocs.org/sdr/ASOA2015050412749), Apr 13, 2015: SKIN. CORRODED. WING PLANK AT 640BB HAS CORROSION IN SEVERAL AREAS. COMPLIED WITH EC/TC EO 600-57-81. C/W IAW REO 601R-57-21-030, REV L.
- [SDR ASOA2015050412748](https://openairdocs.org/sdr/ASOA2015050412748), Apr 13, 2015: SKIN. CORRODED. WING PLANK AT 540BB HAS CORROSION AT INBD SIDE IN NON-CRITICAL AREA. COMPLIED WITH EC/TC EO 600-57-81. C/W IAW REO 601R-57-21-030, REV L.
- [SDR ASOA2015050412747](https://openairdocs.org/sdr/ASOA2015050412747), Apr 13, 2015: FLOORBEAM. CRACKED. FS 621, LT FLOOR SUPPORT ANGLE CRACKED AT LBL 36. REO:601R-53-61-5473, REV HAS BEEN ACCOMPLISHED AND ALL STEPS HAVE BEEN DOCUMENTED AND SIGNED FOR ON A NON-ROUT
- [SDR ASOA2015042912728](https://openairdocs.org/sdr/ASOA2015042912728), Apr 13, 2015: DOOR SILL. CORRODED. CORROSION ON CARGO DOOR SILL FROM FS 621.00 TO FS 574.00. 2 AREAS 0.003 IN. OUT OF LIMITS AT FS 589.00+13 AND FS 605.00+6.25 ENGINEERING REQUIREDD. DAMAGE WAS B
- [SDR ASOA2015042912727](https://openairdocs.org/sdr/ASOA2015042912727), Apr 13, 2015: FLOORBEAM. CORRODED. CORROSION ON FLOORBEAM AT FS 589.00 BETWEEN LBL 18 AND LBL 27. FOUND TO BE OUT OF LIMITS IAW TR 53-27, REQUIRES REPLACEMENT. REMOVED CORRODED FLOORBEAM CAP AT F
- [SDR ASOA2015042912726](https://openairdocs.org/sdr/ASOA2015042912726), Apr 12, 2015: SEAT TRACK. CORRODED. RT SIDE SEAT RAILS FROM FS 454 - FS 559+54 HAS SEVERAL AREAS OF CORROSION AROUND THE LOWER EDGE OF THE COIN HOLES; WORST IS AT FS 474, MARKED WITH ORANGE TAPE. 
- [SDR ASOA2015050412746](https://openairdocs.org/sdr/ASOA2015050412746), Apr 10, 2015: RETAINER. CORRODED. MAIN AVI BAY DOOR SEAL RETAINER IS CORRODED. REMOVED SEAL RETAINER IAW SRM 51-42-06. REPLACED SEAL RETAINERS IAW SRM 51-42-06. PERFORMED OPS TEST OF THE MAIN AV
- [SDR ASOA2015050412745](https://openairdocs.org/sdr/ASOA2015050412745), Apr 7, 2015: FLOOR SUPPORT. CORRODED. CORROSION ON FLOOR SILL AFT OF PAX DOOR AT FS 349.00. REPAIRED FLOOR SILL BETWEEN FS 280 TO FS 409+128 IAW REO 601R-53-00-530, REV A.
- [SDR ASOA2015042912725](https://openairdocs.org/sdr/ASOA2015042912725), Apr 7, 2015: FLOORBEAM. CORRODED. CORROSION FOUND ON AVIONICS BAY FLOORBOARD SUPPORT ANGLE AT FS 333.00. REMOVED FLOORBOARD SUPPORT ANGLE IAW SRM 51-42-06. LOCATED, DRILLED AND INSTALLED FS 333.
- [SDR ASOA2015042912724](https://openairdocs.org/sdr/ASOA2015042912724), Apr 7, 2015: DOOR SILL. CORRODED. SERVICE DOOR SILL, LOWER, ANGLE HAS CORROSION IN SEVERAL AREAS. FOUND CORROSION TO BE OUT OF LIMITS. REMOVED LOWER SILL IAW SRM 51-42-21 AND 51-42-06. LOCATED A
- [SDR ASOA2015042912723](https://openairdocs.org/sdr/ASOA2015042912723), Apr 7, 2015: DOOR SILL. CORRODED. CORROSION ON SERVICE DOOR SILL AT FS 319.70 AND FS 349.00. BLENDED AREA REMOVING CORROSION IAW REO 601R-53-00-530. REPAIRED FLOOR SILL BETWEEN FS 280 TO FS 409+
- [SDR ASOA2015042912722](https://openairdocs.org/sdr/ASOA2015042912722), Apr 7, 2015: FLOOR SUPPORT. CORRODED. CORROSION ON UPPER SURFACE OF FLOOR SUPPORT AROUND 3 FASTENER HOLES BETWEEN FS 310.00 AND FS 349.00 LBL 27. COMPLIED WITH EC/TC REO 601R-53-00-005.
- [SDR ASOA2015042912721](https://openairdocs.org/sdr/ASOA2015042912721), Apr 7, 2015: FLOOR SUPPORT. CORRODED. CORROSION ON UPPER SURFACE OF RT FLOOR SILL STRUCTURE FROM FS 409.00+128 TO FS 559.00. COMPLIED WITH EC/TC REO 601R-53-41-666 01 AND REO 601R-53-41-666, REV C, 
- [SDR ASOA2015042912720](https://openairdocs.org/sdr/ASOA2015042912720), Apr 7, 2015: FRAME. CORRODED. CORROSION ON FRAME AT FS 364.00 BETWEEN LBL 24 & RBL 24. COMPLIED WITH EA 32-2015-138.
- [SDR ASOA2015042912719](https://openairdocs.org/sdr/ASOA2015042912719), Apr 7, 2015: FRAME. CORRODED. CORROSION ON FRAME AT FS 330.00 BETWEEN LBL 24 & RBL 24. FOUND CORROSION TO BE LOCATED ON FRAME SECTOR AT FS 333.00 NOT FS 330.00. CORROSION FOUND OUT OF LIMITS
- [SDR ASOA2015042912718](https://openairdocs.org/sdr/ASOA2015042912718), Apr 7, 2015: FRAME. CORRODED. CORROSION ON FRAME AT FS 319.70 BETWEEN LBL 24 & RBL 24. FOUND CORROSION ON FS 319.70 FRAME OUT OF LIMITS IAW SRM 53-00-00. REMOVED FS 319.70 LOWER FRAME SECTOR
- [SDR ASOA2015042912717](https://openairdocs.org/sdr/ASOA2015042912717), Apr 7, 2015: FRAME. CORRODED. CORROSION ON FRAME AT FS 310.00 BETWEEN LBL 24 & RBL 24. FOUND CORROSION ON FRAME TO BE OUT OF LIMITS IAW SRM 53-00-00. COMPLIED WITH REO 601R-53-21-2612 P1.
- [SDR ASOA2015042912716](https://openairdocs.org/sdr/ASOA2015042912716), Apr 7, 2015: FLOORBEAM. CRACKED. FS 280.00 FLOORBEAM ANGLE AT RBL 9 OTBD & RBL 27 INBD ARE CRACKED. FABRICATED NEW FS 280, RBL 9 CLIP FROM S6144-13, PERFORMED ANGLE 2024T42 .050" IAW REO 601R-5
- [SDR ASOA2015042912715](https://openairdocs.org/sdr/ASOA2015042912715), Apr 7, 2015: FLOORBEAM. CRACKED. FS 280.00 FLOORBEAM ANGLE AT LBL 9 INBD & OTBD ARE CRACKED. FABRICATED NEW FS 280, LBL 9 INBD AND OTBD CLIPS FROM S6144-13, PREFORMED ANGLE 2024T42 .050" IAW RE
- [SDR ASOA2014041010306](https://openairdocs.org/sdr/ASOA2014041010306), Apr 6, 2014: LAMP. BURNED OUT. EMERGENCY LIGHT LAMP INOPERATIVE. REPLACED LAMP, OPS CHECKED GOOD, IAW AMM 33-51-00.
- [SDR ASOA2013121909663](https://openairdocs.org/sdr/ASOA2013121909663), Nov 28, 2013: PRIORITY VALVE. FAILED. GEAR UP DISAGREE WARNING AFTER DEPARTURE. LT AND RT GEAR WERE IN DISAGREEMENT (RED). COMPLIED WITH QRH. MANUAL GEAR HANDLE WAS PULLED IAW QRH. EMERGENCY DECLARE
- [SDR ASOA2013100109138](https://openairdocs.org/sdr/ASOA2013100109138), Sep 27, 2013: LAMP. BURNED OUT. CENTER CEILING EMERGENCY LIGHT INOPERATIVE. REPLACED LAMP, OP'S CHECKED GOOD IAW AMM 33-51-16.
- [SDR ASOA2013053003737](https://openairdocs.org/sdr/ASOA2013053003737), May 10, 2013: SKIN. CRACKED. RIGHT LOWER WING SKIN IS CRACKED .25" LONG AT WS 148.09 - REINFORCING ANGLE IN T/E ABOVE SKIN IS CRACKED .75" LONG. C/W ECTC REO 601R-57-21-130 01 AND REO 601R-
- [SDR ASOA2013053003736](https://openairdocs.org/sdr/ASOA2013053003736), May 8, 2013: ANGLE. CRACKED. FS 621, BULKHEAD AFT SIDE FS 621-625 ANGLES CRACKED. REMOVED CRACKED LT & RT FS 621-625 ANGLES AND INSTALLED SERVICEABLE ANGLES IAW SRM 51-40-11 AND SRM 51-42-0
- [SDR ASOA2013053003735](https://openairdocs.org/sdr/ASOA2013053003735), May 8, 2013: ATTACH BRACKET. CRACKED. PAX DOOR UPPER SILL ATTACHMENT BRACKET CRACKED AT FS 280. REMOVED CRACKED BRACKET AT FS 280, STR 3 IAW SRM 51-42-06. LOCATED & DRILLED NEW SERVICEABLE ANGLE, PN
- [SDR ASOA2013053003734](https://openairdocs.org/sdr/ASOA2013053003734), May 7, 2013: BULKHEAD. CRACKED. FS 621, BULKHEAD FAILS NDT WITH AN INDICATION FSH AT LBL 27.50, WL 130). REPAIRED IAW REO 601R-53-61-1541, REV D.
- [SDR ASOA2013053003733](https://openairdocs.org/sdr/ASOA2013053003733), May 3, 2013: CARGO TRACK. CORRODED. CARGO TRACKS CORRODED AROUND FASTENER HOLES AT LBL 27 AND LBL 9. R & R CARGO TRACKS IAW AMM 20-21-00-910-801.
- [SDR ASOA2013053003732](https://openairdocs.org/sdr/ASOA2013053003732), May 3, 2013: ISOLATOR. CRACKED. PRESSURE BULKHEAD FWD FACE HAS FIVE CRACKED ISOLATORS. R & R ISOLATORS ON FS 621 BULKHEAD IAW SRM 51-42-06.
- [SDR ASOA2013053003731](https://openairdocs.org/sdr/ASOA2013053003731), May 3, 2013: FLOOR SUPPORT. CORRODED. LEFT CABIN FLOOR SUPPORT IS CORRODED AT FOUR NUTPLATE LOCATIONS. DAMAGE IS APPROX BETWEEN FS 409+128 AND FS 559. REPAIRED IAW TASK 51-26-0-110-801, SRM 51-21-11
- [SDR ASOA2013053003730](https://openairdocs.org/sdr/ASOA2013053003730), Apr 30, 2013: SKIN. CRACKED. LEFT LOWER WING SKIN CRACKED .25" LONG AT WS 148.019. C/W EC/TC REO 601R-57-21-130 AND GENERIC REO 601R-57-21-130, REV J. C/W EC/TC REO 601R-57-21-131 AND REO 6
- [SDR ASOA2013053003729](https://openairdocs.org/sdr/ASOA2013053003729), Apr 30, 2013: DRAG ANGLE. CRACKED. PAX DOOR AFT DRAG ANGLE CRACKED. REPAIRED IAW SRM 51-42-06 AND 51-42-10 AND REO 601R-52-11-513, REV A.
- [SDR ASOA2012100202318](https://openairdocs.org/sdr/ASOA2012100202318), Sep 28, 2012: CONTROL LEVER. FAILED. ON SELECTING FLAPS FROM 8 TO 20 DEGREES, FLAPS FAIL CAUTION MESSAGE DISPLAYED. VERIFIED FLAPS STUCK AT 8 DEGREES ON EICAS FLIGHT CONTROL PAGE. COMPLIED WITH QRH
- [SDR ASOA2012091702224](https://openairdocs.org/sdr/ASOA2012091702224), Sep 13, 2012: MOTOR. MALFUNCTIONED. PASSENGER DOOR DOES NOT OPEN FULLY. R & R PASSENGER DOOR POWER ASSIST MOTOR IAW AMM 52-11-08. PERFORMED OPS CHECKS OF THE PWR DOOR ASSIST IAW AMM 52-11-08-720-8
- [SDR ASOA201201454](https://openairdocs.org/sdr/ASOA201201454), Apr 28, 2012: DETECTION SYS. MALFUNCTIONED. DURING FIRE WARNING TEST, DID NOT GET LEFT ENGINE FIRE LOOP-B WARNING MESSAGE AND LEFT FIRE PUSH SWITCH DOES NOT ILLUMINATE. INSPECTED LT ENGINE FIRE LOOPS, NO 
- [SDR ASOA201201315](https://openairdocs.org/sdr/ASOA201201315), Apr 20, 2012: PIN. MISSING. SERVICE DOOR RELEASE HANDLE NOT FUNTIONAL. PIN MISSING. REPLACE MISSING PIN ON SERVICE DOOR RELEASE HANDLE. OPS CHECKED GOOD IAW AMM 52-41-02. (SDR CLOSED)
- [SDR ASOA201100887](https://openairdocs.org/sdr/ASOA201100887), May 4, 2011: ISOLATOR. BROKEN. APPROX RBL 36, WL 92 ON AFT BULKHEAD, ISOLATER BROKEN RT SIDE. R & R RT OTBD ISOLATOR AT WATER LINE 92 ON FS 621 BULKHEAD IAW SRM 51-42-13. THIS REPAIR REQUIRES
- [SDR ASOA201100878](https://openairdocs.org/sdr/ASOA201100878), May 4, 2011: CONNECTOR. MALFUNCTIONED. FWD LEFT EMERGENCY LIGHTS ARE INOP ON TEST. FOUND CONNECTORS J11LY AND P10LY SWAPPED WITH CONNECTORS J20LY AND P21LY. INSTALLED TO ORIGINAL CONFIG AND RESEATED 
- [SDR ASOA201100783](https://openairdocs.org/sdr/ASOA201100783), Apr 15, 2011: FLOORBEAM. CRACKED. FS 280 AFT FLOOR ANGLE IS CRACKED OTBD OF RBL9 AND OTBD LBL9, REPAIRED IAW REO 601R-53-11-926 IAW REO 601R-53-11-926, REV B.
- [SDR ASOA201100777](https://openairdocs.org/sdr/ASOA201100777), Apr 15, 2011: POST. CRACKED. INDICATION NOTED AT FS 409+128 BL 0.00 WK 69.0 RADIUS OF RT CHANNEL APPROX .10" LENGTH, 55 PERCENT. REMOVED POST ASSY IAW SRM 51-42-06, 51-42-21. INSTALLED NEW 
- [SDR ASOA201100776](https://openairdocs.org/sdr/ASOA201100776), Apr 15, 2011: FLOOR SUPPORT. CORRODED. FLOOR SUPPORT CORRODED FS 349 AT SERVICE DOOR SURROUND LOWER AFT FRAME BRACKET. REMOVED CORROSION, FOUND WITHIN LIMITS IAW SRM 53-21-15 AND SRM 53-00-00.
- [SDR ASOA201100775](https://openairdocs.org/sdr/ASOA201100775), Apr 15, 2011: FLOOR SUPPORT. CORRODED. FS 280, FWD FLOOR SUPPORT ANGLE IS CORRODED. R & R FWD FLOOR SUPPORT ANGLE WITH A NEW SERVICEABLE ANGLE IAW SRM 51-42-06. REPAIR CLASSIFIED AS A MINOR.

All 146: https://openairdocs.org/deregistered/N870AS-2023-07-30/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 20130822015649I](https://openairdocs.org/incident/20130822015649I), Aug 22, 2013: Bombardier Inc CL-600-2B19 (N870AS), Dallas, TX, Minor damage. Pilot aborted takeoff departing atlanta for co-pilots seat malfunction, returned to gate to repair seat, took-off landed at Love field in Dallas, upon landing…

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