# N869AS: 2001 Bombardier CL-600-2B19, registration cancelled 2023-04-18

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: April 18, 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: 7479
- Year built: 2001
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: June 10, 2001
- Certificate issued: October 2, 2017
- Last registry action: March 24, 2023
- Mode S code: ABF057
- Owner when cancelled: [Skywest Airlines Inc](https://openairdocs.org/faa-owner/SKYWEST%20AIRLINES%20INC)
- Location: [St George, UT](https://openairdocs.org/faa-place/UT/St%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/N869AS
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=869AS
- Page: https://openairdocs.org/deregistered/N869AS-2023-04-18

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 (126, newest 50)

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

- [SDR SWIA2020072151362](https://openairdocs.org/sdr/SWIA2020072151362), Jun 16, 2020: STRINGER. CORRODED. STRINGER 27 HAS MULTIPLE RIVETS BETWEEN BS 319 AND 333 WAS CORRODED. REPLACED SIX RIVETS ON THE STRINGER IAW SRM, PRESSURE LEAK CHECKED GOOD.
- [SDR SWIA2020072151357](https://openairdocs.org/sdr/SWIA2020072151357), Jun 16, 2020: FLOOR SUPPORT. CORRODED. RIGHT UPPER PRESSURE FLOOR SUPPORT FROM BS 409+128 THRU 559 HAD MULTABLE AREAS OF PITTING CORROSION. THE CORROSION ON RH UPPER PRESSURE FLOOR SUPPORT HAS BEEN R
- [SDR SWIA2020072151356](https://openairdocs.org/sdr/SWIA2020072151356), Jun 16, 2020: FLOOR SUPPORT. CORRODED. LEFT UPPER PRESSURE FLOOR SUPPORT FROM BS 409+128 THRU BS 559 HAD MULTABLE AREAS OF PITTING CORROSION. REMOVED CORROSION ON THE FLOOR SUPPORT IAW REO. FOUND TO 
- [SDR SWIA2020072151355](https://openairdocs.org/sdr/SWIA2020072151355), Jun 16, 2020: STRAP. CORRODED. LEFT BS 559 LBL 27 - RBL 40 STRAP WAS CORRODED. REMOVED AND INSTALLED A NEW STRAP IAW SRM AND DWG.
- [SDR SWIA2020072151354](https://openairdocs.org/sdr/SWIA2020072151354), Jun 16, 2020: STRAP. CORRODED. BS 559, RBL 27 - RBL 40 STRAP WAS CORRODED. REMOVED AND INSTALLED NEW STRAP IAW SRM AND DWG.
- [SDR SWIA2020072151353](https://openairdocs.org/sdr/SWIA2020072151353), Jun 16, 2020: STRINGER. CORRODED. STRINGER 27 BETWEEN BS 333 AND 349 HAD CORROSION AND WAS CHAFED. REPLACED THE STRINGER IAW SRM AND DWG, LEAK CHECKED GOOD.
- [SDR SWIA2020072151352](https://openairdocs.org/sdr/SWIA2020072151352), Jun 15, 2020: FRAME. CORRODED. * THE FRAME AT FS319.00 BETWEEN STRINGER 26R AND 25L HAD CORROSION. REMOVED CORROSION IAW SRM. CORROSION DAMAGE EXTENDS TO MULITIPLE COSSECTIONS AND TOTALS MORE
- [SDR SWIA2020072151361](https://openairdocs.org/sdr/SWIA2020072151361), Jun 14, 2020: ANCHOR FITTING. CORRODED. PAX DOOR AFT ANCHOR FITTING HAD CORRODED HARDWARE. REPLACED THE AFT PASSENGER DOOR COUNTERBALANCE ANCHOR FITTING IAW AMM. ADJUISTMENTS AND OPS CHECKS GOOD AT TH
- [SDR SWIA2020072151360](https://openairdocs.org/sdr/SWIA2020072151360), Jun 14, 2020: ANCHOR FITTING. CORRODED. PAX DOOR FWD ANCHOR FITTING HAD CORRODED HARDWARE. REMOVED CORRODED HARDWARE AND RELPACED WITH 2 NEW BOLTS AND NUTS ON THE PAX DOOR FWD ANCHOR FITTING IAW SRM.
- [SDR SWIA2020072151351](https://openairdocs.org/sdr/SWIA2020072151351), Jun 13, 2020: STIFFENER. CRACKED. *BATT RIB CAP IN R/H WHEEL WELL AT WS 48 IS CRACKED. REMOVED CRACKED ANGLE AND INSTALLED A NEW BATT RIB ANGLE. IAW DWG AND SRM.
- [SDR SWIA2020072151350](https://openairdocs.org/sdr/SWIA2020072151350), Jun 13, 2020: CAP. CRACKED. *BATT RIB CAP IN L/H WHEEL WELL AT WS 48 IS CRACKED. REPLACED LH BATT RIB CAP ANGLE IAW SRM AND DWG.
- [SDR SWIA2020072151349](https://openairdocs.org/sdr/SWIA2020072151349), Jun 13, 2020: ATTACH ANGLE. CRACKED. ATTACH ANGLE ON THE OTBD END OF INTECOSTAL, LOCATED ON THE AFT SIDE OF THE BS 621 BULKHEAD, STRINGER 16R WAS CRACKED. REMOVED AND REPLACED THE ATTACH ANGLE IAW 
- [SDR SWIA2020072151348](https://openairdocs.org/sdr/SWIA2020072151348), Jun 13, 2020: ATTACH ANGLE. CRACKED. ATTACH ANGLE ON OTBD END OF INTECOSTAL, LOCATED ON THE AFT SIDE OF THE BS 621 BULKHEAD AT STRINGER 13R WAS CRACKED. REMOVED AND REPLACED THE ATTACH ANGLE IAW DW
- [SDR SWIA2020072151347](https://openairdocs.org/sdr/SWIA2020072151347), Jun 13, 2020: ATTACH ANGLE. CRACKED. ATTACH ANGLE ON THE OTBD END OF INTECOSTAL, LOCATED ON THE AFT SIDE OF THE BS 621 BULKHEAD AT STRINGER 12R WAS CRACKED. REMOVED AND REPLACED THE ATTACH ANGLE IA
- [SDR SWIA2020072151346](https://openairdocs.org/sdr/SWIA2020072151346), Jun 13, 2020: ATTACH ANGLE. CRACKED. ATTACH ANGLE ON THE OTBD END OF INTECOSTAL, LOCATED ON THE AFT SIDE OF THE BS 621 BULKHEAD AT STRINGER 16L WAS CRACKED. INSTALLED A NEW ATTACH ANGLE IAW SRM AND
- [SDR SWIA2020072151345](https://openairdocs.org/sdr/SWIA2020072151345), Jun 13, 2020: ATTACH ANGLE. CRACKED. ATTACH ANGLE ON THE OTBD END OF INTECOSTAL, LOCATED ON THE AFT SIDE OF THE BS 621 BULKHEAD AT STRINGER 13L WAS CRACKED. INSTALLED A NEW ATTACH ANGLE IAW SRM AND
- [SDR SWIA2020072151344](https://openairdocs.org/sdr/SWIA2020072151344), Jun 13, 2020: DOUBLER. CRACKED. RIGHT WING AUX SPAR LOWER FLANG DOUBLER WAS CRACKED AT RWS 148. REPAIRED THE RIGHT WING AUX SPAR LOWER FLANG DOUBLER IAW REO. LEAK CHECKED GOOD.
- [SDR SWIA2020072151358](https://openairdocs.org/sdr/SWIA2020072151358), Jun 8, 2020: FLOOR PANEL. CRACKED. COCKPIT FLOOR PANEL 221ALF CRACKED ON AFT EDGE. INSTALLED A NEW FLOOR PANEL ON MX 21061583.
- [SDR SWIA2020072151343](https://openairdocs.org/sdr/SWIA2020072151343), Jun 7, 2020: SKIN. DENTED. RIGHT OTBD FLAP LOWER SKIN AFT SECTION BETWEEN STATION 209.39-236.02 HAD TWO SHALLOW DENTS. REPAIRED THE DENTS IAW REO AND SRM.
- [SDR SWIA2020072151342](https://openairdocs.org/sdr/SWIA2020072151342), Jun 7, 2020: RECEPTACLE. GOUGED. CARGO DOOR HANDLE RECEPTACLE HAD TWO GOUGES. BLENDED OUT THE GOUGES ON CARGO DOOR EXTERNAL HANDLE HOUSING IAW STEP 1 OF REO. BLEND LOCATION 1 IS ON THE LOWER FW
- [SDR SWIA2020072151341](https://openairdocs.org/sdr/SWIA2020072151341), Jun 7, 2020: SKIN. CHAFED. CARGO DOOR EXTERIOR, ALONG TOP UPPER DOOR AFT WAS CHAFED. REMOVED EXISTING DAMAGED AND REPAIR DOUBLER FROM THE CARGO DOOR IAW SRM. INSTALLED NEW REPAIR DOUBLER 
- [SDR SWIA201945615](https://openairdocs.org/sdr/SWIA201945615), Mar 8, 2019: WARNING SYSTEM. FALSE ACTIVATION. RECEIVED A GEAR DISAGREE WARNING AND NOSE DOOR WARNING DURING GEAR EXTENSION ON APPROACH. BOTH WARNINGS DISAPPEARED AND GEAR DISPLAYED DOWN AND 3 GREEN WHEN GEA
- [SDR SWIA2018091345077](https://openairdocs.org/sdr/SWIA2018091345077), Aug 19, 2018: SKIN. CHAFED. RT EXTERNAL FUSELAGE SKIN FOUND CHAFED FROM APPROX FS 700.00 TO FS 736.00 AND FROM STR 11R TO STR 10R. (C-CHECK) RO: 09/12/2018. REPAIRED CHAFED SKIN AT AFT END
- [SDR SWIA2018091345076](https://openairdocs.org/sdr/SWIA2018091345076), Aug 8, 2018: FRAME. CRACKED. MULTIPLE CRACKS IN THE ATTACHMENT FLANGE OF FS718 BTWN STR 11R-12R. (C-CHECK) RO: 09/12/2018. REPLACED FRAME SECTION AT FS718 WITH ATTACHMENT FLANGE BTWN STR 11
- [SDR SWIA2018091345069](https://openairdocs.org/sdr/SWIA2018091345069), Aug 2, 2018: BULKHEAD. CRACKED. FS 280 BLKHD WEB REQUIRES DUE TO CRACKS FOUND AT LBL9 AND RBL9. (C-CHECK) RO: 09/12/2018. COMPLIED WITH REPAIR OF THE FS280 BLKHD IAW REO.
- [SDR SWIA2018091345075](https://openairdocs.org/sdr/SWIA2018091345075), Jul 31, 2018: FRAME. CORRODED. FS 605.00 FRAME HAS CORROSION (BOTH SIDES) BETWEEN APPROX STR 21L TO STR 27. (C-CHECK) RO: 09/12/2018. REMOVED AND REPLACED FS605.00 FRAME IAW SRM. ALL CHECKS G
- [SDR SWIA2018091345074](https://openairdocs.org/sdr/SWIA2018091345074), Jul 31, 2018: INTERCOSTAL. CORRODED. THE RT INTERCOSTAL FWD OF THE AVIONICS BAY DOOR CUTOUT, BETWEEN FS 349 AND FS 364 ADJACENT TO STRINGER 27, HAS MULTIPLE SPOTS OF CORROSION. (C-CHECK) RO: 09/12/
- [SDR SWIA2018091345073](https://openairdocs.org/sdr/SWIA2018091345073), Jul 31, 2018: INTERCOSTAL. CORRODED. THE LT INTERCOSTAL FWD OF THE AVIONICS BAY DOOR CUTOUT, BETWEEN FS 349 AND FS 364 ADJACENT TO STRINGER 27, HAS MULTIPLE SPOTS OF CORROSION. (C-CHECK) RO: 09/12/
- [SDR SWIA2018091345072](https://openairdocs.org/sdr/SWIA2018091345072), Jul 31, 2018: FRAME. CORRODED. FS 349 FRAME HAS MULTIPLE SPOTS OF CORROSION ALONG ITS FWD VERTICAL WEB FACE AND AFT WEB FACE AND LOWER FLANGE BETWEEN STRINGER 26L AND STRINGER 26R. (C-CHECK) 
- [SDR SWIA2018091345071](https://openairdocs.org/sdr/SWIA2018091345071), Jul 31, 2018: FRAME. CORRODED. FS 364 FRAME HAS MULTIPLE SPOTS OF CORROSION ALONG ITS FWD FACE LOWER FLANGE FROM THE OUTBOARD SIDE OF STRINGER 26L TO STRINGER 26R. (C-CHECK) RO: 09/12/2018. R
- [SDR SWIA2018091345068](https://openairdocs.org/sdr/SWIA2018091345068), Jul 29, 2018: STRUCTURE. DENTED. SEVERAL DENTS ON RIGHT SIDE OF FUSELAGE BELOW WL 73.50 FS542.00 TO FS581.00. (C-CHECK) RO: 09/12/2018. C/W REPAIR OF SEVERAL DENTS ON RIGHT SIDE OF FUSELAGE BEL
- [SDR SWIA2018091345067](https://openairdocs.org/sdr/SWIA2018091345067), Jul 29, 2018: STRUCTURE. DENTED. PROTRUDING DENT ON RIGHT SIDE OF FUSELAGE BELOW WL 73.50 FS658.00. (C-CHECK) RO: 09/12/2018. REWORKED DENT LOCATED ON FUSELAGE BELOW WL 73.50 AT FS658.00, IAW R
- [SDR SWIA2018091345070](https://openairdocs.org/sdr/SWIA2018091345070), Jul 26, 2018: SKIN. DENTED. MULTIPLE DENTS ON THE LT WING LEADING EDGE AT APPROX WS 137.00. (C-CHECK) RO: 09/12/2018. REPAIRED 4 EA DENTS ON LT WING CENTER L/E SKIN IAW REO.
- [SDR SWIA201743385](https://openairdocs.org/sdr/SWIA201743385), Jun 14, 2017: BRACKET. DAMAGED. STEERING INOPERATIVE CAUTION INFLIGHT. COMPLIED WITH QRH AND RETURN TO FIELD. DECLARED EMERGENCY. REMOVED AND REPLACED THE PROXIMITY SENSOR BRACKET IAW AMM. OPS
- [SDR SWIA201642603](https://openairdocs.org/sdr/SWIA201642603), Sep 26, 2016: BRACKET. CRACKED. AIRCRAFT RETURNED TO THE FIELD WITH A NOSE DOOR OPEN, GEAR DISAGREE MESSAGE. DID NOT DECLARE AN EMERGENCY. R & R THE BENT AND CRACKED PROXIMITY SWITCH SENSOR BR
- [SDR SWIA201641719](https://openairdocs.org/sdr/SWIA201641719), Jan 4, 2016: CONNECTOR. UNSECURE. IN FLIGHT GEAR DISAGREE. SECURED CONNECTOR FOR NOSE GEAR DOORS SEQUENCING VALVE AND ADJUSTED WOW SENSOR, SYSTEMS OPERATE NORMAL.
- [SDR SWIA201540890](https://openairdocs.org/sdr/SWIA201540890), Mar 11, 2015: UNKNOWN. ODOR. BURN SMELL INFLIGHT. INSPECTED AND OPERATED BOTH PACKS USING APU AND ENGINE BLEED FOR SEVERAL MINUTES. DID NOT NOTICE A BURN SMELL. ALSO INSPECTED ALL CABIN LIG
- [SDR SWIA201438834](https://openairdocs.org/sdr/SWIA201438834), Jul 19, 2014: WIRE. BROKEN. GALLEY EMERGENCY EXIT SIGN HAS TWO BROKEN WIRES. REPAIRED WIRES IAW ESPM.
- [SDR SWIA201438833](https://openairdocs.org/sdr/SWIA201438833), Jul 19, 2014: WIRE. BROKEN. FLOOR EXIT SIGN HAS A BROKEN WIRE. REPAIRED THE WIRES IAW ESPM.
- [SDR SWIA201438835](https://openairdocs.org/sdr/SWIA201438835), Jul 11, 2014: WIRE. LOOSE. EXIT SIGN ON LOWER CORNER OF WARDROBE HAS A LOOSE WIRE. REPAIRED WIRE IAW ESPM AND AMM.
- [SDR SWIA201438836](https://openairdocs.org/sdr/SWIA201438836), Jul 9, 2014: FRAME. CORRODED. BS 333 FRAME CORRODED BETWEEN STRINGERS 26L-26R ON FWD AND AFT SIDES. REPLACED FRAME IAW SRM.
- [SDR SWIA201438837](https://openairdocs.org/sdr/SWIA201438837), Jul 8, 2014: INTERCOSTAL. CRACKED. RT SIDE, BS 484 OUTSIDE FUSELAGE INTERCOSTAL HAS SUSPECT CRACK AT UPPER RADIUS. C-CHECK, REPLACED INTERCOSTAL IAW SRM.
- [SDR SWIA201438844](https://openairdocs.org/sdr/SWIA201438844), Jul 7, 2014: ATTACH FITTING. CHAFED. LEFT MLG DOOR STRUT ATTACH FITTING CHAFED, REPAIRED LT MLG DOOR STRUT ATTACH FITTING IAW REO.
- [SDR SWIA201438843](https://openairdocs.org/sdr/SWIA201438843), Jul 7, 2014: STRUT. CHAFED. RIGHT MLG DOOR STRUT CHAFED, C-CHECK. REPAIRED RT MLG DOOR STRUT IAW REO.
- [SDR SWIA201438842](https://openairdocs.org/sdr/SWIA201438842), Jul 7, 2014: BELLCRANK. CHAFED. RIGHT MLG DOOR BELLCRANK CHAFED, C-CHECK, REPAIRED RT MLG DOOR BELLCRANK.
- [SDR SWIA201438841](https://openairdocs.org/sdr/SWIA201438841), Jul 7, 2014: ATTACH FITTING. CHAFED. RIGHT MLG DOOR STRUT ATTACH FITTING CHAFED, C-CHECK, REPLACED RT MLG ATTACH FITTING REF SRM.
- [SDR SWIA201438840](https://openairdocs.org/sdr/SWIA201438840), Jul 7, 2014: VANE. CHAFED. LEFT INBD FLAP VANE, INBD L/E CHAFED. BLENDED CHAFE IAW REO & SRM.
- [SDR SWIA201438839](https://openairdocs.org/sdr/SWIA201438839), Jul 7, 2014: VANE. CHAFED. LEFT INBD FLAP VANE OTBD L/E CHAFED. BLENDED CHAFE IAW REO & SRM.
- [SDR SWIA201438838](https://openairdocs.org/sdr/SWIA201438838), Jul 7, 2014: VANE. CHAFED. RT INBD FLAP VANE INBD L/E CHAFED. BLENDED CHAFE IAW REO & SRM.
- [SDR SWIA201438846](https://openairdocs.org/sdr/SWIA201438846), Jul 6, 2014: STRUCTURE. DAMAGED. CARGO DOOR IS GOUGED & CHAFED IN REPAIR DOUBLER TOP SIDE. BLENDED OUT DAMAGED AREA ON TOP OF REPAIR DOUBLER ON CARGO DOOR IAW SRM. REPLACED DOUBLER IAW REO.

All 126: https://openairdocs.org/deregistered/N869AS-2023-04-18/reports.md

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