# N913SW: 2001 Bombardier CL-600-2B19, registration cancelled 2023-01-24

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: January 24, 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: 7597
- Year built: 2001
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: January 17, 2002
- Certificate issued: February 27, 2018
- Last registry action: September 29, 2020
- Mode S code: ACA375
- 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/N913SW
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=913SW
- Page: https://openairdocs.org/deregistered/N913SW-2023-01-24

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 (215, newest 50)

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

- [SDR SWIA202049252](https://openairdocs.org/sdr/SWIA202049252), Mar 11, 2020: UNKNOWN. FIRE. CREATED FROM FORWARD DISCREPANCY. PLEASE REFERENCE AML 397685, WHEN AIRCRAFT WAS BEING REPOSITIONED FROM TERMINAL TO HANGAR FOR MX, APU WAS STARTED AND AS SOON 
- [SDR SWIA2020031049250](https://openairdocs.org/sdr/SWIA2020031049250), Feb 22, 2020: POST. CRACKED. COMPLY WITH FORM 337 FOR FS409+128 VERTICAL POST CRACKED AT INBOARD LOWER AFT RIVET IN RADIUS AT LBL27. CLASIFIED AS MAJOR REPAIR. (AGING A/C INSP - RO 3/7/2020
- [SDR SWIA2020031049249](https://openairdocs.org/sdr/SWIA2020031049249), Feb 22, 2020: POST. CRACKED. COMPLY WITH FORM 337 FOR FS409+128 VERTICAL POST CRACKED AT OUTBOARD LOWER AFT RIVET IN RADIUS AT LBL18. CLASIFIED AS MAJOR REPAIR. (AGING A/C INSP - RO 3/7/202
- [SDR SWIA2020031049102](https://openairdocs.org/sdr/SWIA2020031049102), Feb 20, 2020: POST. CRACKED. ***** MAJOR ***** FS409+128 VERTICAL POST CRACKED AT OUTBOARD LOWER AFT RIVET IN RADIUS AT LBL18. (AGING AC INSP - RO 3/7/2020) REPAIRED FS409+128 VERTICAL POST
- [SDR SWIA2020031049099](https://openairdocs.org/sdr/SWIA2020031049099), Feb 20, 2020: POST. CRACKED. ***** MAJOR ***** FS409+128 VERTICAL POST CRACKED AT INBOARD LOWER AFT RIVET IN RADIUS AT LBL27. (AGING AC INSP - RO 3/7/2020) REPAIRED FS409+128 VERTICAL POST 
- [SDR SWIA2019061145973](https://openairdocs.org/sdr/SWIA2019061145973), Jun 11, 2019: CONTROL HANDLE. FAILED. AFTER TAKEOFF, THE LANDING GEAR FAILED TO RETRACT; FOLLOWED BY A/SKID INBD AND PARK BRAKE SOV CAUTION MESSAGES. RETURNED TO FIELD. (FLT#5399) REMOVED AND REPLAC
- [SDR SWIA2019405065827](https://openairdocs.org/sdr/SWIA2019405065827), May 6, 2019: SERVO VALVE. FAILED. STEERING INOP CAUTION IN FLIGHT. COMPLIED WITH QRH. (FLT#5311) CLOSED REMOVED AND REPLACED SERVO VALVE IAW AMM.
- [SDR SWIA2018110245220](https://openairdocs.org/sdr/SWIA2018110245220), Oct 19, 2018: SKIN. DENTED. A DENT WAS FOUND ON THE RT INBD FLAP LOWER SKIN. REPAIRED THE SKIN IAW SRM 57-52-00.
- [SDR SWIA2018110245222](https://openairdocs.org/sdr/SWIA2018110245222), Oct 8, 2018: FRAME. CORRODED. BS 605 FRAME FOUND CORRODED. REMOVED AND REPLACED THE ENTIRE FRAME SECTOR IAW SRM 51-42-06.
- [SDR SWIA2018110245219](https://openairdocs.org/sdr/SWIA2018110245219), Oct 7, 2018: FLOOR SUPPORT. CORRODED. RIGHT FLOOR SUPPORT CORRODE AT BS 559. REMOVED AND REPLACED IAW SRM 51-42-06.
- [SDR SWIA2018110245218](https://openairdocs.org/sdr/SWIA2018110245218), Oct 7, 2018: FLOOR SUPPORT. CORRODED. FLOOR SUPPORT CORRODED AT BS 559. REMOVED AND REPLACED IAW SRM 51-42-06.
- [SDR SWIA2018110245217](https://openairdocs.org/sdr/SWIA2018110245217), Oct 6, 2018: FLOORBEAM. CORRODED. COCKPIT FLOORBEAM, BS 280 WAS CORRODED. REMOVED AND REPLACED THE COCKPIT FLOORBEAM ANGLE.
- [SDR SWIA2018110245216](https://openairdocs.org/sdr/SWIA2018110245216), Oct 5, 2018: VANE. GOUGED. RIGHT INBOARD FLAP VANE WAS GOUGED. REPAIRED IAW SRM 51-21-06.
- [SDR SWIA2018110245215](https://openairdocs.org/sdr/SWIA2018110245215), Oct 5, 2018: VANE. WORN. LEFT OUTBOARD FLAP, OUTBOARD VANE MOUNT STRUCTURE WAS WORN. MEASURED REMAINING MATERIAL AND FOUND WITHIN LIMITS IAW REO 601R-57-53-195.
- [SDR SWIA2018110245221](https://openairdocs.org/sdr/SWIA2018110245221), Oct 4, 2018: STRINGER SPLICE. CRACKED. STRINGER SPLICE WAS CRACKED AT ITS ATTACH POINT TO PASSENGER DOOR UPPER SILL, BS 379. REPAIRED THE STRINGER SPLICE IAW SRM 53-00-03.
- [SDR SWIA2018110245214](https://openairdocs.org/sdr/SWIA2018110245214), Oct 4, 2018: STRAP. CORRODED. CORROSION FOUND ONTHE CIRCUMFERENTIAL STRAP BELOW FRAME BS 333. BLENDED THE STRAP IAW SRM 51-21-06.
- [SDR SWIA2018110245213](https://openairdocs.org/sdr/SWIA2018110245213), Oct 4, 2018: BRACKET. CORRODED. CORROSION FOUND ON THE BRACKET ATTACHED TO FRAME AT BS 319. REMOVED AND REPLACED THE BRACKET IAW SRM 51-42-21.
- [SDR SWIA2018110245212](https://openairdocs.org/sdr/SWIA2018110245212), Oct 4, 2018: FRAME. CORRODED. CORROSION FOUND ON THE FWD AND AFT FACES OF THE FRAME AT BS 333. REMOVED THE CORROSION IAW SRM 51-21-06.
- [SDR SWIA2018110245211](https://openairdocs.org/sdr/SWIA2018110245211), Oct 4, 2018: HINGE. CHAFED. SERVICE DOOR INTERIOR HINGE CHAFED. REMOVED AND REPLACED THE SERVICE DOOR HINGE PLATE IAW SRM 51-41-21. OPS CHECKED GOOD
- [SDR SWIA2018110245210](https://openairdocs.org/sdr/SWIA2018110245210), Oct 4, 2018: PANEL. GOUGED. PANEL 326CR GOUGED. REPAIRED THE PANEL IAW REO 601R-55-32-384.
- [SDR SWIA2018110245209](https://openairdocs.org/sdr/SWIA2018110245209), Oct 3, 2018: SKIN. CORRODED. CORROSION FOUND ON THE INNER SKIN, AROUND FORWARD AND AFT ACCESS DOOR CUT-OUTS. REMOVED AND REPLACED THE PAX DOOR SKIN IAW SRM 51-42-06.
- [SDR SWIA2018110245208](https://openairdocs.org/sdr/SWIA2018110245208), Oct 3, 2018: SKIN. CHAFED. RIGHT HORIZONTAL STAB PANEL WAS CHAFED ON THE INNER SKIN. R & R THE SKIN PANEL IAW SRM 51-12-00.
- [SDR SWIA2018110245207](https://openairdocs.org/sdr/SWIA2018110245207), Oct 3, 2018: SKIN. CHAFED. LEFT ELEVATOR SKIN PANEL WAS CHAFED. REPAIRED THE DAMAGE IAW SRM 51-12-00.
- [SDR SWIA2018110245206](https://openairdocs.org/sdr/SWIA2018110245206), Oct 3, 2018: SKIN PANEL. CHAFED. LEFT WING SKIN PANEL WAS CHAFED. BLENDED THE PANEL IAW SRM 51-41-02.
- [SDR SWIA2018110245205](https://openairdocs.org/sdr/SWIA2018110245205), Oct 3, 2018: SKIN. CHAFED. LEFT NACELLE SKIN PANEL WAS CHAFED AT MULTIPLE PLACES. REMOVED AND REPLACED THE SKIN IAW SRM 51-42-06.
- [SDR SWIA2018110245204](https://openairdocs.org/sdr/SWIA2018110245204), Oct 2, 2018: COVER. NICKED. TWO NICKS FOUND JUST AFT OF GROUND AIR LOW PRESSURE COVER. COMPLIED WITH PERMANENT REPAIR OF THE AREA IAW REO 601R-53-61-6734.
- [SDR SWIA2018110245203](https://openairdocs.org/sdr/SWIA2018110245203), Oct 2, 2018: SKIN. DENTED. A DENT WAS FOUND ON THE CARGO DOOR SKIN, AT THE BOTTOM CORNER. REPAIRED THE CARGO DOOR SKIN IAW REO 601R-52-31-299.
- [SDR SWIA2018110245202](https://openairdocs.org/sdr/SWIA2018110245202), Oct 2, 2018: STRUCTURE. DENTED. A DENT WAS FOUND ON THE AFT FUSELAGE TAIL. REPAIRED.
- [SDR SWIA2018110245201](https://openairdocs.org/sdr/SWIA2018110245201), Oct 2, 2018: SKIN. DENTED. A DENT WAS FOUND AFT AND ABOVE THE LT ACM EXHAUST OPENING. REPAIRED THE DENT IAW REO 601R-51-00-309.
- [SDR SWIA2018110245200](https://openairdocs.org/sdr/SWIA2018110245200), Oct 2, 2018: SKIN. DENTED. TWO SMALL DENTS FOUND ON THE RT FUSELAGE BETWEEN BS 589 TO 605. REPAIRED IAW REO 601R-53-61-6734.
- [SDR SWIA2018110245199](https://openairdocs.org/sdr/SWIA2018110245199), Oct 2, 2018: SKIN. DENTED. A DENT WAS FOUND ON THE RT BOTTOM FUSELAGE JUST OUTBOARD FROM NLG. REPAIRED IAW REO 601R-53-11-3333.
- [SDR SWIA2018080744974](https://openairdocs.org/sdr/SWIA2018080744974), Jul 30, 2018: SKIN. DAMAGED. FOUND ELONGATED DAMAGED SCREW HOLE UNDER THE LT MLG ACCESS PANEL ADJACENT TO THE MLG OPENING. BETWEEN LT WS 53.60 - 65.75. REPAIRED WING PLANK IAW REO.
- [SDR SWIA2018051744638](https://openairdocs.org/sdr/SWIA2018051744638), May 6, 2018: ENGINE. FLAMED OUT. CAPTAIN REPORTED THAT DURING APPROACH, RECEIVED A RT MAIN EJECTOR AND RT SCAVENGE EJECTOR CAUTION MESSAGES AND RIGHT AFTER TOUCH DOWN THE RT ENGINE FLAMED OUT. 
- [SDR SWIA201642644](https://openairdocs.org/sdr/SWIA201642644), Sep 16, 2016: STRINGER. DAMAGED. DAMAGE TO STR 0 BETWEEN BS 409+80 AND 409.00+96. REMOVED AND INSTALLED THE STRINGER IAW SRM.
- [SDR SWIA201642643](https://openairdocs.org/sdr/SWIA201642643), Sep 16, 2016: STRINGER. DAMAGED. DAMAGE TO STRINGER 16R BETWEEN BS 409 - 409 + 32. REMOVED AND REPLACED THE STRINGER IAW SRM.
- [SDR SWIA201642648](https://openairdocs.org/sdr/SWIA201642648), Sep 10, 2016: VANE. CHAFED. RIGHT FLAP VANE OTBD LEADING EDGE IS CHAFED. REMOVED AND REPLACED THE FLAP VANE OTBD LEADING EDGE IAW SRM.
- [SDR SWIA201642647](https://openairdocs.org/sdr/SWIA201642647), Sep 10, 2016: VANE. CHAFED. RIGHT FLAP VANE CENTER OF LEADING EDGE IS CHAFED. REMOVED AND REPLACED THE FLAP VANE CENTER LEADING EDGE IAW SRM.
- [SDR SWIA201642646](https://openairdocs.org/sdr/SWIA201642646), Sep 10, 2016: VANE. CHAFED. RIGHT FLAP VANE INBD LEADING EDGE IS CHAFED. REMOVED AND REPLACED THE FLAP VANE INBD LEADING EDGE IAW SRM.
- [SDR SWIA201642645](https://openairdocs.org/sdr/SWIA201642645), Sep 10, 2016: VANE. CHAFED. LEFT FLAP VANE INBD LEADING EDGE IS CHAFED. REMOVED AND REPLACED LT FLAP VANE INBD LEADING EDGE IAW SRM.
- [SDR SWIA201440370](https://openairdocs.org/sdr/SWIA201440370), Dec 6, 2014: SKIN. GOUGED. BS 627, OTBD OF STRINGER 4L, TWO GOUGES ON SKIN. REPAIRED IAW EA
- [SDR SWIA201440379](https://openairdocs.org/sdr/SWIA201440379), Dec 4, 2014: PANEL. CRACKED. PANEL 221BLC CRACKED AND MISSING 6 EA SPACERS. REPAIRED CRACKED PANEL IAW EA AND SRM.
- [SDR SWIA201440388](https://openairdocs.org/sdr/SWIA201440388), Nov 29, 2014: DOOR. CHAFED. RIGHT MLG DOOR HAS CHAFE ON AFT EDGE THRU INNER SKIN NEAR BRUSH. RT MLG DOOR WORKED IAW STS EA COMPLIED WITH STEPS 1 THRU END, IAW SRM, REPAIR COMPLETED. THIS I
- [SDR SWIA201440384](https://openairdocs.org/sdr/SWIA201440384), Nov 25, 2014: VANE. DAMAGED. LT INBD FLAP VANE CENTER CAP FOUND TO BE OUT OF LIMITS. R & R LT INBD FLAP VANE CENTER L/E SKIN, CAP, IAW SRM AND DWG 601R14303, REV J.
- [SDR SWIA201440390](https://openairdocs.org/sdr/SWIA201440390), Nov 24, 2014: SEAT TRACK. CORRODED. SEAT TRACK RBL9 FS 559+86 TO 559+112 CORRODED. REPLACED THE SEAT TRACK IAW AMM AND REO.
- [SDR SWIA201440382](https://openairdocs.org/sdr/SWIA201440382), Nov 24, 2014: PRESSURE PANEL. CRACKED. PRESSURE FLOOR CRACKED IN 2 PLACES AT FS 460 OTBD OF LBL 0.0 AND RBL 0.0. COMPLIED WITH REPAIR OF PRESSURE FLOOR 2 PLACES AT FS 460 OTBD OF BL 0.0. RT & LT SIDE
- [SDR SWIA201440380](https://openairdocs.org/sdr/SWIA201440380), Nov 24, 2014: LEVER. WORN. PAX DOOR PULL IN LEVER IS WORN. REPAIRED THE PASSENGER DOOR PULL IN LEVER IAW REO.
- [SDR SWIA201440378](https://openairdocs.org/sdr/SWIA201440378), Nov 24, 2014: FAIRING. DAMAGED. LEFT HORIZONTAL TIP FAIRING 333AL HAS MULTIPLE ELONGATED HOLES. REPAIRED IAW EA.
- [SDR SWIA201440377](https://openairdocs.org/sdr/SWIA201440377), Nov 24, 2014: DOOR SILL. CORRODED. LEFT CARGO DOOR SILL HAS CORROSION AROUND NUTPLATE HOLES FS 574 TO 621. C-CHECK, RO 12/10/14, BLENDED LT CARGO DOOR SILL CORROSION AROUND NUTPLATE HOLES FS 574 
- [SDR SWIA201440371](https://openairdocs.org/sdr/SWIA201440371), Nov 24, 2014: BULKHEAD. DAMAGED. FWD FACE OF FS 621 REAR PRESSURE BULKHEAD HAS SCREW STRIKES BETWEEN ISOLATOR MOUNTS AS MARKED. C-CHECK, RO 12/10/14. BLENDED SEVERAL AREAS OF SCREW NICKS ON FS 
- [SDR SWIA201440369](https://openairdocs.org/sdr/SWIA201440369), Nov 24, 2014: TRUNNION. DAMAGED. FOUND AN OVERSIZED HOLE ON LT TRUNNION. REPAIRED THE LT TRUNION IAW REO.

All 215: https://openairdocs.org/deregistered/N913SW-2023-01-24/reports.md

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