# N882AS: 2001 Bombardier CL-600-2B19, registration cancelled 2023-03-06

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: March 6, 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: 7503
- Year built: 2001
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: October 24, 2001
- Certificate issued: March 22, 2017
- Last registry action: January 22, 2023
- Mode S code: AC2554
- 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/N882AS
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=882AS
- Page: https://openairdocs.org/deregistered/N882AS-2023-03-06

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 (145, newest 50)

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

- [SDR SWIA2019090646261](https://openairdocs.org/sdr/SWIA2019090646261), Sep 5, 2019: STRUT. FAILED. AFTER TAKE OFF RECEIVED GEAR DISAGREE ON LEFT MAIN, SHOWED RED BOX. COMPLIED WITH QRH, DIVERTED AND PROCEEDED WITH NORMAL LANDING, NO FURTHER INDICATIONS. (FLT#
- [SDR SWIA20190405668](https://openairdocs.org/sdr/SWIA20190405668), Mar 25, 2019: SELECTOR VALVE. FAILED. GEAR DISAGREE ON APPROACH RECEIVED THE NOSE DOOR AND GEAR DISAGREE WARNINGS. THE NOSE GEAR WAS NOT SHOWING DOWN AND GREEN. PER THE QRH, CYCLED THE GEAR, AND THE
- [SDR SWIA2017050243255](https://openairdocs.org/sdr/SWIA2017050243255), May 2, 2017: CARGO TRACK. CORRODED. AFT CARGO TRACK OTBD FLANGE IS CORRODED BS 574 - 589, LBL 9. REMOVED AND REPLACED THE CARGO TRACK IAW REO AND SRM.
- [SDR SWIA2017050243254](https://openairdocs.org/sdr/SWIA2017050243254), May 2, 2017: BULKHEAD WEB. CRACKED. REAR PRESSURE BULKHEAD WEB HAS SIX CRACK INDICATIONS. REPAIRED THE BULKHEAD WEB IAW REO.
- [SDR SWIA2017050243253](https://openairdocs.org/sdr/SWIA2017050243253), May 2, 2017: SKIN. CRACKED. FUSELAGE SKIN AT NLG WHEEL WELL CUT OUT IS CRACKED, BS 235, LBL 6 AND RBL 6. REPAIRED IAW REO.
- [SDR SWIA2017050243252](https://openairdocs.org/sdr/SWIA2017050243252), May 2, 2017: BULKHEAD WEB. DAMAGED. BS 621 BULKHEAD WEB FAILED NDT INSPECTION AT LINTEL FITTING. REPAIRED THE BULKHEAD WEB IAW REO.
- [SDR SWIA2017050243251](https://openairdocs.org/sdr/SWIA2017050243251), May 2, 2017: FRAME. CORRODED. AFT CARGO, BS 605 FRAME CORRODED BETWEEN STRINGERS 22 AND 24L. REMOVED AND REPLACED THE FRAME IAW SRM.
- [SDR SWIA2017050243250](https://openairdocs.org/sdr/SWIA2017050243250), May 2, 2017: ATTACH FITTING. CORRODED. FLOORBEAM ATTACH FITTING AT BS 621, LBL 27 IS CORRODED ON THE INBD SIDE AND GOUGED ON TOP SIDE. REMOVED AND REPLACED THE ATTACH FITTING IAW REO.
- [SDR SWIA2017050243249](https://openairdocs.org/sdr/SWIA2017050243249), May 2, 2017: ATTACH FITTING. GOUGED. FLOORBEAM ATTACH FITTING BS 621 BULKHEAD FORWARD SIDE, RBL 27 GOUGED. REMOVED AND REPLACED THE ATTACHMENT FITTING IAW REO.
- [SDR SWIA2017050243248](https://openairdocs.org/sdr/SWIA2017050243248), May 2, 2017: CARGO TRACK. CORRODED. AFT CARGO TRACK OTBD FLANGE CORRODED. REMOVED AND REPLACED THE CARGO TRACK IAW SRM.
- [SDR SWIA2017050243247](https://openairdocs.org/sdr/SWIA2017050243247), May 2, 2017: FLOORBEAM. CRACKED. BS 280 FLOORBEAM CRACKED LBL 9 AND RBL 9. REPAIRED IAW REO.
- [SDR SWIA2017050243246](https://openairdocs.org/sdr/SWIA2017050243246), May 2, 2017: SEAT TRACK. BUCKLED. INBD SEAT TRACK BUCKLED BETWEEN BS 589 AND 605, LBL 27. INSTALLED A NEW SEAT TRACK IAW SRM.
- [SDR SWIA2017050243244](https://openairdocs.org/sdr/SWIA2017050243244), May 2, 2017: SKIN. DAMAGED. LOWER WINGLET SKIN PANEL DAMAGED. REMOVED AND REPLACED RT WINGLET LOWER SKIN IAW SRM.
- [SDR SWIA2017050243243](https://openairdocs.org/sdr/SWIA2017050243243), May 2, 2017: NOT REPORTED. DAMAGED. DAMAGE AT FS 349.0 BETWEEN STR 19R AND 20R. REPAIRED IAW REO AND SRM.
- [SDR ASOA20160913008A](https://openairdocs.org/sdr/ASOA20160913008A), Sep 13, 2016: DIMMER. BURNED. PILOT REPORTED BURNING ODOR TOWARD LAV AREA. MX REMOVED AND REPLACED THE POWER UNIT DIMMER ON ROW 11AB, 12AB, AND 14AB IAW AMM 33-21-04. OPS CHECKED GOOD. ACFT 
- [SDR ASOA2015032012440](https://openairdocs.org/sdr/ASOA2015032012440), Mar 19, 2015: SWITCH. SHORTED. PASSENGER DOOR VERY DIFFICULT TO OPEN. REQUIRED 2 PEOPLE TO OPEN. AFTER PUSHING IT APPROXIMATELY HALF WAY, IT FREE-FELL AS NORMAL. FOUND ASD POWER ASSIST SWITCH
- [SDR ASOA2015010511998](https://openairdocs.org/sdr/ASOA2015010511998), Dec 30, 2014: DOOR. BINDING. UNABLE TO OPEN MAIN CABIN DOOR. FELT LIKE FORWARD ASSIST MECHANISM WAS STILL ENGAGED AND RESISTING OUR EFFORTS TO PUSH DOOR OPEN. DOOR OPENED BY ITSELF A FEW MI
- [SDR ASOA2014122311922](https://openairdocs.org/sdr/ASOA2014122311922), Dec 4, 2014: SKIN. GOUGED. SEVERAL GOUGES FOUND ON FUSELAGE SKIN. BLENDED GOUGES IAW SRM 51-12-00 AND TR-51-31. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-31. REPAIRED IAW EA 25-2014-363. MA
- [SDR ASOA2014121211882](https://openairdocs.org/sdr/ASOA2014121211882), Dec 2, 2014: SKIN. GOUGED. RT WING LOWER WING ACCESS HOLE FOR ACCESS PANEL 650HB, JUST INBD OF WS 314.50 HAS SCRATCHES IN 2 PLACES REQUIRING ROTO PEENING. THIS REPAIR IS CLASSIFIED AS A M
- [SDR ASOA2014121211881](https://openairdocs.org/sdr/ASOA2014121211881), Dec 2, 2014: BULKHEAD. GOUGED. AFT PRESSURE BULKHEAD GOUGED RBL 27.50. REPAIRED IAW EC/TC REO 601R-53-61-2155.
- [SDR ASOA2014121211880](https://openairdocs.org/sdr/ASOA2014121211880), Dec 2, 2014: BULKHEAD. GOUGED. AFT PRESSURE BULKHEAD FWD FACE GOUGED LBL 18.00. REPAIRED IAW REO 601R-53-61-2155. MAJOR REPAIR.
- [SDR ASOA2014121211879](https://openairdocs.org/sdr/ASOA2014121211879), Dec 2, 2014: BULKHEAD. GOUGED. AFT PRESSURE BULKHEAD FWD FACE GOUGED AT LBL 36.2 JUST BELOW CARGO DOOR TRACK CROSS MEMBER. REPAIRED IAW REO 601R-53-61-2155.
- [SDR ASOA2014121211878](https://openairdocs.org/sdr/ASOA2014121211878), Dec 2, 2014: ATTACH ANGLE. CRACKED. CARGO DOOR TRACK ATTACH ANGLE IS CRACKED AT BS 621. REMOVED AND REPLACED THE ATTACH ANGLE IAW IAW SRM 51-42-21.
- [SDR ASOA2014122311921](https://openairdocs.org/sdr/ASOA2014122311921), Nov 30, 2014: ANGLE. CRACKED. ANGLE AT BS 625, S14L IS CRACKED, MORE THAN 1" INCH, AFT EQUIP BAY PRESSURE BULKHEAD. R & R THE ANGLE IAW SRM 51-42-21.
- [SDR ASOA2014121211877](https://openairdocs.org/sdr/ASOA2014121211877), Nov 30, 2014: ANGLE. CRACKED. ANGLE AT BS 625, S14R IS CRACKED. R & R THE ANGLE IAW SRM 51-42-21.
- [SDR ASOA2014121211876](https://openairdocs.org/sdr/ASOA2014121211876), Nov 30, 2014: ATTACH BRACKET. CRACKED. FUSELAGE STRINGER TO BULKHEAD ATTCHE BRACKET CRACKED AT BS 280 STRINGER 3. REPAIRED IAW SRM 51-42-06-00, SRM 51-42-06-00 AND 51-21-11-00.
- [SDR ASOA2014121211875](https://openairdocs.org/sdr/ASOA2014121211875), Nov 30, 2014: FLAP. GOUGED. PAX DOOR ICE BREAKER CABLE GOUGING PRESSURE VENT FLAP DURING OPS. REPAIRED IAW REO 601R-52-11-1040.
- [SDR ASOA2014122311920](https://openairdocs.org/sdr/ASOA2014122311920), Nov 26, 2014: MOUNT. CORRODED. GALLEY FLOOR MOUNT PLATE INBD OF RBL 9.00 BETWEEN FS 295.00 AND FS 333.00 THE TOP PLATE IS CORRODED. BLENDED CORROSION & EVALUATED MOUNT PLATE & CAP PLATE. PART
- [SDR ASOA2014121211874](https://openairdocs.org/sdr/ASOA2014121211874), Nov 26, 2014: FRAME. CORRODED. STUB FRAMES AT BS 349 CORRODED. REPAIRED IAW SRM 51-21-06-00.
- [SDR ASOA2014121211873](https://openairdocs.org/sdr/ASOA2014121211873), Nov 26, 2014: SEAT TRACK. CORRODED. SEAT TRACK AT BS 559 CORRODED. DETERMINED BEYOND LIMITS IAW SRM 53-21-49, PAGE BLOCK 101-199, FIGURE 101. REMOVED AND REPLACED THE SEAT TRACK IAW SRM 53-01-11-0
- [SDR ASOA2014121211872](https://openairdocs.org/sdr/ASOA2014121211872), Nov 25, 2014: FLOOR SUPPORT. CORRODED. CORROSION ON RT PRESSURE FLOOR SUPPORT BS 513. REPAIRED IAW SRM 51-21-06-00 & 51-42-21-00. MAJOR REPAIR.
- [SDR ASOA2014121211871](https://openairdocs.org/sdr/ASOA2014121211871), Nov 25, 2014: FLOOR SUPPORT. CORRODED. CORROSION ON LT PRESSURE FLOOR SUPPORT BS 499 - 513. REPAIRED IAW SRM 51-21-06-00 & 51-42-21-00. MAJOR REPAIR.
- [SDR ASOA2014121211870](https://openairdocs.org/sdr/ASOA2014121211870), Nov 25, 2014: DOOR SILL. CORRODED. SERVICE DOOR SILL FWD CORNER AT BS 319.70 IS CORRODED. DETERMINED OUT OF LIMITS IAW SRM TR 53-27. REMOVED AND REPLACED THE DOOR SILL IAW SRM 51-42-21, 51-41-02,
- [SDR ASOA2014121211869](https://openairdocs.org/sdr/ASOA2014121211869), Nov 25, 2014: FLOOR SUPPORT. CORRODED. FLOOR SUPPORT BETWEEN BS 310 - 319.70 IS CORRODED. BLENDED AND FOUND OUT OF LIMITS IAW SRM 51-21-06-00. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-42-06,
- [SDR ASOA2014122311919](https://openairdocs.org/sdr/ASOA2014122311919), Nov 24, 2014: DOOR FRAME. CORRODED. AVIONIC DOOR SURROUNDING FRAME AT BS 364 BETWEEN S24L - 24R CORRODED. BLENDED DAMAGE IAW SRM 51-21-06. FOUND TO BE OUT OF LIMITS IAW SRM TR 53-33 53-00-31. REPA
- [SDR ASOA2014122311918](https://openairdocs.org/sdr/ASOA2014122311918), Nov 24, 2014: CONNECTOR. BROKEN. EMERGINCY LIGHT WIRE CONNECTOR BROKEN OFF FUSELAGE SIDE JUST FWD OF SERVICE DOOR. REPLACED EMERGENCY LIGHT WIRE CONNECTOR IAW ESPM 20-16-00. OPS TESTED THE EMER
- [SDR ASOA2014121211868](https://openairdocs.org/sdr/ASOA2014121211868), Nov 24, 2014: HINGE. GOUGED. PASSENGER DOOR HINGE HALF HAS TWO GOUGED LUGS AT NR 2 AND NR 18. REPAIRED IAW REO 601R-52-11-1347. MAJOR REPAIR.
- [SDR ASOA2014121211867](https://openairdocs.org/sdr/ASOA2014121211867), Nov 24, 2014: ISOLATOR. BROKEN. REAR PRESSURE BULKHEAD FWD FACE HAS BROKEN ISOLATOR. R & R ISOLATOR IAW SRM 51-42-06.
- [SDR ASOA2014080811035](https://openairdocs.org/sdr/ASOA2014080811035), Aug 7, 2014: LIGHT. UNSECURE. PAX DOOR ENTRY FWD BULKHEAD EMERGENCY FLOOD LIGHT COVER & LIGHT BAR ARE UNSECURE. R & R PAX DOOR ENTRY FWD BULKHEAD FLOOR EMERGENCY FLOODLIGHT IAW AMM 33-51-19.
- [SDR ASOA2014061710674](https://openairdocs.org/sdr/ASOA2014061710674), Jun 13, 2014: COVER. MISSING. FLOOR LIGHT COVER MISSING BY MAIN DOOR, LIGHT LENS/ COVERS, INCLUDING EMERGENCY LIGHT. REPLACED LIGHT COVER IAW AMM 33-51-10 DEFER CLEARED PLACARD REMOVED.
- [SDR ASOA2014013109819](https://openairdocs.org/sdr/ASOA2014013109819), Jan 27, 2014: BATTERY PACK. FAILED. NR 1 INTERIOR AND EXTERIOR EMERGENCY LIGHTS INOPERATIVE. R & R BATTERY PACK IAW AMM 33-51-04, OPS CHECKED GOOD.
- [SDR ASOA2014011009741](https://openairdocs.org/sdr/ASOA2014011009741), Jan 6, 2014: SWITCH. DIRTY. F/A TRIED OPENING CABIN DOOR AT GATE AND WOULDN'T OPEN. F/O TRIED TO OPEN IT AND IT OPENED WITH DIFFICULTY. AFTER DOOR OPENED, IT STARTED TO RETRACT ON IT'S OWN
- [SDR ASOA2013061203821](https://openairdocs.org/sdr/ASOA2013061203821), Jun 8, 2013: DOOR. UNKNOWN. PASSENGER DOOR WOULD NOT OPEN. ONCE IT OPENED, STARTED TO RETRACT UNCOMMANDED. PERFORMED OP'S TEST OF THE PASSENGER DOOR POWER ASSIST MOTOR IAW AMM 52-11-08. OP
- [SDR ASOA2013052203642](https://openairdocs.org/sdr/ASOA2013052203642), May 17, 2013: LIGHT. SHORTED. CLIMBING THRU 15K, BOTH THE F/O AND CAPT SMELLED HOT ELECTRICAL/ BURNING PLASTIC ODOR. DIVERTED, ONE OF THE GALLEY OVERHEAD LIGHTS HAD A SHORTED, CAUSING THE OD
- [SDR ASOA2013032603256](https://openairdocs.org/sdr/ASOA2013032603256), Mar 22, 2013: LAMP. INOPERATIVE. NR 1 CEILING EMERGENCY LIGHT INOPERATIVE. REPLACED LAMP AND OPS CHECKED GOOD IAW AMM 33-51-010.
- [SDR ASOA2013021203009](https://openairdocs.org/sdr/ASOA2013021203009), Feb 1, 2013: WIRE. CHAFED. WIRE FOR FUEL QTY PROBE IN PANEL 540BB HAS CHAFE DAMAGE, BECAUSE STANDOFF FOR CLAMP IS NOT LOCATED IN CORRECT POSITION. REPAIRED IAW REO 601R-20-12-111 AND REO 
- [SDR ASOA2013021203008](https://openairdocs.org/sdr/ASOA2013021203008), Jan 28, 2013: BULKHEAD. DAMAGED. BS 409+128 PRESSURE BULKHEAD AT LBL 18 HAS TWO TOOLING MARKS, WORST IS APPROX 1.5" L X .125 W X .010 D. REPAIRED IAW REO 601R-53-41-1654.
- [SDR ASOA2013021203007](https://openairdocs.org/sdr/ASOA2013021203007), Jan 26, 2013: WEB. CHAFED. PRESSURE FLOOR SKIN JUST FWD OF FS 559 INBD OF LBL 9 HAS THREE CHAFES WITHIN A 1 INCH AREA. DEEPEST APPROX .010 DEEP. REPAIRED IAW REO 601R-41-1655R.
- [SDR ASOA2013020702980](https://openairdocs.org/sdr/ASOA2013020702980), Jan 26, 2013: FLOOR SUPPORT. CRACKED. FS 460 FLOOR SUPPORT FITTING OTBD OF RBL 9 CRACKED. REMOVED DAMAGED FLOOR SUPPORT FITTING AT FS 460 OTBD OF RBL 9 IAW SRM 51-42-21 & 51-42-06. LOCATED FASTENER 
- [SDR ASOA2013020702979](https://openairdocs.org/sdr/ASOA2013020702979), Jan 26, 2013: FLOOR SUPPORT. CRACKED. FS 484 FLOOR SUPPORT CLIP RBL 27 CRACKED. REMOVED CLIP AT FS 484.00, RBL 27, LOCATED DRILLED UP AND INSTALLED NEW CLIP PN 601R31171-9 IAW SRM 51-40-11 AND SRM 5

All 145: https://openairdocs.org/deregistered/N882AS-2023-03-06/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 20030501008859I](https://openairdocs.org/incident/20030501008859I), May 1, 2003: Cndair CL6002B19 (N882AS), Augusta, GA. (-23) On 05-01-2003, at approximately 0606 local time, atlantic southeast flight 4431 (asa 4431) departed the Augusta Bush regional airport (ags), Augusta,…

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