# N884AS: 2001 Bombardier CL-600-2B19, registration cancelled 2019-11-26 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: November 26, 2019 - 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: 7513 - Year built: 2001 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: October 24, 2001 - Certificate issued: July 31, 2017 - Last registry action: July 31, 2017 - Mode S code: AC2CC2 - 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/N884AS - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=884AS - Page: https://openairdocs.org/deregistered/N884AS-2019-11-26 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 (162, newest 50) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR SWIA201743939](https://openairdocs.org/sdr/SWIA201743939), Nov 1, 2017: O-RING. FAILED. HYD SYSTEM 3 FAILED DURING CRUISE FLIGHT. ZERO PSI. COMPLIED WITH QRH. DECLARED EMERGENCY. PERFORMED A FREEFALL EXTENSION OF LANDING GEAR. R & R THE HYD PUMP 3A - [SDR SWIA2017101243860](https://openairdocs.org/sdr/SWIA2017101243860), Sep 13, 2017: TRUNNION. DAMAGED. UPPER LEFT TRUNNION STRUCTURE ATTACHMENT HOLES, ARE OVERSIZED. STEPPED UP TRUNNION HOLES TO FIRST OVER SIZE IAW REO. - [SDR SWIA2017101243852](https://openairdocs.org/sdr/SWIA2017101243852), Sep 13, 2017: FLOOR SUPPORT. CORRODED. SERVICE DOOR FLOOR SUPPORT BRACKET AT BS 349 CORRODED. REMOVED AND REPLACED BRACKET IAW SRM. - [SDR SWIA2017101243862](https://openairdocs.org/sdr/SWIA2017101243862), Sep 11, 2017: ANGLE. CORRODED. SERVICE DOOR FLOOR SUPPORT ANGLE AT BS 319 IS CORRODED. REMOVED AND REPLACED ANGLE IAW SRM. - [SDR SWIA2017101243858](https://openairdocs.org/sdr/SWIA2017101243858), Sep 10, 2017: FLOOR SUPPORT. CORRODED. FLOOR SUPPORT AT THE PASSENGER DOOR IS CORRODED BETWEEN BS 349 AND 359. REMOVED THE CORROSION IAW REO. - [SDR SWIA2017101243864](https://openairdocs.org/sdr/SWIA2017101243864), Sep 9, 2017: SHEAR TIE. CORRODED. CORROSION ON LOWER FRAME SHEAR TIE AT BS 319. REMOVED AND REPLACED THE SHEAR TIE IAW SRM. - [SDR SWIA2017101243863](https://openairdocs.org/sdr/SWIA2017101243863), Sep 9, 2017: DOUBLER. CORRODED. RT GALLEY MOUNT DOUBLER FWD OF BS 319 IS CORRODED. REMOVED AND REPLACED THE DOUBLER IAW SRM. - [SDR SWIA2017101243857](https://openairdocs.org/sdr/SWIA2017101243857), Sep 9, 2017: BEAM. CORRODED. RIGHT TRANSVERSE BEAM AT BS 349 IS CORRODED. REPAIRED DAMAGE AT IAW REO. - [SDR SWIA201743855](https://openairdocs.org/sdr/SWIA201743855), Sep 9, 2017: FLOOR SUPPORT. DAMAGED. FLOOR SUPPORT AT RBL 27 BETWEEN BS 574 - 621 DAMAGED. REPAIRED FLOOR SUPPORT IAW REO. - [SDR SWIA2017101243853](https://openairdocs.org/sdr/SWIA2017101243853), Sep 9, 2017: SHEAR TIE. CORRODED. CORROSION ON LOWER FRAME BRACKET AT BS 349. REMOVED AND REPLACED LOWER FRAME BRACKET IAW SRM. - [SDR SWIA2017101243856](https://openairdocs.org/sdr/SWIA2017101243856), Sep 8, 2017: FLOOR SUPPORT. CORRODED. CORROSION ON THE RT FLOOR SUPPORT FROM BS 349 - 364. REPAIRED THE DAMAGE IAW REO. - [SDR SWIA2017101243851](https://openairdocs.org/sdr/SWIA2017101243851), Sep 3, 2017: FLOOR SUPPORT. CORRODED. FLOOR SUPPORT AROUND NUTPLATES BETWEEN BS 605.04 AND 574 CORRODED AT CARGO BAY DOOR. FURTHER INVESTIGATION FOUND CARGO DOOR FLOOR SUPPORT TO BE OUT OF LIMITS. I - [SDR SWIA2017101243861](https://openairdocs.org/sdr/SWIA2017101243861), Aug 28, 2017: FRAME. CRACKED. BS 280 FRAME IS CRACKED AT STRINGER 3L. REPAIRED THE FRAME IAW REO. - [SDR SWIA2017101243854](https://openairdocs.org/sdr/SWIA2017101243854), Aug 28, 2017: CHANNEL. CRACKED. CARGO DOOR FWD TRACK LOWER CHANNEL IS CRACKED. REMOVED AND INSTALLED A NEW CHANNEL IAW SRM. - [SDR SWIA201743859](https://openairdocs.org/sdr/SWIA201743859), Aug 24, 2017: SKIN. DENTED. SKIN DENTED AT BS 409+64, STRINGER 15R. REPAIRED IAW REO. - [SDR ASOA2016060714916](https://openairdocs.org/sdr/ASOA2016060714916), Jun 7, 2016: LAMP. BURNED OUT. NR 4 EXIT, EMERGENCY LIGHT INOPERATIVE. REPLACED THE LAMP IAW AMM 33-51-21. OPS CHECKED GOOD. - [SDR ASOA2015121114209](https://openairdocs.org/sdr/ASOA2015121114209), Dec 11, 2015: GENERATOR. SHUTDOWN. ADG DEPLOYED IN FLIGHT DUE TO INADVERTENTLY SHUTTING DOWN OF GEN 1 AND GEN 2 EMERGENCY DECLARED. ACFT RETURNED TO DEPARTURE AFTER T/O. RETRACTED ADG IAW AMM 24- - [SDR ASOA2015102313950](https://openairdocs.org/sdr/ASOA2015102313950), Oct 23, 2015: SPAR. DAMAGED. AFT SPAR ON RT HORIZONTAL STAB TIP FOUND TO BE DAMAGED DUE TO LIGHTNING STRIKE. CUT AWAY BURNED SECTION OF AFT SPAR AND CLEANED UP ALL SHARP EDGES ON MISDRILLED - [SDR ASOA2015070213228](https://openairdocs.org/sdr/ASOA2015070213228), Jun 18, 2015: ANGLE. CORRODED. FS 280 J-ANGLE CORRODED. REMOVED CORRODED J-ANGLE AT FS 280 PT 600-34017-351 IAW SRM 51-42-06. LOCATED, DRILLED & INSTALLED NEW FS 280, J-ANGLE PT 600-34017-351 - [SDR ASOA2015070213227](https://openairdocs.org/sdr/ASOA2015070213227), Jun 10, 2015: FRAME. CRACKED. FS 605, FRAME AND PREVIOUS USED DOUBLER STRAP CRACKED AT UPPER HOLE LOCATION WHERE STANDOFF SB INSTALLED AFTER INSTALLATION AT RT STR 26 AND RT STR 27. LOCATED - [SDR ASOA2015070213226](https://openairdocs.org/sdr/ASOA2015070213226), Jun 8, 2015: FLOORBEAM. CORRODED. CORROSION FOUND AT NUTPLATE LOCATION AT LT FS 561.00, STR 17, BUTT LINE 36 TO 47. COMPLIED WITH EC/TC REO:601R-53-41-666 AND REO:601R-53-41-666, REV C. - [SDR ASOA2015070213225](https://openairdocs.org/sdr/ASOA2015070213225), Jun 5, 2015: SKIN. CRACKED. RIGHT WING PLANK ACCESS HOLE CUTOUT FOR PANEL 650CB HAS INDICATIONS AROUND CIRCUMFERENCE OF LANDING 55 PERCENT FSH, AREA MARKED ON ACFT, FAILED NDT. REMOVED RT - [SDR ASOA2015070213224](https://openairdocs.org/sdr/ASOA2015070213224), Jun 5, 2015: ANGLE. CRACKED. OBLIQUE ANGLE CRACKED AT FS 622- FS 625, STR 14L ABOUT LBL 40. REMOVED OBLIQUE ANGLE IAW SRM 51-42-20. LOCATED, DRILLED AND INSTALLED NEW INTERCOSTAL ANGLE AT F - [SDR ASOA2015070213223](https://openairdocs.org/sdr/ASOA2015070213223), Jun 5, 2015: INTERCOSTAL. CRACKED. INTERCOSTAL FS 621-625, STR 14L, ADJACENT TO SKIN, OTBD FLANGE IS CRACKED. REMOVED CRACKED INTERCOSTAL, PN:601R2350121-5 FROM INTERCOSTAL. IN STEP 3 IAW SRM 51- - [SDR ASOA2015070213222](https://openairdocs.org/sdr/ASOA2015070213222), Jun 3, 2015: INTERCOSTAL. CORRODED. INTERCOSTAL AT BS 349-364, STRINGER 26L IS CORRODED. BLENDED CORROSION FROM INTERCOSTAL 26L AT FS 349-364 MAXIMUM MATERIAL REMOVED .002 IAW SRM 51-21-06, 53-00- - [SDR ASOA2015070213221](https://openairdocs.org/sdr/ASOA2015070213221), Jun 3, 2015: SPLICE PLATE. CORRODED. SPLICE PLATE AT FS 621 RH RBL 41 IS CORRODED. BLENDED CORROSION ON SPLICE PLATE AT FS 621, RBL 41 IAW REO 601R-53-61-4690. MAXIMUM MATERIAL REMOVED .009. REPAIR - [SDR ASOA2015070213220](https://openairdocs.org/sdr/ASOA2015070213220), Jun 3, 2015: SKIN. CORRODED. CORROSION ON LOWER WING PLANK HOLE, 540BB IN SEVERAL LOCATIONS. COMPLIED WITH REO 601R-57-21-030, REV L, ROTO PEENING REWORKED AREA IAW SRM 51-24-11. COMPLIED W - [SDR ASOA2015070213219](https://openairdocs.org/sdr/ASOA2015070213219), Jun 3, 2015: SKIN. CORRODED. CORROSION ON LOWER WING PLANK HOLE, 510AB IN SEVERAL LOCATIONS. COMPLIED WITH REO 601R-57-21-030, REV L, ROTO PEEN OF THE REPAIR SURFACE IAW SRM 51-24-11. COMPL - [SDR ASOA2015070113218](https://openairdocs.org/sdr/ASOA2015070113218), Jun 3, 2015: SKIN. CORRODED. CORRROSION ON LOWER WING PLANK HOLE, 610AB IN SEVERAL AREAS. COMPLIED WITH REO 601R-57-21-030. COMPLIED WITH REO 601R-57-21-030, REV L-ROTO PEEN OF REWORKED SUR - [SDR ASOA2015070113217](https://openairdocs.org/sdr/ASOA2015070113217), Jun 3, 2015: SKIN. CORRODED. CORROSION ON LOWER WING PLANK HOLE, 640BB, IN SEVERAL LOCATIONS. COMPLIED WITH REO 601R-57-21-030. COMPLIED WITH REO 601R-57-21-030, REV L, ROTO-PEENING OF REWO - [SDR ASOA2015070113216](https://openairdocs.org/sdr/ASOA2015070113216), Jun 3, 2015: BULKHEAD WEB. CRACKED. FOUND REAR PRESSURE BULKHEAD WEB HAS MULTIPLE INDICATIONS NOTED AT LBL 27.50, WL 130 APPROX 2.0" IN LENGTH 100 PERCENT FSH. FAILED NDT INSPECTION. UPON MILLING - [SDR ASOA2015070113215](https://openairdocs.org/sdr/ASOA2015070113215), Jun 3, 2015: BULKHEAD WEB. CRACKED. FOUND REAR PRESSURE BULKHEAD WEB HAS MULTIPLE INDICATIONS NOTED AT LBL 36.20 JUST ABOVE WL 73.50 APPROXIMATELY 1.5 IN LENGTH 100 PERCENT FSH. FAILED NDT INSPECT - [SDR ASOA2015070113214](https://openairdocs.org/sdr/ASOA2015070113214), Jun 3, 2015: BULKHEAD WEB. CRACKED. FOUND REAR PRESSURE BULKHEAD WEB HAS MULTIPLE INDICATIONS NOTED AT LBL 27.50 BETWEEN WL 73.50-WL 120.43 APPROXIMATELY 24" IN LENGTH 50 PERCENT FSH. FAILED NDT I - [SDR ASOA2015070113213](https://openairdocs.org/sdr/ASOA2015070113213), Jun 3, 2015: BULKHEAD WEB. CRACKED. FOUND REAR PRESSURE BULKHEAD WEB HAS MULTIPLE INDICATIONS NOTED AT LBL 18.00 BETWEEN WL 121.93-WL 137.5 APPROXIMATELY 2.0" IN LENGTH 50 PERCENT FSH. FAILED NDT - [SDR ASOA2015070113212](https://openairdocs.org/sdr/ASOA2015070113212), Jun 3, 2015: BULKHEAD WEB. CRACKED. FOUND REAR PRESSURE BULKHEAD WEB HAS MULTIPLE INDICATIONS NOTED AT BL 0.0 BETWEEN WL 121.93-WL 137.5 APPROXIMATELY 9.0" IN LENGTH, 50 PERCENT FSH. FAILED NDT IN - [SDR ASOA2015070113211](https://openairdocs.org/sdr/ASOA2015070113211), Jun 3, 2015: BULKHEAD WEB. CRACKED. FOUND REAR PRESSURE BULKHEAD WEB HAS MULTIPLE INDICATIONS NOTED AT RBL 9.5 BETWEEN WL 121.93-WL 137.5 APPROXIMATELY 2.5" IN LENGTH, 50 PERCENT FSH. FAILED NDT I - [SDR ASOA2015070113210](https://openairdocs.org/sdr/ASOA2015070113210), Jun 3, 2015: BULKHEAD WEB. CRACKED. FOUND REAR PRESSURE BULKHEAD WEB HAS MULTIPLE INDICATIONS NOTED AT RBL 18.00 BETWEEN WL 121.93-WL 137.5 APPROXIMATELY 2.5" IN LENGTH 50 PERCENT FSH. FAILED NDT - [SDR ASOA2015070113209](https://openairdocs.org/sdr/ASOA2015070113209), Jun 3, 2015: BULKHEAD WEB. CRACKED. FOUND REAR PRESSURE BULKHEAD WEB HAS MULTIPLE INDICATIONS NOTED AT RBL 27.50 BETWEEN WL 121.43-WL 137.5 APPROXIMATELY 6.0" IN LENGTH, 50 PERCENT FSH. FAILED NDT - [SDR ASOA2015070113208](https://openairdocs.org/sdr/ASOA2015070113208), Jun 3, 2015: BULKHEAD WEB. CRACKED. FOUND REAR PRESSURE BULKHEAD WEB HAS MULTIPLE INDICATIONS NOTED AT RBL 27.50 BETWEEN WL 73.50-WL 120.43 APPROXIMATELY 2.0" IN LENGTH, 50 PERCENT FSH. FAILED NDT - [SDR ASOA2015070113207](https://openairdocs.org/sdr/ASOA2015070113207), Jun 3, 2015: BULKHEAD WEB. CRACKED. FOUND REAR PRESSURE BULKHEAD WEB HAS MULTIPLE INDICATIONS NOTED AT RBL 18.00 BETWEEN WL 73.50-WL 120.43 APPROXIMATELY 3.0" IN LENGTH, 50 PERCENT FSH. FAILED NDT - [SDR ASOA2015070113206](https://openairdocs.org/sdr/ASOA2015070113206), Jun 3, 2015: BULKHEAD WEB. CRACKED. FOUND REAR PRESSURE BULKHEAD WEB HAS MULTIPLE INDICATIONS NOTED AT BL 0.0 BETWEEN WL 73.50-WL 120.43 APPROXIMATELY 2.0" IN LENGTH 50 PERCENT FSH. FAILED NDT INS - [SDR ASOA2015070113205](https://openairdocs.org/sdr/ASOA2015070113205), Jun 3, 2015: BULKHEAD WEB. CRACKED. FOUND REAR PRESSURE BULKHEAD WEB HAS MULTIPLE INDICATIONS NOTED AT LBL 9.50 BETWEEN WL 73.50-WL 120.43 APPROX 4.0" IN LENGTH 50 PERCENT FSH. FAILED NDT INSPECTI - [SDR ASOA2015070113204](https://openairdocs.org/sdr/ASOA2015070113204), Jun 3, 2015: BULKHEAD WEB. CRACKED. FOUND REAR PRESSURE BULKHEAD WEB HAS MULTIPLE INDICATIONS NOTED AT LBL 18.00 BETWEEN WL 73.50, WL 120.43 APPROXIMATELY 12" IN LENGTH, 50 PERCENT FSH. FAILED NDT - [SDR ASOA2015070113203](https://openairdocs.org/sdr/ASOA2015070113203), Jun 3, 2015: POST. CRACKED. FS 409+128, RBL 18 VERT POST INBD AND OTBD SIDES HAVE INDICATIONS NOTED IN THE AFT FLANGE RADII AT WL 69 .250", LONG BY 60 FSH. FAILED NDT. REMOVED INBD POST, P - [SDR ASOA2015070113202](https://openairdocs.org/sdr/ASOA2015070113202), Jun 3, 2015: ATTACH BRACKET. CRACKED. BRACKET ATTACHING FROM STR 3L TO FS 280 IS CRACKED. REMOVED CLEAT IAW SRM 51-42-06. LOCATED, DRILLED AND INSTALLED NEW SERVICEABLE CLEAT IAW SRM 51-40-11 AND 51 - [SDR ASOA2015063013198](https://openairdocs.org/sdr/ASOA2015063013198), Jun 3, 2015: ATTACH ANGLE. CRACKED. STR 3L ATTACHING ANGLES ARE CRACKED JUST AFT OF FS 280. REMOVED ANGLE, PN 600-31057-19 FROM STR 3L AT FS 280 IAW SRM 51-42-06. DRILLED, LOCATED AND INSTALLED NE - [SDR ASOA2015061213102](https://openairdocs.org/sdr/ASOA2015061213102), Jun 3, 2015: POST. CRACKED. FS 409+128, LBL 18 VERT POST INBD AND OTBD SIDES HAVE INDICATIONS NOTED IN THE AFT FLANGE RADII AT WL 69 APPROXIMATELY .250" LONG BY 50 PERCENT FSH. BOTH INDICA - [SDR ASOA2015060813069](https://openairdocs.org/sdr/ASOA2015060813069), Jun 3, 2015: POST. CRACKED. FS 409+128, BL 0 VERT POST LT SIDE HAS AN INDICATION NOTED IN THE AFT FLANGE RADIUS AT WL 69 .250", LONG Y 50 PERCENT FSH, FAILED NDT. REPAIRED IAW ECTC REO 601 - [SDR ASOA2015063013197](https://openairdocs.org/sdr/ASOA2015063013197), Jun 2, 2015: FRAME. CORRODED. CORROSION ON 605 FRAME FROM STR 27 TO STR 24L. FOUND CORROSION ON FS 605, FRAME TO BE OUT OF LIMITS IAW SRM 53-00-00. REMOVED FS 605, FRAME IAW SRM 51-42-06 AND - [SDR ASOA2015063013196](https://openairdocs.org/sdr/ASOA2015063013196), Jun 2, 2015: CROSSBEAM. CORRODED. CORROSION ON CROSSBEAM AT FS 589.00 BETWEEN RBL 9 & LBL 9. BLENDED CORROSION. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-00. .021" MATERIAL REMOVED. REPLACEMENT RE All 162: https://openairdocs.org/deregistered/N884AS-2019-11-26/reports.md ## Other aircraft with N884AS - [Registered now](https://openairdocs.org/aircraft/N884AS): Ea Vision EA J100, S/N EAVUAV502585754 --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.