# N821AS: 1997 Canadair CL-600-2B19, registration cancelled 2017-06-08 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: June 8, 2017 - Status when cancelled: Registration expired - Airframe: [Canadair CL-600-2B19](https://openairdocs.org/model/canadair-cl-600-2b19) (registry code 1900309) - 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: 7194 - Year built: 1997 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: September 26, 1997 - Certificate issued: May 9, 2014 - Last registry action: May 9, 2014 - Mode S code: AB34A3 - 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/N821AS - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=821AS - Page: https://openairdocs.org/deregistered/N821AS-2017-06-08 From the FAA registry file of October 28, 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 Canadair CL-600-2B19: https://openairdocs.org/model/canadair-cl-600-2b19.md ## Service difficulty reports (187, newest 50) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR SWIA201642369](https://openairdocs.org/sdr/SWIA201642369), Jul 28, 2016: WARNING MESSAGE. ILLUMINATED. AIRCRAFT RETURNED TO THE FIELD WITH A GEAR DISAGREE MESSAGE. - [SDR SWIA201541566](https://openairdocs.org/sdr/SWIA201541566), Nov 16, 2015: SENSOR. OUT OF ADJUST. NOSE DOOR OPEN, GEAR DISAGREE WARNING MESSAGE, AFTER GEAR IS SELECTED UP, PERFORMED QRH, MESSAGES CLEARED, RETURNED TO FIELD. ADJUSTED WOW SENSOR. SWUNG GEAR MU - [SDR SWIA2014121940422](https://openairdocs.org/sdr/SWIA2014121940422), Dec 18, 2014: LINE. FAILED. DURING CLIMBOUT, NR 2 ENGINE ROLLED BACK TO IDLE. RETURNED TO FIELD. R & R RT ENGINE P3 LINE TO FUEL CONTROL TUBE ASSEMBLY WITH A SERVICEABLE UNIT IAW AMM. OPS - [SDR SWIA201440083](https://openairdocs.org/sdr/SWIA201440083), Nov 22, 2014: TUBE. BROKEN. PAX DOOR WIRE HARNESS UNDER TOP STEP HAS BROKEN TUBING, REPAIRED THE TUBING IAW GREO. - [SDR SWIA201440081](https://openairdocs.org/sdr/SWIA201440081), Nov 10, 2014: HINGE. GOUGED. PASSENGER DOOR HINGE HALF LUG NR 27 FROM FORWARD SIDE HAS GOUGES. REPAIRED THE HINGE LUG IAW REO. - [SDR SWIA201440079](https://openairdocs.org/sdr/SWIA201440079), Nov 10, 2014: HINGE. GOUGED. PASSENGER DOOR FUSELAGE SIDE HINGE HALF 6TH AND 8TH LUG FROM FORWARD SIDE HAVE GOUGES. BLENDED GOUGE ON PAX DOOR HINGE LUGS NR 6 AND NR 8 IAW REO. - [SDR SWIA201440078](https://openairdocs.org/sdr/SWIA201440078), Nov 10, 2014: STRUCTURE. CRACKED. AFT CARGO BAY AT BS 605 HAS A CRACK AT CARGO DOOR. PERFORMED CUT OUT OF DAMAGED AREA ON FLOOR LANDING PLATE AT FS 605.0, REF REO. PERFORMED ET INSP ON REWORKED - [SDR SWIA201440076](https://openairdocs.org/sdr/SWIA201440076), Nov 10, 2014: ANGLE. CRACKED. LBL 9, BS 280 INBD ANGLE IS CRACKED AT UPPER RADIUS. INSTALLED FABRICATED INBD ANGLE IAW REO. - [SDR SWIA201440075](https://openairdocs.org/sdr/SWIA201440075), Nov 9, 2014: ANGLE. CRACKED. BS 280, RBL 9.0 INBD AND OTBD ANGELS ARE CRACKED AT UPPER RADIUS. R & R THE ANGLES IAW REO. - [SDR SWIA201440073](https://openairdocs.org/sdr/SWIA201440073), Nov 9, 2014: LEVER. WORN. PASSENGER DOOR FORWARD PULL IN LEVER LOBE WORN. REPAIRED IAW REO. - [SDR SWIA201440069](https://openairdocs.org/sdr/SWIA201440069), Nov 9, 2014: FLOOR SKIN. CRACKED. TRU BAY FLOOR SKIN IS CRACKED AT BS 193. REPAIRED TRU BAY FLOOR SKIN IAW REO. - [SDR SWIA201440067](https://openairdocs.org/sdr/SWIA201440067), Nov 9, 2014: BULKHEAD. CRACKED. BS 202 BULKHEAD IS CRACKED AT THE PARKING BRAKE CABLE PASSTHROUGH HOLE. REPAIRED THE BULKHEAD IAW REO. - [SDR SWIA201440066](https://openairdocs.org/sdr/SWIA201440066), Nov 9, 2014: ATTACH ANGLE. CRACKED. CRACKED ATTACH ANGLE STRINGER TO BS 202 BULKHEAD IN AFT LOWER AREA OF NOSE HYDRAULIC COMPARTMENT. R & R ATTACH ANGLE IAW SRM AND EA. - [SDR SWIA201440064](https://openairdocs.org/sdr/SWIA201440064), Nov 8, 2014: STRUCTURE. CORRODED. CORROSION AROUND NUTPLATE HOLE UNDER PANEL 141BL. C-CHECK, REPAIRED IAW REO. - [SDR SWIA201440062](https://openairdocs.org/sdr/SWIA201440062), Nov 8, 2014: FITTING. CHAFED. RIGHT ENGINE THRUST REVERSER HAS BOTTOM INBD MAIN TRACK AFT END FITTING CHAFED, UPPER SIDE. REPAIRED THE THRUST REVERSER INBD LOWER MAIN TRACK AND ANCHOR FITTIN - [SDR SWIA201440061](https://openairdocs.org/sdr/SWIA201440061), Nov 8, 2014: ATTACH FITTING. CHAFED. RIGHT MLG STRUT TO BELLCRANK ATTACHMENT POINT CHAFED. REMOVED AND INSTALLED BOLT ATTACHING RT MLG BELLCRANK TO THE ROD IAW SRM. BLENDED CHAFE DAMAGE ON RT MLG B - [SDR SWIA201440057](https://openairdocs.org/sdr/SWIA201440057), Nov 8, 2014: ATTACH FITTING. CHAFED. LEFT MLG STRUT TO BELLCRANK ATTACHMENT POINT CHAFED. REMOVED AND INSTALLED SCREW ATTACHING BELLCRANK TO THE ROD IAW SRM 51-41-02. BLENDED CHAFE DAMAGE ON LT MLG - [SDR SWIA201440056](https://openairdocs.org/sdr/SWIA201440056), Nov 8, 2014: PANEL. CRACKED. COCKPIT PANEL 221ALC CRACKED & BROKEN IN MULTIPLE PLACES. REPAIRED DAMAGED AREAS ON PANEL IAW EA. - [SDR SWIA201440055](https://openairdocs.org/sdr/SWIA201440055), Nov 8, 2014: PANEL. CHAFED. RIGHT WING BUTTE PANEL 694PB HAS CHAFE DAMAGE ON UPPER SURFACE. REPAIRED PANEL IAW EA. - [SDR SWIA201440054](https://openairdocs.org/sdr/SWIA201440054), Nov 8, 2014: SKIN. DENTED. RIGHT WING INBD GROUND SPOILER HAS MULTIPLE SMALL DENTS ON LOWER SURFACE. DENTS ARE WITHIN ALLOWABLE LIMITS, NO FURTHER ACTION REQUIRED, REF REO. - [SDR SWIA201440053](https://openairdocs.org/sdr/SWIA201440053), Nov 7, 2014: PANEL. FAILED. LEFT UPPER VISOR PANEL 326AL, FAILED GAP CHECK. REPAIR VISOR PANEL IAW REO. - [SDR SWIA201440052](https://openairdocs.org/sdr/SWIA201440052), Nov 7, 2014: PANEL. FAILED. RIGHT UPPER VISOR PANEL 326AR FAILED GAP CHECK. REPAIR VISOR PANEL 326AR IAW REO. - [SDR SWIA201440051](https://openairdocs.org/sdr/SWIA201440051), Nov 7, 2014: SKIN. CHAFED. CARGO BAY DOOR EXTERIOR SKIN HAS SIX CHAFES AROUND THE RIM OF THE DOOR HANDLE. R & R THE DOOR HANDLE ASSY IAW SRM. PERFORMED OPS CHECK OF THE CARGO DOOR WARNING - [SDR SWIA201440050](https://openairdocs.org/sdr/SWIA201440050), Nov 6, 2014: VANE. CRACKED. BOTTOM VANE OF APU EXHAUST OUTLET IS CRACKED. REPAIED IAW REO. - [SDR SWIA201440049](https://openairdocs.org/sdr/SWIA201440049), Nov 6, 2014: STRUCTURE. ERODED. FOUND EROSION ON THE LT ENGINE NOSE COWL, 6 O'CLOCK POSITION, TO BE WITHIN LIMITS. REPAIRED IAW CMM AND REO. - [SDR SWIA201438520](https://openairdocs.org/sdr/SWIA201438520), Jul 2, 2014: FIRE BOTTLE. DISCHARGED. IN FLIGHT GOT CARGO BOTTLE LOW MESSAGE. RETURNED TO DEPARTURE. R & R LT CARGO BOTTLE. - [SDR SWIA201438423](https://openairdocs.org/sdr/SWIA201438423), Jun 25, 2014: LINE. BLOWN. RETURNED TO FIELD WITH A BLOWN FIRE BOTTLE. REINSTALLED A DISCONNECTED LINE BLOWING HOT AIR ON THE FIRE BOTTLE. - [SDR SWIA201438299](https://openairdocs.org/sdr/SWIA201438299), Jun 21, 2014: FIRE BOTTLE. FAILED. CARGO BOTTLE LOW MESSAGE. REPLACED THE SMALL CARGO FIRE BOTTLE. - [SDR SWIA201437412](https://openairdocs.org/sdr/SWIA201437412), May 5, 2014: O-RING. LEAKING. WITH PACKS ON, APU STRONG FUEL ODOR THROUGHOUT FLIGHT DECK AND CABIN. WITH PACKS ON ENGINES ODOR DIMINISHES. REPLACED O-RING ON FUEL CONTROL ELBOW TO FUEL SOLEN - [SDR SWIA201436226](https://openairdocs.org/sdr/SWIA201436226), Feb 4, 2014: LIGHT. INOPERATIVE. LOWER EXIT LIGHTS ON MAIN CABIN DOOR & GALLEY SERVICE DOOR ARE BURNED OUT. FLT 2938 RELAMPED. - [SDR SWIA201335501](https://openairdocs.org/sdr/SWIA201335501), Dec 6, 2013: BATTERY PACK. DISCHARGED. EMERGENCY LIGHTS DO NOT ILLUMINATE. FLT 2971 CHARGED EMERGENCY LIGHTS BATTERY PACKS. - [SDR SWIA201333514](https://openairdocs.org/sdr/SWIA201333514), May 20, 2013: WIRE. OUT OF POSITION. EMERGENCY EXIT LIGHT NEAR MAIN CABIN DOOR DOES NOT ILLUMINATE. REPOSITIONED WIRES BEHIND EMERGENCY LIGHT. - [SDR SWIA201333466](https://openairdocs.org/sdr/SWIA201333466), May 12, 2013: PROXIMITY SWITCH. FAILED. RECEIVED PASSENGER DOOR OUTER HANDLE CAUTION MESSAGE. REPLACED PROXIMITY SWITCH. OPS CHECKED GOOD. - [SDR SWIA201333224](https://openairdocs.org/sdr/SWIA201333224), Apr 9, 2013: UNKNOWN. FUMES. SMELLING FUMES IN CABIN. (FLT 2980) INSPECTED APU ENCLOSURE. BOTH AC PACKS HAVE NORMAL INDICATION WITH NO SIGNS OF OVERHEATING. NO SMOKE SMELLS NOTED. - [SDR SWIA201333114](https://openairdocs.org/sdr/SWIA201333114), Mar 31, 2013: FAN. MALFUNCTIONED. ELECTRICAL SMOKE SMELL COMING FROM GALLEY A/C VENT. NO SMOKE AND NO PAX ON BOARD. (FLT 2962) REPLACED GALLEY EXHAUST FAN. OPS CHECK GOOD AT THIS TIME. P/N ON: A - [SDR SWIA201332822](https://openairdocs.org/sdr/SWIA201332822), Feb 17, 2013: LIGHT. INOPERATIVE. OVERHEAD EMERGENCY EXIT ROW LIGHT BURNED OUT. (FLT 2850) RELAMPED EMERGENCY LIGHT. - [SDR SWIA201332771](https://openairdocs.org/sdr/SWIA201332771), Feb 7, 2013: BRAKE. SEIZED. LEFT MAIN BRAKE SEIZED. (FLT 2988) REPLACED NR 1 MLG WHEEL ASSEMBLY, RE-INSTALLED QUICK DISCONNECT. P/N 501071-1 S/N ON FEB01-3686 S/N OFF APR97-1354 P/N 501052 - [SDR SWIA201232667](https://openairdocs.org/sdr/SWIA201232667), Dec 30, 2012: FLOOR SUPPORT. CORRODED. FLOOR SUPPORT AT FS 621 LBL 9 UNDER FLOORBOARD 281JLF HAS FRETTING CORROSION. (C-CHECK) INSTALLED NEW FLOOR SUPPORT AT LBL 9 FS 574-621 IAW REO. - [SDR SWIA201232666](https://openairdocs.org/sdr/SWIA201232666), Dec 30, 2012: ACCESS PANEL. CORRODED. RIGHT WING ACCESS PANEL 650HB HOLE HAS SIGNS OF CORROSION IN SEVERAL AREAS. (C-CHECK) CORROSION AT LOWER WING PLANK COMMON TO PANEL 650HB REPAIRED IAW REO. - [SDR SWIA201232665](https://openairdocs.org/sdr/SWIA201232665), Dec 30, 2012: ACCESS PANEL. CORRODED. RIGHT WING ACCESS PANEL 650BB HOLE HAS SIGNS OF CORROSION IN SEVERAL AREAS. (C-CHECK) LOWER WING PLANK CUTOUT COMMON TO PANEL 650BB REPAIRED IAW REO. - [SDR SWIA201232664](https://openairdocs.org/sdr/SWIA201232664), Dec 30, 2012: ACCESS PANEL. CORRODED. RIGHT WING ACCESS PANEL 640FB HOLE HAS SIGNS OF CORROSION IN SEVERAL AREAS. (C-CHECK) RIGHT LOWER WING PLANK CUTOUT COMMON TO PANEL 640FB REWORKED IAW REO. - [SDR SWIA201232663](https://openairdocs.org/sdr/SWIA201232663), Dec 30, 2012: ACCESS PANEL. CORRODED. RIGHT WING ACCESS PANEL 640DB HOLE HAS SIGNS OF CORROSION IN SEVERAL AREAS. (C-CHECK) RIGHT LOWER WING PLANK CUTOUT COMMON TO PANEL 640DB REWORKED IAW REO. - [SDR SWIA201232662](https://openairdocs.org/sdr/SWIA201232662), Dec 30, 2012: ACCESS PANEL. CORRODED. RIGHT WING ACCESS PANEL 640AB HOLE HAS SIGNS OF CORROSION IN SEVERAL AREAS. (C-CHECK) RIGHT LOWER WING PLANK ACCESS PANEL CUTOUT COMMON TO PANEL 640AB REWORKED - [SDR SWIA201232661](https://openairdocs.org/sdr/SWIA201232661), Dec 30, 2012: ACCESS PANEL. CORRODED. RIGHT WING ACCESS PANEL 640BB HOLE HAS SIGNS OF CORROSION IN SEVERAL AREAS. (C-CHECK) LOWER WING PLANK COMMON TO PANEL 640BB REPAIRED IAW REO. - [SDR SWIA201232660](https://openairdocs.org/sdr/SWIA201232660), Dec 30, 2012: ACCESS PANEL. CORRODED. LEFT WING ACCESS PANEL 550HB HOLE HAS SIGNS OF CORROSION IN SEVERAL AREAS. (C-CHECK) LOWER WING PLANK CUTOUT COMMON TO PANEL 550HB REPAIRED IAW REO. - [SDR SWIA201232659](https://openairdocs.org/sdr/SWIA201232659), Dec 30, 2012: ACCESS PANEL. CORRODED. LEFT WING ACCESS PANEL 550AB HOLE HAS SIGNS OF CORROSION IN SEVERAL AREAS. (C-CHECK) LEFT LOWER WING PLANK COMMON TO ACCESS PANEL 550AB REWORKED IAW REO. - [SDR SWIA201232658](https://openairdocs.org/sdr/SWIA201232658), Dec 30, 2012: ACCESS PANEL. CORRODED. LEFT WING ACCESS PANEL 540EB HOLE HAS SIGNS OF CORROSION IN SEVERAL AREAS. (C-CHECK) LOWER WING PLANK CUTOUT COMMON TO PANEL 540EB REWORKED IAW REO. - [SDR SWIA201232657](https://openairdocs.org/sdr/SWIA201232657), Dec 30, 2012: ACCESS PANEL. CORRODED. LEFT WING ACCESS PANEL 540BB HOLE HAS SIGNS OF CORROSION IN SEVERAL AREAS. (C-CHECK) MARKED AREAS OF LOWER WING PLANK COMMON TO PANEL 540BB REWORKED IAW REO. - [SDR SWIA201232656](https://openairdocs.org/sdr/SWIA201232656), Dec 30, 2012: ACCESS PANEL. CRACKED. LEFT WING ACCESS PANEL 510AB HOLE HAS SIGNS OF CORROSION IN SEVERAL AREAS. (C-CHECK) LOWER WING PLANK CUTOUT COMMON TO PANEL 510AB REWORKED IAW REO. - [SDR SWIA201232655](https://openairdocs.org/sdr/SWIA201232655), Dec 28, 2012: BULKHEAD. CRACKED. CRACK NOTED AND MARKED ON FS 621 BULKHEAD WEB, FWD FACE, ABOVE UPPER CARGO DOOR TRACK FITTING. (C-CHECK) REPAIRED FS 621 BULKHEAD WEB, FWD FACE, ABOVE UPPER CAR All 187: https://openairdocs.org/deregistered/N821AS-2017-06-08/reports.md ## Other aircraft with N821AS - [Registered now](https://openairdocs.org/aircraft/N821AS): Samuel Russell S-21 OUTBOUND, S/N 12200153, built 2025 --- 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.