# N983CA: 1997 Canadair CL-600-2B19, registration cancelled 2017-06-08

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: June 8, 2017
- Status when cancelled: Valid registration
- 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: 7169
- Year built: 1997
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: July 7, 1997
- Certificate issued: February 14, 2008
- Last registry action: August 10, 2016
- Mode S code: ADB67C
- 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/N983CA
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=983CA
- Page: https://openairdocs.org/deregistered/N983CA-2017-06-08

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 Canadair CL-600-2B19: https://openairdocs.org/model/canadair-cl-600-2b19.md

## Service difficulty reports (167, newest 50)

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

- [SDR SWIA201440173](https://openairdocs.org/sdr/SWIA201440173), Nov 26, 2014: WIRE HARNESS. FAULTY. WOW INPUT CAUTION MESSAGE RECEIVED DURING GEAR RETRACTION. MESSAGE DISAPPEARED AFTER LANDING GEAR REACHED SELECTED POSITION. FLT 2378. REPLACED RT OTBD MAIN HAR
- [SDR SWIA201440003](https://openairdocs.org/sdr/SWIA201440003), Nov 18, 2014: PCU. FAILED. DIVERTED DUE TO HYD 2A LOW PRESSURE CAUTION AT CRUISE. R & R PCU ASSY IAW AMM. OPS CHECK GOOD, NO LEAKING NOTED.
- [SDR SWIA201439644](https://openairdocs.org/sdr/SWIA201439644), Oct 12, 2014: SEAT TRACK. DAMAGED. RT SIDE AFT SEAT TRACK HAS DAMAGE BS 559.0+54. C-CHECK, THE DAMAGE WAS TRIMMED, NDT ENSURED A CRACK FREE CONDITION, AND THE REWORKED AREA WAS RESTORED TO MATCH 
- [SDR SWIA201439651](https://openairdocs.org/sdr/SWIA201439651), Oct 10, 2014: FLOOR SUPPORT. CORRODED. FLOOR SUPPORT UPPER CAP AT LBL 9 BS 569-619. C-CHECK, REPLACED THE FLOOR SUPPORT IAW SRM AND REO.
- [SDR SWIA201439650](https://openairdocs.org/sdr/SWIA201439650), Oct 10, 2014: FLOOR SUPPORT. CORRODED. FLOOR SUPPORT UPPER CAP AT LBL 27 BS 569-619. C-CHECK, REPLACED THE FLOOR SUPPORT IAW REO.
- [SDR SWIA201439649](https://openairdocs.org/sdr/SWIA201439649), Oct 8, 2014: STRAP. CORRODED. FLOOR STRAP AT BS 310 TO 280, LBL 36 CORROSION OUT OF LIMITS. C-CHECK, REMOVED AND INSTALLED NEW FABRICATED FLOOR CAP STRAP, PN: 601R38670-55 IAW SRM.
- [SDR SWIA201439660](https://openairdocs.org/sdr/SWIA201439660), Oct 7, 2014: SKIN. CHAFED. LT INBD FLAP VANE L/E SKIN OTBD END CHAFED. REPLACED THE SKIN IAW SRM AND REO.
- [SDR SWIA201439659](https://openairdocs.org/sdr/SWIA201439659), Oct 7, 2014: SKIN. CHAFED. LT INB FLAP VANE L/E SKIN AT INBD END CHAFED. REPLACED THE SKIN IAW SRM AND REO.
- [SDR SWIA201439658](https://openairdocs.org/sdr/SWIA201439658), Oct 7, 2014: SKIN. CHAFED. LT INBD FLAP VANE L/E SKIN CHAFED. REPLACED THE SKIN IAW REO.
- [SDR SWIA201439664](https://openairdocs.org/sdr/SWIA201439664), Oct 6, 2014: FLOOR SUPPORT. CORRODED. UPPER FLOOR SUPPORT AT FS 609 AND 603, LBL 9 HAS CORROSION AT NUTPLATE LOCATIONS. C-CHECK, RO: 10/21/2014, REPLACED FLOOR SUPPORT UPPER CAP ANGLE AT LBL 9 FS 56
- [SDR SWIA201439663](https://openairdocs.org/sdr/SWIA201439663), Oct 6, 2014: SUPPORT. MECHANIC ERROR. RIGHT WING L/E SUPPORT STRUCTURE DAMAGED AT TACK RIVET LOCATIONS AT WS 341, UPPER AND LOWER SUPPORT FLANGE. C-CHECK, PERFORMED PERMANENT REPAIR ON RT WING L/E S
- [SDR SWIA201439662](https://openairdocs.org/sdr/SWIA201439662), Oct 6, 2014: HINGE. GOUGED. PASSENGER DOOR PIANO HINGE HALF ON DOOR SIDE HAS GOUGES AT LUGS NR 8, NR 10 AND LAST LUG, FROM FWD TO AFT OF ACFT. REPAIRED IAW REO.
- [SDR SWIA201439655](https://openairdocs.org/sdr/SWIA201439655), Oct 6, 2014: BULKHEAD WEB. CRACKED. BS 621, BULKHEAD WEB HAS CRACK AT LBL 27.5 AT TOP OF CARGO DOOR TRACK. C-CHECK, REPAIRED IAW REO.
- [SDR SWIA201439654](https://openairdocs.org/sdr/SWIA201439654), Oct 6, 2014: BULKHEAD WEB. CRACKED. BS 621, BULKHEAD WEB HAS TWO CRACKS AT RBL 27.5. C-CHECK, REPAIRED IAW REO.
- [SDR SWIA201439653](https://openairdocs.org/sdr/SWIA201439653), Oct 6, 2014: STIFFENER. CRACKED. BS 409+128 VERTICAL POST AT RBL 18.0 IS CRACKED ON INBD AFT RADIUS. C-CHECK, R & R THE POST IAW SRM.
- [SDR SWIA201439652](https://openairdocs.org/sdr/SWIA201439652), Oct 6, 2014: STIFFENER. CRACKED. FS 409 +128 VERTICAL POST AT BL 0 IS CRACKED ON LT SIDE AFT RADIUS. C-CHECK, R & R VERTICAL POST IAW REO.
- [SDR SWIA201439648](https://openairdocs.org/sdr/SWIA201439648), Oct 6, 2014: DOOR SILL. CRACKED. AFT CARGO DOOR SILL CRACKED. C-CHECK, REPAIRED IAW REO.
- [SDR SWIA201439647](https://openairdocs.org/sdr/SWIA201439647), Oct 6, 2014: FRAME. CRACKED. AFT CARGO BAY AT BS 605, STRINGER 9 LT SIDE ABOVE CARGO DOOR CUTOUT. FRAME IS CRACKED AT RADIUS. C-CHECK, REPAIRED THE FRAME IAW REO.
- [SDR SWIA201439657](https://openairdocs.org/sdr/SWIA201439657), Oct 5, 2014: SKIN. CHAFED. LEFT AILERON LOWER L/E SKIN CHAFED AT OTBD END. C-CHECK, BLENDED LT AILERON LOWER L/E SKIN IAW REO.
- [SDR SWIA201439661](https://openairdocs.org/sdr/SWIA201439661), Oct 4, 2014: SKIN. CHAFED. RT AILERON PANEL 699AB IS CHAFED. DRILLED AND LOCATED NEW AILERON LOWER SKIN PANEL IAW REO.
- [SDR SWIA201439656](https://openairdocs.org/sdr/SWIA201439656), Oct 4, 2014: SKIN. GOUGED. GOUGE IN PANEL 599AB. C-CHECK, BLENDED LT AILERON LOWER L/E SKIN 559AB IAW REO.
- [SDR SWIA201439646](https://openairdocs.org/sdr/SWIA201439646), Oct 4, 2014: SKIN. DENTED. LEFT SIDE FUSELAGE SKIN AT BS 409 JUST BELOW STRINGER 16L IS DENTED. C-CHECK, REWORKED IAW EA.
- [SDR SWIA201439645](https://openairdocs.org/sdr/SWIA201439645), Oct 4, 2014: SKIN. DENTED. DENT FOUND ON PAX DOOR OUTER SKIN. C-CHECK, REWORKED IAW EA.
- [SDR SWIA2014061738200](https://openairdocs.org/sdr/SWIA2014061738200), Jun 13, 2014: TILLER. FAILED. DURING FLIGHT, STEERING INOPERATIVE MESSAGE ILLUMINATED. RAN QRH THREE TIMES. MESSAGE PERSISTS. RETURN TO DEPARTURE. ON LANDING GEAR DOWN LANDING CHECK TRIED 1 
- [SDR SWIA201437761](https://openairdocs.org/sdr/SWIA201437761), May 28, 2014: WIRE. BROKEN. INTERIOR EMERGENCY LIGHT ON FWD WINDSCREEN INOPERATIVE. REPAIRED BROKEN WIRE ON FWD WINDSCREEN EMERGENCY LIGHT.
- [SDR SWIA201436660](https://openairdocs.org/sdr/SWIA201436660), Mar 8, 2014: CHARGER. FAILED. EMERGENCY EXIT ROW SIDE WALL LIGHT DOES NOT ILLUMINATE. FLT 5571 REPLACED AFT BATTERY CHARGER & BATTERY, PN AD-2013-1A, SN ON 67803 & SN OFF 64830.
- [SDR SWIA201436659](https://openairdocs.org/sdr/SWIA201436659), Mar 7, 2014: BATTERY PACK. DISCHARGED. MULTIPLE EMERGENCY LIGHTS NOT WORKING. REPLACED ALL FOUR BATTERY SUPPLY PACKS & REPLACED NR 1 & NR 3 BATTERY CHARGER, PN AD-2013-1A, SN ON 64830, SN OFF 99705, 
- [SDR SWIA201436578](https://openairdocs.org/sdr/SWIA201436578), Feb 27, 2014: LIGHT. INOPERATIVE. EMERGENCY EXIT AT MIDDLE OF CABIN HAS BURNED OUT LIGHT BULB. FLT 6495 RELAMPED.
- [SDR SWIA201436369](https://openairdocs.org/sdr/SWIA201436369), Feb 18, 2014: BULKHEAD. GOUGED. BULKHEAD 621 IN AFT EQUIPMENT BAY Z MEMBER HAS A GOUGE APPROXIMATELY 8 INCHES DOWN FROM TOP, MEASURES 0.32 INCHES X 0.4 INCHES WITH A DEPTH OF .027 INCHES. C-CH
- [SDR SWIA201436251](https://openairdocs.org/sdr/SWIA201436251), Feb 2, 2014: BATTERY. DISCHARGED. OVERHEAD CEILING EMERGENCY EXIT FWD SIGN DOES NOT ILLUMINATE. FLT 5482 CHARGED BATTERY & ALL EMERGENCY LIGHTS ARE OPERATIVE.
- [SDR SWIA201436121](https://openairdocs.org/sdr/SWIA201436121), Jan 24, 2014: LIGHT. INOPERATIVE. LAST OVERHEAD EMERGENCY LIGHT IS BURNED OUT. FLT 5621 RELAMPED.
- [SDR SWIA201436050](https://openairdocs.org/sdr/SWIA201436050), Jan 17, 2014: LIGHT. INOPERATIVE. NR 3 EMERGENCY OVERHEAD LIGHT IS BURNED OUT. FLT 6426 RELAMPED.
- [SDR SWIA201436028](https://openairdocs.org/sdr/SWIA201436028), Jan 15, 2014: LIGHT. INOPERATIVE. EMERGENCY EXIT SIGN ABOVE ROW 8 IS BURNED OUT. FLT 6372 RELAMPED.
- [SDR SWIA201435924](https://openairdocs.org/sdr/SWIA201435924), Jan 2, 2014: LIGHT. INOPERATIVE. NR 3 EMERGENCY OVERHEAD LIGHT IS BURNED OUT. FLT 5412 RELAMPED.
- [SDR SWIA201335508](https://openairdocs.org/sdr/SWIA201335508), Dec 4, 2013: BATTERY PACK. DISCHARGED. NR 3 EMERGENCY OVERHEAD LIGHT & EMERGENCY OVERHEAD EXIT SIGN AT ROW 8 DO NOT ILLUMINATE. FLT 6394 ALLOWED ELBP TO CHARGE 7 WARM UP.
- [SDR SWIA201334845](https://openairdocs.org/sdr/SWIA201334845), Oct 7, 2013: LIGHT. INOPERATIVE. NR 4 EMERGENCY OVERHEAD LIGHT IS BURNED OUT. FLT#5622 RELAMPED.
- [SDR SWIA201333544](https://openairdocs.org/sdr/SWIA201333544), May 23, 2013: BRACKET. FAILED. NOSE DOOR AND GEAR DISAGREE WARNING MESSAGES, FOLLOWED QRH AND MANUALLY EXTENDED GEAR. REPLACED THE NLG LOWER AFT WEIGHT OFF WHEELS SENSOR BRACKET AND ADJUSTED 
- [SDR SWIA201333524](https://openairdocs.org/sdr/SWIA201333524), May 22, 2013: WIRE HARNESS. FAILED. NOSE-GEAR UP DISAGREE MASTER WARNING. REPLACED NR 1 DOWNLOCK, NLG HARNESS IAW AMM. PERFORMED GEAR SWINGS. OPS CHECK GOOD, PN: 17300-253.
- [SDR SWIA201333178](https://openairdocs.org/sdr/SWIA201333178), Apr 8, 2013: DOOR SEAL. COLLAPSED. LOSS OF PRESSURIZATION DUE TO PORTION OF PAX DOOR SEAL COLLAPSING. (FLT 6266) REPLACED PAX DOOR SEAL. LEAK CHECKS AND OPS CHECKS GOOD.
- [SDR SWIA201333146](https://openairdocs.org/sdr/SWIA201333146), Apr 2, 2013: WIRE HARNESS. FAILED. RECEIVED GEAR DISAGREE WARNING MESSAGE SHOWING NOSE GEAR HASH MARKS. (FLT 6367) REPLACED NR 1 DOWNLOCK PROX SENSOR NLG HARNESS IAW AMM. GEAR SWINGS NORMALLY.
- [SDR SWIA201332951](https://openairdocs.org/sdr/SWIA201332951), Mar 5, 2013: BATTERY PACK. DISCHARGED. UPPER EMERGENCY EXIT SIGN AT ROW 8 CD AND LOWER EMERGENCY EXIT SIGN IN ROW 8 A/B DO NOT ILLUMINATE. (FLT 6369) FOUND BATTERY PACK FOR EMERGENCY LIGHTS ON OVERWI
- [SDR SWIA201332900](https://openairdocs.org/sdr/SWIA201332900), Feb 15, 2013: FLOOR SUPPORT. CRACKED. FS 621 LEFT FLOOR SUPPORT ANGLE IS CRACKED JUST I/B OF CARGO SILL. (C-CHECK) REPLACED THE LEFT CARGO FLOOR SUPPORT ANGLE AT FS 621 IAW REO.
- [SDR SWIA201332905](https://openairdocs.org/sdr/SWIA201332905), Feb 8, 2013: STRUCTURE. CRACKED. LEFT ENGINE PYLON TRAILING EDGE HAS CRACK AND DELAMINATION. (C-CHECK) REPAIRED CRACK AND DELAMINATION AT LEFT ENGINE PYLON TRAILING EDGE IAW STS EA.
- [SDR SWIA201332901](https://openairdocs.org/sdr/SWIA201332901), Feb 8, 2013: POST. CRACKED. CRACK NOTED AND MARKED IN FS 409+128 VERTICAL POST AT RBL 18, O/B C-CHANNEL IN AFT RADIUS. (C-CHECK) REMOVED AND REPLACED VERTICAL POST O/B SIDE AT FS 409+128 R
- [SDR SWIA201332547](https://openairdocs.org/sdr/SWIA201332547), Jan 10, 2013: ARM. OUT OF ADJUST. UPON ARRIVAL, COULD NOT OPEN THE MAIN CABIN DOOR. (FLT 5311) ADJUSTED INNER RELEASE ARM POWER TENSION AND INSPECTED OUTER HANDLE LINKAGES WITH NO FURTHER DEFECT
- [SDR SWIA201232503](https://openairdocs.org/sdr/SWIA201232503), Dec 31, 2012: HANDLE. JAMMED. CANNOT OPEN THE MAIN CABIN DOOR FROM THE OUTSIDE. (FLT 5349) OPENED PAX DOOR IAW AMM. AFTER INITIAL ATTEMPT DOOR HANDLE NO LONGER JAMMED. OP CHECK NORMAL UPON N
- [SDR SWIA201232282](https://openairdocs.org/sdr/SWIA201232282), Dec 3, 2012: LIGHT. INOPERATIVE. EMERGENCY OVERHEAD LIGHT 1 AND 2, AND EMERGENCY FLOOR LIGHT 8A BURNED OUT. (FLT 5393) RELAMPED EMERGENCY.
- [SDR SWIA201232157](https://openairdocs.org/sdr/SWIA201232157), Nov 12, 2012: STRUT. FAILED. GEAR DISAGREE WARNING MESSAGE WITH NOSE WHEEL REMAINING IN DOWN AND LOCKED POSITION. WOW INPUT CAUTION MESSAGE APPEARED AS WELL. (FLT 5412) REMOVED AND REPLACED
- [SDR SWIA201231954](https://openairdocs.org/sdr/SWIA201231954), Oct 12, 2012: ANTENNA. FAILED. CAPTAIN'S RADIO ALTIMETER AND FIRST OFFICER'S RADIO ALTIMETER DIFFER MORE THAN 300 FEET FROM 2500 FEET. (FLT 5565) REPLACED THE F/O'S RECEIVE ANTENNA IN REFEREN
- [SDR SWIA201231779](https://openairdocs.org/sdr/SWIA201231779), Sep 12, 2012: WIRE HARNESS. FAILED. GEAR DISAGREE WARNING MESSAGE ASSOCIATED WITH YELLOW INDICATION FOR NOSE GEAR. (FLT 5310) REPLACED NLG DOWNLOCK NR 1 HARNESS (PSIGA) ASSEMBLY IN REFERENCE TO AM

All 167: https://openairdocs.org/deregistered/N983CA-2017-06-08/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 19980713023159I](https://openairdocs.org/incident/19980713023159I), Jul 13, 1998: Cndair CL6002B19 (N983CA), Rochester, NY. Precautionary landing roc due hydraulic problem. Low pressure. Hydraulic flex line leaking at fuselage nacelle.

## Other aircraft with N983CA

- [Registered now](https://openairdocs.org/aircraft/N983CA): Embraer-Empresa Brasileira De EMB-500, S/N 50000029, built 2009

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