# N984CA: 1997 Canadair CL-600-2B19, registration cancelled 2017-05-03

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: May 3, 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: 7171
- Year built: 1997
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: June 30, 1997
- Certificate issued: February 5, 2008
- Last registry action: August 10, 2016
- Mode S code: ADBA33
- 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/N984CA
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=984CA
- Page: https://openairdocs.org/deregistered/N984CA-2017-05-03

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 (174, newest 50)

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

- [SDR SWIA201641882](https://openairdocs.org/sdr/SWIA201641882), Feb 12, 2016: RESERVOIR. FAILED. RETURNED TO DEPARTURE, DUE TO A GEAR DISAGREE. R & R NR 3 HYDRAULIC RESERVOIR IAW AMM. OPS CHECKS GOOD, NO LEAKS NOTED.
- [SDR SWIA201540793](https://openairdocs.org/sdr/SWIA201540793), Feb 27, 2015: WATER SEPARATOR. CONTAMINATED. RETURNED TO THE FIELD FOR SMOKE IN THE LAV. CREW REPORTED SMOKE COMING FROM GASPERS. FOUND GLYCOL IN WATER SEPARATOR. REPLACED NR 1AND NR 2 WATER SEPARATORS. OP
- [SDR SWIA201440016](https://openairdocs.org/sdr/SWIA201440016), Nov 14, 2014: SKIN. GOUGED. WHILE PERFORMING BLENDING FOR EXTERIOR SKIN GOUGES FOR ADF ANTENNA ON MX TRANS 11509318, DISCOVERED 4 EACH LIGHTNING STRIKES AT ADF ANTENNA MOUNT HOLES. C-CHECK
- [SDR SWIA201440046](https://openairdocs.org/sdr/SWIA201440046), Nov 8, 2014: VANE. CHAFED. LEFT INBD FLAP VANE CHAFED AT OTBD L/E. BLENDED THE CHAFE IAW REO.
- [SDR SWIA201440045](https://openairdocs.org/sdr/SWIA201440045), Nov 8, 2014: VANE. CHAFED. LEFT INBD FLAP VANE CHAFED AT INBD L/E. BLENDED THE CHAFE IAW REO.
- [SDR SWIA201440042](https://openairdocs.org/sdr/SWIA201440042), Nov 8, 2014: HINGE. GOUGED. PASSENGER DOOR HINGE 5TH LUG BACK IS GOUGED ON THE FUSELAGE SIDE. BLENDED AND FOUND WITHIN LIMITS. IAW REO.
- [SDR SWIA201440040](https://openairdocs.org/sdr/SWIA201440040), Nov 8, 2014: SKIN. DEBONDED. RT WING OTBD L/E 630KL IS DEBONDED. BONDED RT WING OTBD L/E, 630KL IAW REO.
- [SDR SWIA201440038](https://openairdocs.org/sdr/SWIA201440038), Nov 8, 2014: SKIN. DEBONDED. RT WING INBD L/E 620JL IS DEBONDED. BONDED RT WING INBD L/E IAW REO.
- [SDR SWIA201440037](https://openairdocs.org/sdr/SWIA201440037), Nov 8, 2014: SEAT TRACK. CORRODED. SEAT TRACK AT RBL 9.0 FROM BS 599 - 599+86 CORRODED. R & R THE SEAT TRACK IAW AMM & REO.
- [SDR SWIA201440035](https://openairdocs.org/sdr/SWIA201440035), Nov 8, 2014: SEAT TRACK. CORRODED. SEAT TRACK AT RBL 9.0 BS 409+126 - 599 HAS CORROSION. R & R SEAT TRACK IAW AMM & REO.
- [SDR SWIA201440034](https://openairdocs.org/sdr/SWIA201440034), Nov 8, 2014: SEAT TRACK. CORRODED. SEAT TRACK AT RBL 9.0 FROM BS 399 - 409+126 HAS CORROSION. R & R SEAT TRACK IAW AMM & REO.
- [SDR SWIA201440033](https://openairdocs.org/sdr/SWIA201440033), Nov 8, 2014: SEAT TRACK. CORRODED. SEAT TRACK AT LBL 9.0 FROM BS 399 - 409+126 HAS CORROSION. R & R SEAT TRACK IAW AMM & REO
- [SDR SWIA201440032](https://openairdocs.org/sdr/SWIA201440032), Nov 8, 2014: PRESSURE DECK. CRACKED. PRESSURE FLOOR AT BS 458 - 462 CRACKED BETWEEN BL 0.0 AND RBL 9.0. REPAIRED IAW REO. PERFORMED PRESSURIZATION CHECK IAW AMM.
- [SDR SWIA201440031](https://openairdocs.org/sdr/SWIA201440031), Nov 8, 2014: PRESSURE DECK. CRACKED. PRESSURE FLOOR AT BS 458 - 462 CRACKED BETWEEN BL 0.0 AND LBL 9.0. REPAIRED IAW REO. PERFORMED PRESSURIZATION CHECK IAW AMM.
- [SDR SWIA201440030](https://openairdocs.org/sdr/SWIA201440030), Nov 8, 2014: BULKHEAD WEB. CRACKED. CRACK AT FWD PRESSURE BULKHEAD WEB COMMON TO PARKING BRAKE FITTING, 3 O'CLOCK POSITION WHEN LOOKING FORWARD, REPAIRED IAW REO. PRESSURE CHECKED GOOD.
- [SDR SWIA201440019](https://openairdocs.org/sdr/SWIA201440019), Nov 8, 2014: BULKHEAD WEB. CRACKED. CRACK NOTED ON FS621 BULKHEAD WEB, FWD FACE, ALONG LBL36.2 AT APPROXIMATELY WL 75 NEAR FLOOR LEVEL. C-CHECK, REPAIRED CRACK IAW REO. PARTS REMOVED WEIGHT 0.01 L
- [SDR SWIA201440018](https://openairdocs.org/sdr/SWIA201440018), Nov 8, 2014: BULKHEAD WEB. CRACKED. CRACK NOTED ON BS 621 BULKHEAD WEB, FWD FACE ALONG BL 0 AT WL 90. C-CHECK. REPAIRED CRACK ON FS 621 BULKHEAD IAW REO. PRESSURE CHECK GOOD. COMPLIED WITH ST 51-9
- [SDR SWIA201440044](https://openairdocs.org/sdr/SWIA201440044), Nov 7, 2014: PANEL. CRACKED. PANEL 221CLC HAS CRACKS AROUND SCREW HOLE. REPAIRED CRACKS AROUND SCREW HOLE ON PANEL IAW EA.
- [SDR SWIA201440043](https://openairdocs.org/sdr/SWIA201440043), Nov 7, 2014: VANE. CHAFED. RIGHT WING INBD FLAP VANE L/E CHAFED 91.5 INCHES FROM OTBD END. BLENDED CHAFE IAW REO.
- [SDR SWIA201440041](https://openairdocs.org/sdr/SWIA201440041), Nov 7, 2014: PANEL. CRACKED. PANEL 222CLC, HAS CRACKS AROUND SCREW HOLE. REPAIRED PANEL IAW EA.
- [SDR SWIA201440039](https://openairdocs.org/sdr/SWIA201440039), Nov 7, 2014: VANE. CHAFED. RIGHT WING INBD FLAP VANE L/E CHAFED 43 INCHES FROM OTBD END. BLENDED CHAFE IAW REO AND SRM. FOUND WITHIN LIMITS IAW REO.
- [SDR SWIA201440036](https://openairdocs.org/sdr/SWIA201440036), Nov 7, 2014: VANE. CHAFED. RIGHT WING INBD FLAP VANE L/E CHAFED 7.5" FROM OTBD END. BLENDED IAW REO. FOUND WITHIN LIMITS IAW REO.
- [SDR SWIA201440028](https://openairdocs.org/sdr/SWIA201440028), Nov 7, 2014: SKIN. DENTED. LEFT INBD FLAP HAS DENT ON LOWER SKIN OUTBD OF PANEL 584AB. REPAIRED IAW EA.
- [SDR SWIA201440024](https://openairdocs.org/sdr/SWIA201440024), Nov 7, 2014: ATTACH FITTING. CHAFED. LEFT MLT DOOR ROD ATTACH LUG ON DOOR IS CHAFED. C-CHECK, R & R THE LT MLG DOOR ATTACHMENT LUG REF SRM & REO.
- [SDR SWIA201440023](https://openairdocs.org/sdr/SWIA201440023), Nov 7, 2014: ROD END. CHAFED. LEFT MLG DOOR ROD END IS CHAFED AT THE BELLCRANK END. R & R THE LT MLG DOOR STRUT IAW AMM, DWG AND REO.
- [SDR SWIA201440022](https://openairdocs.org/sdr/SWIA201440022), Nov 7, 2014: BELLCRANK. CHAFED. LT MLG DOOR BELLCRANK END IS CHAFED AT THE DOOR ROD CONNECTION END. R & R THE LT MLG DOOR BELLCRANK ASSY REF AMM, COMPLIED WITH REO AND DWG.
- [SDR SWIA201440021](https://openairdocs.org/sdr/SWIA201440021), Nov 7, 2014: ROD END. CHAFED. RIGHT MLG DOOR ROD END IS CHAFED AT THE BELLCRANK END. R & R THE RT MLG DOOR STRUT.
- [SDR SWIA201440020](https://openairdocs.org/sdr/SWIA201440020), Nov 7, 2014: BELLCRANK. CHAFED. RT MLG DOOR BELLCRANK END IS CHAFED AT THE DOOR ROD CONNECTION END. C-CHECK, OUT OF LIMITS IAW DWG. R & R RT MLG DOOR BELLCRANK ASSY, REF AMM, CW REO.
- [SDR SWIA201440017](https://openairdocs.org/sdr/SWIA201440017), Nov 7, 2014: VANE. CHAFED. LEFT INBD FLAP VANE CHAFED AT CENTER L/E. BLENDED IAW REO.
- [SDR SWIA201440015](https://openairdocs.org/sdr/SWIA201440015), Nov 7, 2014: VANE. GOUGED. RT WING INBD FLAP VANE L/E HAS SMALL GOUGE 27.5" FROM OTBD END. BLENDED IAW REO.
- [SDR SWIA201440014](https://openairdocs.org/sdr/SWIA201440014), Nov 7, 2014: VANE. CHAFED. RT WING INBD FLAP VANE L/E CHAFED 70.5" FROM OTBD END. BLENDED AND REPAIRED IAW REO.
- [SDR SWIA201440012](https://openairdocs.org/sdr/SWIA201440012), Nov 7, 2014: SKIN. CHAFED. LEFT AILERON UPPER L/E CHAFED. LT AILERON UPPER L/E SHROUD FOUND TO BE OUT OF LIMITS IAW REO REPLACED.
- [SDR SWIA201440048](https://openairdocs.org/sdr/SWIA201440048), Nov 6, 2014: SKIN. FAILED. DENTED LT FUSELAGE SKIN PANEL ON NOSE, BELOW CAPTAIN'S WINDOW. REPAIRED IAW REO.
- [SDR SWIA201440029](https://openairdocs.org/sdr/SWIA201440029), Nov 6, 2014: PANEL. DAMAGED. PANEL 326AR, ZONE 300 FAILED GAP CHECK. CONTOURED VISOR PANEL. FOUND WITHIN LIMITS IAW REO.
- [SDR SWIA201440027](https://openairdocs.org/sdr/SWIA201440027), Nov 6, 2014: PANEL. FAILED. PANEL 326BR, ZONE 300 FAILED GAP CHECK, CONTOURED VISOR PANEL. FOUND WITHIN LIMITS IAW REO.
- [SDR SWIA201440026](https://openairdocs.org/sdr/SWIA201440026), Nov 6, 2014: PANEL. FAILED. PANEL 326BL, ZONE 300, FAILED GAP CHECK, CONTOURED VISOR PANEL IAW REO AND AMM.
- [SDR SWIA201440025](https://openairdocs.org/sdr/SWIA201440025), Nov 6, 2014: PANEL. DAMAGED. PANEL 326AL ZONE 300, FAILED GAP CHECK, CONTOURED VISOR PANEL 326AL. FOUND WITHIN LIMITS IAW REO.
- [SDR SWIA2014061938226](https://openairdocs.org/sdr/SWIA2014061938226), Jun 17, 2014: TORQUE LINK. GALLED. LT ENGINE FORWARD MOUNT TORQUE LINK ASSEMBLY HAS GALLING IN BUSHING. INSTALLED NEW LINK ON THE LT ENGINE FWD YOKE MOUNT IAW AMM.
- [SDR SWIA2014061938225](https://openairdocs.org/sdr/SWIA2014061938225), Jun 17, 2014: BUSHING. GALLED. LT ENGINE FORWARD MOUNT YOKE BUSHING HAS GALLING. INSTALLED NEW LT ENGINE FWD YOKE MOUNT IAW AMM.
- [SDR SWIA201437643](https://openairdocs.org/sdr/SWIA201437643), May 19, 2014: LAMP. BURNED OUT. LEFT OVERWING EMERGENCY LIGHT IS BURNED OUT. R & R LT OVERWING EXTERIOR EMERGENCY LIGHT LAMP IAW AMM.
- [SDR SWIA201437668](https://openairdocs.org/sdr/SWIA201437668), May 17, 2014: AUTOPILOT SYS. DISCONNECTED. AUTOPILOT INITIATED UNCOMMANDED PITCH CHANGE A/P WAS MANUALLY DISCONNECTED, FLIGHT PATH CORRECTED AND REENGAGED WITHOUT FURTHER INCIDENT. PERFORMED SERVO SPIN T
- [SDR SWIA201437403](https://openairdocs.org/sdr/SWIA201437403), May 7, 2014: BUSHING. DAMAGED. LEFT ENGINE AFT MOUNT THRUST SHAFT SPHERICAL BUSHING AND SPHERICAL BUSHING HOUSING HAS CORRODED. REPLACED LT ENGINE AFT MOUNT THRUST SHAFT SPHERICAL BUSHING AND
- [SDR SWIA201437053](https://openairdocs.org/sdr/SWIA201437053), Apr 6, 2014: LAMP. BURNED OUT. FORWARD EMERGENCY LIGHT OVERHEAD LIGHT IS BURNED OUT, REPLACED LAMP.
- [SDR SWIA201436785](https://openairdocs.org/sdr/SWIA201436785), Mar 16, 2014: SIGN. BURNED OUT. LOWER RIGHT OVERWING EXIT EMERGENCY SIGN IS BURNED OUT. REPLACED SIGN AND INVERTER.
- [SDR SWIA201334853](https://openairdocs.org/sdr/SWIA201334853), Oct 7, 2013: LIGHT. INOPERATIVE. CEILING EMERGENCY LIGHT IN AFT POSITION BURNED OUT. FLT#5374 RELAMPED, PN 1317.
- [SDR SWIA201334381](https://openairdocs.org/sdr/SWIA201334381), Aug 22, 2013: LIGHT. INOPERATIVE. CEILING POD LIGHT ABEAM BURNED OUT. FLT#6224 RELAMPED.
- [SDR SWIA201333497](https://openairdocs.org/sdr/SWIA201333497), May 17, 2013: PUMP. FAILED. RECEIVED GEAR DISAGREE WARNING MSG. BY THE TIME WE RAN CHECKLIST, ISSUE SELF-CORRECTED. NO PROBLEMS WITH LANDING GEAR EXTENSION ON LANDING. REPLACED 3A ELECTRIC
- [SDR SWIA201333361](https://openairdocs.org/sdr/SWIA201333361), Apr 14, 2013: WEB. CRACKED. TRU WEB IS CRACKED AT FS 193 RIGHT. (C-CHECK) REPAIRED TRU WEB AT FS 193.00 RIGHT IAW REO.
- [SDR SWIA201333360](https://openairdocs.org/sdr/SWIA201333360), Apr 14, 2013: WEB. CRACKED. TRU WEB IS CRACKED AT FS 193 LEFT. (C-CHECK) INSTALLED REPAIR ON TRU WEB FS 193 LEFT IAW REO.
- [SDR SWIA201333359](https://openairdocs.org/sdr/SWIA201333359), Apr 13, 2013: CAP. WORN. LEFT INBD FLAP, INBD FLAP VANE CAP IS WORN BEYOND LIMITS. (C-CHECK) REPLACED WORN LEFT INBD FLAP, INBD FLAP VANE CAP IAW SRM.

All 174: https://openairdocs.org/deregistered/N984CA-2017-05-03/reports.md

## FAA accident and incident reports (2)

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 19990103005459I](https://openairdocs.org/incident/19990103005459I), Jan 3, 1999: Cndair CL6002B19 (N984CA), Syracuse, NY. (-5) On Sunday, January 3, 1999, at 1638 local, a CL-600, N984CA, operated by comair airlines, enroute to toronto international airport, diverted to Syracuse…
- [Incident 19980406008899I](https://openairdocs.org/incident/19980406008899I), Apr 6, 1998: Cndair CL6002B19 (N984CA), Orbisonia, PA. Narrative: COMM833 eastbound level at FL240 with usa 1027 also eastbound overhead descending to FL250. COMM833 reports responding to a TCAS ra and descending.…

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