# N416SW: 1995 Canadair CL-600-2B19, registration cancelled 2019-02-04

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: February 4, 2019
- 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: 7089
- Year built: 1995
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: November 5, 1998
- Certificate issued: January 6, 2016
- Last registry action: May 7, 2018
- Mode S code: A4EC0F
- Owner when cancelled: [Wells Fargo Trust Co Na Trustee](https://openairdocs.org/faa-owner/WELLS%20FARGO%20TRUST%20CO%20NA%20TRUSTEE)
- Location: [Salt Lake City, UT](https://openairdocs.org/faa-place/UT/Salt%20Lake%20City)
- Owner type: Corporation
- Owner's area on the map: 40.7558° N, 111.8843° W: Placed by OpenAirDocs at the center of ZIP code 84111, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N416SW
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=416SW
- Page: https://openairdocs.org/deregistered/N416SW-2019-02-04

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 (178, newest 50)

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

- [SDR SWIA201642311](https://openairdocs.org/sdr/SWIA201642311), Jul 19, 2016: MODULE. FAILED. AT FL270, EN ROUTE, THE CABIN ALTITUDE WARNING CAME ON & ALL THE MASKS IN THE CABIN DEPLOYED. THE CREW & PASSENGERS DONNED THEIR OXYGEN MASKS. THE CREW DECLARED
- [SDR SWIA201541567](https://openairdocs.org/sdr/SWIA201541567), Nov 16, 2015: PUMP. FAILED. HYD 3A LOW PRESS CAUTION 1800 PSI. REQUIRED EMERGENCY GEAR EXTENSION. AFTER EXTENSION DOWN TO 1500 PSI QTY IN FLIGHT SHOWN 80 PERCENT BEFORE GEAR EXTENSION. ON 
- [SDR SWIA201440498](https://openairdocs.org/sdr/SWIA201440498), Dec 27, 2014: COVER. UNSERVICEABLE. UPPER SHROUD FOR LT WINDSCREEN ON INBD SIDE IS UNSERVICEABLE. REPAIRED TURNBUCKLE COVER IAW EA.
- [SDR SWIA201440497](https://openairdocs.org/sdr/SWIA201440497), Dec 27, 2014: PLACARD. CRACKED. APU ECU "NO STEP" COVER IS CRACKED. REPAIRED APU ECU "NO STEP" COVER IAW EA.
- [SDR SWIA201440496](https://openairdocs.org/sdr/SWIA201440496), Dec 23, 2014: SKIN. DENTED. LEFT MIDDLE WING L/E 530JL HAS A DENT AT APPROXIMATE WS 200. HAND DRESSED THE DENT IAW REO.
- [SDR SWIA201440495](https://openairdocs.org/sdr/SWIA201440495), Dec 23, 2014: SKIN. DENTED. LT INBD WING L/E PANEL HAS TWO DENTS AT APPROXIMATE WS92.0 AND WS124.5. DRESSED BACK THE DENTS IAW REO.
- [SDR SWIA201440540](https://openairdocs.org/sdr/SWIA201440540), Dec 15, 2014: HAND RAIL. DAMAGED. PAX DOOR FWD HAND RAIL, DENTED FWD UPPER CORNER COVER AND DAMAGED ATTACH FASTENER. REPAIRED AND RESTORED FINISH IAW SRM AND REO.
- [SDR SWIA201440539](https://openairdocs.org/sdr/SWIA201440539), Dec 15, 2014: HAND RAIL. DAMAGED. PAX DOOR AFT HANDRAIL, DENTED AFT UPPER CORNER COVER AND DAMAGED ATTACH FASTENER. REPAIRED AND RESTORED FINISH IAW SRM AND REO.
- [SDR SWIA201440538](https://openairdocs.org/sdr/SWIA201440538), Dec 12, 2014: POST. CRACKED. BS 409+128 BL 0, RT SIDE OF POST CRACKED AT TOP. INSTALLED POST ASSEMBLY IAW SRM AND REO.
- [SDR SWIA201440537](https://openairdocs.org/sdr/SWIA201440537), Dec 11, 2014: FLOOR SUPPORT. GOUGED. FLOOR SUPPORT AT BS 435, LBL 43 IS DAMAGED OUT OF LIMITS. A REPAIR DOUBLER WAS FABRICATED AND INSTALLED IAW EA.
- [SDR SWIA201440536](https://openairdocs.org/sdr/SWIA201440536), Dec 8, 2014: FRAME. CRACKED. LEFT INTERIOR FUSELAGE FRAME AT BS 559 + 32 AT STRINGER 6L IS CRACKED. INSTALLED REPAIR 6 IAW EA.
- [SDR SWIA201440535](https://openairdocs.org/sdr/SWIA201440535), Dec 8, 2014: PICCOLO TUBE. GOUGED. LEFT WING OTBD PICCOLO TUBE IS GOUGED AT THE OTBD END. REPAIRED LT WING OTBD PICCOLO TUBE IAW EA.
- [SDR SWIA201440534](https://openairdocs.org/sdr/SWIA201440534), Dec 8, 2014: DUCT. BROKEN. RT PSU DUCT RISER AF BS 953 HAS A BROKEN DUCT ON THE AFT SIDE. : REPAIR COMPLETE IAW EA.
- [SDR SWIA201440533](https://openairdocs.org/sdr/SWIA201440533), Dec 8, 2014: FRAME. CRACKED. FUSELAGE FRAME AT BS 409+80 IS CRACKED AT STRINGER 6L. REPAIRED THE FRAME IAW SRM AND STS EA.
- [SDR SWIA201440532](https://openairdocs.org/sdr/SWIA201440532), Dec 6, 2014: FLOOR SUPPORT. CORRODED. LEFT FLOOR SUPPORT FROM BS 473.15 - 513 HAS CORROSION. THE CORROSION WAS BLENDED IAW REO.
- [SDR SWIA201440531](https://openairdocs.org/sdr/SWIA201440531), Dec 6, 2014: FLOOR SUPPORT. CORRODED. LEFT FLOOR SUPPORT FROM BS 409.128 - 473.15 HAS CORROSION. REMOVED THE CORROSION IAW REO.
- [SDR SWIA201440530](https://openairdocs.org/sdr/SWIA201440530), Dec 6, 2014: FLOOR SUPPORT. CORRODED. RIGHT FLOOR SUPPORT BS 409.128 - 473.15 HAS CORROSION. CORROSION WAS BLENDED IAW REO.
- [SDR SWIA201440529](https://openairdocs.org/sdr/SWIA201440529), Dec 6, 2014: FLOOR SUPPORT. CORRODED. RIGHT FLOOR SUPPORT ANGLE FROM BS 473.15 - 513 CORRODED. THE CORROSION WAS BLENDED IAW REO.
- [SDR SWIA201440528](https://openairdocs.org/sdr/SWIA201440528), Dec 6, 2014: FLOOR SUPPORT. CORRODED. RIGHT FLOOR SUPPORT ANGLE FROM BS 513 - 559 CORRODED. CORROSION WAS BLENDED IAW REO.
- [SDR SWIA201440527](https://openairdocs.org/sdr/SWIA201440527), Dec 6, 2014: FLOOR PANEL. CORRODED. LEFT FLOOR PANEL FROM BS 409.128 - 559 HAS CORROSION. BLENDED CORROSION IAW REO.
- [SDR SWIA201440526](https://openairdocs.org/sdr/SWIA201440526), Dec 6, 2014: FLOOR PANEL. CORRODED. RIGHT FLOOR PANEL FROM BS 409.128 559 HAS CORROSION. REMOVED CORROSION IAW REO.
- [SDR SWIA201440525](https://openairdocs.org/sdr/SWIA201440525), Dec 5, 2014: POST. CRACKED. BS 409+128 VERTICAL POST AT LBL 18 INBD RADIUS CRACKED. INSTALLED A NEW VERTICAL POST ASSEMBLY IAW REO AND SRM.
- [SDR SWIA201440524](https://openairdocs.org/sdr/SWIA201440524), Dec 5, 2014: POST. CRACKED. BS 409+128 VERTICAL POST AT BL 0, CRACKED. INSTALLED A NEW POST ASSY IAW SRM AND REO.
- [SDR SWIA201440523](https://openairdocs.org/sdr/SWIA201440523), Dec 5, 2014: BULKHEAD WEB. CRACKED. BS 621 BULKHEAD WEB HAS ONE CRACK LOCATED AT LBL 18. INSTALLED A REPAIR IAW REO.
- [SDR SWIA201440522](https://openairdocs.org/sdr/SWIA201440522), Dec 5, 2014: BULKHEAD WEB. CRACKED. BS 621 BULKHEAD WEB HAS TWO CRACKS LOCATED AT BL 0. INSTALLED A REPAIR IAW REO.
- [SDR SWIA201440521](https://openairdocs.org/sdr/SWIA201440521), Dec 5, 2014: BULKHEAD WEB. CRACKED. FS 621 BULKHEAD WEB HAS ONE CRACK AT RBL 9.5. REPAIR DOUBLER, TRIPLER AND FILLER WERE FABRICATED AND INSTALLED IAW REO.
- [SDR SWIA201440520](https://openairdocs.org/sdr/SWIA201440520), Dec 5, 2014: LINE. LOOSE. TWO MOTIVE FLOW LINES INSIDE THE FUEL PRESSURE BOX ARE LOOSE. REINFORCED THE FUEL LINES IN FUEL PRESSURE BOX IAW REO.
- [SDR SWIA201440519](https://openairdocs.org/sdr/SWIA201440519), Dec 5, 2014: LOUVER. LOOSE. RIGHT RAM AIR EXHAUST DUCT HAS LOOSE LOUVERS. REPAIRED RIGHT ACM RAM AIR EXHAUST DUCT LOUVERS IAW REO.
- [SDR SWIA201440518](https://openairdocs.org/sdr/SWIA201440518), Dec 4, 2014: LOUVER. LOOSE. LEFT RAM AIR EXHAUST DUCT HAS LOOSE LOUVERS. REPAIRED THE LEFT ACM RAM AIR EXHAUST DUCT LOUVERS, IAW REO.
- [SDR SWIA201440517](https://openairdocs.org/sdr/SWIA201440517), Dec 4, 2014: FLOOR SUPPORT. CORRODED. LBL 9 FLOOR SUPPORT UPPER CAP BETWEEN BS 574 - 621 HAS CORROSION AT NUTPLATE LOCATIONS. INSTALLED NEW FLOOR SUPPORT CAP IAW SRM AND REO.
- [SDR SWIA201440516](https://openairdocs.org/sdr/SWIA201440516), Dec 4, 2014: FLOOR SUPPORT. CORRODED. LBL 27, FLOOR SUPPORT UPPER CAP BETWEEN BS 574 - 621 HAS CORROSION AT NUTPLATE LOCATIONS. INSTALLED NEW FLOOR SUPPORT CAP IAW SRM AND REO.
- [SDR SWIA201440515](https://openairdocs.org/sdr/SWIA201440515), Dec 4, 2014: SEAT TRACK. CORRODED. LBL9 SEAT TRACK BETWEEN FS 559+112 AND FS 574 HAS CORROSION. C-CHECK, REPLACED SEAT TRACK AT LBL 9 FS 559+112 - FS574 IAW REO.
- [SDR SWIA201440514](https://openairdocs.org/sdr/SWIA201440514), Dec 4, 2014: SEAT TRACK. CORRODED. LBL9 SEAT TRACK AT BS 559+90 HAS CORROSION. REPLACED THE SEAT TRACK IAW REO.
- [SDR SWIA201440513](https://openairdocs.org/sdr/SWIA201440513), Dec 4, 2014: SEAT TRACK. CORRODED. LBL 9 SEAT TRACK AT FS 615 HAS CORROSION AROUND FASTENERS. REPLACED SEAT TRACK AT LBL 9, FS 615 IAW REO.
- [SDR SWIA201440512](https://openairdocs.org/sdr/SWIA201440512), Dec 3, 2014: STRIKER. DENTED. PAX DOOR SEAL STRIKER REPAIR IN AFT UPPER CORNER IS BENT/DENTED. C-CHECK, R & R EXISTING REPAIR STRIP ON PAX DOOR SEAL STRIKER IN AFT UPPER CORNER IAW REO.
- [SDR SWIA201440511](https://openairdocs.org/sdr/SWIA201440511), Dec 2, 2014: SHROUD. CHAFED. LEFT LOWER AILERON SHROUD PANEL 599CB IS CHAFED. BLENDED CHAFE ON LT LOWER AILERON SHROUD PANEL 599CB IAW REO.
- [SDR SWIA201440510](https://openairdocs.org/sdr/SWIA201440510), Dec 2, 2014: SHROUD. CHAFED. LEFT LOWER AILERON SHROUD PANEL 599BB IS CHAFED. BLENDED CHAFE ON LT LOWER AILERON SHROUD PANEL 599BB IAW REO.
- [SDR SWIA201440509](https://openairdocs.org/sdr/SWIA201440509), Dec 2, 2014: SHROUD. CHAFED. LT LOWER AILERON SHROUD PANEL 599AB IS CHAFED., BLENDED CHAFE ON LT LOWER AILERON SHROUD PANEL 599AB IAW REO.
- [SDR SWIA201440508](https://openairdocs.org/sdr/SWIA201440508), Dec 2, 2014: SKIN. CHAFED. LT INBD FLAP VANE, INBD OF INBD ACTUATOR L/E SKIN CHAFED. BLENDED CHAFE ON LT INBD FLAP VANE, INBD OF INBD ACTUATOR L/E SKIN IAW REO.
- [SDR SWIA201440507](https://openairdocs.org/sdr/SWIA201440507), Dec 2, 2014: SKIN. CHAFED. LEFT INBD FLAP VANE, MIDWAY BETWEEN INBD AND CENTER ACTUATOR L/E SKIN CHAFED. BLENDED CHAFE ON LT INBD FLAP VANE, MIDWAY BETWEEN INBD AND CENTER ACTUATOR L/E SK
- [SDR SWIA201440506](https://openairdocs.org/sdr/SWIA201440506), Dec 2, 2014: VANE. CHAFED. LT INBD FLAP VANE, OTBD OF CENTER ACTUATOR L/E SKIN CHAFED. BLENDED CHAFE ON LT INBD FLAP VANE, OTBD OF CENTER ACTUATOR L/E SKIN IAW REO.
- [SDR SWIA201440505](https://openairdocs.org/sdr/SWIA201440505), Dec 2, 2014: VANE. CHAFED. LEFT INBD FLAP VANE, BETWEEN OTBD AND CENTER ACTUATOR L/E SKIN CHAFED. C-CHECK, BLENDED CHAFE ON LT INBD FLAP VANE, BETWEEN OTBD AND CENTER ACTUATOR L/E SKIN IA
- [SDR SWIA201440504](https://openairdocs.org/sdr/SWIA201440504), Dec 2, 2014: VANE. CHAFED. LEFT INBD FLAP VANE, OTBD OF OTBD ACTUATOR L/E SKIN CHAFED. BLENDED CHAFE IAW REO.
- [SDR SWIA201440503](https://openairdocs.org/sdr/SWIA201440503), Dec 1, 2014: PANEL. FAILED. HORIZONTAL STABILIZER VISOR PANEL 326BR RT LOWER. CONTOURED THE VISOR PANEL IAW REO.C.
- [SDR SWIA201440502](https://openairdocs.org/sdr/SWIA201440502), Dec 1, 2014: PANEL. FAILED. HORIZONTAL STABILIZER VISOR PANEL 326BL, LT LOWER. CONTOURED THE VISOR PANEL IAW REO.
- [SDR SWIA201440501](https://openairdocs.org/sdr/SWIA201440501), Dec 1, 2014: PANEL. FAILED. HORIZONTAL STABILIZER VISOR PANEL 326AR RT UPPER. CONTOURED THE VISOR PANEL IAW REO.
- [SDR SWIA201440500](https://openairdocs.org/sdr/SWIA201440500), Dec 1, 2014: HOUSING. GOUGED. PAX DOOR EXTERIOR HANDLE HOUSING HAS A GOUGE. PAX DOOR EXTERIOR HANDLE HOUSING BLENDED OUT IAW EA.
- [SDR SWIA201440499](https://openairdocs.org/sdr/SWIA201440499), Nov 30, 2014: SKIN. DENTED. ONE DENT BS 654.5 - 672.2 S18-21L. COLDWORKED DENT TO ORIGINAL CONTOUR IAW EA.
- [SDR SWIA201439961](https://openairdocs.org/sdr/SWIA201439961), Nov 15, 2014: FRAME. CORRODED. FUSELAGE FRAME CORRODED. PAINT LIFTING AND BUBBLED AT STA 319 AND STRINGER 26 LT. REPAIRED IAW REO AND SRM.
- [SDR SWIA201438088](https://openairdocs.org/sdr/SWIA201438088), May 24, 2014: BRACKET. LOOSE. RT ENGINE HAS LOOSE 10TH STAGE BLEED DUCT ISOLATORS. C-CHECK, REPLACED ISOLATORS.

All 178: https://openairdocs.org/deregistered/N416SW-2019-02-04/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 20040125005769I](https://openairdocs.org/incident/20040125005769I), Jan 25, 2004: Cndair CL6002B19 (N416SW), Palm Springs, CA, Minor damage. (-23) On 01/25/2004, during takeoff, swia flight #3948 (ont/slc) nose landing gear failed to retract. The aircraft diverted to psp (due to swia mx facility).…

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