# N8932C: 2004 Bombardier CL-600-2B19, registration cancelled 2025-10-01

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: October 1, 2025
- Exported to: South Africa
- Status when cancelled: Valid registration
- Airframe: [Bombardier CL-600-2B19](https://openairdocs.org/model/bombardier-cl-600-2b19) (registry code 1390008)
- Engine: [GE CF34-3B1](https://openairdocs.org/engine/ge-cf34-3b1) (registry code 30070)
- Data sheets: [TCDS A21EA-1](https://openairdocs.org/tcds/A21EA-1), [TCDS E15NE](https://openairdocs.org/tcds/E15NE) (OpenAirDocs)
- Serial number: 7932
- Year built: 2004
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: August 18, 2006
- Certificate issued: July 28, 2025
- Last registry action: July 28, 2025
- Mode S code: AC531A
- Owner when cancelled: [Gold Coast Aviation](https://openairdocs.org/faa-owner/GOLD%20COAST%20AVIATION)
- Location: [Fort Lauderdale, FL](https://openairdocs.org/faa-place/FL/Fort%20Lauderdale)
- Owner type: Corporation
- Owner's area on the map: 26.1860° N, 80.1727° W: Placed by OpenAirDocs at the center of ZIP code 33309, within about 2 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N8932C
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=8932C
- Page: https://openairdocs.org/deregistered/N8932C-2025-10-01

From the FAA registry file of November 7, 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 (81, newest 50)

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

- [SDR REXA2022092102119](https://openairdocs.org/sdr/REXA2022092102119), Sep 13, 2022: LIGHT. INOPERATIVE. LH FWD OVER-WING EXTERNAL EMERGENCY LIGHT INOP REMOVED & REPLACED LH EXTERNAL EMERGENCY LIGHT HOUSING PER CRJ 200 AMM 33-51-21. PN ON/OFF BM1-0006-002, OPS CHEC
- [SDR REXA2022040500561](https://openairdocs.org/sdr/REXA2022040500561), Apr 4, 2022: POST. CRACKED. DURING COMPLIANCE OF CRJ-200 JOB CARD: 53-160-635 AT FS409+128, RBL27, A CRACK WAS FOUND AT THE VERTICAL BEAM LOWER IB FLANGE THROUGH THE BOTTOM MOST RIVET WHER
- [SDR REXA2021062400463](https://openairdocs.org/sdr/REXA2021062400463), Jun 21, 2021: HANDLE. CRACKED. PAX. DOOR OUTER HANDLE IS CRACKED. J/C 52-830-300. PAX DOOR OUTER HANDLE REMOVED AND REPLACED IAW CRJ200 AMM 52-11-03.
- [SDR REXA2021062400456](https://openairdocs.org/sdr/REXA2021062400456), Jun 21, 2021: RIB. CRACKED. LH MLG BATT. RIB IS CRACKED W.S.53.60. REPAIRED CRACKED REFERENCING REO 601R-57-046B.
- [SDR REXA2021062400455](https://openairdocs.org/sdr/REXA2021062400455), Jun 21, 2021: PLATE. CRACKED. AFT CARGO STEP PLATE IS DAMAGED. REMOVED AND REPLACED WITH NEW AFT CARGO STEP PLATE IAW AMM 53-60-55.
- [SDR REXA2021062400454](https://openairdocs.org/sdr/REXA2021062400454), Jun 21, 2021: RIB. CORRODED. EXTENSIVE CORROSION ON RH WING BATT RIB WEB W.S 48.60. REPAIRED R/H BATT RIB @ WS 48.60 IAW EA # CRJ257-11783.
- [SDR REXA2021062400453](https://openairdocs.org/sdr/REXA2021062400453), Jun 18, 2021: SKIN. DENTED. DENT ON L/H I/B FLAP UPPER SKIN @ W.S. 139. REPAIRED L/H I/B FLAP UPPER SKIN IAW REO#601R-57-52-058
- [SDR REXA2021062400458](https://openairdocs.org/sdr/REXA2021062400458), Jun 17, 2021: FLANGE. CRACKED. APU ENCLOSURE IS CRACKED ON UPPER AFT LH DOOR FLANGE. REPAIRED DAMAGE ON UPPER AFT L/H APU ENCLOSURE DOOR FLANGE IAW BOMBA REO 601R-49-11-071 REV NC DATED 11-22
- [SDR REXA2021062400462](https://openairdocs.org/sdr/REXA2021062400462), Jun 15, 2021: HOUSING. CRACKED. SERVICE DOOR PROX. SENSOR HOUSING IS CRACKED. J/C 52-840-503. ADJUSTED PROXIMITY SWITCH ON THE HANDLE MECHANISM TO (1.27MM) AND OPPS CHECK IAW AMM CRJ200-52-70-
- [SDR REXA2021062400460](https://openairdocs.org/sdr/REXA2021062400460), Jun 4, 2021: HOUSING. CRACKED. GROUND POWER RECEPTACLE HOUSING CRACKED ON INSIDE. J/C 53-12-301. REMOVED & REPLACED GROUND POWER RECEPTACLE HOUSING, P/N 600-33283-33 IAW BOMB. REO#601R-53-11-
- [SDR REXA2021062400457](https://openairdocs.org/sdr/REXA2021062400457), Jun 3, 2021: RETAINER. CRACKED. PAX DOOR LOWER SEAL RETAINER IS CRACKED. REPAIRED PAX DOOR LOWER SEAL RETAINER IAW REO601R-52-11-915.
- [SDR REXA2021062400459](https://openairdocs.org/sdr/REXA2021062400459), May 26, 2021: SUPPORT. CRACKED. AFT EQUIP. BAY DOOR CUTOUT LH SIDE SUPPORT STRUCTURE IS CRACKED. REMOVED AND REPLACED AFT EQUIPTMENT BAY DOOR CUTOUT L/H SIDE SUPPORT STRUCTURE IAW CRJ200 SRM 5
- [SDR SWIA2019123147480](https://openairdocs.org/sdr/SWIA2019123147480), Dec 10, 2019: VANE. CHAFED. LH IB FLAP VANE IS CHAFED AT ALL 3 LEADING EDGE CONTACT POINTS (C-CHECK) RO 12/27/2019 REMOVED AND REPLACED LH IB FLAP REF CAMP # 20077637 FOR REPLACEMENT.
- [SDR SWIA2019123147478](https://openairdocs.org/sdr/SWIA2019123147478), Dec 10, 2019: FRAME. CORRODED. FRAME 605 IS CORRODED ON BOTH SIDES OF FRAME BETWEEN STR26R AND STR26L (C-CHECK) RO 12/27/2019 REPAIRED FRAME AT FS 605 IAW BOMBARDIER REO.
- [SDR SWIA2019123147474](https://openairdocs.org/sdr/SWIA2019123147474), Dec 10, 2019: FRAME. CORRODED. FRAME 574IS CORRODED ON BOTH SIDES BETWEEN STR26L AND STR25R (C-CHECK) RO 12/27/2019 PERFORMED A MAJOR REPAIR TO FRAME 574 BETWEEN STR26L AND STR25R IAW REO. CO
- [SDR SWIA2020013147472](https://openairdocs.org/sdr/SWIA2020013147472), Dec 10, 2019: FRAME. CORRODED. FRAME 589 IS CORRODED ON BOTH SIDES BETWEEN STR25R AND STR25L (C-CHECK) RO 12/27/2019 REPAIRED FRAME AT FS 589 COMMON TO STRINGERS 25R AND 25 L IAW BOMBARDIER R
- [SDR SWIA2019123147477](https://openairdocs.org/sdr/SWIA2019123147477), Dec 8, 2019: BULKHEAD. CRACKED. CRACK ON 621 BULKHEAD LOWER I/B CORNER OF LINTEL FITTING 0.350" 100%FSH. (C-CHECK) RO 12/27/2019 REPAIRED CRACK ON FS621 BULKHEAD COMMON TO INBD CORNER OF LINTE
- [SDR SWIA2019123147479](https://openairdocs.org/sdr/SWIA2019123147479), Dec 2, 2019: BULKHEAD WEB. CHAFED. FS621 RPB WEB SMALL CHAFES FROM CONTACT WITH SCREWS AT WL103 IN 7EA AREAS AT RBL18, RBL27, RBL36, LBL7, LBL9, LBL18, AND LBL27 (C-CHECK) RO 12/27/2019 REPAIRED 
- [SDR SWIA2019123147476](https://openairdocs.org/sdr/SWIA2019123147476), Dec 2, 2019: BULKHEAD WEB. CRACKED. 3EA AREAS OF CRACK INDICATIONS NOTED ON FS621 RPB WEB, 2EA IN THE HEEL LINE AREA OF VERT POSTS, 1ST AT BL0 WL108.5-WL111.5 50%FSH, 2ND AT LBL36 WL78.75-WL79.25 
- [SDR SWIA2019123147475](https://openairdocs.org/sdr/SWIA2019123147475), Dec 2, 2019: POST. CRACKED. FS409+128 RBL18 I/B VERT POST HAS A CRACK INDICATION NOTED IN THE AFT FLANGE RADIUS AT WL69 .325 LONG BY 70%FSH. FAILED NDT (C-CHECK) RO 12/27/2019 PERFORMED A 
- [SDR SWIA2019123147473](https://openairdocs.org/sdr/SWIA2019123147473), Dec 2, 2019: ATTACH ANGLE. CRACKED. FS409+128 BL0 L/H VERT POST HAS A CRACK INDICATION NOTED IN THE AFT FLANGE RADIUS AT WL69 .275 LONG BY 50%FSH. FAILED NDT (C-CHECK) RO 12/27/2019 PERFORMED A MA
- [SDR SWIA2019072346082](https://openairdocs.org/sdr/SWIA2019072346082), Jul 23, 2019: WARNING SYSTEM. ACTIVATED. RIGHT MAIN LANDING GEAR DIDN€™T INDICATE DOWN TWENTY SECONDS AFTER SELECTING DOWN. GEAR DISAGREE. (FLT#3952) CLOSED DEFERRED LANDING GEAR RETRACTION SYSTEM IAW
- [SDR SWIA201744000](https://openairdocs.org/sdr/SWIA201744000), Nov 13, 2017: STRUCTURE. DENTED. DENTS AT APPROX FS 735 TO FS 755 BETWEEN STR 24L, 25L AND BETWEEN STR 24R, 25R. (C-CHECK) RO: 11/18/2017 REPAIRED DENT ON LT FUSELAGE IAW REO.
- [SDR SWIA201743999](https://openairdocs.org/sdr/SWIA201743999), Nov 9, 2017: VANE. CHAFED. RT INBD FLAP VANE INBD VANE CAP IS CHAFED. (C-CHECK) RO: 11/18/2017 REMOVED AND REPLACED THE RT INBOARD FLAP VANE, INBOARD LEADING EDGE VANE CAP IAW SRM.
- [SDR SWIA201642429](https://openairdocs.org/sdr/SWIA201642429), Aug 11, 2016: PSEU. FAILED. GEAR DISAGREE AFTER EXTENDING THE GEAR FOR LANDING. INITIALLY ALL GEAR WERE DOWN AND GREEN BUT THEN THE NOSE GEAR GREEN INDICATION WENT OUT AND THE GEAR DISAGRE
- [SDR SWIA201642166](https://openairdocs.org/sdr/SWIA201642166), May 31, 2016: DOWNLOCK SENSOR. MALFUNCTIONED. GEAR DISAGREE WHEN SELECTED GEAR UP, NLG WAS HATCHED YELLOW AND MLG WERE BOTH UP. R & R NLG DOWNLOCK SENSOR NR 2 IAW AMM, ADJUSTED NLG DOWNLOCK NR 2 IAW AMM, SW
- [SDR SWIA201641907](https://openairdocs.org/sdr/SWIA201641907), Feb 24, 2016: PROXIMITY SENSOR. FAILED. CREW RECEIVED A GEAR DISAGREE ON APPROACH, SHOWING THE NOSE GEAR NOT DOWN AND LOCKED. MISSED APPROACH, FOLLOWED THE QRH AND DECLARED AN EMERGENCY. THE FLIGHT LA
- [SDR SWIA201541641](https://openairdocs.org/sdr/SWIA201541641), Nov 10, 2015: SEAT TRACK. CORRODED. RIGHT CENTER CABIN SEAT TRACK AT APPROXIMATELY FS 349 TO FS 409+128 HAS EVIDENCE OF CORROSION. R & R RT CENTER SEAT TRACK FS 364.0 TO FS 399.0 IAW AMM AND R & R
- [SDR SWIA201541640](https://openairdocs.org/sdr/SWIA201541640), Nov 9, 2015: SEAT TRACK. CORRODED. LEFT CENTER CABIN SEAT TRACK AR APPROXIMATELY FS349 TO FS409+128 HAS EVIDENCE OF CORROSION. R & R LT CENTER SEAT TRACK FS 364.0 TO FS 399.0 IAW AMM AND R & R LT
- [SDR SWIA201541639](https://openairdocs.org/sdr/SWIA201541639), Nov 8, 2015: FRAME. CORRODED. AVIONICS BAY BELOW FLOORBOARD THERE IS CORROSION AT FS 333.0, FRAME AT STR 27. BLENDED AND REMOVED CORROSION FROM FS 333.0, STR 27 IAW SRM AND EA.
- [SDR SWIA201541638](https://openairdocs.org/sdr/SWIA201541638), Nov 8, 2015: VANE. CHAFED. RIGHT INBD FLAP VANE OTBD L/E CHAFED. R & R RT INBD FLAP VANE OTBD L/E SKIN IAW SRM AND EA.
- [SDR SWIA201541637](https://openairdocs.org/sdr/SWIA201541637), Nov 8, 2015: VANE. CHAFED. RIGHT INBD FLAP VANE CENTER L/E CHAFED. R & R RT INBD FLAP VANE CENTER L/E SKIN IAW SRM AND EA.
- [SDR SWIA201541636](https://openairdocs.org/sdr/SWIA201541636), Nov 8, 2015: VANE. CHAFED. LEFT INBD FLAP VANE CENTER L/E CHAFED. R & R LT INBD FLAP VANE CENTER L/E SKIN IAW SRM AND EA.
- [SDR REXA2014111100910](https://openairdocs.org/sdr/REXA2014111100910), Nov 7, 2014: STRUCTURE. DENTED. TWO DENTS ON THE LT FUSELAGE TO BE OUT OF LIMITS. THE DENTS MEASURE 2.13 INCHES X 1.75 INCHES X .025 INCHES DEEP & 4.75 INCHES X 2.63 INCHES X .065 INCHES DEEP.
- [SDR REXA2014103001085](https://openairdocs.org/sdr/REXA2014103001085), Oct 30, 2014: WIRE HARNESS. DAMAGED. GEAR DISAGREE, NOSE GEAR DID NOT RETRACT, STEERING REMAINED ACTIVE. NO OTHER INDICATIONS NOTED BEFOREHAND. FOUND DAMAGE TO NLG HARNESS & BRACKET. R & R HARNESS 
- [SDR REXA2014072400735](https://openairdocs.org/sdr/REXA2014072400735), Jul 24, 2014: BULB. INOPERATIVE. SERVICE DOOR EMERGENCY LIGHT HAS ONE BULB INOPERATIVE. REPLACED BULB IAW AMM 33-51-13.
- [SDR REXA2014070100646](https://openairdocs.org/sdr/REXA2014070100646), Jul 1, 2014: INVERTER. INOPERATIVE. SECTION OF EMER FLOOR LIGHT STRIP INOPERATIVE. R & R NR 2 INVERTER IAW AMM 33-51-07. OPERATIONAL CHECK GOOD.
- [SDR REXA2014060800574](https://openairdocs.org/sdr/REXA2014060800574), Jun 8, 2014: LIGHT. DISCONNECTED. EMER LIGHTS OUT FROM ROW 2 - 5. CONNECTED EMER LIGHT STRIP AT ROW 2 - 5 IAW AMM 33-51-01. NO FURTHER DISCREPANCY.
- [SDR REXA2014050100413](https://openairdocs.org/sdr/REXA2014050100413), May 1, 2014: BATTERY. DISCHARGED. WHEN PERFORMING SERVICE CHECK FOUND FLOOR TRACK EMERGENCY LIGHTS INOPERATIVE. R & R NR 2 EMERGENCY BATTERY IAW AMM 33-51-04, OPERATIONS CHECKED GOOD.
- [SDR REXA2014042000392](https://openairdocs.org/sdr/REXA2014042000392), Apr 20, 2014: CONTROL UNIT. FAULTY. BRAKES FEEL LIKE THEY ARE STICKING. COULDN’T TAXI SINGLE ENG. TEMP'S APPEAR NORMAL, 3'S. TAKES MORE POWER THAN NORMAL TO GET ACFT TO MOVE. PEDAL FEEL ISN`T NORM
- [SDR REXA2014012300136](https://openairdocs.org/sdr/REXA2014012300136), Jan 23, 2014: HYDRAULIC SYSTEM. CONTAMINATED. AFTER TAKEOFF WHILE GEAR WAS COMING UP, RECEIVED NR 3 HYD SIC LOW PRESS CAUTION, FOLLOWED BY A GEAR UP DISAGREE WARNING. THE MAIN GEAR WAS RED & THE NOSE GEAR W
- [SDR REXA2014012300134](https://openairdocs.org/sdr/REXA2014012300134), Jan 23, 2014: ACTUATOR. FAILED. FLAPS FAIL AT 20 AFTER TAKEOFF WOULD NOT RETRACT. -27C CLEAR NO DE-ICE FLUID APPLIED TODAY LAND WT 41000 IAW 165 KTS 1 MIN INTO FLT. R & R ALL 8 FLAP ACTUATORS 
- [SDR REXA2014011600121](https://openairdocs.org/sdr/REXA2014011600121), Jan 16, 2014: STRAP. BROKEN. FIRST OFFICER`S FLASHLIGHT BROKEN. REPLACED FIRST OFFICER`S FLASHLIGHT BREAKAWAY STRAP, NO FURTHER DEFECTS NOTED AT THIS TIME, AMM 25-60-00.
- [SDR REXA2014010200101](https://openairdocs.org/sdr/REXA2014010200101), Jan 2, 2014: BRACKET. DAMAGED. NOSE GEAR WOULD NOT COME UP, GEAR DISAGREE MASTER WARNING AFTER TAKEOFF, UP, DN, UP. COMPLIED WITH PA 05-018 REV. FOUND NLG CTR EXTENDED PROXIMITY SENSOR BRACKE
- [SDR REXA2013122802422](https://openairdocs.org/sdr/REXA2013122802422), Dec 28, 2013: LIGHT. INOPERATIVE. FLOOR EMERGENCY LIGHTS ARE OUT FROM ROW 9 AFT. DID OPS TEST OF THE BATTERY PACK EMERGENCY LIGHT, OPS CHECKED GOOD IAW AMM 33-51-04-740-801.
- [SDR REXA2013121302316](https://openairdocs.org/sdr/REXA2013121302316), Dec 12, 2013: BULKHEAD. CHAFED. FS 621 BULKHEAD 29.5 INCHES ABOVE THE FLOOR HAS 6 CHAFE MARKS FROM SCREW HEADS. REPAIRED IAW REO 601R-53-61-2155.
- [SDR REXA2013111302253](https://openairdocs.org/sdr/REXA2013111302253), Nov 13, 2013: INVERTER. INOPERATIVE. EMERGENCY FLOOR PATH LIGHTING, ROWS 2 THRU 5 INOPERATIVE. R & R INVERTER PS2LY IAW AMM 33-51-07. OPS CHECK GOOD.
- [SDR REXA2013100201757](https://openairdocs.org/sdr/REXA2013100201757), Sep 30, 2013: BATTERY PACK. DISCHARGED. LEFT EMERGENCY LIGHT INOPERATIVE. CHARGED EMERGENCY LIGHT BATTERY PACK, OPS CHECKED GOOD IAW AMM 33-51-04.
- [SDR REXA2013100201756](https://openairdocs.org/sdr/REXA2013100201756), Sep 30, 2013: BATTERY PACK. DISCHARGED. EMERGENCY LIGHTS INOPERATIVE AT ROW 2 AND 5. CHARGED NR 2 BATTERY, LIGHTS OPS CHECKED GOOD IAW AMM 33-51-04.
- [SDR REXA2013071401367](https://openairdocs.org/sdr/REXA2013071401367), Jul 14, 2013: LIGHT. INOPERATIVE. EMERGENCY LIGHT OUT ON OVERHEAD PANEL. COMPLIED WITH OPS CHECK IAW AMM 33-50-04. OPS CHECKED NORMAL. OK FOR SERVICE.

All 81: https://openairdocs.org/deregistered/N8932C-2025-10-01/reports.md

## NTSB investigations (1)

From the NTSB's public API. Aircraft are matched to registry aircraft by N-number and event date, checked against the reported serial number, make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [NTSB CHI05FA077](https://openairdocs.org/ntsb/CHI05FA077), Mar 12, 2005: Bombardier CL-600-2B19 (N8932C), Milwaukee, WI, substantial damage. Probable cause: the captain's failure to adequately compensate for the crosswind conditions, and his failure to maintain directional control during landing. Contributing factors include the captain's failure to land…

## 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 20100903045771I](https://openairdocs.org/incident/20100903045771I), Sep 3, 2010: Bombardier CL-600-2B19 (N8932C), Minneapolis, MN, Minor damage. Crew was careless in pushing back a pinnacle crj into a waiting crj, poi is requiring retraining of ground crew.
- [Accident 20050311024829A](https://openairdocs.org/incident/20050311024829A), Mar 11, 2005: Cndair CL6002B19 (N8932C), Milwaukee, WI, Substantial damage. (-23) On March 11, 2005, at 2302 central daylight time, a Bombardier CL-600-2B, N8932C, operated by pinnacle aviation as "flagship 2823" received substantial…

## Other aircraft with N8932C

- [Cancelled 1995-03-20](https://openairdocs.org/deregistered/N8932C-1995-03-20): Caddell Lynn MANGOOS A1, S/N 1. Triennial form not returned. Owner: [Caddell H Lynn](https://openairdocs.org/faa-owner/CADDELL%20H%20LYNN), [Avondale, AZ](https://openairdocs.org/faa-place/AZ/Avondale)
- [Cancelled (date not recorded)](https://openairdocs.org/deregistered/N8932C-undated): Piper PA-22, S/N 221534. N-number assigned, not yet registered

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