# N8903A: 2004 Bombardier CL-600-2B19, registration cancelled 2024-12-23

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: December 23, 2024
- Exported to: Kenya
- Status when cancelled: Valid registration
- Airframe: [Bombardier CL-600-2B19](https://openairdocs.org/model/bombardier-cl-600-2b19) (registry code 1390008)
- 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: 7903
- Year built: 2004
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: February 2, 2004
- Certificate issued: April 8, 2024
- Last registry action: April 8, 2024
- Mode S code: AC4816
- Owner when cancelled: [Bank Of Utah Trustee](https://openairdocs.org/faa-owner/BANK%20OF%20UTAH%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/N8903A
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=8903A
- Page: https://openairdocs.org/deregistered/N8903A-2024-12-23

From the FAA registry file of November 5, 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 (63, newest 50)

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

- [SDR REXA2022081601867](https://openairdocs.org/sdr/REXA2022081601867), Aug 6, 2022: INVERTER. INOPERATIVE. LH INTERIOR EMERGENCY DOOR BOTTON SIGN INOP. R/R INVERTER @ LOCATION FS 424L IAW CRJ 200 AMM 31-5-07. OPS CHECK GOOD. PN ON/OFF 5925-7.
- [SDR SWIA2020022748868](https://openairdocs.org/sdr/SWIA2020022748868), Feb 27, 2020: WARNING MESSAGE. MULTIPLE FAIL. AFTER TAKE WE GOT STEERING INOP CAUTION MESSAGE . FOLLOW BY A WOW IMPUT CAUTION AND A WOW OUTPUT FAIL STATUS MESSAGE C/W QRH AND RETURN TO FIELD WITH NO OVER WE
- [SDR SWIA20190405731](https://openairdocs.org/sdr/SWIA20190405731), Apr 4, 2019: UPLOCK. FAILED. ON APPROACH RIGHT GEAR DISAGREE WARNING MESSAGE. CYCLED GEAR, ALL THREE GREEN INDICATION. LANDED WITHOUT INCIDENT. (FLT#7427) REMOVED AND REPLACED RT MLG UPLOCK
- [SDR SWIA2018060444750](https://openairdocs.org/sdr/SWIA2018060444750), May 20, 2018: STRAP. CORRODED. CABIN FLOORBEAM STRAP CORRODED AT BS 559, LBL 35. REMOVE AND REPLACED THE STRAP IAW SRM.
- [SDR SWIA2018060444749](https://openairdocs.org/sdr/SWIA2018060444749), May 12, 2018: FLOORBEAM. CORRODED. FLOORBEAM FITTING AT BS 615, LBL 27 HAD CORROSION ON THE OTBD FLANGE. PERFORMED A REPAIR TO THE FLOORBEAM IAW REO.
- [SDR SWIA2018060444748](https://openairdocs.org/sdr/SWIA2018060444748), May 11, 2018: FLOOR SUPPORT. CORRODED. LBL 27 FLOOR SUPPORT UPPER CAP INBOARD AND OUTBOARD FLANGES CORRODED BETWEEN BS 569 AND 610. REMOVED AND REPLACED THE FLOOR SUPPORT IAW REO.
- [SDR SWIA2018060444747](https://openairdocs.org/sdr/SWIA2018060444747), May 11, 2018: FLOOR SUPPORT. CORRODED. LEFT FLOOR SUPPORT CORRODED AT NUTPLATE LOCATIONS BETWEEN BS 574 AND 621 AND ONE SHEARED RIVET AT BS 589. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM.
- [SDR SWIA2018060444746](https://openairdocs.org/sdr/SWIA2018060444746), May 8, 2018: SKIN. CHAFED. LEFT INBD FLAP VANE LEADING EDGE SKIN CHAFED NEAR OTBD END. REPLACED THE FLAP VANE LEADING EDGE SKIN IAW SRM.
- [SDR SWIA2018060444745](https://openairdocs.org/sdr/SWIA2018060444745), May 8, 2018: SKIN. CHAFED. LEFT INBD FLAP VANE LEADING EDGE SKIN CHAFED NEAR INBD END. REMOVED AND REPLACED FLAP VANE IAW SRM.
- [SDR SWIA2018060444744](https://openairdocs.org/sdr/SWIA2018060444744), May 8, 2018: VANE. CHAFED. RIGHT INBD FLAP VANE TRAILING EDGE UPPER SURFACE CHAFED NEAR THE INBD END OF VANE. BLENDED THE DAMAGE IAW SRM AND REO.
- [SDR SWIA201642205](https://openairdocs.org/sdr/SWIA201642205), May 20, 2016: VANE. CHAFED. LEFT INBD FLAP VANE L/E MIDDLE SECTION CHAFED. R & R LT INBD FLAP VANE L/E MIDDLE SECTION AT APPROXIMATELY LT WS 93 - 130 IAW SRM AND EA.
- [SDR SWIA201642204](https://openairdocs.org/sdr/SWIA201642204), May 17, 2016: VANE. CHAFED. RIGHT INBD FLAP VANE LE CHAFED INBD SIDE. THE L/E SECTION WAS REMOVED, NEW OTBD MID SECTION, PN: 601R14303-52, WAS INSTALLED IAW SRM.
- [SDR SWIA201541253](https://openairdocs.org/sdr/SWIA201541253), Jun 4, 2015: BATTERY PACK. INOPERATIVE. ALL EMERGENCY LIGHTS ARE INOPERATIVE. REPLACED NR 1 AND 2 EMERGENCY BATTERY PACKS IAW AMM. OPS CHECKED GOOD.
- [SDR REXA2014100301015](https://openairdocs.org/sdr/REXA2014100301015), Oct 3, 2014: LIGHT. INOPERATIVE. EMERGENCY STRIP LIGHT AT 1C INOPERATIVE. R & R EMER FLOOR LIGHT STRIP AT 1C IAW AMM 33-51-01. OPERATIONS CHECKED GOOD, OK FOR SERVICE.
- [SDR REXA2014092701001](https://openairdocs.org/sdr/REXA2014092701001), Sep 27, 2014: DOOR SEAL. DIRTY. LOUD SQUEAL FROM MAIN CABIN DOOR DURING DESCENT. PRESSURIZATION WAS NORMAL. INSPECTED DOOR SEAL & CLEANED SEAL IAW 52-11-10. OPERATIONS CHECKED DOOR, NO DEFECT 
- [SDR REXA2014060200546](https://openairdocs.org/sdr/REXA2014060200546), Jun 2, 2014: B-NUT. LOOSE. GOT A VERY STRONG SMELL OF FUEL IN FLIGHT CHECK WITH THE FLIGHT ATTENDANT & SHE DID NOT SMELL ANYTHING IN THE CABIN, ALL INDICATIONS NORMAL. WORE O2 MASK TO LAN
- [SDR REXA2014052800531](https://openairdocs.org/sdr/REXA2014052800531), May 28, 2014: CONNECTOR. NOT SEATED. FLOOR TRACK EMERGENCY LIGHT STRIP INOPERATIVE ROW 1. RESEATED CONNECTOR FOR AFFECTED STRIP OPERATIONS CHECKED GOOD IAW AMM 33-51-21.
- [SDR REXA2014041800389](https://openairdocs.org/sdr/REXA2014041800389), Apr 18, 2014: BATTERY. DISCHARGED. ON PREFLIGHT FOUND FIRST OFFICER'S FLASHLIGHT DEAD. REPLACED BATTERY IN FLASHLIGHT IAW STANDARDS PRACTICES CH 20.
- [SDR REXA2014041600067](https://openairdocs.org/sdr/REXA2014041600067), Apr 11, 2014: SKIN. CORRODED. LOWER WING PLANK ACCESS HOLE FOR PANEL 510AB HAS CORROSION MEASURING 10" X 0.185" X 0.007" DEEP. REPAIRED IAW REO 601R-57-21-030.
- [SDR REXA2014041400064](https://openairdocs.org/sdr/REXA2014041400064), Apr 11, 2014: SKIN. CORRODED. LEFT LOWER WING PLANK ACCESS HOLE 540DB HAS CORROSION AROUND NON-CRITICAL REGION, MEASURING 4 INCHES X 0.185 INCHES X 0.001 INCHES DEEP. REPAIRED IAW REO 601R-5
- [SDR REXA2014041400063](https://openairdocs.org/sdr/REXA2014041400063), Apr 11, 2014: SKIN. GOUGED. RIGHT WING LOWER SKIN SURFACE GOUGED ADJACENT TO ACCESS PANEL 650LB APPROX WS 341. REPAIRED IAW SRM 57-21-31.
- [SDR REXA201404140062](https://openairdocs.org/sdr/REXA201404140062), Apr 11, 2014: ANGLE. CORRODED. FS 621 ANGLE BETWEEN LBL 9 & LBL 27 HAS CORROSION AROUND 2 FASTENER HOLES MEASURING 0.007 INCHES DEEP MAX. REPAIRED IAW SRM 53-00-00.
- [SDR REXA2014041400061](https://openairdocs.org/sdr/REXA2014041400061), Apr 11, 2014: FITTING. CRACKED. FS 621 BULKHEAD LINTEL FITTING CRACKED. REPAIRED IAW REO 601R-53-61-1230.
- [SDR REXA2014041300057](https://openairdocs.org/sdr/REXA2014041300057), Apr 11, 2014: SKIN. CORRODED. RIGHT WING LOWER PLANK ACCESS HOLE 650AB HAS CORROSION AT NON-CRITICAL AREAS 2.0 INCHES X 0.185 INCHES X 0.002 INCHES DEEP AT WS 163.00. REPAIRED IAW REO 601R-5
- [SDR REXA2014041300056](https://openairdocs.org/sdr/REXA2014041300056), Apr 11, 2014: SKIN. CORRODED. RIGHT WING LOWER PLANK ACCESS HOLE 640DB HAS CORROSION AT NON-CRITICAL AREAS 2.0 INCHES X 0.185 INCHES X 0.001 INCHES DEEP AT WS 95.95. REPAIRED IAW REO 601R-57
- [SDR REXA2014041300055](https://openairdocs.org/sdr/REXA2014041300055), Apr 11, 2014: SKIN. CORRODED. RIGHT WING LOWER PLANK ACCESS HOLE 640BB HAS CORROSION AT NON-CRITICAL AREAS 7.0 INCHES X 0.185 INCHES X 0.002 INCHES DEEP AT WS 54.897. REPAIRED IAW REO 601R-5
- [SDR REXA2014041300054](https://openairdocs.org/sdr/REXA2014041300054), Apr 11, 2014: SKIN. CORRODED. RIGHT WING LOWER PLANK ACCESS HOLE 610AB HAS CORROSION AT NON-CRITICAL AREAS 3.75 INCHES X 0.185 INCHES X 0.002 INCHES DEEP AT WS 12.245. REPAIRED IAW REO 601R-
- [SDR REXA2014041200053](https://openairdocs.org/sdr/REXA2014041200053), Apr 10, 2014: SKIN. CORRODED. RIGHT WING LOWER WING PLANK ACCESS HOLE 650FB HAS CORROSION AT NON-CRITICAL AREAS MEASURING 1.0 INCHES X 0.185 INCHES X 0.002 INCHES DEEP AT WS 274.319. REPAIRE
- [SDR REXA2014041200052](https://openairdocs.org/sdr/REXA2014041200052), Apr 10, 2014: SKIN. CORRODED. RIGHT WING LOWER WING PLANK ACCESS HOLE 650BB HAS CORROSION AT NON-CRITICAL AREAS MEASURING 1.75 INCHES X 0.185 INCHES X 0.001 INCHES DEEP AT WS 188.04. REPAIRE
- [SDR REXA2014040800049](https://openairdocs.org/sdr/REXA2014040800049), Apr 8, 2014: BULKHEAD. DENTED. FS 621 PRESS BULKHEAD FWD SIDE HAS A DENT APPROXIMATELY 6 INCHES OTBD OF RBL 27 & 8 INCHES UP FROM THE FLOOR MEASURING 3.45 INCHES X 3.4 INCHES X 0.041 INCHES D
- [SDR REXA2014041000050](https://openairdocs.org/sdr/REXA2014041000050), Apr 7, 2014: BULKHEAD. CHAFED. FS 621 BULKHEAD FWD SIDE HAS 10 MARKS FROM FASTENERS CHAFE BETWEEN 15 INCHES & 30 INCHES FROM FLOOR & LBL 27 & RBL 27.5 UP TO 0.008 INCHES DEEP. REPAIRED IAW RE
- [SDR REXA2014040500044](https://openairdocs.org/sdr/REXA2014040500044), Apr 2, 2014: SKIN. GOUGED. GOUGE IN THE RT LOWER WING SKIN AT WS 330.25. THE AREA AFTER CLEAN UP MEASURES 1.90” X .800” X .003” DEEP. REPAIRED IAW CRJ257-02409.
- [SDR REXA2014040500046](https://openairdocs.org/sdr/REXA2014040500046), Apr 1, 2014: FITTING. CRACKED. FS 280 OTBD CLIP AT RBL 9 CRACKED. REPAIRED IAW REO 601R-53-11-171.
- [SDR REXA2014040400042](https://openairdocs.org/sdr/REXA2014040400042), Apr 1, 2014: SKIN. CORRODED. RT & LT LOWER WINGS SKINS AT AFT EDGES OF PANEL 193AB FRETTING CORROSION & CHAFFING. RT SIDE 0.025" DEEP. LT SIDE 0.015" DEEP. REPAIRED IAW REO 601R-57-21-880.
- [SDR REXA2014040300041](https://openairdocs.org/sdr/REXA2014040300041), Apr 1, 2014: SKIN. GOUGED. RIGHT WING LOWER SKIN SURFACE GOUGED ADJACENT TO ACCESS PANEL 650LB. BLENDED AND IS WITHIN LIMITS IAW SRM 57-21-31.
- [SDR REXA2014032000308](https://openairdocs.org/sdr/REXA2014032000308), Mar 20, 2014: FLAP. MALFUNCTIONED. FLAPS FAIL EICAS, OCCURRED IN FLT ON APPROACH DURING FLAP EXTENSION. FAILED AT FLAP 30 DEG, AIRSPEED 160, TIME INTO FLIGHT 1 HR 10MIN. OAT +5 DEG C TAT. COMPLET
- [SDR REXA2014030400252](https://openairdocs.org/sdr/REXA2014030400252), Mar 4, 2014: SEAL. MISSING. FLIGHT DECK PBE IS MISSING A SEAL. RE SECURED FLIGHT DECK PBE SEAL IAW CRJ AMM 25-63-00.
- [SDR REXA2013101001769](https://openairdocs.org/sdr/REXA2013101001769), Oct 10, 2013: LIGHT. DAMAGED. EMERGENCY EXIT FLOODLIGHT ON GALLEY BY SERVICE DOOR DAMAGED. REPLACED EMERGENCY LIGHT IAW AMM 33-51-19. OPS TESTED OK.
- [SDR REXA2013011400144](https://openairdocs.org/sdr/REXA2013011400144), Jan 14, 2013: LIFE VEST. UNSERVICEABLE. ONE INFANT LIFE VEST BAG TORN. COMPLIED WITH PA 25-096A BY INSTALLING INFANT LIFE VEST.
- [SDR REXA2083001201301](https://openairdocs.org/sdr/REXA2083001201301), Aug 30, 2012: BRACKET. CRACKED. LEFT ENGINE THRUST REVERSER STOW SWITCH BRACKET CRACKED. REMOVED AND REPLACED THRUST REVERSER SWITCH MOUNTING PLATE ASSY IAW AMM 78-37-01. OPS CHECKED GOOD.
- [SDR REXA2012082301091](https://openairdocs.org/sdr/REXA2012082301091), Aug 22, 2012: ANGLE. CRACKED. CRACK FOUND IN FS 559 SEMI-PRESSURE BULKHEAD CAP ANGLE AT RBL18 AND LBL18. REPAIRED IAW REO 601R-53-41-260 AND 601R-53-41-609.
- [SDR REXA2012071301155](https://openairdocs.org/sdr/REXA2012071301155), Jul 13, 2012: LIGHT. INOPERATIVE. CABIN OVERHEAD EMERGENCY EXIT FLOOD LIGHT AT SEAT 3B INOPERATIVE.
- [SDR REXA2012041000493](https://openairdocs.org/sdr/REXA2012041000493), Apr 10, 2012: SWITCH. FAILED. RIGHT THRUST REVERSER WOULD NOT DEPLOY ON LANDING. REMOVED AND REPLACED RT THRUST REVERSER DEPLOY SWITCH IAW AMM 78-37-01. OPS CHECKED GOOD, OK FOR SERVICE.
- [SDR REXA201100726](https://openairdocs.org/sdr/REXA201100726), Oct 14, 2011: SENSING ELEMENT. DEFECTIVE. RT 14TH DUCT MASTER WARNING ON CLIMBOUT - FORWARD SECTION OF ENGINE BLEED SHOWED RED. REMOVED AND REPLACED RT 14TH STAGE PYLON DUCT HEAT SENSE ELEMENT A 58WK IA
- [SDR REXA201100664](https://openairdocs.org/sdr/REXA201100664), Oct 7, 2011: BULKHEAD. CRACKED. FS 202.75 BULKHEAD HAS A CRACK INDICATION LOCATED AT 9 O’CLOCK POSITION AT THE PASS THROUGH HOLE (REF PA 53-015). REPAIRED IAW BOMBARDIER REO 601R-53-11-563 AND
- [SDR REXA201100549](https://openairdocs.org/sdr/REXA201100549), Aug 3, 2011: STRUCTURE. DAMAGED. RUDDER DAMAGE AT RS 131.17 TO RS 133.33 FWD LT SIDE DAMAGE IS APPROX 1.5L X 1.2W. REPAIRED IAW BOMBARDIER REO 601R-55-41-140.
- [SDR REXA201100463](https://openairdocs.org/sdr/REXA201100463), Jul 18, 2011: FLOOR SUPPORT. CRACKED. FLOOR SUPPORT INTERCOSTAL AT FS 484.0 IS CRACKED AT RBL 36.0. REPAIRED IAW REO 601R-53-41-059 AND BSC S/R 601R-53-00030B.
- [SDR REXA201100462](https://openairdocs.org/sdr/REXA201100462), Jul 18, 2011: INTERCOSTAL. CRACKED. FLOOR SUPPORT INTERCOSTAL AT FS 484.0 IS CRACKED AT LBL 36.0. REPAIRED IAW REO 601R-53-41-059 AND BSC S/R 601R-53-00030B.
- [SDR REXA201100464](https://openairdocs.org/sdr/REXA201100464), Jul 17, 2011: STRUCTURE. CORRODED. MINOR CORROSION AROUND FASTENERS FROM FS 559+16 - FS 559+32 STR 26L TO 26R. REMOVED MINOR CORROSION AROUND FASTENERS FROM FS 559+16 TO FS 559+32 STR 26L TO 26R 
- [SDR REXA201100497](https://openairdocs.org/sdr/REXA201100497), Jul 16, 2011: SILL. CORRODED. TWO EACH NUT PLATE HOLES HAVE MINOR CORROSION AT FS 559+96 RBL 45 ON FLOOR SILL. REPAIRED IAW BOMBARDIER SERVICES CORP EO 601R-53-L00118 AND ASSOCIATED 8110-3 D

All 63: https://openairdocs.org/deregistered/N8903A-2024-12-23/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 20100903045781I](https://openairdocs.org/incident/20100903045781I), Sep 3, 2010: Bombardier CL-600-2B19 (N8903A), Minneapolis, MN, Minor damage. One pinnacle crj was pushed back from gate into another pnnacle crj waiting for it's gate.
- [Incident 20080317833069I](https://openairdocs.org/incident/20080317833069I), Mar 17, 2008: Cndair CL6002B19 (N8903A), La Crosse, WI, No damage. (-23) The flight attendant was initially described as unruly because she had an altercation with the gate agent in La Crosse (lse) as a result of a passenger…

## Other aircraft with N8903A

- [Cancelled 1953-10-07](https://openairdocs.org/deregistered/N8903A-1953-10-07): Beech B35, S/N D-2601. Owner: [Dr Prout F J](https://openairdocs.org/faa-owner/DR%20PROUT%20F%20J), [Ceder Rapdis, IA](https://openairdocs.org/faa-place/IA/Ceder%20Rapdis)

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