# N528CA: 2003 Bombardier CL-600-2B19, registration cancelled 2019-06-26 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: June 26, 2019 - Exported to: United Kingdom - 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: 7841 - Year built: 2003 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: September 19, 2003 - Certificate issued: October 15, 2018 - Last registry action: November 14, 2018 - Mode S code: A6A6D9 - Owners when cancelled: [Delta Material Services LLC](https://openairdocs.org/faa-owner/DELTA%20MATERIAL%20SERVICES%20LLC), [Dept 673](https://openairdocs.org/faa-owner/DEPT%20673) - Location: [Atlanta, GA](https://openairdocs.org/faa-place/GA/Atlanta) - Owner type: LLC - Owner's area on the map: 33.6604° N, 84.3865° W: Placed by OpenAirDocs at the center of ZIP code 30354, within about 2 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N528CA - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=528CA - Page: https://openairdocs.org/deregistered/N528CA-2019-06-26 From the FAA registry file of October 31, 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 (46) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR ASOA20161206247](https://openairdocs.org/sdr/ASOA20161206247), Dec 6, 2016: BATTERY PACK. CORRODED. EMERGENCY LIGHTS OUT IN GALLEY AND MID CABIN. REMOVED AND REPLACED BATTERY PACK ASSY PER AMM 33-51-04. OPS CHECKED GOOD, NO FURTHER DEFECTS NOTED. - [SDR ASOA2014041810381](https://openairdocs.org/sdr/ASOA2014041810381), Apr 17, 2014: LAMP. BURNED OUT. FWD ORANGE SEGMENT OF EMERGENCY FLOOR PATH LIGHTS INOPERATIVE. R & R EMERGENCY FLOOR PATH LIGHT FLEXIBLE LAMP NR 1 IAW AMM 33-51-01. OPS CHECK GOOD. SDR CLOSED. - [SDR ASOA2014031010107](https://openairdocs.org/sdr/ASOA2014031010107), Mar 6, 2014: LIGHT. INOPERATIVE. CABIN FLOOR FORWARD MOST EMERGENCY LIGHT STRIP, ORANGE, INOPERATIVE. PERFORMED THE OPS TEST OF THE EMERGENCY FLOOD LIGHTS IAW AMM 33-51-00. OPS CHK GOOD. - [SDR ASOA2013090608962](https://openairdocs.org/sdr/ASOA2013090608962), Sep 3, 2013: CONNECTOR. DISCONNECTED. EMERGENCY LIGHT STRIP ABOVE PAX DOOR DOES NOT ILLUMINATE. REINSTALLED CONNECTOR FOR EMERGENCY EXIT SIGN IAW AMM 33-51-01. - [SDR ASOA2013050603474](https://openairdocs.org/sdr/ASOA2013050603474), Apr 30, 2013: BATTERY PACK. DISCHARGED. EMERGENCY LIGHT AT ROW 5 INOPERATIVE. FOUND BATTERY PACK TO BE DISCHARGED. CHARGED BATTERY PACK. OPS CHECKED GOOD IAW AMM 33-51-00. - [SDR ASOA2013050303472](https://openairdocs.org/sdr/ASOA2013050303472), Apr 22, 2013: SKIN. DAMAGED. RT OTBD FLAP DAMAGED ON T/E. 41" FROM INBD END, DAMAGE IS APPROX 10" L. COMPLIED WITH MAJOR REPAIR IAW REO 601R-57-53-041, REV A, DATED 2004/05/07. COMPLIED WIT - [SDR ASOA2013050303471](https://openairdocs.org/sdr/ASOA2013050303471), Apr 8, 2013: FLOOR PANEL. DENTED. PRESSURE FLOOR SKIN HAS 1 EA DENT MEASURING 4.256" LONG X 1.980" WIDE X .015" DEEP AND HAS 5 EA GOUGES WITH MAX DAMAGE BEING .730" LONG X .062" WIDE X .008" DEE - [SDR ASOA2013050303470](https://openairdocs.org/sdr/ASOA2013050303470), Apr 8, 2013: BULKHEAD. DAMAGED. AT FS 621.00 BULKHEAD LBL 30 WL 135 THERE IS A DRILL START .150" WIDE .031" DEEP AND .150" FROM CENTER OF FIRE BLOCK HOLE/NUTPLATE AT .1562" TO CENTER OF DRILL - [SDR ASOA2013050203469](https://openairdocs.org/sdr/ASOA2013050203469), Apr 6, 2013: BUSHING. DAMAGED. LT BUSHINGS AT HORIZONTAL STAB HINGE ARE DAMAGED. REPAIRED IAW REO 601R-55-00-045 REV B, 2013/04/27. MAJOR REPAIR - [SDR ASOA2013042503445](https://openairdocs.org/sdr/ASOA2013042503445), Apr 5, 2013: INTERCOSTAL. CRACKED. FS 621.00 CRACKED INTERCOSTAL STRINGER 13L,. REMOVED CRACKED INTERCOSTAL IAW SRM 51-42-21. LOCATED & DRILLED NEW INTERCOSTAL IAW SRM 51-40-11. INSTALLED INTERCO - [SDR ASOA2013042503444](https://openairdocs.org/sdr/ASOA2013042503444), Apr 4, 2013: BULKHEAD. CRACKED. FOUND REAR PRESSURE BULKHEAD WEB HAS INDICATION NOTED AT LBL 27.50 WL 130 APPROX .2" IN LENGTH 60 PERCENT FSH FAILED NDT INSPECTION. REPAIRED IAW REO 601R-53-61 - [SDR ASOA2013042503443](https://openairdocs.org/sdr/ASOA2013042503443), Apr 3, 2013: BULKHEAD. CRACKED. FOUND FS 559 BULKHEAD WEB RT SIDE HAS INDICATION NOTED APPROX .3" IN LENGTH 50 PERCENT FSH AT WL 59.10 INBD OF RBL 18.0. FAILED NDT INSPECTION. REPAIRED IAW REO - [SDR ASOA2013042503442](https://openairdocs.org/sdr/ASOA2013042503442), Apr 3, 2013: POST. CRACKED. FOUND FS 409.00+128 VERTICAL POST BL 0.00 RT SIDE HAS INDICATION NOTED AT AFT FLANGE RADIUS WL 69.0 APPROX .2" IN LENGTH 50 PERCENT FSH. FAILED NDT INSPECTION. - [SDR ASOA2013020702965](https://openairdocs.org/sdr/ASOA2013020702965), Feb 3, 2013: CIRCUIT CARD. UNSERVICEABLE. UNCOMMANDED FULL RT RUDDER DEFECTION IN FLT ON A/P, NO EICAS MSG OVER POWERED, DISCONNECTED A/P AND YD, WERE ABLE TO RETRIM (ENROUTE, ACFT DIVERTED TO GSO DUE T - [SDR ASOA2012081702076](https://openairdocs.org/sdr/ASOA2012081702076), Aug 13, 2012: SWITCH. ILLUMINATED. LEFT THRUST REVERSER UNLOCK MESSAGE. EMERGENCY DECLARED. R & R STOW SWITCH IAW AMM 78-37-01. OPS CHECKED GOOD. - [SDR ASOA201201674](https://openairdocs.org/sdr/ASOA201201674), May 22, 2012: SENSING ELEMENT. BROKEN. LT 10TH DUCT IN FLIGHT FOLLOWED CHECK LIST IT DID NOT GO OUT. DELCARED EMERGENCY AND RETURNED TO ATC (AFTER T/O ACFT RETURNED TO DEPARTURE AFTER T/O -- EMERGENC - [SDR ASOA201201237](https://openairdocs.org/sdr/ASOA201201237), Apr 9, 2012: FITTING. CRACKED. REAR PRESSURE BULKHEAD CRACKED AT MACHINE FITTING (LINTEL FITTING) AT CARGO DOOR CUTOUT. REPAIRED IAW REO 601R-53-61-1230, REV C. - [SDR ASOA201201235](https://openairdocs.org/sdr/ASOA201201235), Apr 9, 2012: PRESSURE BLKHD. CRACKED. REAR PRESSURE BULKHEAD CRACKED AT RBL 36.20. REPAIRED IAW REO 601R-53-61-1285, REV D AND REO 601R-53-61-1285 REV D. - [SDR ASOA201201219](https://openairdocs.org/sdr/ASOA201201219), Apr 6, 2012: WIRE. BROKEN. WIRE BROKEN ON EMERGENCY FLOOR TRACK LIGHTING AT FWD END. REPLACED CRIMP CONNECTOR ON RT FWD EMERGENCY LIGHT FLOOR STRIP LIGHTING WIRE IAW ESPM 20-17-00. OPS TE - [SDR ASOA201101683](https://openairdocs.org/sdr/ASOA201101683), Sep 9, 2011: CONNECTOR. DAMAGED. EMERGENCY LIGHTS INOPERATIVE, CENTER TWO SECTIONS AND FWD WHITE SECTION AT FLOOR POSITIONS. R & R FWD WHITE EMERG LIGHT SECTION IAW AMM 33-51-01-000-801 AND 33- - [SDR ASOA201101559](https://openairdocs.org/sdr/ASOA201101559), Aug 22, 2011: ATTACH FITTING. CRACKED. CLIP AT FS 484.00, RBL 27 CRACKED. R & R A NEW CLIP AT FS 484.00, RBL 27 IAW SRM 51-42-21. THIS REPAIR IS CLASSIFIED AS A MINOR REPAIR. - [SDR ASOA201101558](https://openairdocs.org/sdr/ASOA201101558), Aug 22, 2011: BEAM. CRACKED. FS 280 TRANSVERSE BEAM CRACKED IN WEB OTBD OF RBL 9. THIS DISCREPANCY AND THE AFT J-ANGLES ON JOB 8784121, OP 159 IS BEING REPAIRED AS ONE IAW REO 601R-53-11-92 - [SDR ASOA201101557](https://openairdocs.org/sdr/ASOA201101557), Aug 22, 2011: FLOORBEAM. CRACKED. FS 280 TRANVERSE BEAM UPPER AFT J-ANGLE CRACKED OTBD OF LBL 9 AND RBL 9. REPAIRED IAW REO 601R-53-11-926 REV B. - [SDR ASOA201101556](https://openairdocs.org/sdr/ASOA201101556), Aug 22, 2011: ANGLE. CORRODED. PASSENGER DOOR CUTOUT LOWER ANGLE HAS CORROSION AROUND HOLE FOR PROXIMITY SENSOR. REMOVED CORROSION IAW SRM 51-21-06 AND FOUND THE REMOVED MATERIAL (0.003) WITH - [SDR ASOA201101555](https://openairdocs.org/sdr/ASOA201101555), Aug 22, 2011: ANGLE. CRACKED. CARGO DOOR FWD TRACK LOWER C-CHANNEL ANGLE CRACKED. R & R DAMAGED C-CHANNEL IAW SRM 51-41-06 & 51-41-04. REPAIR IS CLASSIFIED AS A MINOR REPAIR. - [SDR ASOA201101554](https://openairdocs.org/sdr/ASOA201101554), Aug 22, 2011: DRAG ANGLE. CRACKED. PASSENGER DOOR AFT DRAG ANGLE CRACKED. REPAIRE IAW REO 601R-52-11-513 AND REO NR 610R-52-11-513, REV A. - [SDR ASOA201101553](https://openairdocs.org/sdr/ASOA201101553), Aug 22, 2011: WEB. CRACKED. PASSENGER DOOR FWD WEB CRACKED AT 4TH RISER. REPAIRED IAW REO 601R-52-11-702. - [SDR ASOA201101522](https://openairdocs.org/sdr/ASOA201101522), Aug 17, 2011: DOOR. NONE. LEFT EMERGENCY OVERWING EXIT FAILS FUNCTION TEST, FORCE TO OPERATE HANDLE EXCEEDS 40 LBS. PERFORMED FUNCT TEST OF THE LT EMERGENCY EXIT IAW AMM 52-21-00-720-801 - [SDR ASOA201101072](https://openairdocs.org/sdr/ASOA201101072), May 27, 2011: ATTACH FITTING. CRACKED. FS 625, OBLIQUE CLIP IS CRACKED. REMOVED CLIP IAW SRM 51-42-20. COMPLIED WITH EDDY CURENT INSP IAW NDTM 51-20-06, PART 1 53-00-096, PART 6 AND COMFIRMED CRACK. - [SDR ASOA201101071](https://openairdocs.org/sdr/ASOA201101071), May 27, 2011: DOUBLER. CRACKED. LT SIDE FS 640.00 DOUBLER CRACKED AT CUTOUT RADIUS FOR ENGINE SUPPORT BEAM ATTACH POINT. REPAIRED. - [SDR REXA201100128](https://openairdocs.org/sdr/REXA201100128), Feb 16, 2011: WARNING SYSTEM. ACTIVATED. GEAR DISAGREE NOSE DOOR WARNING NOSE GEAR NEVER CAME UP DEFERRED PER MEL 32-30-01. - [SDR REXA201000234](https://openairdocs.org/sdr/REXA201000234), Oct 24, 2010: CONNECTOR. DIRTY. DURING CLIMB, PASSING 27000FT CARGO BOTTLE LOW CAUTION MESSAGE CAUTION MESSAGE EXTINGUISHED DESCENDING THROUGH 11000FT. REMOVED, CLEANED, RESECURED CONNECTOR ON - [SDR REXA201000136](https://openairdocs.org/sdr/REXA201000136), Sep 10, 2010: UNKNOWN. ODOR. FUMES IN COCKPIT/CABIN LED TO DIVERSION. APU OFF/BLEEDS ON ENGINES/SMELLED LIKE CIGARETTE BURNING/NO VISIBLE SMOKE. PERFORMED GROUND RUNS WITH BLEEDS ON ENGINES - [SDR REXA201000092](https://openairdocs.org/sdr/REXA201000092), Jun 7, 2010: SELECTOR VALVE. MALFUNCTIONED. UPON CLIMBOUT AFTER THE CLIMB CHECK, HAD A GEAR DISAGREE MSTR WARNING. THE NOSE GEAR WAS THE ONE IN DISAGREEMENT. THE F/O START THE QRH, THE WARNING WENT AWAY. - [SDR COMA0760474](https://openairdocs.org/sdr/COMA0760474), Jul 11, 2007: ECU. FAULTY. FLIGHT 5011 - FLAP FAIL CAUTION RECEIVED ON TAXI OUT. RETURNED TO GATE. REPLACED FECU. NO FURTHER DEFECTS. - [SDR COMA0760261](https://openairdocs.org/sdr/COMA0760261), Mar 15, 2007: WINDSHIELD. CRACKED. CAPTAIN'S WINDSHIELD INNER PANEL SHATTERED. PROCEEDED TO CVG WITHOUT INCIDENT. REPLACED CAPTAIN'S WINDSHIELD. - [SDR COMA0760150](https://openairdocs.org/sdr/COMA0760150), Feb 6, 2007: FLAP SYSTEM. MALFUNCTIONED. FLIGHT 5115 - DURING YUL APPROACH RECEIVED A FLAP FAIL CAUTION MESSAGE. COMPLIED WITH AD 2006-12-21 FLAP CAUTION MESSAGE -FIRST EVENT- MAINTENANCE ACTION, PARAG - [SDR COMA0760080](https://openairdocs.org/sdr/COMA0760080), Jan 26, 2007: SHAFT. DAMAGED. FLIGHT 5510 - FLAP FAIL MESSAGE AT 8 DEGREES. LANDED WITHOUT INCIDENT. PERFORMED EO 27-046 AD INCLUDING FLAP SHAFT REJUVENATION. NO FURTHER DEFECTS. - [SDR COMA0660501](https://openairdocs.org/sdr/COMA0660501), Aug 18, 2006: SKIN PANEL. CRACKED. PAX DOOR SECOND STEP DOWN FORWARD AND AFT SKINS CRACKED UNDER BRACKETS WHERE HAND RAILS STOW WHEN DOWN. AFT SKIN ALSO CRACKED THIRD STEP DOWN IN RADIUS OF TREAD - [SDR COMA0660103](https://openairdocs.org/sdr/COMA0660103), Jan 28, 2006: GENERATOR. FAULTY. FLIGHT 5104 - CLIMBING OUT OF AUS DURING GEAR RETRACTION, THE AIR DRIVE GENERATOR DEPLOYED, FLIGHT RETURNED TO THE FIELD. REPLACED THE ADG AUTO DEPLOY CONTROL P - [SDR COMA0560199](https://openairdocs.org/sdr/COMA0560199), Mar 21, 2005: WINDOW. CRACKED. FLIGHT 5380 PILOTS SIDE WINDOW CRACKED. REPLACED PILOTS SIDE WINDOW. - [SDR COMA0560072](https://openairdocs.org/sdr/COMA0560072), Jan 22, 2005: HYDRAULIC SYSTEM. LOW. FLIGHT 5045 - DURING APPROACH TO BOS, RECEIVED A GEAR DISAGREE FOLLOWED BY A HYDRAULIC NR 3 LOW PRESSURE CAUTION, CREW DECLARED AN EMERGENCY, FOLLOWED QRH AND L - [SDR COMA0460288](https://openairdocs.org/sdr/COMA0460288), Apr 23, 2004: PITOT LINE. CONTAMINATED. FLIGHT 5208 ABORTED TAKEOFF AT 75 KTS DUE TO INOPERATIVE STANDBY AIRSPEED INDICATION. PURGED WATER FROM THE STANDBY PITOT SYSTEM LINE. - [SDR COMA0460058](https://openairdocs.org/sdr/COMA0460058), Jan 14, 2004: CONTROL UNIT. MALFUNCTIONED. FLIGHT 5710 STAB TRIM AND MACH TRIM DISENGAGED DURING T/O. REPLACED THE HSTCU. - [SDR COMA0460009](https://openairdocs.org/sdr/COMA0460009), Dec 30, 2003: ENGINE. FLUCTUATES. FLIGHT 5732 N1 AND N2 AND F/F FLUCTUATING. COULD NOT DUPLCIATE. GROUND RUNS WERE NORMAL AND SATISFACTORY. - [SDR COMA0360420](https://openairdocs.org/sdr/COMA0360420), Sep 21, 2003: WARNING LIGHT. ILLUMINATED. DURING DECENT INTO DTW RECEIVED A FLAP FAIL CAUTION MESSAGE AT 20 DEGREE FLAP POSITION. COMPLIED WITH AD 98-20-01 FLAP CAUTION MESSAGE (FIRST EVENT) FLAP SYSTEM ## Other aircraft with N528CA - [Registered now](https://openairdocs.org/aircraft/N528CA): Cirrus Design SR22, S/N 11208, built 2026 - [Cancelled 1991-07-30](https://openairdocs.org/deregistered/N528CA-1991-07-30): Cessna 152, S/N 15279693. Second triennial mailing, no response. Owner: [Phillips Mark L F](https://openairdocs.org/faa-owner/PHILLIPS%20MARK%20L%20F), [Goleta, CA](https://openairdocs.org/faa-place/CA/Goleta) --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.