# N8907A: 2004 Bombardier CL-600-2B19, registration cancelled 2023-02-24 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: February 24, 2023 - 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: 7907 - Year built: 2004 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: February 18, 2004 - Certificate issued: December 17, 2021 - Last registry action: December 17, 2021 - Mode S code: AC48A2 - Owner when cancelled: [Delta Air Lines Inc](https://openairdocs.org/faa-owner/DELTA%20AIR%20LINES%20INC) - Location: [Atlanta, GA](https://openairdocs.org/faa-place/GA/Atlanta) - Owner type: Corporation - 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/N8907A - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=8907A - Page: https://openairdocs.org/deregistered/N8907A-2023-02-24 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 (69, newest 50) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR REXA2017111401174](https://openairdocs.org/sdr/REXA2017111401174), Nov 14, 2017: WIRE. BROKEN. PAX DOOR EMERGENCY EXIT SIGN INOPERATIVE. FOUND A BROKEN WIRE. REPAIRED THE WIRE IAW ESPM 20-16-00. OPS TESTED GOOD. - [SDR REXA2017101501099](https://openairdocs.org/sdr/REXA2017101501099), Oct 15, 2017: ELEMENT. MALFUNCTIONED. RT 14TH STAGE DUCT WARNING MESSAGE WITH AURAL AND CHIME WARNINGS. COMPLIED WITH QRH BY CLOSING THE 14TH STAGE SOV AND SELECTING 14TH STAGE ISOLATION VALVE TO OP - [SDR REXA2017083000950](https://openairdocs.org/sdr/REXA2017083000950), Aug 30, 2017: WHEEL. INOPERATIVE. ABORTED TAKEOFF, DUE TO UNABLE TO MAINTAIN DIRECTIONAL CONTROL. ABORTED AT LESS THAN 60 KTS NOSE WHEEL NEVER LEFT THE GROUND. CHECKED LT & RT NWS IAW AMM 32-51- - [SDR REXA2017040500429](https://openairdocs.org/sdr/REXA2017040500429), Apr 5, 2017: CONNECTOR. NOT SEATED. CABIN EMERGENCY LIGHTS ROWS 9 CD - 12 CD INOPERATIVE. SEATED THE CONNECTOR IAW AMM 33-51-01. OPS CHECKED GOOD. - [SDR REXA2016090301676](https://openairdocs.org/sdr/REXA2016090301676), Sep 3, 2016: PUMP. MALFUNCTIONED. LEFT ENGINE ROLLED BACK TO IDLE AT 1000 FT. N1 & ITT NORMAL FOR IDLE N2 70% ACCOMPLISHED QRH ENGINE SHUTDOWN. R & R THE ENGINE FUEL PUMP IAW AMM 73-11-01, R & R - [SDR REXA2016061001011](https://openairdocs.org/sdr/REXA2016061001011), Jun 10, 2016: CAP. BROKEN. AT SEAT 12D CONNECTION FOR FLOOR TRACK EMERGENCY LIGHTING BROKEN. R & R THE EMERGENCY FLOOR LIGHT END CAP, P40LY, IAW AMM 33-51-01, OPS CHECK GOOD. - [SDR REXA2016052800956](https://openairdocs.org/sdr/REXA2016052800956), May 28, 2016: COVER. UNSECURE. PLASTIC COVER OVER FLOOR EMERGENCY LIGHT NEAR 1CD, 2CD & 3CD ARE LOOSE & COMING UP. SECURED PLASTIC COVER AS REQUIRED. - [SDR REXA2016051900843](https://openairdocs.org/sdr/REXA2016051900843), May 19, 2016: COVER. UNSECURE. RIGHT REAR FLOOR COVERING FOR EMER LIGHTS CAME OFF. SECURED EMER LIGHT FLOOR COVER IAW AMM 33-51-01. OK FOR SERVICE. - [SDR REXA2016051600787](https://openairdocs.org/sdr/REXA2016051600787), May 16, 2016: COVER. LOOSE. FLOOR EMER LIGHT STRIP LOOSE. REINSTALLED PLASTIC COVER ON EMER FLOOR TRACK LIGHTING. - [SDR REXA2016050900711](https://openairdocs.org/sdr/REXA2016050900711), May 9, 2016: COVER. LOOSE. PLASTIC COVER OVER FLOOR EMER LIGHTING STRIP LOOSE NEXT TO FIRST TWO ROWS ON FIRST OFFICERS SIDE OF PLANE. SECURED EMER LIGHTING STRIP AS REQUIRED. - [SDR REXA2016042600657](https://openairdocs.org/sdr/REXA2016042600657), Apr 26, 2016: PBE. UNSERVICEABLE. COCKPIT PBE BAG TORN. REPLACED COCKPIT PBE AS REQUIRED IAW AMM 35-30-00 & SUBTASK 35-30-00-941-007, PN ON & OFF MR-10047N. - [SDR REXA2016021000149](https://openairdocs.org/sdr/REXA2016021000149), Feb 10, 2016: FLASHLIGHT. INOPERATIVE. FLIGHT ATTENDANT EMER FLASHLIGHT INOPERATIVE. OPENED DEFERRAL IAW MEL 25-61-04. ENTERED IN MM02 & PLACARD INSTALLED, OK FOR SERVICE. TEMP FLASHLIGHT PROVIDED IA - [SDR REXA2016020400146](https://openairdocs.org/sdr/REXA2016020400146), Feb 4, 2016: COWLING. CHAFED. OUTBOARD LE OF COWL 445AT, NEAR LATCH IS CHAFED. REPAIRED CHAFE IAW CMM 71-12-01 REPAIR SRS104. - [SDR REXA2016020300145](https://openairdocs.org/sdr/REXA2016020300145), Feb 3, 2016: POST. CRACKED. LEFT LOWER FITTING ON WINDSHIELD CENTER POST, AT FS 202.75 IS CRACKED. REMOVED LT LOWER FITTING & REPLACED WITH NEW FITTING IAW SRM 51-42-20. - [SDR REXA2016020200144](https://openairdocs.org/sdr/REXA2016020200144), Feb 2, 2016: SUPPORT ANGLE. BROKEN. RIGHT UPPER THRUST REVERSER TRACK STAND FAIRING, SUPPORT Z ANGLE BROKEN. R & R SUPPORT Z ANGLE IAW MM 20-42-06. - [SDR REXA2016012900148](https://openairdocs.org/sdr/REXA2016012900148), Jan 29, 2016: BRACKET. CRACKED. IN RIGHT WW THE BRAKE PRESS TRANSDUCER BRACKET IS CRACKED. R & R BRAKE PRESS TRANSDUCER BRACKET IN RT MLG WW IAW SRM 51-42-22 & SRM 51-41-02. - [SDR REXA2016012600142](https://openairdocs.org/sdr/REXA2016012600142), Jan 26, 2016: ATTACH ANGLE. CRACKED. LEFT WING INBD LE FUEL MANIFOLD, ATTACH ANGLE CRACKED AT OTBD LOWER RADIUS. REMOVED CRACK BY EDGE BLENDING IAW SRM 57-00-00. - [SDR REXA2016012500143](https://openairdocs.org/sdr/REXA2016012500143), Jan 25, 2016: SKIN. CHAFED. RIGHT WING INBD FLAP VANE LE IS CHAFED IN 3 AREAS. REMOVED & INSTALLED 3 EA LE SKINS IAW SRM 51-42-11. - [SDR REXA2016012300139](https://openairdocs.org/sdr/REXA2016012300139), Jan 23, 2016: DRAG ANGLE. CRACKED. PASSENGER DOOR AFT DRAG ANGLE CRACKED. REMOVED DAMAGED AREA, FABRICATED, LOCATED & INSTALLED REPAIR PARTS IAW REO 601R-52-11-513 REV B. RESTORED TO ORIGINAL FIN - [SDR REXA2016012100140](https://openairdocs.org/sdr/REXA2016012100140), Jan 21, 2016: PLATE. CRACKED. INBOARD FLAP LE PANEL 684JB, MOUNTING PLATE CRACKED. FABRICATED 2 EACH INBD FLAP LE PANEL 684JB MOUNTING PLATES IAW SRM 51-40-11. - [SDR REXA2016012000138](https://openairdocs.org/sdr/REXA2016012000138), Jan 20, 2016: DRAG ANGLE. CRACKED. RIGHT WW DRAG ANGLE ADJACENT TO BATT RIB CRACKED. REMOVED RT WW DRAG ANGLE & INSTALLED NEW DRAG ANGLE IAW SRM 51-42-21. - [SDR REXA2016011900141](https://openairdocs.org/sdr/REXA2016011900141), Jan 19, 2016: ANGLE. CRACKED. AFT ACCESSORY COMPARTMENT, AFT BULKHEAD, OTBD LBL 36, ANGLE IS CRACKED. R & R CRACKED ANGLE WITH A SERVICEABLE FABRICATED REPAIR ANGLE IAW SRM 51-42-21. - [SDR REXA2016011900135](https://openairdocs.org/sdr/REXA2016011900135), Jan 19, 2016: FITTING. CORRODED. BATHTUB FITTING AT FS 461.0 & OTBD OF RBL 9 IS CRACKED. REMOVED FITTING, LOCATED & INSTALLED NEW FITTING IAW SRM 51-40-11, 51-42-06 & 53-41-43. - [SDR REXA2016011800137](https://openairdocs.org/sdr/REXA2016011800137), Jan 18, 2016: FITTING. CRACKED. CLIP UNDER CARGO DOOR SILL AT FS 589.00 IS CRACKED. REMOVED CLIP UNDER CARGO DOOR SILL & REPLACED WITH NEW CLIP IAW SRM 51-42-20. - [SDR REXA2016011800136](https://openairdocs.org/sdr/REXA2016011800136), Jan 18, 2016: SEAT TRACK. CORRODED. SEAT RAIL BEAM, LBL 27, OTBD FLANGE, FS 574.00 TO FS 608.00, IS CORRODED AT FASTENER HOLES. R & R SEAT RAIL BEAM WITH NEW BEAM IAW SRM REO 601R-53-61-3778. - [SDR REXA2015102700994](https://openairdocs.org/sdr/REXA2015102700994), Oct 27, 2015: LIFE VEST. UNSERVICEABLE. THREE INFANT LIFE VESTS HAVE DAMAGED PACKAGES. R & R ALL THREE INFANT LIFE VEST IAW PA 25-096A. - [SDR REXA2015102700993](https://openairdocs.org/sdr/REXA2015102700993), Oct 27, 2015: FLASHLIGHT. INOPERATIVE. FIRST OFFICERS EMER FLASHLIGHT DOES NOT SHOW A CHARGE. DEFERRED FLASHLIGHT IAW MEL 25-61-04, CAT C. UPDATED PLACARD INSTALLED. R & R FIRST OFFICERS FLASHLIGHT I - [SDR REXA2015091300859](https://openairdocs.org/sdr/REXA2015091300859), Sep 13, 2015: WARNING SYSTEM. FALSE ACTIVATION. GEAR DISAGREE AFTER ROTATION, WHEN GEAR LEVER WAS SELECTED TO UP, RETRACTION, WITHIN 6 SECONDS OF HANDLE MOVEMENT, MANUAL RELEASE WAS PULLED. ALSO STEERING INOP - [SDR REXA2015071900722](https://openairdocs.org/sdr/REXA2015071900722), Jul 19, 2015: UNKNOWN. SMOKE. LEFT INNER BRAKE, TIRE WHEEL ASSEMBLY, SMOKE COMING FROM BRAKE AREA AFTER LANDING. BTMS WAS 7, 8, 3 & 3 IN GATE, AFTER 5 MINUTES AFTER LANDING. PERFORMED VISUAL - [SDR REXA2015063000630](https://openairdocs.org/sdr/REXA2015063000630), Jun 30, 2015: HOSE. LEAKING. OXYGEN HOSE FOUND LEAKING DURING INSTALLATION & LEAK CHECKS OF CREW OXYGEN STOWAGE BOX. R & R OXYGEN HOSE IAW AMM 35-11-15. OPERATIONS & LEAK CHECKED GOOD. OK F - [SDR REXA2015032900350](https://openairdocs.org/sdr/REXA2015032900350), Mar 29, 2015: WARNING SYSTEM. FALSE ACTIVATION. FLAP FAIL MASTER CAUTION MSG AFTER LANDING, ON TAXI IN ON GND WHILE RETRACTING, FAILED AT 27' TEMP OAT 1C. REFER TO AML PAGE 3177544 DISC 1, FLAP FAIL MSG AFTER - [SDR REXA2014121001177](https://openairdocs.org/sdr/REXA2014121001177), Dec 10, 2014: LIGHT. INOPERATIVE. EMERGENCY EXIT FLOOR PATH LIGHTING INOPERATIVE AT SEAT 1C. REPAIRED EMER FLOOR TRACK LIGHTING IAW MM CH 33-51-01. SEE NON-ROUTINE N61000 FOR WORK COMPLETED. - [SDR REXA2014083100852](https://openairdocs.org/sdr/REXA2014083100852), Aug 31, 2014: CAGE. DAMAGED. CARGO COMPARTMENT FWD SMOKE DETECTOR CAGE IS DAMAGED. R & R CARGO SMOKE DETECTOR NR 1 CAGE ASSEMBLY IAW AMM 26-15-01. OPERATIONS CHECKED OK. - [SDR REXA2014041900072](https://openairdocs.org/sdr/REXA2014041900072), Apr 18, 2014: BULKHEAD. CRACKED. FS 280 BULKHEAD WEB OTBD OF RBL 9 & LBL 9 IS CRACKED. REPAIRED IAW REO 601R-53-11-171 & 601R-53-11-136. - [SDR REXA2014041800070](https://openairdocs.org/sdr/REXA2014041800070), Apr 17, 2014: STIFFENER. CHAFED. STIFFENER ON AFT SIDE OF FS 621 BULKHEAD AT BL 0 BEHIND ISOLATION VLV IS CHAFED. REPAIRED IAW REO 601R-53-61-1523. - [SDR REXA2014041500066](https://openairdocs.org/sdr/REXA2014041500066), Apr 15, 2014: SKIN. DENTED. THE DAMAGE CONSISTS OF A DENT TO THE FUSELAGE SKIN MEASURING 3.9” X 3.2” X 0.085” DEEP AFT OF THE PRODUCTION SKIN SPLICE AT FS 333 & BETWEEN STRINGER 20R & STRI - [SDR REXA2014041500065](https://openairdocs.org/sdr/REXA2014041500065), Apr 15, 2014: FRAME. CORRODED. FOUND CORROSION TO THE FRAME AT FS 605. CORROSION WAS BLENDED FROM THE VERTICAL WEB RESULTING 3” X 2” X 0.007” DEEP MATERIAL REMOVAL. CORROSION WAS ALSO NOTED B - [SDR REXA2014013100156](https://openairdocs.org/sdr/REXA2014013100156), Jan 31, 2014: LIFE VEST. UNSERVICEABLE. FLIGHT ATTENDANT`S LIFE VEST BAG TORN. R & R LIFE VEST IAW AMM 25-61-03. - [SDR REXA2013082501607](https://openairdocs.org/sdr/REXA2013082501607), Aug 25, 2013: AUTOPILOT SYS. MALFUNCTIONED. AT FL 290, AUTOPILOT HAD AN UNCOMMANNDED PITCH UP THAT CAUSED THE ACFT TO CLIMB APPROX 200 FT. - [SDR REXA2013072501106](https://openairdocs.org/sdr/REXA2013072501106), Jul 21, 2013: SKIN. DENTED. THE FUSELAGE SKIN DENTED MEASURING 2.710" X 1.5" X .0655" DEEP WITH MATERIAL LOSS FROM BLENDING MEASURING .007" MAXIMUM DEPTH OVER AND SURROUNDING THE DAMAGED A - [SDR REXA2013061201183](https://openairdocs.org/sdr/REXA2013061201183), Jun 12, 2013: CONTAINER. TORN. CAPTAIN'S LIFE VEST BAG TORN. R & R LIFE VEST IAW AMM 25-61-03. - [SDR REXA2013010600115](https://openairdocs.org/sdr/REXA2013010600115), Jan 6, 2013: SIGN. LOOSE. EXIT SIGN OVER GALLEY SERVICE DOOR LOOSE. REMOVED AND REPLACED SERVICE DOOR EMERGENCY EXIT SIGN IAW AMM 33-51-13. OPS CHECKS GOOD. OK FOR SERVICE. - [SDR REXA2012121401775](https://openairdocs.org/sdr/REXA2012121401775), Dec 14, 2012: BATTERY. DISCHARGED. FLIGHT ATTENDANT FLASHLIGHT NOT BLINKING. REPLACED FLIGHT ATTENDANT'S FLASHLIGHT BATTERY IAW 25-60-00. OPS CHECK GOOD. AIRCRAFT OK FOR SERVICE. - [SDR REXA2012121201766](https://openairdocs.org/sdr/REXA2012121201766), Dec 12, 2012: SIGN. BROKEN. GALLEY EMERGENCY EXIT SIGN BROKEN. RE-ATTACHED EMERGENCY LIGHT IAW AMM 33-51-09. - [SDR REXA2012070701057](https://openairdocs.org/sdr/REXA2012070701057), Jul 7, 2012: SWITCH. INOPERATIVE. MACH TRIM WILL NOT ENGAGE. REMOVED AND REPLACED MACH TRIM ENGAGE SWITCH AND OPS CHECKS GOOD IAW AMM 22-21-00. - [SDR REXA2012051300729](https://openairdocs.org/sdr/REXA2012051300729), May 13, 2012: SWITCH. DIRTY. AILERON TRIM IS DIFFICULT TO MOVE TO THE LEFT. REMOVED DEBRIS FROM AILERON TRIM SWITCH, CHECKS NORMAL IAW AMM 27-11-00. OK FOR SERVICE. - [SDR REXA2012041700526](https://openairdocs.org/sdr/REXA2012041700526), Apr 17, 2012: LANDING GEAR. MALFUNCTIONED. NLG GEAR DISAGREE. PROBLEM OCCURRED ON TAKEOFF NOSE GEAR WOULD NOT RETRACT. NOSE GEAR NEVER MOVED FROM THE DOWN AND LOCKED POSITION AS VERIFIED BY CODES. S35 SH - [SDR REXA2012032100404](https://openairdocs.org/sdr/REXA2012032100404), Mar 21, 2012: PROXIMITY SWITCH. OUT OF ADJUST. GEAR DISAGREE ON LANDING (GEAR EXTENSION). FOUND NOSE GEAR UPLOCK PIN STICKING AND FOUND SEVERAL PROX SWITCHES OUT OF ADJUSTMENT. ADJUSTED SWITCHES, LUBED ROLLE - [SDR REXA2012021800264](https://openairdocs.org/sdr/REXA2012021800264), Feb 18, 2012: UNKNOWN. ODOR. ON APPROACH AT 7000 FT, FLIGHT ATTENDANT INDICATED A STRONG GASOLINE ODOR IN REAR OF AIRCRAFT AROUND LAVATORY. RAN PACKS WITH ENGINES, AND APU IAW AMM'S 72-20-0 - [SDR REXA201200125](https://openairdocs.org/sdr/REXA201200125), Jan 15, 2012: LIGHT. INOPERATIVE. EMERGENCY LIGHT FLOOR STRIP AT SEAT 6CD IS INOP. REMOVED AND REPLACED THE 6CD POSITION EMERGENCY FLOOR LIGHT STRIP IAW AMM 33-51-01. OPS CHECKS GOOD. THIS CLEAR All 69: https://openairdocs.org/deregistered/N8907A-2023-02-24/reports.md ## Other aircraft with N8907A - [Cancelled 1963-11-07](https://openairdocs.org/deregistered/N8907A-1963-11-07): Beech B35, S/N D-2605. Owner: [Yonce J Lloyd](https://openairdocs.org/faa-owner/YONCE%20J%20LLOYD), [St Petersburg, FL](https://openairdocs.org/faa-place/FL/St%20Petersburg) --- 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.