# N834AS: 1998 Bombardier CL-600-2B19, registration cancelled 2015-07-07 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: July 7, 2015 - 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: 7254 - Year built: 1998 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: August 28, 1998 - Certificate issued: April 30, 2004 - Last registry action: January 10, 2014 - Mode S code: AB6747 - Owner when cancelled: [U S Bank Na Trustee](https://openairdocs.org/faa-owner/U%20S%20BANK%20NA%20TRUSTEE) - Location: [Boston, MA](https://openairdocs.org/faa-place/MA/Boston) - Owner type: Corporation - Owner's area on the map: 42.3582° N, 71.0519° W: Placed by OpenAirDocs at the center of ZIP code 02110, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N834AS - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=834AS - Page: https://openairdocs.org/deregistered/N834AS-2015-07-07 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 Bombardier CL-600-2B19: https://openairdocs.org/model/bombardier-cl-600-2b19.md ## Service difficulty reports (170, newest 50) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR ASOA2014070310803](https://openairdocs.org/sdr/ASOA2014070310803), Jun 30, 2014: STRUCTURE. DAMAGED. RT SIDE OF RUDDER HAS DAMAGE. COMPLIED WITH ALL STEPS OF EA 25-2014-193, JOB COMPLETE. MAJOR REPAIR IAW GMM 5-3. - [SDR ASOA2013101009198](https://openairdocs.org/sdr/ASOA2013101009198), Sep 27, 2013: SKIN. CRACKED. SMALL CRACK IN LT LOWER WING PLANK STA 148. REPAIRED IAW REO 601R-57-51-660 AND REO 601R-57-21-130. - [SDR ASOA2013101009197](https://openairdocs.org/sdr/ASOA2013101009197), Sep 25, 2013: BULKHEAD. CRACKED. BULKHEAD AT FS 280, LBL 28, WL 85.50 HAS STANDOFF, BROKEN OFF WITH RIVET PULLED THROUGH AND HAS A CRACK EXTENDING 1" FROM HOLE. REMOVED DAMAGE IAW REO 601R-53-1 - [SDR ASOA2013100809174](https://openairdocs.org/sdr/ASOA2013100809174), Sep 23, 2013: ANGLE. CRACKED. ANGLE LBL 45 AT BS 605 ANGLE CRACKED AT FRAME. REMOVED CRACKED ANGLE AND REPLACED WITH NEW. LOCATED AND DRILLED FRAME ANGLE SECTION IAW SRM 51-42-21. LOCATED AN - [SDR ASOA2013101009196](https://openairdocs.org/sdr/ASOA2013101009196), Sep 20, 2013: SKIN. CRACKED. RIGHT LOWER WING PLANK BOOST PUMP LANDING FOR PANEL 610CB HAS MULTIPLE INDICATIONS NOTED ON HORZ AND VERT SURFACES GREATER THAN 50 PERCENT FSH AROUND ENTIRE CIR - [SDR ASOA2013101009195](https://openairdocs.org/sdr/ASOA2013101009195), Sep 18, 2013: BULKHEAD WEB. CRACKED. FOUND REAR PRESSURE BULKHEAD WEB HAS INDICATIONS NOTED AT LBL 36.20 APPROX WL 79 TO WL 81 2" IN LENGTH 100 PERCENT FSH. FAILED NDT INSPECTION. REPAIRED IAW REO - [SDR ASOA2013101009194](https://openairdocs.org/sdr/ASOA2013101009194), Sep 18, 2013: BULKHEAD WEB. CORRODED. FOUND REAR PRESSURE BULKHEAD WEB HAS INDICATIONS NOTED AT BL 0.0 APPROX WL 89 TO WL 113 24" IN LENGTH 100 PERCENT FSH. FAILED NDT INSPECTION. REPAIRED IAW SRM C - [SDR ASOA2013100809173](https://openairdocs.org/sdr/ASOA2013100809173), Sep 18, 2013: SKIN. DENTED. FUSELAGE SKIN AT FWD LOWER CORNER OF PAX DOOR SURROUND IS DENTED APPROX 1 L X .50 W X .30 D. CUT AWAY DAMAGED SKIN AT PAX DOOR CUTOUT OF FWD LWR CORNER IAW SRM - [SDR ASOA2013101109200](https://openairdocs.org/sdr/ASOA2013101109200), Sep 17, 2013: HINGE. CHAFED. PASSENGER DOOR HINGE ON FUSELAGE SIDE HAS (1 EA) LUG CHAFED APPROXIMATELY .003" DEEP ON LUG NR 13 COUNTING FROM FRONT TO BACK AND HINGE IS CHAFED APPROXIMATELY - [SDR ASOA2013101109199](https://openairdocs.org/sdr/ASOA2013101109199), Sep 17, 2013: BULKHEAD WEB. GOUGED. REAR PRESSURE BULKHEAD FWD FACE ABOVE FLOOR HAS SEVERAL GOUGES RANGING FROM .003 TO .010 DEEP. BLENDED GOUGES IAW STEP NR 1 OF REO 601R-53-61-2155. - [SDR ASOA2013101009193](https://openairdocs.org/sdr/ASOA2013101009193), Sep 17, 2013: ANGLE. CORRODED. IN PASSENGER COMPARTMENT AT FS 280.00 BETWEEN LBL 9.00 TO RBL 9.00 THE TRANSVERSE BEAM TOP ANGLE IS CORRODED. REMOVED CORRODED ANGLE IAW SRM 51-42-06. LOCATED A - [SDR ASOA2013101009192](https://openairdocs.org/sdr/ASOA2013101009192), Sep 17, 2013: SEAT TRACK. CORRODED. IN PASSENGER COMPARTMENT BETWEEN FS 348.00 TO 409.00+116 ON RBL 9.00 THE SEAT TRACK IS CORRODED AT SEVERAL LOCATIONS. REMOVED CORRODED SEAT TRACK FROM RBL 9.00 - [SDR ASOA2013101009191](https://openairdocs.org/sdr/ASOA2013101009191), Sep 17, 2013: FLOORBEAM. CORRODED. IN PASSENGER COMPARTMENT BETWEEN FS 409.00 RBL 9.00 THE FLOORBEAM ATTACHMENT HOLES FOR THE FLOORBOARD ARE CORRODED. REMOVED FLOORBEAM CAP IAW SRM'S 51-42-06 AND - [SDR ASOA2013101009190](https://openairdocs.org/sdr/ASOA2013101009190), Sep 17, 2013: ATTACH ANGLE. CRACKED. IN PASSENGER COMPARTMENT AT FS 280.00 ON RBL 9.00 THE ATTACHMENT ANGLE IS CRACKED (RT). REMOVED DAMAGED CLIP FROM FS 280 ON RBL 9 OTBD PREVIOUSLY INSTALLED IAW - [SDR ASOA2013100809172](https://openairdocs.org/sdr/ASOA2013100809172), Sep 17, 2013: POST. CRACKED. FOUND FS 409+128, VERTICAL POST RBL 18.0 INBD AND OTBD SIDES HAVE CRACK INDICATIONS NOTED APPROX .2 INCHES IN LENGTH 50 PERCENT AND 100 PERCENT FSH. FAILED NDT - [SDR ASOA2013100809171](https://openairdocs.org/sdr/ASOA2013100809171), Sep 17, 2013: POST. CRACKED. FOUND FS 409+128 VERTICAL POST LBL 18.0 INBD AND OTBD SIDES HAVE CRACK INDICATIONS NOTED APPROX .2 INCHES IN LENGTH 60 PERCENT FSH AT AFT FLANGE RADIUS. FAILED - [SDR ASOA2013100809170](https://openairdocs.org/sdr/ASOA2013100809170), Sep 17, 2013: FLOORBEAM. CORRODED. IN PASSENGER CABIN FS 349 BETWEEN LBL 27 TO 36, FLOORBEAM TOP CAP IS CORRODED. REMOVED ANGLE IAW SRM 51-42-06. INSTALLED NEW ANGLE IAW SRM 51-42-06, 51-42-21 AN - [SDR ASOA2013100709167](https://openairdocs.org/sdr/ASOA2013100709167), Sep 17, 2013: FLOOR SUPPORT. CORRODED. IN PASSENGER COMPARTMENT BETWEEN FS 280 TO 319.7 ON RBL 36.00 FLOOR SUPPORT AT SEVERAL LOCATIONS IS CORRODED. REPAIRED IAW REO 601R-53-00-530. - [SDR ASOA2013100709166](https://openairdocs.org/sdr/ASOA2013100709166), Sep 17, 2013: FLOOR SUPPORT. CORRODED. IN PASSENGER COMPARTMENT AT FS 319.00 ON RBL 36 THE SERVICE DOOR CUTOUT FLOORBOARD ATTACHMENT ANGLE IS CORRODED. RT FLOOR SILL SUPPORT BETWEN FS 310 AND FS 319 - [SDR ASOA2013100709165](https://openairdocs.org/sdr/ASOA2013100709165), Sep 17, 2013: SEAT TRACK. CORRODED. IN PASSENGER COMPARTMENT BETWEEN FS 364 - 398 ON RBL 9.00 THE SEAT TRACK IS CORRODED AT SEVERAL LOCATIONS. REMOVED SEAT TRACK FS 364.00 TO FS 398.00, RBL 9 IAW - [SDR ASOA2013100709164](https://openairdocs.org/sdr/ASOA2013100709164), Sep 17, 2013: SEAT TRACK. CORRODED. IN PASSENGER COMPARTMENT BETWEEN FS 364 TO 398 ON LBL 9.00 THE SEAT TRACK IS CORRODED AT SEVERAL LOCATIONS. REMOVED SEAT TRACK. LOCATED & DRILLED SERVICEABLE SE - [SDR ASOA2013100709163](https://openairdocs.org/sdr/ASOA2013100709163), Sep 17, 2013: SEAT TRACK. CORRODED. IN PASSENGER COMPARTMENT BETWEEN FS 409.00+116 TO FS 559.00+5 ON RBL 9.00 THE SEAT TRACK IS CORRODED AT SEVERAL LOCATIONS. REMOVED SEAT TRACK 3X RING HARDWARE. - [SDR ASOA2013100709162](https://openairdocs.org/sdr/ASOA2013100709162), Sep 17, 2013: FLOOR SUPPORT. CORRODED. IN PASSENGER COMPARTMENT AT FS 449.85 ON LBL 36.00 THE FLOOR SUPPORT IS CORRODED. COMPLIED WITH EC/TC REO 601R-53-41-666 AND REO 601R-53-41-666, REV C. - [SDR ASOA2013100709161](https://openairdocs.org/sdr/ASOA2013100709161), Sep 17, 2013: ANGLE. CRACKED. IN AFT EQUIPMENT COMPARTMENT AT FS 625.00, BL 45.00, STRINGER 14L AND AT WL 97.5 THE LT INTERCOSTAL, OBLIQUE, ANGLE IS CRACKED APPROX 1.1 LONG. REMOVED DAMAGED - [SDR ASOA2013100709160](https://openairdocs.org/sdr/ASOA2013100709160), Sep 17, 2013: ANGLE. CRACKED. IN PASSENGER COMPARTMENT AT FS 484.00 RBL 27.00 THE INTERCOSTAL REPAIR ANGLE IS CRACKED. R & R INTERCOSTAL ANGLE, PN 601R31171-9 FS 484.00, RBL 27.00 IAW SRM 51 - [SDR ASOA2013100709159](https://openairdocs.org/sdr/ASOA2013100709159), Sep 17, 2013: ISOLATOR. CRACKED. CARGO AFT BULKHEAD HAS ONE BROKEN ISOLATOR UNDER PNL 281FLW. R & R BROKEN ISOLATOR WITH SERVICEABLE ISOLATOR IAW SRM 51-42-10 AND SRM 51-42-13. - [SDR ASOA2013100709158](https://openairdocs.org/sdr/ASOA2013100709158), Sep 17, 2013: ISOLATOR. CRACKED. CARGO AFT BULKHEAD HAS ONE BROKEN ISOLATOR UNDER PANEL 281GLW. R & R BROKEN ISOLATOR WITH A SERVICEABLE ISOLATOR IAW SRM 51-42-13 AND SRM 51-42-10. - [SDR ASOA2013101009189](https://openairdocs.org/sdr/ASOA2013101009189), Sep 16, 2013: FLOORBEAM. CORRODED. IN CARGO COMPARTMENT AT FS 605.00 ON RBL 9.00 THE FLOORBEAM AROUND FLOORBOARD ATTACHMENT HOLES IS CORRODED. REMOVED FLOORBEAM UPPER CAP AT RBL 9 BETWEEN 569 & F - [SDR ASOA2013101009188](https://openairdocs.org/sdr/ASOA2013101009188), Sep 16, 2013: FLOOR SUPPORT. CORRODED. IN CARGO BAY BETWEEN FS 574.00 TO 621.00 ON LBL 36.00 THE CARGO DOOR CUTOUT FLOOR SUPPORT AROUND FLOORBOARD ATTACHMENT HOLES IS CORRODED. REMOVED CORRODED CARGO - [SDR ASOA2013101009187](https://openairdocs.org/sdr/ASOA2013101009187), Sep 16, 2013: SKIN. CORRODED. RT WING PLANK ACCESS HOLE 640AB LIP HAS SEVERAL AREAS OF PITTING/CORROSION. REPAIRED IAW REO 601R-57-21-030. - [SDR ASOA2013101009186](https://openairdocs.org/sdr/ASOA2013101009186), Sep 16, 2013: SKIN. CORRODED. RT WING PLANK ACCESS HOLE 640BB LIP HAS SEVERAL AREAS OF PITTING/CORROSION. REPAIRED IAW REO 601R-57-21-030 AND REO 601R-57-21-2004. - [SDR ASOA2013100309147](https://openairdocs.org/sdr/ASOA2013100309147), Sep 16, 2013: FLOOR SUPPORT. CORRODED. PAX CABIN BS 449.85 RBL 36 FLOOR SUPPORT IS CORRODED. COMPLIED WITH ECTC REO 601R-53-41-666 AND REO 601R-53-41-666, REV C. - [SDR ASOA2013100309146](https://openairdocs.org/sdr/ASOA2013100309146), Sep 16, 2013: FLOOR SUPPORT. CORRODED. PAX CABIN BS 559+32 LBL 36.00 THE FLOOR SUPPORT CORRODED. COMPLIED WITH EC/TC REO 601R-53-00-526 AND GREO 601R-53-00-526 REV. - [SDR ASOA2013100309145](https://openairdocs.org/sdr/ASOA2013100309145), Sep 16, 2013: FLOOR SUPPORT. CORRODED. PAX CABIN FS 559+57 LBL 36 FLOOR SUPPORT IS CORRODED. COMPLIED WITH EC/TC REO 601R-53-00-526 AND GREO 601R-53-00-526 REV. - [SDR ASOA2013100309144](https://openairdocs.org/sdr/ASOA2013100309144), Sep 16, 2013: FLOORBEAM. CORRODED. IN CARGO BAY BS 598 LBL 9 FLOORBEAM CORRODED. REPAIRED IAW REO 601R-53-61-5029 AND REO 601R-53-00-005. - [SDR ASOA2013100309143](https://openairdocs.org/sdr/ASOA2013100309143), Sep 16, 2013: FLOOR SUPPORT. CORRODED. IN CARGO BAY BETWEEN BS 574 - 621 LBL 27 FLOOR SUPPORT AROUND ATTACHMENT HOLES CORRODED. REMOVED FLOOR SUPPORT IAW SRM 51-42-06 AND SRM 51-42-21. LOCATED AND DR - [SDR ASOA2013042603455](https://openairdocs.org/sdr/ASOA2013042603455), Apr 24, 2013: BATTERY. INOPERATIVE. CAPTAIN`S FLASHLIGHT NOT WORKING. REPLACED BATTERIES IAW AMM 52-61-00. - [SDR ASOA2012083102156](https://openairdocs.org/sdr/ASOA2012083102156), Aug 28, 2012: BATTERY PACK. INOPERATIVE. EMERGENCY LIGHT AFT OF GALLEY INOPERATIVE. R & R BATTERY PACK IAW AMM 33-51-04. OPS CHECKED GOOD. - [SDR ASOA2012061501801](https://openairdocs.org/sdr/ASOA2012061501801), Jun 11, 2012: DOOR FRAME. CRACKED. FOUND CRACK ON SERVICE DOOR FRAME. ON FWD DOOR SEAL STRIKER. REMOVED AND INSTALLED NEW SEAL STRIKER, IAW SRM 51-42-06, 51-23-00. - [SDR ASOA201102021](https://openairdocs.org/sdr/ASOA201102021), Oct 21, 2011: BATTERY. DISCHARGED. EMERGENCY LIGHTS INOPERATIVE WITH SWITCH ON. CHARGED BATTERY PACK. - [SDR ASOA201101845](https://openairdocs.org/sdr/ASOA201101845), Oct 3, 2011: FLOOR SUPPORT. CORRODED. PRESSURE FLOOR SKIN ANGLES HAVE CORROSION BETWEEN FS 409.00 +128 AND FS 559.00 RT SIDE. RECEIVED AND COMPLIED WITH EC/TC REO 601R-53-41-666 AND REO 601R-53-41-6 - [SDR ASOA201101840](https://openairdocs.org/sdr/ASOA201101840), Oct 2, 2011: BATTERY PACK. INOPERATIVE. FLOOR LEVEL EMERGENCY LIGHT AT SERVICE DOOR INOPERATIVE. REPLACE EMERGENCY LIGHT ASSY AT SVC DOOR, FLOOR LEVER REF AMM 33-51-10-000-801 (ASSY BROKEN) REPLACED E - [SDR ASOA201101839](https://openairdocs.org/sdr/ASOA201101839), Oct 2, 2011: BATTERY PACK. INOPERATIVE. EMERGENCY LIGHT OVERWING THE LAST ONE AFT OF EMERGENCY EXIT ON LT AND RT INOPERATIVE. REPLACE BATTERY PACK NR4 IAW AMM 33-51-04-000-801. REPLACED NR 4 BATTERY P - [SDR ASOA201101809](https://openairdocs.org/sdr/ASOA201101809), Sep 26, 2011: PLACARD. WRONG PART. LEFT EMERGENCY EXIT HAS WRONG PLACARD INSTALLED. REMOVED INCORRECT PLACARD IAW AMM 11-30-00-000-801 AND INSTALLED CORRECT PLACARD, IAW AMM 11-30-00-400-801, - [SDR ASOA201101748](https://openairdocs.org/sdr/ASOA201101748), Sep 16, 2011: FLOORBEAM. CORRODED. FLOORBEAM HAS CORROSION AT FS 349.00. REPAIRED IAW REO 601R-53-21-1361. - [SDR ASOA201101795](https://openairdocs.org/sdr/ASOA201101795), Sep 15, 2011: FRAME. CRACKED. BS 280 FRAME APPEARS TO BE CRACKED AFT LOWER SIDE NEAR LBL9.00. COMPLIED WITH ECTC REO 601R-53-11-171. - [SDR ASOA201101732](https://openairdocs.org/sdr/ASOA201101732), Sep 14, 2011: DRAG ANGLE. CRACKED. POSSIBLE CRACK FOUND AT FASTNER LOCATION ON PAX DOOR UNDER AFT DRAG ANGLE. REPAIRED IAW REO 601R-52-11-1991. - [SDR ASOA201101706](https://openairdocs.org/sdr/ASOA201101706), Sep 12, 2011: SUPPORT. CORRODED. RT SIDE WINDSCREEN SUPPORT STRUCTURE AT FS 349 CORRODED. REMOVED AND REPLACED WINDSCREEN SUPPORT ANGLE & FITTING IAW SRM 51-42-06 & SRM 51-42-21. - [SDR ASOA201101705](https://openairdocs.org/sdr/ASOA201101705), Sep 12, 2011: BRACKET. CRACKED. PILOTS WINDSHIELD SIDE POST LOWER BRACKET CRACKED. R & R BRACKET IAW SRM 51-47-21. - [SDR ASOA201101688](https://openairdocs.org/sdr/ASOA201101688), Sep 9, 2011: SEAT TRACK. CORRODED. SEAT TRACK CORRODED AT RBL 9 AND FS 364.00. CLEANED CORROSION IAW SRM 51-21-11. CORROSION FOUND TO BE OUT OF LIMITS IAW SRM 53-21-49. REMOVED SEAT TRACK IAW AMM All 170: https://openairdocs.org/deregistered/N834AS-2015-07-07/reports.md ## Other aircraft with N834AS - [Registered now](https://openairdocs.org/aircraft/N834AS): Boeing 757-204, S/N 28834 --- 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.