# N829AS: 1998 Canadair CL-600-2B19, registration cancelled 2015-02-20

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: February 20, 2015
- Status when cancelled: Valid registration
- Airframe: [Canadair CL-600-2B19](https://openairdocs.org/model/canadair-cl-600-2b19) (registry code 1900309)
- 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: 7232
- Year built: 1998
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: April 22, 1998
- Certificate issued: April 23, 2004
- Last registry action: January 10, 2014
- Mode S code: AB525B
- 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/N829AS
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=829AS
- Page: https://openairdocs.org/deregistered/N829AS-2015-02-20

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 Canadair CL-600-2B19: https://openairdocs.org/model/canadair-cl-600-2b19.md

## Service difficulty reports (134, newest 50)

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

- [SDR ASOA2014031410127](https://openairdocs.org/sdr/ASOA2014031410127), Mar 10, 2014: LIGHT. DAMAGED. EMERGENCY FLOODLIGHT DAMAGED. R & R FLOODLIGHT IAW AMM 33-51-19. OPS CHECKED GOOD. NO FURTHER ACTION.
- [SDR ASOA2013092709106](https://openairdocs.org/sdr/ASOA2013092709106), Sep 26, 2013: BULB. BURNED OUT. LT AFT EXTERNAL EMERGENCY LIGHT IS INOPERATIVE. R & R BULB IAW AMM 33-51-21. OPS CHECKED GOOD.
- [SDR ASOA2013051003501](https://openairdocs.org/sdr/ASOA2013051003501), Apr 26, 2013: INTERCOSTAL. CORRODED. INTERCOSTAL AFT OF MAIN AVI DOOR CUTOUT AT FS 394 - 409, S26L HAS MINOR CORROSION ON FWD END OF ATTACH FLANGE. REPAIRED IAW SRM 51-42-06.
- [SDR ASOA2013051003500](https://openairdocs.org/sdr/ASOA2013051003500), Apr 19, 2013: SKIN. CORRODED. LT SIDE LOWER WING PLANK ACCESS HOLE FOR PANEL 540DB HAS INDICATIONS OF CORROSION ON LANDING APPROX 55 PERCENT, FULL SCREEN HEIGHT. ACCESS HOLE FAILED NDT. REPA
- [SDR ASOA2013051003499](https://openairdocs.org/sdr/ASOA2013051003499), Apr 19, 2013: SKIN. CORRODED. ACCESS HOLE FOR PANEL 650GB ON LOWER WING PLANK HAS INDICATIONS OF CORROSION ON LANDING APPROX 58 PERCENT FULL SCREEN HEIGHT. ACCESS HOLE 650GB FAILED NDT. REPA
- [SDR ASOA2013051003498](https://openairdocs.org/sdr/ASOA2013051003498), Apr 19, 2013: SKIN. CORRODED. ACCESS HOLE 610AB LOWER WING PLANK ACCESS HOLE HAS INDICATIONS OF CORROSION ON LANDING APPROX 50 PERCENT FULL SCREEN HOLE. ACCESS HOLE FAILED NDT. REPAIRED IAW 
- [SDR ASOA2013051003497](https://openairdocs.org/sdr/ASOA2013051003497), Apr 15, 2013: FLOOR SUPPORT. CORRODED. RT FLOOR SUPPORT FS 449.85 HAS CORROSION AROUND 1 FLOORBOARD NUTPLATE HOLE. REPAIRED IAW REO 601R-53-41-1689.
- [SDR ASOA2013051003496](https://openairdocs.org/sdr/ASOA2013051003496), Apr 15, 2013: POST. CRACKED. FOUND FS 409+128 VERTICAL POST BL 0.0 RT SIDE HAS INDICATION NOTED AT AFT FLANGE RADIUS WL 69 APPROX .2" IN LENGTH 60 PERCENT FSH. FAILED NDT INSPECTION. REMOVE
- [SDR ASOA2013051003495](https://openairdocs.org/sdr/ASOA2013051003495), Apr 15, 2013: POST. CRACKED. FOUND FS 409+128 VERTICAL POST RBL 18.0 INBD SIDE HAS INDICATION NOTED AT AFT FLANGE RADIUS WL 69.0 APPROX .2" IN LENGTH 50 PERCENT FSH. FAILED NDT INSPECTION. 
- [SDR ASOA2013050903492](https://openairdocs.org/sdr/ASOA2013050903492), Apr 15, 2013: BULKHEAD. CRACKED. FOUND REAR PRESSURE BULKHEAD WEB HAS INDICATION NOTED AT LBL 27.50 WL 130 APPROX .4" IN LENGTH 100 PERCENT FSH FAILED NDT INSPECTION. REPAIRED IAW REO 601R-53-6
- [SDR ASOA2013050903491](https://openairdocs.org/sdr/ASOA2013050903491), Apr 12, 2013: PANEL. CORRODED. LT WING LWR WING PLANK ACCESS HOLE 510AB HAS PITTING/CORROSION AT INBD LOCATION. REPAIRED IAW EO 600-57-81 & REO 601R-57-21-030, REV J.
- [SDR ASOA2013050903490](https://openairdocs.org/sdr/ASOA2013050903490), Apr 12, 2013: PANEL. CORRODED. LEFT WING LWR WING PLANK ACCESS HOLE 540BB HAS PITTING/CORROSION AT INBD AND OTBD LOCATIONS. REPAIRED IAW EO 600-57-81 & REO 601R-57-21-030, REV J.
- [SDR ASOA2013050903489](https://openairdocs.org/sdr/ASOA2013050903489), Apr 12, 2013: SKIN. CORRODED. RT WING LOWER WING PLANK ACCESS HOLE 640AB CORRODED AT AFT LOCATION. REPAIRED IAW EO 600-57-81 & REO 601R-57-21-030, REV J.
- [SDR ASOA2013050903488](https://openairdocs.org/sdr/ASOA2013050903488), Apr 12, 2013: SKIN. CORRODED. RT WING LOWER WING PLANK ACCESS HOLE 640BB HAS CORROSION AT FWD AND AFT LOCATIONS. REPAIRED IAW EO 600-57-81 & REO 601R-57-21-030, REV J.
- [SDR ASOA2013051003494](https://openairdocs.org/sdr/ASOA2013051003494), Apr 11, 2013: FLOOR SUPPORT. CRACKED. FS 484 FLOOR SUPPORT ANGLE AT RBL 27 IS CRACKED. REMOVED ANGLE IAW SRM 51-42-21. LOCATED AND DRILLED NEW SERVICEABLE ANGLE IAW SRM 51-40-11. INSTALLED NEW ANGLE
- [SDR ASOA2013050903487](https://openairdocs.org/sdr/ASOA2013050903487), Apr 11, 2013: SILL. CORRODED. SERVICE DOOR FLOOR SILL IS CORRODED. REMOVED CORRODED SILL PLATE FROM SERVICE DOOR SURROUND STRUCTURE IAW SRM 51-42-21. LOCATED AND DRILLED NEW SILL PLATE IAW S
- [SDR ASOA2013050903486](https://openairdocs.org/sdr/ASOA2013050903486), Apr 11, 2013: FLOOR SUPPORT. CRACKED. FS 484, FLOOR SUPPORT ANGLE AT RBL 27 IS CRACKED. REMOVED CLIP PN 601R31171-9 IAW SRM 51-42-21 AT FS 484 RBL 27. LOCATED AND DRILLED NEW SERVICEABLE CLIP PN 601
- [SDR ASOA2013050803482](https://openairdocs.org/sdr/ASOA2013050803482), Apr 11, 2013: ANGLE. CRACKED. LT OTBD FLAP MIDDLE HINGE POINT OTBD ATTACH ANGLE FOR 595BB IS CRACKED IN RADIUS 2.5". DRILLED UP NEW SERVICEABLE ATTACH ANGLE IAW SRM 51-40-11. INSTALLED NEW S
- [SDR ASOA2013050803481](https://openairdocs.org/sdr/ASOA2013050803481), Apr 9, 2013: FRAME. CRACKED. LT FS 718 FRAME PREVIOUS REPAIR SHOWS VISUAL SIGNS OF A CRACK BETWEEN STRINGERS 10L AND 12L. REPLACED SECTION OF FRAME BS 718 FROM STR 5L-21L IAW SRM 51-42-06 A
- [SDR ASOA2013050803480](https://openairdocs.org/sdr/ASOA2013050803480), Apr 9, 2013: FRAME. CRACKED. RT FS 718, FRAME PREVIOUS REPAIR SHOWS VISUAL SIGNS OF A CRACK BETWEEN STRINGERS 10R AND 12R. REMOVED SECTION OF FRAME STATION 718 BETWEEN STR 5R AND 21R IAW SR
- [SDR ASOA2012110602429](https://openairdocs.org/sdr/ASOA2012110602429), Nov 2, 2012: LIGHT. DAMAGED. ROW 1CD EMERGENCY FLOOR STRIP DAMAGED. R & R ROW 1CD EMERGENCY FLOOR TRACK STRIP IAW CRJ 200 33-51-01, NO FURTHER DEFECTS.
- [SDR ASOA201201285](https://openairdocs.org/sdr/ASOA201201285), Apr 16, 2012: BULB. BURNED OUT. AFT EMERGENCY CEILING LIGHT INOPERATIVE. R & R AFT EMERGENCY CEILING LIGHT BULB. OP'S CHECKED GOOD.
- [SDR ASOA201200159](https://openairdocs.org/sdr/ASOA201200159), Jan 13, 2012: FLAP SYSTEM. MALFUNCTIONED. FLAPS FAILED, 22 DEG LT, 20 DEG RT. EMERGENCY DECLARED. TROUBLESHOT FLAP SYSTEM IAW FIM 27-50-00 WITH NO DEFECTS NOTED. PEFORMED OPS TEST OF THE FECU FLAP SYS I
- [SDR ASOA201102278](https://openairdocs.org/sdr/ASOA201102278), Nov 26, 2011: TORQUE LINK. DISCONNECTED. GEAR DISAGREE. NOSE GEAR WOULD NOT COME UP. C/W QRH ALSO WOW INPUT CAUTION MESSAGE. (ACFT RETURNED TO DEPARTURE AFTER T/O -- EMERGENCY DECLARED AS A PRECAUTION)
- [SDR ASOA201101267](https://openairdocs.org/sdr/ASOA201101267), Jul 4, 2011: DOOR. BINDING. COULD NOT GET MAIN CABIN DOOR TO OPEN UPON ARRIVAL. OPS CHECK OG MAIN CABIN DOOR IAW AMM 52-10-00, OK FOR SERVICE.
- [SDR ASOA201100534](https://openairdocs.org/sdr/ASOA201100534), Mar 22, 2011: SEAT TRACK. CORRODED. CARGO BAY SEAT TRACK CORRODED. LOCATED AND DRILLED SEAT TRACK IAW SRM 51-40-11. INSTALLED NEW SEAT TRACK IAW SRM 51-41-02. THIS REPAIR IS CLASSIFIED AS A MINOR 
- [SDR ASOA201100614](https://openairdocs.org/sdr/ASOA201100614), Mar 17, 2011: CHANNEL. CORRODED. PAX DOOR BOTTOM INSIDE (WITH DOOR IN THE CLOSED POSITION) HAS MINOR CORROSION ON CHANNEL & SEVERAL RIVETS. REMOVED FASTENERS IN AREA & CLEANED AREA OF CHANNEL, 
- [SDR ASOA201100530](https://openairdocs.org/sdr/ASOA201100530), Mar 17, 2011: INTERCOSTAL. CRACKED. PAX DOOR LOWER FWD INTERCOSTAL ARE CRACKED. REMOVED CRACKED LOWER FWD INTERCOSTAL FROM THE PAX DOOR IAW SRM 51-42-06. DRILLED & INSTALLED NEW SERVICEABLE INTERC
- [SDR ASOA201100521](https://openairdocs.org/sdr/ASOA201100521), Mar 17, 2011: ATTACH FITTING. CORRODED. PAX DOOR FRAME CLIPS ON BOTTOM END AT FS 320.10, 329.50 AND 338.00 ARE CORRODED. REMOVED 5 CORRODED FRAME CLIPS FROM UPPER (HINGE) SECTION. FIT, DRILLED & INSTA
- [SDR ASOA201100499](https://openairdocs.org/sdr/ASOA201100499), Mar 16, 2011: ISOLATOR. BROKEN. FS 621.00 PRESSURE BULKHEAD HAS ISOLATOR CRACKED. R & R ISOLATOR IAW SRM 51-42-06. MINOR REPAIR.
- [SDR ASOA201100498](https://openairdocs.org/sdr/ASOA201100498), Mar 16, 2011: FRAME. CORRODED. FUSELAGE FRAME AT FS 333.00 HAS SEVERAL AREAS OF CORROSION ON FWD SIDE OF FRAME BETWEEN STR 25L AND STR 25R.
- [SDR ASOA201100520](https://openairdocs.org/sdr/ASOA201100520), Mar 11, 2011: FLOOR SUPPORT. CORRODED. CARGO FLOOR SUPPORT AT LBL 27 OTBB SIDE HAS MINOR CORROSION AROUND NUTPLATES FROM FS 621 TO FS 559+112. REMOVED LBL 27.0 FLOOR SUPPORT CAP FROM FS 559+112 TO FS
- [SDR ASOA201100466](https://openairdocs.org/sdr/ASOA201100466), Mar 11, 2011: INTERCOSTAL. CRACKED. FS 484, INTERCOSTAL CLIP IS CRACKED AT LBL 36. REINSTALLED PULLEY MOUNTS IAW CRJ 200 AMM 20-24-00-910-801. REPAIR TO THE INTERCOSTALS AT FS 484 BETWEEN BL 27 AN
- [SDR ASOA201100476](https://openairdocs.org/sdr/ASOA201100476), Mar 10, 2011: DRAG ANGLE. CRACKED. PAX DOOR AFT DRAG ANGLE CRACKED. REMOVED & INSTALLED NEW DRAG ANGLE PN 600-31907-17 IAW SRM 51-42-06/-13.
- [SDR ASOA201100463](https://openairdocs.org/sdr/ASOA201100463), Mar 10, 2011: FLOORBEAM. CORRODED. FS 280 TRANSVERSE BEAM FWD "J" CHANNEL CORRODED FROM LBL 9 TO RBL 9. INSTALLED NEW CHANNEL IAW SRM 51-42-06.
- [SDR ASOA201100462](https://openairdocs.org/sdr/ASOA201100462), Mar 10, 2011: FLOORBEAM. CORRODED. FS 280 TRANSVERSE BEAM UPPER AFT "J" CHANNEL IS CORRODED FROM LBL 18 TO RBL 36 AT SEVERAL LOCATIONS. FOUND TO BE WITHIN ALLOWABLE DAMAGE LIMITS IAW SRM 53-00-00
- [SDR ASOA201100461](https://openairdocs.org/sdr/ASOA201100461), Mar 10, 2011: FLOORBEAM. CORRODED. FLOORBEAM AT FS 349.00 HAS CORROSION FROM RBL 27 TO RBL 36. REMOVED FLOORBEAM IAW SRM 51-21-06. REPAIRED FLOORBEAM THREATED FOR CORROSION PREVENTION IAW SRM 51-
- [SDR ASOA201100460](https://openairdocs.org/sdr/ASOA201100460), Mar 10, 2011: FRAME. CORRODED. FUSELAGE FRAME AT FS 319.70 HAS SEVERAL AREAS OF CORROSION BETWEEN STR 25L AND STR 25R. FOUND CORROSION DAMAGE ON FRAME SECTOR AT FS 319.70 BETWEEN STRINGERS 25
- [SDR ASOA201100459](https://openairdocs.org/sdr/ASOA201100459), Mar 10, 2011: FRAME. CORRODED. FUSELAGE FRAME AT FS 333.00 HAS SEVERAL AREAS OF CORROSION ON FWD SIDE OF FRAME BETWEEN STR 25L AND STR 25R. FOUND TO BE BEYOND ALLOWABLE DAMAGE LIMITS IAW SRM 
- [SDR ASOA201100529](https://openairdocs.org/sdr/ASOA201100529), Mar 9, 2011: LIGHT. UNSERVICEABLE. PAX DOOR INTERIOR HANDLE "PULL TO EXIT" SIGN WORN. INSTALLED NEW SERVICEABLE PAX DOOR "PULL TO EXIT" BETA LIGHT IAW AMM 33-51-09-400-801. FUNC TEST GOOD IAW AMM
- [SDR ASOA201100446](https://openairdocs.org/sdr/ASOA201100446), Mar 7, 2011: SEAT TRACK. CORRODED. SEAT TRACK CORRODED. REMOVED SEAT TRACK IAW AMM 53-01-11-000-802. INSTALLED NEW SERVICEBLE SEAT TRACKS IAW AMM 53-01-11-400-802.
- [SDR ASOA201100445](https://openairdocs.org/sdr/ASOA201100445), Mar 7, 2011: FLOORBEAM. CRACKED. FS 280.0 FLOORBEAM CLIPS CRACKED AT RBL 9 AND LBL 9. REMOVED AND REPLACED FLOORBEAM FWD CLIPS IAW SRM 51-42-21, REO 60R-53-11-2088 & REO 601R-53-11-926.
- [SDR ASOA201100444](https://openairdocs.org/sdr/ASOA201100444), Mar 7, 2011: LIGHT. INOPERATIVE. RT NR1 POSITION LIGHT INOPERATIVE. INSTALLED NEW LIGHT.
- [SDR ASOA201001782](https://openairdocs.org/sdr/ASOA201001782), Nov 14, 2010: UNKNOWN. ODOR. RECEIVED RT PACK HIGH TEMP CAUTION. MESSAGE DURING CLIMB WITH PACK IN MANUAL MODE. FLIGHT ATTENDANT REPORTED A BURNING SMELL/FOG IN THE CABIN. QRH ACTIONS RETUR
- [SDR ASOA201000398](https://openairdocs.org/sdr/ASOA201000398), Mar 17, 2010: PROXIMITY SWITCH. OUT OF ADJUST. ON DEPARTURE,WHEN SELECTING GEAR UP, RECEIVED "GEAR DISAGREE" WARNING MSG. COMPLIED WITH QRH AND RETURNED TO DEPARTURE. CVR CB OPENED ON RETURN TO GATE. (ACFT R
- [SDR ASOA20100049](https://openairdocs.org/sdr/ASOA20100049), Jan 15, 2010: BULKHEAD. CRACKED. REPAIRED CRACKED LT 202.75 PRESSURE BULKHEAD IAW EC/TC REO 601R-53-11-563 ON WO 145548. JC7020037 1/16/10, ITEM: 1. REPAIRED CRACKED LT 202.75 PRESSURE BULKHEAD
- [SDR ASOA201000049](https://openairdocs.org/sdr/ASOA201000049), Jan 15, 2010: BULKHEAD. CRACKED. LEFT FS 202.75 PRESSURE BULKHEAD CRACKED AT PARKING BRAKE CABLE HOLE. REPAIRED CRACKED LT 202.75 PRESSURE BULKHEAD IAW EC/TC REO 601R-53-11-563 ON WO 145548. RE
- [SDR ASOA200901342](https://openairdocs.org/sdr/ASOA200901342), Dec 3, 2009: FLAP SYSTEM. FAILED. FLAPS FAIL AT 30 DEG ON APPROACH (EMERGENCY DECLARED).
- [SDR ASOA200901104](https://openairdocs.org/sdr/ASOA200901104), Oct 4, 2009: LIGHT. INOPERATIVE. LOWER EMERGENCY LIGHT IN PAX ENTRY AREA INOP.
- [SDR ASOA200900728](https://openairdocs.org/sdr/ASOA200900728), Jun 28, 2009: DOOR. BINDING. PAX DOOR HARD TO OPEN.

All 134: https://openairdocs.org/deregistered/N829AS-2015-02-20/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 ATL03IA090](https://openairdocs.org/ntsb/ATL03IA090), May 8, 2003: Canadair CL-600-2B19 (N829AS), Chattanooga, TN, incident, no damage. Probable cause: Excessive wear on the bushings and the right aileron inboard and outboard power control unit output link resulting in the upward movement of the right aileron during cruise climb, uncommanded right…

## FAA accident and incident reports (1)

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 20030508014979I](https://openairdocs.org/incident/20030508014979I), May 8, 2003: Cndair CL6002B19 (N829AS), Chattanooga, TN. (-23) Flight crew reported inflight control problems with atlanta center and requested divert to Chattanooga from planned flight atlanta-toronto. Aircraft…

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