Aircraft record

N829AS1998 Canadair CL-600-2B19

DeregisteredUnclaimedSource: FAA, updated Oct 19, 2026

This N-number isn't registered right now. Below is its last known registration, canceled Feb 20, 2015.

Safety record in brief:1 NTSB incident (May 2003)4 ADs may apply134 service difficulty reports

Registration: Deregistered
Last based in: Boston, MA; owner city / state
Engine: CF34 SERIES · 9,140 lb thrust; Ge
Owners: 1; since 2004
NTSB events: 1; 2003
ADs may apply: 4; confirm with A&P
Service reports: 134; since 1995

Registration

FAA Aircraft Registry · Oct 19, 2026

Last registered owner: U S Bank NA Trustee
Owner type: Corporation
City, state: Boston, MA
Certificate issued: Apr 23, 2004
Canceled: Feb 20, 2015
Airworthiness: Standard · Transport
Airworthiness date: Apr 22, 1998

We never show street addresses, even though they appear in the public FAA file. Individual owners are shown by city and state only.

Airframe & engine

FAA Registry + type data

Airframe

Manufacturer: Canadair
Model: CL-600-2B19
Year: 1998
Serial number: 7232
Aircraft type: Fixed wing multi engine
Category: Land
Certification: Type Certificated
Seats: 55
Engines: 2
Max takeoff weight: 20,000 and over lb
Mode S code: AB525B

Engine

Make and model: Ge Cf34 Series
Type: Turbo-fan
Power: 9,140 lb thrust

Total time and engine hours aren't public. They appear here once the owner adds logbooks.

Ownership history

Ownership history from FAA records

2004 – 2015U S Bank NA TrusteeBoston, MA

Individual owners are shown by city and state only.

Safety record

NTSB · Oct 15, 2026 · FAA ADs · Oct 19, 2026 · SDRs · Oct 16, 2026

NTSB events (1)

Incident

May 8, 2003 · Chattanooga, TN

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 roll. A factor in the accident was inadequate maintenance inspection procedure by the aircraft manufacture for the aileron system backlash check performed by the operator. The inspection procedure did…

Injuries: None
Report: ATL03IA090

From NTSB records; matched by serial number.Read NTSB report (search CAROL for ATL03IA090)

Accident history for this model

ADs published since 1998 that may apply (4)

These match the airframe or engine model. Whether each one applies, and whether it's been complied with, depends on serial numbers, equipment and logbook entries. Applicability must be confirmed by a mechanic against the aircraft's records.

AD	Subject	Effective	Applies to
2004-07-18	Bombardier Model CL-600-2B19 (Regional Jet Series 100 & 440) Airplanes	May 11, 2004	Airframe (CL-600-2B19)Certain serial numbers: CL-600-2B19 7375–7632. Only with: Equipped with landing gear control handle assemblies Canadair P/N 601R50967-7 (Vendor P/N 7-45502-1) or Canadair P/N 601R50967-9 (Vendor P/N 7-45502-3).
2000-14-17	Bombardier Model CL-600-2B19 Series Airplanes	Aug 28, 2000	Airframe (CL-600-2B19)Certain serial numbers: CL-600-2B19 7003–7207. Only with: Except airplanes on which Canadair Regional Jet Service Bulletin S.B. 601R-34-094, Revision B, dated November 14, 1997, has been accomplished.
2000-01-12	Bombardier Model CL-600-2B19 (Regional Jet Series 100) Series Airplanes	Feb 17, 2000	Airframe (CL-600-2B19)Certain serial numbers: CL-600-2B19 7003–7185. Only with: Except airplanes on which Canadair Regional Jet Service Bulletin 601R-53-046, Revision B, or 601R-53-047, Revision D, has been accomplished.
95-04-05	Bombardier (Formerly Canadair) Model CL-600-2B19 (Regional Jet Series 100) Series…	Apr 7, 1995	Airframe (CL-600-2B19)Certain serial numbers: CL-600-2B19 7003–on

AI-extracted — verify against original. Matched from each AD's applicability section; ADs replaced by a later AD are left out.

Service Difficulty Reports (134)

Reports of failures and defects that operators and repair stations sent to the FAA since 1995. A report describes one finding; it is not an accident.

Lights · light · damagedMar 10, 2014
EMERGENCY FLOODLIGHT DAMAGED. R & R FLOODLIGHT IAW AMM 33-51-19. OPS CHECKED GOOD. NO FURTHER ACTION.
From FAA Service Difficulty Reports; matched by N-number and serial number.
Lights · bulb · burned outSep 26, 2013
LT AFT EXTERNAL EMERGENCY LIGHT IS INOPERATIVE. R & R BULB IAW AMM 33-51-21. OPS CHECKED GOOD.
From FAA Service Difficulty Reports; matched by N-number and serial number.
Fuselage · intercostal · corrodedApr 26, 2013
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.
From FAA Service Difficulty Reports; matched by N-number and serial number.

Show all 10 reports

Wings · skin · corrodedApr 19, 2013
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 EC/TC EO 600-57-81 & REO 601R-57-21-030, REV J.
From FAA Service Difficulty Reports; matched by N-number and serial number.
Wings · skin · corrodedApr 19, 2013
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. REPAIRED IAW EC/TC EO 600-57-81 & REO 601R-57-21-030, REV J.
From FAA Service Difficulty Reports; matched by N-number and serial number.
Wings · skin · corrodedApr 19, 2013
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. REPAIRED IAW EC/TC EO 600-57-81 & REO 601R-57-21-030, REV J.
From FAA Service Difficulty Reports; matched by N-number and serial number.
Fuselage · bulkhead · crackedApr 15, 2013
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-53-61-1541.
From FAA Service Difficulty Reports; matched by N-number and serial number.
Fuselage · post · crackedApr 15, 2013
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. REMOVED FS 409+128, RBL 18.0 CRACKED POST ASSY DRILLED, LOCATED FASTENER HOLES IAW SRM 51-42-06 AND 51-42-22. INSTALLED NEW INBD SIDE POST…
From FAA Service Difficulty Reports; matched by N-number and serial number.
Fuselage · post · crackedApr 15, 2013
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. REMOVED RT POST FORM LT POST AT FS 409.00+182 BL 0.0 IAW SRM 51-42-06. INSTALLED NEW SERVICEABLE RT SIDE FS 409+128, BL 0, VERTICAL POST TO SAME…
From FAA Service Difficulty Reports; matched by N-number and serial number.
Fuselage · floor support · corrodedApr 15, 2013
RT FLOOR SUPPORT FS 449.85 HAS CORROSION AROUND 1 FLOORBOARD NUTPLATE HOLE. REPAIRED IAW REO 601R-53-41-1689.
From FAA Service Difficulty Reports; matched by N-number and serial number.

Showing the 10 most recent of 134 reports.

Sources

FAA Aircraft RegistryRegistration, owner city and state, airframe, engineupdated Oct 19, 2026
NTSB accident and incident databaseAccidents and incidents since 1982updated Oct 15, 2026
FAA Airworthiness Directives (Federal Register)ADs published since 1998updated Oct 19, 2026
FAA Service Difficulty ReportsReports since 1995updated Oct 16, 2026

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