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N438SW

Registered aircraft · 2001 Bombardier CL-600-2B19 · GE CF34 series

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Serial number: 7574
Year built: 2001
Type: Fixed wing multi engine
Engine: Turbo-fan
Airworthiness: Standard, transport
Airworthiness date: November 16, 2001
Certificate issued: March 28, 2024
Expires: March 31, 2031
Mode S code: A5427B
Registered owners: Corporate Flight Management Inc DBA Contour Aviation
Location: Smyrna, TN
Owner type: Corporation

Bombardier CL-600-2B19Airframe model · 55 seats · 2 engines · 396 registered TCDS A21EA-1Airframe · Bombardier CL-600-2B19 Engine modelGE CF34 series

From the FAA registry file of October 20, 2026. The registry lists only the engine series, so ADs for every GE CF34 model are included below.

On this page

Airworthiness directives that may apply · 200

Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment. Not a compliance determination.

1981In forceSuperseded2026

ADs by the year they took effect: 277 ADs
1981	1
1982	6
1988	1
1993	1
1994	6
1995	4
1996	2
1997	5
1998	4
1999	8
2000	7
2001	9
2002	9
2003	15
2004	14
2005	14
2006	16
2007	12
2008	19
2009	9
2010	16
2011	10
2012	7
2013	8
2014	6
2015	5
2016	7
2017	6
2018	3
2019	6
2020	10
2021	5
2022	8
2023	6
2024	3
2025	6
2026	3

Airframe · Bombardier CL-600-2B19

AD 2026-13-02NavigationEffective Jul 1, 2026 AD 2026-05-05Flight controlsEffective Mar 23, 2026 · Supersedes AD 2023-23-02 AD 2026-02-03Flight controlEffective Feb 5, 2026

See all 278 ADs

Information bulletins that may apply · 10

Advisory, not mandatory. Matched the same way as ADs.

Airframe · Bombardier CL-600-2B19

SAIB NM-10-06Oxygen Inspection of Third Crewmember Oxygen HoseIssued Oct 20, 2009 SAIB NM-09-03Engine Fuel and Control - Implementing Fuel Tank System Airworthiness LimitationsIssued Dec 11, 2008 SAIB NM-07-26Flap failures during cold weather operationsIssued Apr 5, 2007 SAIB NE-07-25Thrust reverser access cowlsIssued Apr 3, 2007 SAIB NM-07-11Brake System AccumulatorsIssued Nov 24, 2006 SAIB NM-05-60Issued Jun 17, 2005 SAIB NM-05-55Issued Jun 2, 2005 SAIB NM-05-53Issued May 18, 2005 SAIB NM-05-31Issued Feb 4, 2005

Engine · GE CF34 series

SAIB NE-04-77Issued Aug 12, 2004

NTSB investigations · 1

Matched to this aircraft by N-number and event date.

NTSB CEN25LA070Accident · No injuriesClass 4 · LimitedFinal reportStringtown, MSBird strike.Jan 3, 2025 · Substantial damage

FAA incident reports · 1

FAA accident and incident reports matched to this aircraft by N-number and event date.

Accident 20250102000019ADescent · Greenville, MSAircraft struck a flock of medium to large birds while on descent to the glh airport and sustained damage to the nose Cone, forward fuselage, leading edge of right winglet, number one engine, and vertical stabilizer.Jan 2, 2025 · Substantial damage

Service difficulty reports · 145

SDR SWIA202264770None · crackedPAX DOOR ANGLE, NEAR DOOR HINGE HAS A CRACK. MARKED. (FILED CLOSED) REPLACED PAX DOOR UPPER ANGLE NEAR DOOR HINGE IN REFERENCE TO CRJ 200 SRM 51-42-06Mar 1, 2022 · N438SW · Cndair CL6002B19 · Fuselage, Equipment Attach Fittings SDR SWIA202157732Skin · dentedRH INBOARD FLAP LOWER SKIN HAS DENT APPROX. 6" INBOARD OF INBOARD EDGE AND 2" FWD OF TRAILING EDGE. (FILED CLOSED)COMPLIED WITH PERMANENT REPAIR OF THE RH INBOARD FLAP LOWER SKIN 6" INBOARD OF THE INBOARD EDGE AND 2" FWD OF THE TRAILING EDGE IN REFERENCE TApr 18, 2021 · N438SW · Cndair CL6002B19 · Trailing Edge Flaps SDR SWIA202157729Intercostal · crackedFRAME 621.00 INTERCOSTAL CONNECTING TO Z-MEMBER AT STR 14R CRACKED. (CRJ-200 SRM 53-61-17 ITEM #50) (FILED CLOSED) REMOVED AND REPLACED FRAME 621.00 INTERCOSTAL CONNECTING TO Z-MEMBER AT STR 14R IN REF TO SRM 51-42-06. COMPLIED WITH TASK CARD 51-900-1Apr 18, 2021 · N438SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure

See all 145 reports