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N135EV

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2009 Bombardier CL-600-2D24 · GE CF34-8C5

Open in FAA registry

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Registered owner
Delta Air Lines Inc
Location
Atlanta, GA
Owner type
Corporation
Serial number
15225
Year built
2009
Type
Fixed wing multi engine
Engine
Turbo-fan
Airworthiness
Standard, transport
Airworthiness date
April 30, 2009
Certificate issued
April 30, 2009
Expires
March 31, 2030
Mode S code
A08E3C
Bombardier CL-600-2D24Airframe model · 95 seats · 2 engines · 314 registeredTCDS A21EA-1Airframe · Bombardier CL-600-2D24TCDS E00063ENEngine · GE CF34-8C5

From the FAA registry file of October 24, 2026.

On this page

Airworthiness directives that may apply · 130

Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.

2003In forceSuperseded2026
See all 155 ADs

Information bulletins that may apply · 4

Advisory, not mandatory.

NTSB investigations

No NTSB investigations matched to N135EVMatched by N-number and event date, checked against the reported serial number, make and model. Investigations from before this aircraft carried the mark are under Earlier aircraft. Investigations on Bombardier CL-600-2D24 aircraft

FAA incident reports · 1

FAA accident and incident reports matched to this aircraft by N-number and event date, checked against the reported make and model.

Incident 20091214052429ICruise/Level Flight · Atlanta, GAHydraulic system two volume dropped to 5%, edp and pump 2B both gave caution messages. Pressure stayed @ 2800 until final approach. Total time for edp pump was at 55 minutes. Total time for pump 2A was at 20 minutes. System 2 volume dropped to 0% on final (10…Dec 14, 2009 · No damage

Service difficulty reports · 134

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

SDR REXA2025011401094Bulkhead Web · corrodedCORROSION FOUND ON BS 280 RT BULKHEAD LOWER WEB. REPAIRED FS 280.00 R/H LOWER WEB IAW SRM 53-11-10-201-004-A01.Jan 13, 2026 · N135EV · Cndair CL6002D24 · Fuselage Main, BulkheadSDR REXA2025011401093Bulkhead Web · corrodedCORROSION FOUND ON BS 280 LT BULKHEAD LOWER WEB. INSTALLED BS 280 LT CAP ANGLE IAW SRM 51-42-06-001-001-A01, SRM 51-42-13-001-001-A01, AND SRM 51-42-22-001-001-A01. FABRICATED, LOCATED AND DRILLED NEW REPAIR PARTS, LHS LOWER WEB, AND LT BUTTSTRAP, IAW SRM 53Jan 13, 2026 · N135EV · Cndair CL6002D24 · Fuselage Main, BulkheadSDR REXA2025011101087Floorbeam · crackedTHE LH LOWER CORROSION CAP ANGLE PN CC670-34096-2 ON THE RH FS 280 BULKHEAD IS CRACKED. REMOVED FS 280.00 BULKHEAD LH CAP ANGLE IAW CRJ-900 SRM 51-42-06-001-001-A01, SRM 51-42-13-001-001-A01. LOCATED AND DRILLED NEW FS 280.00 LH CAP ANGLE P/N: CC670-34096-2S, Jan 3, 2026 · N135EV · Cndair CL6002D24 · Fuselage Main, Floor Beam
See all 134 reports

STCs that may be installed · 139

Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.

See all 139 STCs