Airliner

N715SK

2004 Bombardier CL-600-2C10

Registered 1 NTSB/FAA record
Built
2004
Serial
10179
Class
Airliner
Engines
2 × Ge CF34 series
Status
Current as of October 2026
Registered owner
Skywest Airlines Inc (Corporation)
Based
St George, UT
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Registration record

N715SK on the FAA register

Type
2004 Bombardier CL-600-2C10
Serial
10179
Engines
2 × Ge CF34 series
Registered owner
Skywest Airlines Inc
St George, UT
Certificate issued
2005-01-10
Airworthiness date
2004-11-19
Registration expires
2029-04-30
Airworthiness class
Standard · transport
Mode S (hex)
A9903A
Mode S (octal)
52310072
Seats (type)
80
Weight class
20,000 lb and over
Status
Current as of October 2026
Registry history

Timeline

  • 2029-04-30
    Registration expires (renewal due).
  • 2017-06-10
    Incident at Chicago, IL; damage: minor.
  • 2005-01-10
    Certificate of registration issued as N715SK.
  • 2004-11-19
    Airworthiness date on the current FAA record (standard category (transport)).
Overview

About N715SK

N715SK is a 2004 Bombardier CL-600-2C10, serial number 10179. The FAA register lists Skywest Airlines Inc as the registrant in St George, Utah. The current certificate of registration was issued on January 10, 2005 and expires on April 30, 2029.

The FAA aircraft reference file describes the type as an airliner, two Ge CF34 series engines and 80 seats. Its airworthiness certificate is standard category (transport), dated November 19, 2004.

N715SK has 1 accident/incident record on file (most serious damage: minor); details are below.

Safety record

Accident & incident history

2017-06-10 Incident · Chicago, IL Damage: Minor NTSB · ENG17IA028
Reported aircraft: Bombardier CL 600 2C10
Probable cause: A Bombardier CRJ700 No. 1 engine failure caused by buckling of the combustion outer liner due to fatigue cracks. The liner buckling resulted in airflow disruption and reduced engine performance. The engine fuel control unit attempted to compensate for the decrease in engine performance by increasing the fuel flow rate. The combustion liner damage and increased fuel flow led to incomplete combustion of the fuel injected into the combustion chamber. Unconsumed fuel then ignited downstream of the combustion chamber (delayed ignition) and resulted in high pressure turbine thermal damage, and the eventual separation of a high pressure turbine 2nd stage nozzle vane segment. The separated vane…

Sources: NTSB aviation accident database and CAROL case system, FAA preliminary accident & incident notices. Search accident records

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Data: FAA Aircraft Registry (October 2026), including deregistered aircraft; NTSB and FAA accident data; fyiAero listing history. Individual owners' names are shown to signed-in users and street addresses are never shown. Type figures are published specifications, not this aircraft's.