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Airworthiness Directive

AD 2004-26-02: GE Aircraft Engines (GE) CF34-3A, CF34-3A2, CF34-1A, CF34-3A1, CF34-3B, and CF34-3B1…

Airworthiness Directives; GE Aircraft Engines (GE) CF34-3A, CF34-3A2, CF34-1A, CF34-3A1, CF34-3B, and CF34-3B1 Series Turbofan Engines

Effective
Jan 26, 2005
Published
Dec 22, 2004
Registered aircraft
482

Models this AD may apply to

AI-extracted — verify against original

Matched from the AD's applicability section. Applicability must be confirmed by a mechanic against the aircraft's records.

Engines

  • GE CF-34-1A
  • GE CF34-3A
  • GE CF34-3A1
  • GE CF34-3A2
  • GE CF34-3B
  • GE CF34-3B1
  • Only with: HPC forward spool P/N 6078T56P03 or 6078T56P04 installed.
  • Only with: HPC forward spool P/N 6078T56P03 or 6078T56P04 installed.

Applicability

From the AD text
This AD applies to GE CF34-3A, CF34-3A2, CF34-1A, CF34-3A1, CF34-3B, and CF34-3B1 series turbofan engines with high pressure compressor (HPC) forward spool, part number (P/N) 6078T56P03 or 6078T56P04, installed. These engines are installed on, but not limited to, Bombardier series Business Jet Model CL-600-2A12 (CL-601), Bombardier series Business Jet Model CL-600-2B16 (CL-601-3A, CL-601-3R, and CL-604), and Bombardier series Regional Jet Model CL-600-2B19 (Regional Jet Series 100 and 440) airplanes.

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