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Airworthiness Directive

AD 2003-25-08: Rolls-Royce Corporation (Formerly Allison Engine Company) AE 3007A1, AE 3007A1/1, AE…

Airworthiness Directives; Rolls-Royce Corporation (Formerly Allison Engine Company) AE 3007A1, AE 3007A1/1, AE 3007A1/3, AE 3007A3, AE 3007A1E, and AE 3007A1P Turbofan Engines

Effective
Jan 21, 2004
Published
Dec 17, 2003
Registered aircraft
10

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

  • ALLISON AE 3007A1
  • ALLISON AE 3007A1/1
  • ALLISON AE 3007A1/3
  • ALLISON AE 3007A1E
  • ALLISON AE 3007A1P
  • ALLISON AE 3007A3
  • Only with: 1st to 2nd stage turbine spacer P/N 23069627, 23070989, 23072849, or 23075364 installed.
  • Only with: 1st to 2nd stage turbine spacer P/N 23069627, 23070989, 23072849, or 23075364 installed.

Applicability

From the AD text
This AD applies to Rolls-Royce Corporation (formerly Allison Engine Company) AE 3007A1, AE 3007A1/1, AE 3007A1/3, AE 3007A3, AE 3007A1E, and AE 3007A1P turbofan engines, with 1st to 2nd stage turbine spacer part number (P/N) 23069627, 23070989, 23072849, or 23075364 installed. These engines are installed on, but not limited to, EMBRAER EMB-135 and EMB-145 series airplanes.

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