Airworthiness Directive · Amendment 39-11221 · Pratt & Whitney JT9D Series Turbofan Engines
Pratt & Whitney JT9D Series Turbofan Engines
Pratt & Whitney (PW) JT9D-3A, -7, -7H, -7A, -7AH, -7F, -7J, -20, and -20J series turbofan engines, with Combustion Chamber Outer Casing (CCOC), part numbers (P/Ns) 644801, 693294, 709016, 729237, 729238, and 729239, installed. These engines are installed on but not limited to certain models of Boeing 747 and McDonnell Douglas DC-10 series aircraft.
This amendment adopts a new airworthiness directive (AD), applicable to certain Pratt & Whitney (PW) JT9D series turbofan engines, that requires initial and repetitive in-shop eddy current and on-wing ultrasonic inspections of the Combustion Chamber Outer Casing (CCOC) forward flange (L-flange) fillet radius for cracking, and replacing cracked L-flanges with serviceable parts. Replacement with an improved L-flange constitutes terminating action to the repetitive inspections. This amendment is prompted by reports of CCOC rupture due to cracking in the L-flange fillet radius. The actions specified by the proposed AD are intended to prevent CCOC rupture due to cracking, which could result in an uncontained engine failure and damage to the aircraft.
The aircraft, engines and makers this AD names, by the model designations in its text. A model listed here may still be outside the AD's serial ranges.
