Airworthiness Directive · Amendment 39-19332 · Turbine section
General Electric Company Turbofan Engines
This AD applies to General Electric Company (GE) GEnx-1B64, -1B64/P1, -1B64/P2, -1B67, -1B67/P1, -1B67/P2, -1B70, -1B70/75/P1, -1B70/75/P2, -1B70/P1, -1B70/P2, -1B70C/P1, -1B70C/P2, -1B74/75/P1, and -1B74/75/P2 engines with air/oil extension duct, part number (P/N) 2332M85P01 or 2331M25G03, installed.
We are adopting a new airworthiness directive (AD) for all General Electric Company (GE) GEnx-1B engines. This AD was prompted by a report of a center vent tube (CVT) failure leading to a loss of oil pressure and subsequent in-flight engine shutdown. This AD requires removal of an affected extension duct and replacing it with a part eligible for installation. We are issuing this AD to address the unsafe condition on these products.
At the next engine shop visit after the effective date of this AD, remove air/oil extension ducts, P/N 2332M85P01 or 2331M25G03, and replace with a part eligible for installation.
For the purpose of this AD, an “engine shop visit” is the induction of an engine into the shop for maintenance involving the separation of pairs of major mating engine case flanges, except for the following situations, which do not constitute an engine shop visit:
(1) Separation of engine flanges solely for the purposes of transportation of the engine without subsequent maintenance.
(2) Separation of engine flanges solely for the purpose of replacing the fan or propulsor without subsequent maintenance.
After the effective date of this AD, do not install an air/oil extension duct, P/N 2332M85P01 or 2331M25G03, into a fan mid shaft assembly.
