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September 20, 2020

FAA Statement on House Transportation & Infrastructure Committee Report

FAA 'Looks Forward To Working With The Committee To Implement Improvements Identified' (In The Report)

The FAA has responded to the long awaited report from the House of Representatives Committee on Transportation & Infrastructure has been published and as many government reports are wont to do, it places a lot of blame... but not always prioritized according to the realities of the situation at hand. We noted in our original report that 'While the politicians were patting themselves on the back generously, the report fails to prioritize the ponderous issues involved with the airlines (and the training issues associated with them), that the airlines involved in the two accidents, presented. It also makes sweeping judgments about improper/fraud

AD 2020-18-14 Prompted By A Report From The Manufacturer That A Subsurface Anomaly Was Found

The FAA is adopting a new airworthiness directive (AD) for all General Electric Company (GE) GE90-110B1 and GE90-115B model turbofan engines with a certain high-pressure turbine (HPT) rotor stage 2 disk installed. This AD was prompted by a report from the manufacturer that a subsurface anomaly was found on a HPT rotor stage 2 disk. This AD requires an ultrasonic inspection (USI) of the HPT rotor stage 2 disk and, depending on the result of the inspection, replacement of the HPT rotor stage 2 disk with a part eligible for installation. The FAA is issuing this AD to address the unsafe condition on these products. This AD is effective October 21, 2020.

AD 2020-18-09 Prompted By A Report Of An Engine Experiencing An Uncontained Release Of LPT Blades

The FAA is adopting a new airworthiness directive (AD) for all Honeywell International Inc. (Honeywell) ALF502L, ALF502L-2, ALF502L-2A, ALF502L-2C, ALF502L-3, ALF502R-3, ALF502R-3A, ALF502R-4, ALF502R-5, ALF502R-6, LF507-1F, and LF507-1H model turbofan engines. This AD was prompted by a report of an engine experiencing an uncontained release of low-pressure turbine (LPT) blades. This AD requires initial and repetitive visual inspections of the overspeed fuel solenoid valve assembly and the fuel filter outlet. Depending on the results of these inspections, the AD may require inspection of the adjacent fuel system tube assemblies as well as replacement