Airworthiness Directives; General Electric Company (GE) CF6-80E1A2 and -80E1A4 Turbofan Engines; Correction
airworthiness · Rule · Final rule; request for comments correction. · Published 2004-01-14 · Effective 2004-01-14 · 69 FR 2062
Document
Document number
04-760
Federal Register citation
69 FR 2062
Type
Rule
Action
Final rule; request for comments correction.
Category
airworthiness
Manufacturer
General Electric Company (GE) CF6-80E1A2 and -80E1A4 Turbofan
Publication date
2004-01-14
Effective date
2004-01-14
FAA docket
Docket No. 2003-NE-26-AD
Abstract
This document makes a correction to Airworthiness Directive (AD) 2003-26-11 applicable to GE CF6-80E1A2 and -80E1A4 turbofan engines with left vertical link bolts part number (P/N) 1304M26P02 installed, and pylon attachment bolts originally torqued to 450-500 lb ft. That AD was published in the Federal Register on January 6, 2004 (69 FR 494). The SUPPLEMENTARY INFORMATION paragraph title, first sentence, and first three words of the second sentence of that paragraph were inadvertently omitted. This document corrects that omission. In all other respects, the original document remains the same.