Airworthiness Directives; Lockheed Model 382, 382B, 382E, 382F, and 382G Series Airplanes
airworthiness · Rule · Final rule; correction. · Published 1996-08-16 · Effective 1996-07-15 · 61 FR 42549
Document
Document number
96-20872
Federal Register citation
61 FR 42549
Type
Rule
Action
Final rule; correction.
Category
airworthiness
Publication date
1996-08-16
Effective date
1996-07-15
FAA docket
Docket No. 95-NM-10-AD
Abstract
This document corrects information that appeared in airworthiness directive (AD) 96-12-20, amendment 39-9663, that was published in the Federal Register on June 10, 1996 (61 FR 29279). This AD is applicable to certain Lockheed Model 382, 382B, 382E, 382F, and 382G series airplanes. Among other things, it requires visual inspections to detect loose, missing, or deformed fasteners in the upper truss mounts of certain engines. This action corrects a reference to the outboard and inboard engines, which should have referred to the outboard and inboard truss mounts.