# Airworthiness Directives; Lockheed Model 382, 382B, 382E, 382F, and 382G Series Airplanes
> **Rule** · Final rule; correction. · Published 1996-08-16 · Effective 1996-07-15 · 61 FR 42549
## Document
- **Document number:** 96-20872
- **Category:** airworthiness
- **Type:** Rule
- **Action:** Final rule; correction.
- **Citation:** 61 FR 42549
- **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.

## Source
- [Federal Register document](https://www.federalregister.gov/documents/1996/08/16/96-20872/airworthiness-directives-lockheed-model-382-382b-382e-382f-and-382g-series-airplanes)
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