# Airworthiness Directives; The Boeing Company Airplanes
> **Rule** · Final rule. · Published 2015-06-16 · Effective 2015-07-21 · 80 FR 34244
## Document
- **Document number:** 2015-14397
- **Category:** airworthiness
- **Manufacturer:** The Boeing Company
- **Type:** Rule
- **Action:** Final rule.
- **Citation:** 80 FR 34244
- **Publication date:** 2015-06-16
- **Effective date:** 2015-07-21
- **FAA docket:** Docket No. FAA-2014-0575
## Abstract

We are adopting a new airworthiness directive (AD) for all The Boeing Company Model 747-8F and 747-8 series airplanes. This AD was prompted by reports of delamination damage to leading edge (LE) variable camber krueger (VCK) flaps. This AD requires repetitive inspections to detect delamination damage of the lightning strike applique (LSA) on certain LE VCK flaps, and corrective actions if necessary. We are issuing this AD to detect and correct delamination damage to certain LE VCK flaps, which can reduce the lightning strike protection capability on certain LE VCK flaps and result in an uncommanded motion of the trailing edge flap system; such uncommanded flap motion, without shutdown of the trailing edge or leading edge flaps, could cause unexpected changes in lift, potentially resulting in asymmetric lift and loss of control of the airplane.

## Source
- [Federal Register document](https://www.federalregister.gov/documents/2015/06/16/2015-14397/airworthiness-directives-the-boeing-company-airplanes)
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