# Airworthiness Directives; Bombardier Model CL-215-1A10 and CL- 215-6B11 Series Airplanes; Correction
> **Rule** · Direct final rule; correction. · Published 1998-05-04 · Effective 1998-07-09 · 63 FR 24389
## Document
- **Document number:** 98-11560
- **Category:** airworthiness
- **Manufacturer:** Bombardier Model CL-215-1A10 and CL- 215-6B11 Series
- **Type:** Rule
- **Action:** Direct final rule; correction.
- **Citation:** 63 FR 24389
- **Publication date:** 1998-05-04
- **Effective date:** 1998-07-09
- **FAA docket:** Docket No. 98-NM-05-AD
## Abstract

This document corrects an error that appeared in amendment 39- 10458 that was published in the Federal Register on April 10, 1998 (63 FR 17672). The error resulted in the inadvertent omission of the applicability statement of the amendment. This amendment is applicable to certain Bombardier Model CL-215-1A10 and CL-215-6B11 series airplanes. This amendment requires repetitive inspections to detect cracking on certain wing to fuselage frame-angles, and repair, if necessary.

## Source
- [Federal Register document](https://www.federalregister.gov/documents/1998/05/04/98-11560/airworthiness-directives-bombardier-model-cl-215-1a10-and-cl--215-6b11-series-airplanes-correction)
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