# Airworthiness Directives; Construcciones Aeronauticas, S.A. (CASA) Model CN-235 Series Airplanes
> **Rule** · Final rule. · Published 1999-04-01 · Effective 1999-05-06 · 64 FR 15659
## Document
- **Document number:** 99-7690
- **Category:** airworthiness
- **Type:** Rule
- **Action:** Final rule.
- **Citation:** 64 FR 15659
- **Publication date:** 1999-04-01
- **Effective date:** 1999-05-06
- **FAA docket:** Docket No. 98-NM-219-AD
## Abstract

This amendment adopts a new airworthiness directive (AD), applicable to certain CASA Model CN-235 series airplanes. This amendment requires a one-time visual inspection to detect relative movement or deformation of the joint areas of the rear attaching supports and lower skin of the left and right outer flaps; repetitive borescopic inspections to detect cracking of the spar and of the rear internal support fittings of the outer flaps; and corrective actions, if necessary. This amendment also provides for optional terminating action for the repetitive inspections. This amendment is prompted by issuance of mandatory continuing airworthiness information by a foreign civil airworthiness authority. The actions specified by this AD are intended to detect and correct fatigue cracking of the rear internal support fittings of the outer flap structure, which could result in failure of the outer flaps, and consequent reduced controllability of the airplane.

## Source
- [Federal Register document](https://www.federalregister.gov/documents/1999/04/01/99-7690/airworthiness-directives-construcciones-aeronauticas-sa-casa-model-cn-235-series-airplanes)
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