# Airworthiness Directives; Boeing Model 737-200 Series Airplanes
> **Rule** · Final rule. · Published 2008-03-12 · Effective 2008-04-16 · 73 FR 13109
## Document
- **Document number:** E8-4674
- **Category:** airworthiness
- **Manufacturer:** Boeing Model 737-200 Series
- **Type:** Rule
- **Action:** Final rule.
- **Citation:** 73 FR 13109
- **Publication date:** 2008-03-12
- **Effective date:** 2008-04-16
- **FAA docket:** Docket No. FAA-2007-0228
## Abstract

We are adopting a new airworthiness directive (AD) for certain Boeing Model 737-200 series airplanes. This AD requires repetitive inspections to detect cracking of the support fittings of the Krueger flap actuators, and corrective actions if necessary. This AD also requires eventual replacement of any existing aluminum support fitting on each wing with a steel fitting, and modification of the aft attachment of the actuator. Doing these actions terminates the repetitive inspection requirements. This AD results from reports of cracking due to fatigue and stress corrosion of the support fittings of the Krueger flap actuator. We are issuing this AD to prevent cracking of the support fittings, which could result in fracturing of the actuator attach lugs, separation of the actuator from the support fitting, severing of the hydraulic lines, resultant loss of hydraulic fluids, and consequent reduced controllability of the airplane.

## Source
- [Federal Register document](https://www.federalregister.gov/documents/2008/03/12/E8-4674/airworthiness-directives-boeing-model-737-200-series-airplanes)
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