# Airworthiness Directives; Boeing Model 747-200C and 747-200F Series Airplanes
> **Rule** · Final rule. · Published 2005-05-23 · Effective 2005-06-27 · 70 FR 29442
## Document
- **Document number:** 05-9981
- **Category:** airworthiness
- **Manufacturer:** Boeing Model 747-200C and 747-200F Series
- **Type:** Rule
- **Action:** Final rule.
- **Citation:** 70 FR 29442
- **Publication date:** 2005-05-23
- **Effective date:** 2005-06-27
- **FAA docket:** Docket No. FAA-2005-20024
## Abstract

The FAA is adopting a new airworthiness directive (AD) for all Boeing Model 747-200C and 747-200F series airplanes. This AD requires repetitive inspections for cracking of the left and right C-3 frame upper closure fittings of the nose cargo door, and corrective actions if necessary. This AD also provides an optional modification that, if done, terminates inspections in certain areas. This AD is prompted by reports indicating that fatigue cracking was found in the inboard flange above the flight deck floor on the C-3 frame upper closure fittings of the nose cargo door. We are issuing this AD to detect and correct cracking of the C-3 frame upper closure fittings, which could extend and result in rapid depressurization of the airplane.

## Source
- [Federal Register document](https://www.federalregister.gov/documents/2005/05/23/05-9981/airworthiness-directives-boeing-model-747-200c-and-747-200f-series-airplanes)
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