# Special Conditions: Airbus Model A380-800 Airplane, Transient Engine Failure Loads
> **Rule** · Final special conditions. · Published 2006-10-20 · Effective 2006-10-06 · 71 FR 61869
## Document
- **Document number:** E6-17534
- **Category:** other
- **Type:** Rule
- **Action:** Final special conditions.
- **Citation:** 71 FR 61869
- **Publication date:** 2006-10-20
- **Effective date:** 2006-10-06
- **FAA docket:** Docket No. NM322
## Abstract

These special conditions are issued for the Airbus A380-800 airplane. This airplane will have novel or unusual design features when compared to the state of technology envisioned in the airworthiness standards for transport category airplanes. Some of these novel or unusual design features are associated with the high bypass engines used on the Model A380. For these design features, the applicable airworthiness regulations do not contain adequate or appropriate safety standards regarding transient engine failure loads. These proposed special conditions contain the additional safety standards that the Administrator considers necessary to establish a level of safety equivalent to that established by the existing airworthiness standards. Additional special conditions will be issued for other novel or unusual design features of the Airbus Model A380-800 airplane.

## Source
- [Federal Register document](https://www.federalregister.gov/documents/2006/10/20/E6-17534/special-conditions-airbus-model-a380-800-airplane-transient-engine-failure-loads)
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