federal_register: 2014-18660
This data as json
| document_number | title | type | abstract | publication_date | pub_year | pub_month | html_url | pdf_url | agency_names | agency_ids | excerpts | regulation_id_numbers |
|---|---|---|---|---|---|---|---|---|---|---|---|---|
| 2014-18660 | Special Conditions: Airbus Model A350-900 Airplane; Flight-Envelope Protection, Normal Load-Factor (G) Limiting | Rule | These special conditions are issued for Airbus Model A350-900 airplanes. These airplanes will have a novel or unusual design feature associated with a flight-control system that prevents the pilot from inadvertently or intentionally exceeding the positive or negative airplane limit load factor. The applicable airworthiness regulations do not contain adequate or appropriate safety standards for this design feature. These 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. | 2014-08-07 | 2014 | 8 | https://www.federalregister.gov/documents/2014/08/07/2014-18660/special-conditions-airbus-model-a350-900-airplane-flight-envelope-protection-normal-load-factor-g | https://www.govinfo.gov/content/pkg/FR-2014-08-07/pdf/2014-18660.pdf | Transportation Department; Federal Aviation Administration | 492,159 | These special conditions are issued for Airbus Model A350-900 airplanes. These airplanes will have a novel or unusual design feature associated with a flight-control system that prevents the pilot from inadvertently or intentionally exceeding the... |