Federal Aviation Administration December 19, 2005 – Federal Register Recent Federal Regulation Documents
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Airworthiness Directives; Aviointeriors S.p.A. (formerly ALVEN), Series 312 Box Mounted Seats; Correction
This document makes a correction to Airworthiness Directive (AD) 2005-20-26. That AD applies to Aviointeriors S.p.A. (formerly ALVEN), series 312 box mounted seats. That AD published in the Federal Register on October 12, 2005 (70 FR 59243). This document corrects the AD number in the Amendatory section. In all other respects, the original document remains the same.
Special Conditions; Envoy Aerospace; EFIS on the Raytheon Model B200, B200C, 300, B300, and B300C; Protection of Systems for High Intensity Radiated Fields (HIRF)
These special conditions are issued to Envoy Aerospace, 5027 Switch Grass Lane, Naperville, Illinois 60564-5368, for a Supplemental Type Certificate for the Raytheon B200, B200C, 300, B300, and B300C models. These models will have novel and unusual design features when compared to the state of technology envisaged in the applicable airworthiness standards. These novel and unusual design features include the installation of an electronic flight instrument system (EFIS) and a navigation display. The EFIS consists of the Universal Avionics, Inc. EFI-890R system for which the applicable regulations do not contain adequate or appropriate airworthiness standards for the protection of these systems from the effects of high intensity radiated fields (HIRF). The installation includes three EFI-890R Flat Panel Displays (two Primary Flight Displays Pilot/Copilot and one Navigational Display), and supporting equipment. These special conditions contain the additional safety standards that the Administrator considers necessary to establish a level of safety equivalent to the airworthiness standards applicable to these airplanes.
Special Conditions: Raytheon Aircraft Company Model HS.125 Airplanes; High-Intensity Radiated Fields (HIRF)
These special conditions are issued for a Raytheon Aircraft Company Model HS.125 airplane modified by AeroMech Incorporated. This modified airplane will have a novel or unusual design feature when compared to the state of technology envisioned in the airworthiness standards for transport category airplanes. The modification incorporates the installation of Innovative Solutions and Support air data display units (ADDU). These systems perform critical functions. The applicable airworthiness regulations do not contain adequate or appropriate safety standards for the protection of these systems from the effects of high-intensity radiated fields (HIRF). 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.
Proposed Advisory Circular 25.21-1X, Performance and Handling Characteristics in the Icing Conditions Specified in Part 25, Appendix C
This notice announces the extension of the comment period for Notice of availability of proposed Advisory Circular (AC) 25.21-1X, and request for comments, which was published in the Federal Register on November 4, 2005 (70 FR 67303), and closes on January 3, 2006. In that notice, the FAA invited public comment on a proposed AC which provides guidance on a means, but not the only means, of compliance with the proposed certification requirements for performance and handling characteristics of transport category airplanes affected by flight in the icing conditions defined in appendix C of Title 14, Code of Federal Regulations (CFR) part 25. This extension of the comment period is necessary to give all interested persons an opportunity to present their views on the proposed AC.
Proposed Revisions to Advisory Circular 25-7A, Flight Test Guide for Certification of Transport Category Airplanes
This notice requests comments regarding proposed revisions to Advisory Circular (AC) 25-7A, ``Flight Test Guide for Certification of Transport Category Airplanes.'' Advisory Circular 25-7A provides guidance on acceptable means, but not the only means, of demonstrating compliance with the airworthiness standards for transport category airplanes. The proposed revisions would remove the guidance material associated with certification for flight in icing conditions. This material is addressed in NPRM No. 05-10, ``Airplane Performance and Handling Qualities In Icing Conditions'' and the guidance material proposed in AC 25.21-1, ``Performance And Handling Characteristics In The Icing Conditions Specified In Part 25, Appendix C.'' This notice provides interested persons an opportunity to comment on the proposed revisions to AC 25-7A.
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