Federal Aviation Administration February 25, 2005 – Federal Register Recent Federal Regulation Documents

Proposed Amendment of Class E Airspace; Parsons, TN
Document Number: 05-3615
Type: Proposed Rule
Date: 2005-02-25
Agency: Federal Aviation Administration, Department of Transportation
This notice proposes to amend Class E5 airspace at Parsons, TN. The Beech River Regional Airport is being constructed at Parsons, TN. As a result, airspace must be established to contain the Area Navigation (RNAV) Global Positioning System (GPS) Runway (RWY) 19 Standard Instrument Approach Procedure (SIAP) to Beech River Regional Airport. Controlled airspace extending upward from 700 feet Above Ground Level (AGL) is needed to contain the SIAP.
Special Conditions: Cessna Aircraft Company Model 501 Airplanes; High Intensity Radiated Fields (HIRF)
Document Number: 05-3614
Type: Rule
Date: 2005-02-25
Agency: Federal Aviation Administration, Department of Transportation
These special conditions are issued for Cessna Aircraft Company Model 501 airplanes modified by Garrett Aviation Services. These airplanes will have novel and unusual design features when compared to the state of technology envisioned in the airworthiness standards for transport category airplanes. The modification incorporates the installation of Electronic Flight Displays with Engine Indication and Flight Information Systems. 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.
RTCA Special Committee 189/EUROCAE Working Group 53: Air Traffic Services (ATS) Safety and Interoperability Requirements
Document Number: 05-3613
Type: Notice
Date: 2005-02-25
Agency: Federal Aviation Administration, Department of Transportation
The FAA is issuing this notice to advise the public of a meeting of RTCA Special Committee 189/EUROCAE Working Group 53: Air Traffic Services (ATS) Safety and Interoperability Requirements.
RTCA Special Committee 135/EUROCAE Working Group 14: Environmental Conditions and Test Procedures for Airborne Equipment
Document Number: 05-3612
Type: Notice
Date: 2005-02-25
Agency: Federal Aviation Administration, Department of Transportation
The FAA is issuing this notice to advise the public of a meeting of RTCA Special Committee 135/EUROCAE Working Group 14: Environmental Conditions and Test Procedures for Airborne Equipment.
RTCA Special Committee 159: Global Positioning System (GPS)
Document Number: 05-3611
Type: Notice
Date: 2005-02-25
Agency: Federal Aviation Administration, Department of Transportation
The FAA is issuing this notice to advise the public of a meeting of RTCA Special Committee 159: Global Positioning System.
Establishment of Class D and E Airspace; Olive Branch, MS and Amendment of Class E Airspace; Memphis, TN
Document Number: 05-3610
Type: Rule
Date: 2005-02-25
Agency: Federal Aviation Administration, Department of Transportation
This action confirms the new effective date for the establishment of Class D and E4 airspace at Olive Branch, MS and the amendment of Class E5 airspace at Memphis, TN. The construction of a new Federal contract tower with a weather reporting system was delayed; therefore, the effective date of the establishment of Class D and E4 airspace and amendment of Class E5 airspace was also delayed.
Universal Access Transceiver Equipment
Document Number: 05-3609
Type: Notice
Date: 2005-02-25
Agency: Federal Aviation Administration, Department of Transportation
This notice announces the availability of, and requests comments on, proposed Technical Standard Order (TSO)-C154a, Universal Access Transceiver (UAT) Automatic Dependent Surveillance-Broadcast (ADS-B) Equipment Operating on the Frequency of 978 MHz. In this TSO, we (the Federal Aviation Administration, or FAA) refer to a revised minimum performance standard (MPS)RTCA Inc., Document (RTCA/DO)-282A, Minimum Operational Performance Standards for Universal Access Transceiver (UAT) Automatic Dependent Surveillance Broadcast (ADS-B), dated July 29, 2004. We also add Appendix 1, which lists corrections to RTCA/DO-282A since its date of issuance. The TSO also supports an optional frequency Diplexer. The Diplexer allows the ATCRBS/Mode S Transponder and the UAT equipment developed under this TSO to share antennas. This TSO is for manufacturers of Universal Access Transceiver ADS-B equipment or UAT Diplexer seeking a TSO authorization or letter of design approval. In it, we tell them what MPS their UAT equipment must meet for approval and identification with the TSO-C154a marking.
Nickel-Cadmium and Lead-Acid Batteries
Document Number: 05-3608
Type: Notice
Date: 2005-02-25
Agency: Federal Aviation Administration, Department of Transportation
This notice announces the availability of, and requests comments on, a proposed Technical Standard Order (TSO) on nickel- cadmium and lead-acid batteries. These batteries power aircraft equipment (emergency and standby systems, plus engine or APU starting). The TSO prescribes minimum performance standards for these batteries to be identified with the marking ``TSO-C173.''
Aircraft Audio Systems and Equipment
Document Number: 05-3607
Type: Notice
Date: 2005-02-25
Agency: Federal Aviation Administration, Department of Transportation
This notice announces the availability of, and requests comments on proposed Technical Standard Order (TSO)-C139, Aircraft Audio Systems and Equipment. The proposed TSO is for audio systems designers, manufacturers, and installers seeking a TSO authorization or letter of design approval. In it, we (the Federal Aviation Administration, or FAA) describe what minimum performance standards (MPS) their audio systems and equipment must meet for approval and identification with applicable TSO marking. We also combine and update the requirements of TSO-C50c, Audio Selector Panels and Amplifers; TSO- 57a, Headsets and Speakers; and TSO-C58a, Aircraft Microphones (except carbon).
Aircraft Clamps
Document Number: 05-3606
Type: Notice
Date: 2005-02-25
Agency: Federal Aviation Administration, Department of Transportation
This notice announces the availability of, and requests comment on, a proposed Technical Standard Order (TSO) on aircraft clamps. The TSO prescribes minimum performance standards that aircraft clamps must meet to be identified with the making ``TSO-C171.''
Airworthiness Directives; Saab Model SAAB SF340A and SAAB 340B Series Airplanes
Document Number: 05-3281
Type: Rule
Date: 2005-02-25
Agency: Federal Aviation Administration, Department of Transportation
The FAA is adopting a new airworthiness directive (AD) for certain Saab Model SAAB SF340A and SAAB 340B series airplanes. This AD requires repetitive inspections for wear of the brushes and leads and for loose rivets of the direct current (DC) starter generator, and related investigative/corrective actions if necessary. This AD is prompted by reports of premature failures of the DC starter generator prior to scheduled overhaul. We are issuing this AD to prevent failure of the starter generator, which could cause a low voltage situation in flight and result in increased pilot workload and reduced redundancy of the electrical powered systems.
Airworthiness Directives; Short Brothers Model SD3-60 Series Airplanes
Document Number: 05-3268
Type: Rule
Date: 2005-02-25
Agency: Federal Aviation Administration, Department of Transportation
The FAA is adopting a new airworthiness directive (AD) for all Short Brothers Model SD3-60 series airplanes. This AD requires, for certain airplanes, repetitive inspections for cracking of the balance weight brackets of the elevator trim tabs, and replacement of any cracked bracket with a new or reworked bracket that conforms to the approved design standard. This AD also provides for an optional terminating action for the repetitive inspections. This AD is prompted by reports indicating that balance weight brackets have been found cracked on both the left and right elevator trim tabs. We are issuing this AD to prevent failure of the balance weight bracket for the elevator trim tab, which could cause loss of the balance weight. This could result in incorrect trim during takeoff and landing, and reduced controllability of the airplane.
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