Federal Aviation Administration January 11, 2012 – Federal Register Recent Federal Regulation Documents
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Airworthiness Directives; Agusta S.p.A. Helicopters
We propose to adopt a new airworthiness directive (AD) for all Agusta S.p.A. (Agusta) Model A109, A109A, A109A II, A109C, A109K2, A109E, A109S, and A119 helicopters. This proposed AD is prompted by a mandatory continuing airworthiness information (MCAI) AD issued by the European Aviation Safety Agency (EASA), which is the Technical Agent for the Member States of the European Community. The MCAI AD states that a Model A109E helicopter has experienced a failure of the tail rotor pitch control link assembly caused by a production defect. The proposed actions are intended to prevent failure of a tail rotor pitch control link and subsequent loss of control of the helicopter.
Harmonization of Airworthiness Standards for Transport Category Airplanes-Landing Gear Retracting Mechanisms and Pilot Compartment View
The Federal Aviation Administration amends the airworthiness standards for transport category airplanes on landing gear retracting mechanisms and the pilot compartment view. For the landing gear retracting mechanism, this rulemaking adopts the 1-g stall speed as a reference stall speed instead of the minimum speed obtained in a stalling maneuver and adds an additional requirement to keep the landing gear and doors in the correct retracted position in flight. For the pilot compartment view, this rulemaking revises the requirements for pilot compartment view in precipitation conditions. This action eliminates regulatory differences between the airworthiness standards of the U.S. and the European Aviation Safety Agency (EASA), without affecting current industry design practices.
Authorization To Use Lower Than Standard Takeoff, Approach and Landing Minimums at Military and Foreign Airports
This rulemaking would allow qualified operators to conduct lower than standard instrument flight rules (IFR) airport operations at military airports or outside the United States when authorized to do so by their operations specifications. This action is necessary because the current regulatory section limits certain operators to a takeoff minimum visibility of 1 mile, and a landing minimum visibility of \1/2\ mile when conducting IFR operations at those airports, even when the operator has demonstrated the ability to safely conduct operations in lower visibility. The intended effect of this final rule is to bring the identified regulatory section into alignment with other sections of the regulations that currently permit lower than standard IFR operations at domestic civilian, foreign, and military airports when authorized to do so.
Petition for Exemption; Summary of Petition Received
This notice contains a summary of a petition seeking relief from specified requirements of 14 CFR. The purpose of this notice is to improve the public's awareness of, and participation in, this aspect of FAA's regulatory activities. Neither publication of this notice nor the inclusion or omission of information in the summary is intended to affect the legal status of the petition or its final disposition.
Special Conditions: The Boeing Company, Model 767-300; Seats With Inflatable Lapbelts
These special conditions are issued for the Boeing Model 767- 300 series airplanes. These airplanes will have a novel or unusual design feature associated with seats with inflatable lapbelts. 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.
Emergency Locator Transmitters (ELTs)
This notice announces the FAA's intent to cancel TSO-C91a, Emergency Locator Transmitter (ELT) Equipment. The effect of the cancelled TSO will result in no new TSO-C91a design or production approvals. However, cancellation will not affect production according to an existing TSO authorization (TSOA). Articles produced under an existing TSOA can still be installed according to existing airworthiness approvals and applications for new airworthiness approvals will still be processed. This action does not impact operation of TSO-C91a ELTs, and these ELTs will continue to satisfy the 14 Code of Federal Regulation (14 CFR) Sec. 91.207 ELT equipage requirement.
Proposed Establishment of Restricted Areas R-5402, R-5403A, R-5403B, R-5403C, R-5403D, R-5403E, R-5403F; Devils Lake, ND
This action extends the comment period for an NPRM that was published on November 28, 2011. In that document, the FAA proposed to establish restricted area airspace within the Devils Lake East Military Operations Area (MOA), overlying Camp Grafton Range, in the vicinity of Devils Lake, ND. This extension is a result of a request from the North Dakota Aviation Council (NDAC), representing eight member groups including the Airport Association of North Dakota, North Dakota Business Aviation Association, North Dakota Pilots Association, North Dakota Professional Aviation Mechanics Association, and North Dakota Flying Farmers, to extend the comment period to the proposal.
Notice of Passenger Facility Charge (PFC) Approvals and Disapprovals
The FAA publishes a monthly notice, as appropriate, of PFC approvals and disapprovals under the provisions of the Aviation Safety and Capacity Expansion Act of 1990 (Title IX of the Omnibus Budget Reconciliation Act of 1990) (Pub. L. 101-508) and Part 158 of the Federal Aviation Regulations (14 CFR part 158). This notice is published pursuant to paragraph d of Sec. 158.29.
Airworthiness Directives; Schempp-Hirth Flugzeugbau GmbH Gliders
We are adopting a new airworthiness directive (AD) for Schempp-Hirth Flugzeugbau GmbH Model Discus 2cT gliders. This AD results from mandatory continuing airworthiness information (MCAI) issued by an aviation authority of another country to identify and correct an unsafe condition on an aviation product. The MCAI describes the unsafe condition as small cracks which have been found on engine pylons in the area of the lower engine support that have not been detected during the standard daily inspection. This condition, if not detected and corrected, could lead to an engine pylon failure resulting in loss of control of the glider. We are issuing this AD to require actions to address the unsafe condition on these products.
Airworthiness Directives; Various Aircraft Equipped With Rotax Aircraft Engines 912 A Series Engine
We are adopting a new airworthiness directive (AD) for various aircraft equipped with Rotax Aircraft Engines 912 A series engine. This AD results from mandatory continuing airworthiness information (MCAI) issued by the aviation authority of another country to identify and correct an unsafe condition on an aviation product. The MCAI describes the unsafe condition as a deviation in the manufacturing process of certain part number 888164 crankshafts that may cause cracks on the surface of the crankshaft on the power take off side, which could lead to failure of the crankshaft support bearing and possibly result in an in-flight engine shutdown and forced landing. We are issuing this AD to require actions to address the unsafe condition on these products.
Airworthiness Directives; Socata Airplanes
We are adopting a new airworthiness directive (AD) for Socata Model TBM 700 airplanes. This AD results from mandatory continuing airworthiness information (MCAI) issued by an aviation authority of another country to identify and correct an unsafe condition on an aviation product. The MCAI describes the unsafe condition as installation of the wrong (switched) aileron control cables in the wing. This unsafe condition could lead to restricted movement of the aileron, resulting in reduced control of the airplane. We are issuing this AD to require actions to address the unsafe condition on these products.
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