Federal Aviation Administration June 11, 2010 – Federal Register Recent Federal Regulation Documents
Results 1 - 5 of 5
Modification of Jet Routes J-32, J-38, and J-538; Minnesota
This action modifies Jet Routes J-32 and J-38 by terminating portions of the routes that are no longer needed at the Duluth, MN, VHF omnidirectional range/tactical air navigation (VORTAC) that are no longer needed. This action also modifies the J-538 airway description to align it with the corresponding segment of J-538 contained in Canadian airspace. This action is necessary for the safety and management of instrument flight rules (IFR) operations within the National Airspace System (NAS).
Revision of Class E Airspace; Galena, AK
This action revises Class E airspace at Galena, AK, to accommodate three amended Standard Instrument Approach Procedures (SIAPs) and the development of one Obstacle Departure Procedure (ODP) at the Edward G. Pitka Sr. Airport. The FAA is taking this action to enhance safety and management of Instrument Flight Rules (IFR) operations at Edward G. Pitka Sr. Airport.
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. 1A158.29.
Airworthiness Directives; Microturbo Saphir 20 Model 095 Auxiliary Power Units (APUs)
We are adopting a new airworthiness directive (AD) for the products listed above. This AD results from mandatory continuing airworthiness information (MCAI) issued by the European Aviation Safety Agency (EASA) to identify and correct an unsafe condition on an aviation product. The MCAI describes the unsafe condition as:
Airworthiness Directives; Bell Helicopter Textron Canada Model 222, 222B, 222U, 230, and 430 Helicopters
This amendment supersedes an existing airworthiness directive (AD) for the specified Bell Helicopter Textron Canada (BHTC) helicopters, that currently requires certain checks and inspections of the tail rotor blades. If a crack is found, the existing AD requires replacing the tail rotor blade (blade) with an airworthy blade before further flight. This amendment requires the same checks and inspections of the blades until they are required to be replaced and removes certain serial numbered and specifically coded blades from the applicability of the AD. This amendment is prompted by the approved rework of certain blades and two newly redesigned blades, which, if installed, constitute terminating action for the inspection requirements. The actions specified by this AD are intended to detect a crack in a blade, and to prevent loss of a blade and subsequent loss of control of the helicopter.
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