Federal Aviation Administration November 2014 – Federal Register Recent Federal Regulation Documents

In accordance with the Paperwork Reduction Act of 1995, FAA invites public comments about our intention to request the Office of Management and Budget (OMB) approval to renew an information collection. The Federal Register Notice with a 60-day comment period soliciting comments on the following collection of information was published on September 3, 2014, vol. 79, no. 170, pages 52405-52406. The information will determine if applicant proposals for conducting commercial space launches can be accomplished according to regulations issued by the Office of the Associate Administrator for Commercial Space Transportation.

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.

This document corrects errors that appeared in final special conditions docket no. FAA-2013-0894, which was published in the Federal Register on December 20, 2013 (78 FR 76980). The errors are in the document's special conditions stage (notice vs. final) and special conditions number.

We are adopting a new airworthiness directive (AD) for certain The Boeing Company Model DC-9-10, DC-9-20, and DC-9-30 series airplanes. This AD was prompted by an evaluation by the design approval holder (DAH) indicating that the improved (shot-peened) aft fuselage non-ventral pressure bulkhead tee is subject to widespread fatigue damage (WFD). This AD requires repetitive inspections for cracking of the improved (shot-peened) non-ventral aft pressure bulkhead tees, and replacement if necessary. We are issuing this AD to detect and correct fatigue cracking of the improved (shot-peened) non-ventral aft pressure bulkhead tees connecting the bulkhead web to the fuselage, which could result in reduced structural integrity and rapid decompression of the airplane.

We are superseding Airworthiness Directive (AD) 2013-10-06, for all Airbus Model A330-200 Freighter, A330-200, A330-300, A340-200, A340-300, A340-500, and A340-600 series airplanes. AD 2013-10-06 required an inspection to identify the installed windshields, and replacement of any affected windshield. This new AD requires expanding the inspection area to 15 additional windshields' serial numbers. This AD was prompted by several reports of a burning smell and/or smoke in the cockpit during cruise phase, leading in some cases, to diversion to alternate airports. We are issuing this AD to prevent significantly increased workload for the flightcrew, which could, under some flight phases and/or circumstances, constitute an unsafe condition.

These special conditions are issued for Airbus Model A350-900 series airplanes. These airplanes will have novel or unusual design features, associated with flight-envelope protection in icing and non- icing conditions, that use low-speed incidence protection and an alpha- floor function that automatically advances throttles whenever the airplane angle of attack reaches a predetermined value. The applicable airworthiness regulations do not contain adequate or appropriate safety standards for these design features. 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.

This action extends the comment period for the Notice of availability of proposed revision to Advisory Circular for Aviation Safety Action Program (ASAP) that was published on September 5, 2014. In that document, the FAA proposed to clarify FAA policy, facilitate achievement of an ASAP's safety goals, and encourage wider participation in the program. Multiple industry groups have requested that the FAA extend the comment period closing date to allow time to prepare comments.

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.

This action confirms the effective date of the direct final rule published on July 28, 2014, and responds to the comments received on that direct final rule. The rule permits the pilot in command of a helicopter air ambulance to assess the weather at a departure point where current weather observations are not available and allows the pilot to depart if the observed ceiling and visibility is greater than certain weather minimums. This action will allow a pilot to utilize the minimum takeoff visibilities depicted in a published obstacle departure procedure, or in the absence of such a procedure, when the pilot observed ceiling and visibility is greater than the minimum ceiling and visibility limitations required by specific helicopter air ambulance rules. This change to the current regulation will permit helicopter air ambulance flights to enter the National Airspace System (NAS) under Instrument Flight Rules (IFR) when visibilities and ceilings are below Visual Flight Rules (VFR), thus increasing the safety of the flight.