Department of Transportation February 27, 2014 – Federal Register Recent Federal Regulation Documents
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Changes to Production Certificates and Approvals
The FAA is proposing changes to its certification procedures and identification requirements for aeronautical products and articles. The proposed changes would: require production approval holders to identify an accountable manager who would be responsible for, and have authority over, their production operations and serve as the primary contact with the FAA; allow production approval holders to issue authorized release documents for aircraft engines, propellers, and articles; permit production certificate holders to manufacture and install interface components; require production approval holders to ensure that each supplier-provided product, article, or service conforms to the production approval holder's requirements and establish a supplier-reporting process for products, articles, or services that have been released from or provided by the supplier and subsequently found not to conform to the production approval holder's requirements; and remove the requirement that fixed-pitch wooden propellers be marked using an approved fireproof method. This proposal is necessary to update our regulations by revising certification and marking requirements to reflect the current global aeronautical manufacturing environment, thereby promoting aviation safety.
Consensus Standards, Light-Sport Aircraft
This notice announces the availability of two new and eight revised consensus standards relating to the provisions of the Sport Pilot and Light-Sport Aircraft rule issued July 16, 2004, and effective September 1, 2004. ASTM International Committee F37 on Light Sport Aircraft developed the new and revised standards with Federal Aviation Administration (FAA) participation. By this notice, the FAA finds the new and revised standards acceptable for certification of the specified aircraft under the provisions of the Sport Pilot and Light-Sport Aircraft rule.
Government/Industry Aeronautical Charting Forum Meeting
This notice announces the bi-annual meeting of the Federal Aviation Administration (FAA) Aeronautical Charting Forum (ACF) to discuss informational content and design of aeronautical charts and related products, as well as instrument flight procedures development policy and design criteria.
Agency Information Collection Activities: Request for Comments for a New Information Collection
In compliance with the Paperwork Reduction Act (PRA) of 1995 (44 U.S.C. 3501-3521), this notice announces that FHWA will submit the collection of information described below to the Office of Management and Budget (OMB) for review and comment. The Federal Register Notice with a 60-day comment period soliciting comments on the following collection of information was published on December 20, 2013. The PRA submission describes the nature of the information collection and its expected cost and burden.
Airworthiness Directives; Bombardier, Inc. Airplanes
We propose to adopt a new airworthiness directive (AD) for certain Bombardier, Inc. Model CL-215-6B11 (CL-215T Variant), and CL- 215-6B11 (CL-415 Variant) airplanes. This proposed AD was prompted by several reports indicating that shorter nacelle strut bushings were inadvertently installed on certain airplanes. This proposed AD would require a general visual inspection of the left and right nacelle upper strut bushings; installation of the bolts and preload indicating (PLI) washers, if necessary; and replacement of the bushing or repair of the bushing installation, if necessary. We are proposing this AD to detect and correct inadequate nacelle strut bushings, which provide insufficient engagement in the strut fork end, and could deform under the bearing load and lead to the failure of the joint.
Airworthiness Directives; Airbus Airplanes
We propose to supersede airworthiness directive (AD) 2007-06- 12, that applies to certain Airbus Model A330-200 and A330-300 airplanes. AD 2007-06-12 requires, for certain airplanes, reinforcement of the structure of the center fuselage by installing external stiffeners (butt straps) at frame (FR) 53.3 on the fuselage skin between left-hand (LH) and right-hand (RH) stringer (STR) 13, and related investigative and corrective actions. Since we issued AD 2007- 06-12, we have determined that the compliance times must be reduced in order to address the unsafe condition. This proposed AD would reduce the compliance times for reinforcing the structure of the center fuselage at FR 53.3. We are proposing this AD to prevent fatigue cracking of the fuselage, which could result in reduced structural integrity of the fuselage.
Airworthiness Directives; Airbus Airplanes
We propose to supersede Airworthiness Directives (AD) 2006-21- 08, AD 2007-14-01, AD 2008-25-02, AD 2010-04-09, AD 2011-01-02, and AD 2012-16-05, for certain Airbus Model A330 and 340 series airplanes. AD 2006-21-08, AD 2007-14-01, AD 2008-25-02, AD 2010-04-09, AD 2011-01-02, and AD 2012-16-05 currently require revising the maintenance program or inspection program to incorporate certain maintenance requirements and airworthiness limitations for fuel tank systems. Since we issued AD 2006-21-08, AD 2007-14-01, AD 2008-25-02, AD 2010-04-09, AD 2011-01-02, and AD 2012-16-05, we have determined that more restrictive maintenance requirements and airworthiness limitations are necessary. This proposed AD would require a new maintenance or inspection program revision. We are proposing this AD to prevent the potential of ignition sources inside fuel tanks, which, in combination with flammable fuel vapors, could result in fuel tank explosions and consequent loss of the airplane.
Airworthiness Directives; Embraer S.A. Airplanes
We propose to supersede Airworthiness Directive (AD) 2012-07- 08, for all Embraer S.A. Model ERJ 170 airplanes. AD 2012-07-08 currently requires revising the Airworthiness Limitations Section (ALS) of the Instructions for Continued Airworthiness (ICA) to incorporate new structural inspection requirements. Since we issued AD 2012-07-08, we have determined that more restrictive maintenance requirements and airworthiness limitations are necessary. This proposed AD would require revising the maintenance or inspection program to incorporate new inspections. We are proposing this AD to detect and correct fatigue cracking of structural components, which could result in reduced structural integrity of the airplane.
Next Phase of the Regulatory Review of Existing DOT Regulations
In accordance with Executive Order 13563, ``Improving Regulation and Regulatory Review,'' the Department of Transportation (Department, DOT, or we) is conducting a review of its existing regulations to evaluate their continued validity and determine whether they are crafted effectively to solve current problems. On February 16, 2011, the Department began a process to review existing regulations, which included a public meeting and various other opportunities to solicit public comments. That process resulted in a Plan for Implementation of Executive Order 13563 that was released in August 2011. Additionally, the Department has regularly updated the list of regulations that are under review or further study and provided updates on timing of the review. The latest update was released in January 2014 and can be found at https://www.reginfo.gov. (See Appendix D of the Department's semi-annual Regulatory Agenda.) In continuing this effort, the Department again invites the public to comment on the next phase of its retrospective regulatory review process.
Airworthiness Directives; Saab AB, Saab Aerosystems Airplanes
We are adopting a new airworthiness directive (AD) for certain Saab AB, Saab Aerosystems Model 340A (SAAB/SF340A) and SAAB 340B airplanes modified by Supplemental Type Certificate SA7971SW. This AD was prompted by reports of smoke, a burning odor, and possible fire in the flight deck and cabin of the airplane, which was caused by brushes wearing beyond their limits in the air conditioning motor. This AD requires an inspection to determine if a certain air compressor motor is installed, an inspection to determine the age of a certain compressor hour meter since new or overhauled, and repetitive replacement of the brushes on affected air conditioning compressor motor units. As an option to the replacement, this AD allows pulling the air conditioning circuit breaker and adding a placard. We are issuing this AD to detect and correct worn brushes contacting the commutator, which could result in a fire under the cabin floor with no means to detect or extinguish the fire.
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