Federal Aviation Administration July 5, 2016 – Federal Register Recent Federal Regulation Documents

Special Conditions: JAMCO America, Inc., Boeing Model 777-300ER, Dynamic Test Requirements for Single-Occupant Oblique (Side-Facing) Seats With Inflatable Restraints
Document Number: 2016-15784
Type: Rule
Date: 2016-07-05
Agency: Federal Aviation Administration, Department of Transportation
This document corrects omissions in docket no. FAA-2015-8298, special conditions no. 25-611-SC, which was published in the Federal Register on March 16, 2016 (81 FR 13969). The special conditions in the published document are incomplete. This correction replaces the entire special conditions section from that which appeared in the original Federal Register publication.
Acceptance Criteria for Portable Oxygen Concentrators Used on Board Aircraft; Correction
Document Number: 2016-15770
Type: Rule
Date: 2016-07-05
Agency: Federal Aviation Administration, Department of Transportation, Office of the Secretary
This document corrects a final rule which replaces the existing process by which the Federal Aviation Administration (Agency or FAA) approves portable oxygen concentrators (POC) for use on board aircraft in air carrier operations, commercial operations, and certain other operations using large aircraft. The FAA currently assesses each POC make and model on a case-by-case basis and if the FAA determines that a particular POC is safe for use on board an aircraft, the FAA conducts rulemaking to identify the specific POC model in an FAA regulation. The final rule replaces the current process and allows passengers to use a POC on board an aircraft if the POC satisfies certain acceptance criteria and bears a label indicating conformance with the acceptance criteria. The labeling requirement only affects POCs intended for use on board aircraft that were not previously approved for use on aircraft by the FAA. Additionally, the rulemaking will eliminate redundant operational requirements and paperwork requirements related to the physician's statement. As a result, the rulemaking will reduce burdens for POC manufacturers, passengers who use POCs while traveling, and affected aircraft operators. The final rule also made conforming amendments to the Department of Transportation's (Department or DOT) rule implementing the Air Carrier Access Act (ACAA) to require carriers to accept all POC models that meet FAA acceptance criteria as detailed in this rule.
Notice of Request To Release Airport Property
Document Number: 2016-15766
Type: Notice
Date: 2016-07-05
Agency: Federal Aviation Administration, Department of Transportation
The FAA proposes to rule and invites public comment on the release of land at Waterloo Regional Airport, Waterloo, Iowa, under the provisions of 49 U.S.C. 47107(h)(2).
Special Conditions: Kestrel Aircraft Company, Model K-350 Turboprop, Lithium Batteries
Document Number: 2016-15765
Type: Rule
Date: 2016-07-05
Agency: Federal Aviation Administration, Department of Transportation
These special conditions are issued for the Kestrel Aircraft Company, Model K-350 Turboprop airplane. This airplane will have a novel or unusual design feature associated with the installation of a rechargeable lithium battery. 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.
Membership in the National Parks Overflights Advisory Group Aviation Rulemaking Committee
Document Number: 2016-15762
Type: Notice
Date: 2016-07-05
Agency: Federal Aviation Administration, Department of Transportation
By Federal Register notice (See 81 FR 24686-24687, April 26, 2016) the National Park Service (NPS) and the Federal Aviation Administration (FAA) invited interested persons to apply to fill one current vacancy on the National Parks Overflights Advisory Group (NPOAG) Aviation Rulemaking Committee (ARC). The notice invited interested persons to apply to fill the opening to represent environmental concerns. This notice informs the public of the person selected to fill that current opening.
Revisions to the Civil Penalty Inflation Adjustment Tables
Document Number: 2016-15744
Type: Rule
Date: 2016-07-05
Agency: Federal Aviation Administration, Department of Transportation
This interim final rule is the catch-up inflation adjustment to civil penalty amounts that may be imposed for violations of Federal Aviation Administration regulations, as required by the Federal Civil Penalties Inflation Adjustment Act Improvements Act of 2015.
Airworthiness Directives; Airbus Helicopters
Document Number: 2016-15624
Type: Rule
Date: 2016-07-05
Agency: Federal Aviation Administration, Department of Transportation
We are publishing a new airworthiness directive (AD) for Airbus Helicopters Model AS332L2 and Model EC225LP helicopters, which was sent previously to all known U.S. owners and operators of these helicopters. This AD immediately prohibits flight of all Model AS332L2 and EC225LP helicopters. This AD is prompted by an accident involving an EC225LP helicopter in which the main rotor hub (MRH) detached from the main gearbox (MGB). These actions are intended to prevent failure of the main rotor system and subsequent loss of control of the helicopter.
Airworthiness Directives; Bombardier, Inc. Airplanes
Document Number: 2016-15357
Type: Rule
Date: 2016-07-05
Agency: Federal Aviation Administration, Department of Transportation
We are adopting a new airworthiness directive (AD) for certain Bombardier, Inc. Model DHC-8-400 series airplanes. This AD requires an inspection to determine if certain left and right main landing gear (MLG) retract actuator rod ends are installed and repetitive liquid penetrant inspections (LPIs) of affected left and right MLG retract actuator rod ends, and corrective actions if necessary. This AD also provides optional terminating action for the inspections. This AD was prompted by a report of cracked MLG retract actuator rod ends. We are issuing this AD to detect and correct fatigue cracking of the left and right MLG retract actuator rod ends, which could lead to left or right MLG collapse.
Airworthiness Directives; Airbus Airplanes
Document Number: 2016-15356
Type: Rule
Date: 2016-07-05
Agency: Federal Aviation Administration, Department of Transportation
We are adopting a new airworthiness directive (AD) for all Airbus Model A300 series airplanes; and Model A300 B4-600, B4-600R, and F4-600R series airplanes, and Model A300 C4-605R Variant F airplanes (collectively called Model A300-600 series airplanes). This AD was prompted by a report of cracking of the lower tension bolt area at the rib one junction (both sides) of the lower wing. This AD requires repetitive inspections for cracking of the fasteners and of the fitting around the fastener holes at the frame (FR) 40 lower wing location, and corrective actions if necessary. We are issuing this AD to detect and correct crack initiation of the fittings of the FR40 lower wing locations, which could result in reduced structural integrity of the airplane.
Airworthiness Directives; The Boeing Company Airplanes
Document Number: 2016-15355
Type: Rule
Date: 2016-07-05
Agency: Federal Aviation Administration, Department of Transportation
We are superseding Airworthiness Directive (AD) 2008-05-06 for certain The Boeing Company Model 737-100, -200, -300, -400, and -500 series airplanes. AD 2008-05-06 required repetitive inspections for fatigue cracking in the longitudinal floor beam web, upper chord, and lower chord located at certain body stations, and repair if necessary. This new AD requires, for certain airplanes, an inspection to determine if tapered fillers are installed, and related investigative and corrective actions if necessary. This AD was prompted by reports of cracks in the center wing box longitudinal floor beams, upper chord, and lower chord. We are issuing this AD to detect and correct fatigue cracking of the upper and lower chords and web of the longitudinal floor beams, which could result in rapid loss of cabin pressure.
Airworthiness Directives; The Boeing Company Airplanes
Document Number: 2016-15291
Type: Rule
Date: 2016-07-05
Agency: Federal Aviation Administration, Department of Transportation
We are superseding Airworthiness Directive (AD) 2012-12-04, for certain The Boeing Company Model 737-300, -400, and -500 series airplanes. AD 2012-12-04 required repetitive external detailed inspections and nondestructive inspections to detect cracks in the fuselage skin along the chem-mill steps at stringers S-1 and S-2R, between station (STA) 400 and STA 460, and repair if necessary. This new AD requires a preventive modification of the fuselage skin at crown stringers S-1 and S-2R. This new AD also reduces the inspection threshold for certain airplanes. This AD was prompted by a determination that, for certain airplanes, the skin pockets adjacent to the Air Traffic Control (ATC) antenna are susceptible to widespread fatigue damage. We are issuing this AD to detect and correct fatigue cracking of the fuselage skin panels at the chem-mill steps, which could result in sudden fracture and failure of the fuselage skin panels, and consequent rapid decompression of the airplane.