Federal Aviation Administration October 30, 2015 – Federal Register Recent Federal Regulation Documents

Special Conditions: Honda Aircraft Company (Honda) Model HA-420, HondaJet; Cruise Speed Control System
Document Number: 2015-27700
Type: Rule
Date: 2015-10-30
Agency: Federal Aviation Administration, Department of Transportation
These special conditions are issued for the Honda Aircraft Company HA-420 airplane. This airplane will have a novel or unusual design feature(s) associated with the use of a cruise speed control system. 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.
Airworthiness Directives; The Boeing Company Airplanes
Document Number: 2015-27447
Type: Proposed Rule
Date: 2015-10-30
Agency: Federal Aviation Administration, Department of Transportation
We propose to adopt a new airworthiness directive (AD) for all The Boeing Company Model 767 airplanes. This proposed AD was prompted by a determination that certain splice plate locations of the aft pressure bulkhead web are hidden and cannot be inspected using existing manufacturer service information. This proposed AD would require repetitive open-hole high frequency eddy current (HFEC) inspections for cracking of the aft pressure bulkhead web. We are issuing this AD to detect and correct cracking in the aft pressure bulkhead web, which could result in rapid decompression and loss of structural integrity.
Airworthiness Directives; Fiberglas-Technik Rudolf Lindner GmbH & Co. KG Gliders
Document Number: 2015-27440
Type: Rule
Date: 2015-10-30
Agency: Federal Aviation Administration, Department of Transportation
We are adopting a new airworthiness directive (AD) for all Fiberglas-Technik Rudolf Lindner GmbH & Co. KG Models G103 TWIN ASTIR, G103 TWIN II, and G103A TWIN II ACRO 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 a broken bell-crank installed in the air brake control system. We are issuing this AD to require actions to address the unsafe condition on these products.
This site is protected by reCAPTCHA and the Google Privacy Policy and Terms of Service apply.