Federal Aviation Administration August 22, 2016 – Federal Register Recent Federal Regulation Documents

Agency Information Collection Activities: Requests for Comments; Clearance of Renewed Approval of Information Collection: Application for Employment With the Federal Aviation Administration
Document Number: 2016-20006
Type: Notice
Date: 2016-08-22
Agency: Federal Aviation Administration, Department of Transportation
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 information collected is used to evaluate the qualifications of applicants for a variety of positions within the FAA.
Agency Information Collection Activities: Requests for Comments; Clearance of Renewed Approval of Information Collection: Bird/Other Wildlife Strike Report
Document Number: 2016-20004
Type: Notice
Date: 2016-08-22
Agency: Federal Aviation Administration, Department of Transportation
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. Wildlife strike data are collected to develop standards and monitor hazards to aviation.
Notice of Release From Federal Surplus Property and Grant Assurance Obligations at Redding Municipal Airport (RDD), Redding, California
Document Number: 2016-20001
Type: Notice
Date: 2016-08-22
Agency: Federal Aviation Administration, Department of Transportation
The Federal Aviation Administration (FAA) proposes to rule and invites public comment on the application for a release of approximately 1.10 acres of airport property at the Redding Municipal Airport (RDD), Redding, California from all conditions contained in the Surplus Property Deed and Grant Assurances because the parcel of land is not needed for airport purposes. The land requested to be released is separated from the airport by Airport Road and located outside the airport fence at the southwest corner of the airport property. The release will allow the City of Redding to sell the property at its fair market value, thereby benefiting the Airport and serving the interest of civil aviation. The proposed use will be compatible with the airport and will not interfere with the airport or its operation.
Special Conditions: Garmin International, Beechcraft Corporation Model 400A Airplanes; Airplane Electronic-System Security Protection From Unauthorized External Access
Document Number: 2016-20000
Type: Rule
Date: 2016-08-22
Agency: Federal Aviation Administration, Department of Transportation
These special conditions are issued for the Beechcraft Corporation (Beechcraft) Model 400A airplane. This airplane, as modified by Garmin International (Garmin), will have a novel or unusual design feature when compared to the state of technology envisioned in the airworthiness standards for transport-category airplanes. These airplanes will have a digital-systems network architecture composed of several connected networks that may allow access to or by external computer systems and networks, and may otherwise result in airplane electronic-system security vulnerabilities without appropriate protection. 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.
Special Conditions: Bombardier Inc. Model BD-700-2A12 and BD-700-2A13 Airplanes; Airplane Electronic-System Security Protection From Authorized Internal Access
Document Number: 2016-19994
Type: Rule
Date: 2016-08-22
Agency: Federal Aviation Administration, Department of Transportation
These special conditions are issued for the Bombardier Inc. (Bombardier) Model BD-700-2A12 and BD-700-2A13 airplanes. These airplanes will have novel or unusual design features, specifically, digital systems architecture composed of several connected data networks that will have the capability to allow connectivity of the passenger-service computer systems to the airplane critical systems and data networks. 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.
Special Conditions: Bombardier Aerospace Inc. Model BD-700-2A12 and BD-700-2A13 Airplanes; Automatic Speed Protection for Design Dive Speed
Document Number: 2016-19993
Type: Rule
Date: 2016-08-22
Agency: Federal Aviation Administration, Department of Transportation
These special conditions are issued for the Bombardier Aerospace Inc. (Bombardier) Model BD-700-2A12 and BD-700-2A13 airplanes. These airplanes will have a novel or unusual feature when compared to the state of technology envisioned in the airworthiness standards for transport-category airplanes. This design feature is associated with a reduced margin between design cruising speed, VC/MC, and design diving speed, VD/ MD, based on the incorporation of a high-speed-protection system that limits nose-down pilot authority at speeds above VD/MD. 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.
EUROCAE WG-96/RTCA SC-236 Joint Plenary #1 Standards for Wireless Avionics Intra-Communication System (WAIC) Within 4200-4400 MHz
Document Number: 2016-19944
Type: Notice
Date: 2016-08-22
Agency: Federal Aviation Administration, Department of Transportation
The FAA is issuing this notice to advise the public of a meeting of EUROCAE WG-96/RTCA SC-236 Joint Plenary #1 Standards for Wireless Avionics Intra-Communication System (WAIC) within 4200-4400 MHz. Please inform adrian.cioranu@eurocae.net of your intention to attend the meeting. Please inform also peter.anders@airbus.com, the host of the meeting. Find information direction & maps: https://goo.gl/maps/ rkHxCEfN1sL2.
Airworthiness Directives; The Boeing Company Airplanes
Document Number: 2016-19936
Type: Proposed Rule
Date: 2016-08-22
Agency: Federal Aviation Administration, Department of Transportation
We propose to adopt a new airworthiness directive (AD) for all The Boeing Company Model DC-9-81 (MD-81), DC-9-82 (MD-82), DC-9-83 (MD- 83), and DC-9-87 (MD-87) airplanes; and Model MD-88 airplanes. This proposed AD was prompted by a report of fatigue cracking in a rear spar lower cap of the horizontal stabilizer. This proposed AD would require repetitive inspections for cracking of the rear spar lower caps of the horizontal stabilizer, post-modification and post-repair inspections, and corrective actions if necessary. This proposed AD also provides an optional terminating fatigue life enhancement modification. We are proposing this AD to detect and correct fatigue cracking in the rear spar lower caps of the horizontal stabilizer, which, paired with cracking in adjacent areas, could adversely affect the structural integrity of the airplane.
Airworthiness Directives; The Boeing Company Airplanes
Document Number: 2016-19935
Type: Proposed Rule
Date: 2016-08-22
Agency: Federal Aviation Administration, Department of Transportation
We propose to adopt a new airworthiness directive (AD) for all The Boeing Company Model 737-100, -200, -200C, -300, -400, and -500 series airplanes. This proposed AD was prompted by reports of skin cracking found at the corners of the aft entry and aft galley doorways. This proposed AD would require repetitive inspections for cracking of the corners of the aft entry and aft galley doorways; and repair if necessary, which would terminate the repetitive inspections of the repaired areas. We are proposing this AD to detect and correct cracking of the corners of the aft entry and aft galley doorways, which could result in rapid decompression and consequent reduced structural integrity of the airplane.