Final Documents/Your Two Cents—May 2016 This list includes Federal Register (FR) publications such as rules, Advisory Circulars (ACs), policy statements and related material of interest to ARSA members. The date shown is the date of FR publication or other official release. Proposals opened for public comment represent your chance to provide input on rules and policies that will affect you. Agencies must provide the public notice and an opportunity for comment before their rules or policies change. Your input matters. Comments should be received before the indicated due date; however, agencies often consider comments they receive before drafting of the final document begins. Hyperlinks provided in blue text take you to the full document. If this link is broken, go to http://www.regulation.gov. In the keyword or ID field, type “FAA” followed by the docket number.
May 2, 2016
Articles
FAA Air Traffic Report Low clouds are expected to delay flights around Boston (BOS), the New York area (EWR, JFK, LGA), Philadelphia (PHL), San Francisco (SFO) and the Washington, D.C., area (BWI, DCA, IAD) this morning. Thunderstorms and rain in North Texas (DAL, DFW) and Houston (HOU, IAH) could also slow traffic today.
Rules
AD: Airbus Airplanes Published 05/02/2016 Docket #: FAA-2015-2458 Effective date 06/06/2016 The FAA is adopting a new AD for all Airbus Model A318, A319, A320, and A321 series airplanes. This AD requires, for certain airplanes, repetitive replacements of the fixed fairing upper and lower attachment studs of both left-hand (LH) and the right-hand (RH) MLG; and repetitive inspections for corrosion, wear, fatigue cracking, and loose studs of each forward stud assembly of the fixed fairing door upper and lower forward attachment of both LH and RH MLG; and replacement if necessary. This AD also provides an optional terminating modification for the repetitive replacements of the fixed fairing upper and lower attachment studs.
AD: Airbus Airplanes Published 05/02/2016 Docket #: FAA-2015-6539 Effective date 06/06/2016 The FAA is adopting a new AD for all Airbus Model A318-111 and -112 airplanes; Model A319-111, - 112, -113, -114, and -115 airplanes; Model A320-211, -212, and -214 airplanes; and Model A321- 111, -112, -211, -212, and -213 airplanes. This AD requires repetitive detailed inspections of the right and left forward engine mounts, and corrective action if necessary. These inspections are required by AD 2015-05-02. This AD reduces the compliance times for those inspections.
AD: Airbus Helicopters (Previously Eurocopter France) Published 05/02/2016 Docket #: FAA-2015-3970 Effective date 06/06/2016 The FAA is superseding AD 2014-12-51 for Airbus Helicopters (previously Eurocopter France) Model EC130B4 and EC130T2 helicopters. AD 2014-12-51 required repetitively inspecting the tailboom to Fenestron junction frame (junction frame) for a crack. This new AD retains the requirements of AD 2014-12-51, changes the applicability from helicopters with certain hours time-in-service (TIS) to junction frames with certain hours TIS, and adds a compliance time for sling cycles to the junction frame inspection interval. The actions of this AD are intended to detect a crack and to prevent failure of the junction frame, which could result in loss of the Fenestron and subsequent loss of control of the helicopter.
AD: Bombardier, Inc. Airplanes Published 05/02/2016 Docket #: FAA-2015-4814 Effective date 06/06/2016 The FAA is adopting a new AD for certain Bombardier, Inc. Model CL-600-2B19 (Regional Jet Series 100 & 440) airplanes. This AD requires replacement of incorrectly calibrated AOA transducers. We are issuing this AD to detect and replace incorrectly calibrated AOA transducers; incorrect calibration of the transducers could result in late activation of the stick pusher.
AD: Bombardier, Inc. Airplanes Published 05/02/2016 Docket #: FAA-2015-3988 Effective date 06/06/2016 The FAA is superseding AD 2014-17-51 for certain Bombardier, Inc. Model CL-600-2B16 airplanes. AD 2014-17-51 required inspecting the inboard flap fasteners of the hinge-box forward fitting at Wing Station (WS) 76.50 and WS 127.25 to determine the orientation and condition of the fasteners, as applicable, and replacement or repetitive inspections of the fasteners if necessary. AD 2014-17-51 also provided for optional terminating action for the requirements of that AD. This new AD requires accomplishment of the previously optional terminating action.
AD: DG Flugzeugbau GmbH Gliders Published 05/02/2016 Docket #: FAA-2015-1130 Effective date 06/06/2016 The FAA is revising AD 2015-09-04 for DG Flugzeugbau GmbH Model DG-1000T gliders equipped with a Solo Kleinmotoren Model 2350 C engine. 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 engine shaft failure and consequent propeller detachment. We are issuing this AD to require actions to address the unsafe condition on these products.
AD: Dassault Aviation Airplanes Published 05/02/2016 Docket #: FAA-2014-0657 Effective date 06/06/2016 The FAA is adopting a new AD for certain Dassault Aviation Model FALCON 2000, FALCON 2000EX, MYSTERE-FALCON 900, and FALCON 900EX airplanes. This AD was prompted by reports of a co-pilot sliding aft on his seat during take-off at rotation. This AD requires replacement of certain springs installed on the pilot and co-pilot seats.
AD: Mitsubishi Heavy Industries, Ltd. Airplanes Published 05/02/2016 Docket #: FAA-2016-1363 Effective date 06/06/2016 The FAA is adopting a new AD for certain Mitsubishi Heavy Industries, Ltd. Models MU-2B-30, MU- 2B-35, MU-2B-36, MU-2B-36A, and MU-2B-60 airplanes. 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 reports of cracks found in the attach fittings of the main landing gear oleo strut. We are issuing this AD to require actions to address the unsafe condition on these products.
AD: Piper Aircraft, Inc. Airplanes Published 05/02/2016 Docket #: FAA-2014-0338 Effective date 06/06/2016 The FAA is adopting a new AD for certain Piper Aircraft, Inc. Model PA-31-350 airplanes. This AD requires inspecting the fuel hose assembly and the turbocharger support assembly for proper clearance between them, inspecting each assembly for any sign of damage, and making any necessary repairs or replacements.
AD: The Boeing Company Airplanes Published 05/02/2016 Docket #: FAA-2015-1428 Effective date 06/06/2016 The FAA is adopting a new AD for certain The Boeing Company Model 777-200 and -300 series airplanes. This AD requires repetitive inspections for cracking of the left side and right side forward outer chords of the pivot bulkhead, and related investigative and corrective actions if necessary. This AD also provides a modification of the pivot bulkhead, which would terminate the repetitive inspections.
Proposed Rule
NPRM AD: Bombardier, Inc. Airplanes Published 05/02/2016 Docket #: FAA-2016-6148 Comments due 06/16/2016 The FAA proposes to adopt a new AD for certain Bombardier, Inc. Model DHC-8-400 series airplanes. This proposed AD would require a general visual inspection for corrosion of the thermostats' mounting surfaces and fuselage skin surface, corrective actions if necessary, and relocating the existing thermostats.
NPRM: Proposed Amendment of Class D Airspace and Revocation of Class E Airspace; Columbus, Ohio State University Airport, OH, and Amendment of Class E Airspace; Columbus, OH Published 05/02/2016 Docket #: FAA-2015-1649 This action withdraws the NPRM published in the Federal Register on June 24, 2015, proposing to amend Class D and Class E airspace and remove Class E airspace in the Columbus, OH, area. The FAA has determined that withdrawal of that NPRM is warranted as a second NPRM for the same airspace action was issued in July 2015.
May 3, 2016
Articles
FAA Air Traffic Report Rain and thunderstorms continue this morning along the East Coast and across the Midwest, likely leading to delays for flights arriving into the New York area (JFK, LGA, EWR) and the Washington DC area (DCA, IAD, BWI). Flights to and from Florida and cities on the East Coast and Midwest will likely be re- routed around the weather, possibly causing some delays. Morning fog could slow traffic in Atlanta (ATL), Charlotte (CLT), Detroit (DTW) and San Francisco (SFO).
FAA Proposes Policy Change to PFC Funding for Airport Rail Projects Today, the FAA issued a Federal Register Notice seeking public comment on proposed changes in the Passenger Facility Charge program. Currently, passenger facility charge (PFC) funds may support rail projects that are on airport property only if they are for the exclusive use of airport patrons and employees. The proposed change would expand the funding eligibility to include selected additional elements of airport rail projects meeting certain criteria, even if they are not solely for the exclusive use of airport patrons and employees.
Rules
Final Rule: IFR Altitudes; Miscellaneous Amendments Published 05/03/2016 Docket #: FAA-2016-10009 This amendment adopts miscellaneous amendments to the required IFR (instrument flight rules) altitudes and changeover points for certain Federal airways, jet routes, or direct routes for which a minimum or maximum en route authorized IFR altitude is prescribed. This regulatory action is needed because of changes occurring in the National Airspace System. These changes are designed to provide for the safe and efficient use of the navigable airspace under instrument conditions in the affected areas.
Proposed Rule
NPRM AD: Airbus Airplanes Published 05/03/2016 Docket #: FAA-2016-6144 Comments due 06/17/2016 The FAA proposes to adopt a new AD for certain Airbus Model A318, A319, and A320 series airplanes; Model A330-200, -200 Freighter, and -300 series airplanes; and Model A340-200, -300, - 500, and -600 series airplanes. This proposed AD would require modifying the fuel quantity indicating system (FQIS) to prevent development of an ignition source inside the center fuel tank due to electrical fault conditions. This proposed AD would also provide alternative actions for cargo airplanes.
NPRM AD: Airbus Airplanes Published 05/03/2016 Docket #: FAA-2016-6143 Comments due 06/17/2016 The FAA proposes to adopt a new AD for all Airbus 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), and Model A310 series airplanes. This proposed AD would require modifying the fuel quantity indicating system (FQIS) to prevent development of an ignition source inside the center fuel tank due to electrical fault conditions. This proposed AD would also provide alternative actions for cargo airplanes.
NPRM AD: Dassault Aviation Airplanes Published 05/03/2016 Docket #: FAA-2016-6146 Comments due 06/17/2016 The FAA proposes to adopt a new AD 2008-19-08, for all Dassault Aviation Model Falcon 10 airplanes. AD 2008-19-08 currently requires repetitive replacement of the flexible hoses installed in the wing (slat) anti-icing system with new hoses. Since we issued AD 2008-19-08, additional reports were received of collapse of the flexible hoses installed in the slat anti-icing systems on airplanes equipped with new, improved hoses. This proposed AD would require reducing the life limit of these flexible hoses, which would reduce the repetitive replacement intervals.
NPRM AD: The Boeing Company Airplanes Published 05/03/2016 Docket #: FAA-2016-6139 Comments due 06/17/2016 The FAA proposes to adopt a new AD for certain The Boeing Company Model 737-600, -700, -700C, -800, -900, and -900ER series airplanes. This proposed AD would require modifying the fuel quantity indicating system (FQIS) to prevent development of an ignition source inside the center fuel tank due to electrical fault conditions. This proposed AD would also provide alternative actions for cargo airplanes.
NPRM AD: The Boeing Company Airplanes Published 05/03/2016 Docket #: FAA-2016-6145 Comments due 06/17/2016 The FAA proposes to adopt a new AD for certain The Boeing Company Model 747-400, 747-400D, and 747-400F series airplanes. This proposed AD would require modifying the fuel quantity indicating system (FQIS) to prevent development of an ignition source inside the center fuel tank due to electrical fault conditions. This proposed AD would also provide alternative actions for cargo airplanes.
NPRM AD: Proposed Amendment of Class E Airspace for the Following Arkansas Towns; Blytheville, AR; Brinkley, AR; Clarksville, AR; and DeQueen, AR Published 05/03/2016 Docket #: FAA-2016-4172 Comments due 06/17/2016 This action proposes to modify Class E airspace extending upward from 700 feet above the surface at Arkansas International Airport, Blytheville, AR; Blytheville Municipal Airport, Blytheville, AR; Frank Federer Memorial Airport, Brinkley, AR; Clarksville Municipal Airport, Clarksville, AR; and J. Lynn Helms Sevier County Airport, De Queen, AR.
NPRM: Proposed Amendment of Class E Airspace for the Following Indiana Towns; Goshen, IN; Greencastle, IN; Huntingburg, IN; North Vernon, IN; Rensselaer, IN; Tell City, IN; and Washington, IN; and Revocation of Class E Airspace; Vincennes, IN Published 05/03/2016 Document #: 2016-10177 Comments due 06/17/2016 This action proposes to modify Class E airspace extending upward from 700 feet above the surface at Vigil I. Grissom Municipal Airport, Bedford, IN; Goshen Municipal Airport, Goshen, IN; Putnam County Airport, Greencastle, IN; Huntingburg Airport, Huntingburg, IN; North Vernon Airport, North Vernon, IN; Jasper County Airport, Rensselaer, IN; Perry County Municipal Airport, Tell City, IN; and Daviess County Airport, Washington, IN.
NPRM: Proposed Amendment of Class E Airspace for the Following Minnesota Towns; Hutchinson, MN; Jackson, MN; Pipestone, MN; Two Harbors, MN; and Waseca, MN Published 05/03/2016 Document #: FAA-2016-4271 Comments due 06/17/2016 This action proposes to modify Class E airspace extending upward from 700 feet above the surface at Hutchinson Municipal Airport-Butler Field, Hutchinson, MN; Jackson Municipal Airport, Jackson, MN; Pipestone Municipal Airport, Pipestone, MN; Richard B. Helgeson Airport, Two Harbors, MN; and Waseca Municipal Airport, Waseca, MN. Decommissioning of the non-directional radio beacon (NDB), cancellation of NDB approaches, and implementation of area navigation (RNAV) procedures have made this action necessary for the safety and management of Instrument Flight Rules (IFR) operations at the above airports.
NPRM: Proposed Amendment of Class E Airspace for the following Michigan Towns; Alma, MI; Bellaire, MI; Cadillac, MI; Drummond Island, MI; Gladwin, MI; Holland, MI; and Three Rivers, MI Published 05/03/2016 Document #: FAA-2016-4629 Comments due 06/17/2016 This action proposes to modify Class E airspace extending upward from 700 feet above the surface at Gratiot Community Airport, Alma, MI; Antrim County Airport, Bellaire, MI; Wexford County Airport, Cadillac, MI; Drummond Island Airport, Drummond Island, MI; Charles C. Zettel Memorial Airport, Gladwin, MI; Park Township Airport and West Michigan Regional Airport, Holland, MI; and Three Rivers Municipal Dr. Haines Airport, Three Rivers, MI.
NPRM: Proposed Revocation of Class E Airspace; Alliance, NE; and Amendment of Class E Airspace for the Following Nebraska Towns; Albion, NE; Alliance, NE; Gothenburg, NE; Holdrege, NE; Imperial, NE; Lexington, NE; and Millard Airport, Omaha, NE Published 05/03/2016 Docket #: FAA-2016-5388 Comments due 06/17/2016 This action proposes to remove Class E surface area airspace at Alliance Municipal Airport, Alliance, NE; and modify Class E airspace extending upward from 700 feet above the surface at Albion Municipal Airport, Albion, NE; Alliance Municipal Airport, Alliance, NE; Quinn Field, Gothenburg, NE; Brewster Field Airport, Holdrege, NE; Imperial Municipal Airport, Imperial, NE; Jim Kelly Field, Lexington, NE; and Millard Airport, Omaha, NE.
Flight Standards Information Management System (FSIMS)
FSIMS: HA-420, Part 91 and Part 135 Issued 05/04/2016 Revision 0 of the Honda Aircraft Company HA-420 Master Minimum Equipment List.
Notices
Notice: Agency Information Collection Activities: Requests for Comments; Clearance of Renewed Approval of Information Collection: Application for Employment With the Federal Aviation Administration Published 05/03/2016 Document #: 2016-10344 Comments due 07/05/2016 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 a currently approved information collection. The information collected is used to evaluate the qualifications of applicants for a variety of positions within the FAA.
Notice: Passenger Facility Charge (PFC) Program: Eligibility of Ground Access Projects Meeting Certain Criteria Published 05/03/2016 Document #: 2016-10334 Comments due 06/02/2016 The FAA proposes to amend its “Notice of Policy Regarding the Eligibility of Airport Ground Access Transportation Projects for Funding Under the Passenger Facility Charge (PFC) Program,” 1 regarding the requirements for PFC funding of on-airport, rail access projects.
Notice: Agency Information Collection Activities: Requests for Comments; Clearance of Renewed Approval of Information Collection: Bird/Other Wildlife Strike Report Published 05/03/2016 Document #: 2016-10347 Comments due 07/05/2016 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 a previously approved information collection. Wildlife strike data are collected to develop standards and monitor hazards to aviation.
Notice: Agency Information Collection Activities: Requests for Comments; Clearance of Renewed Approval of Information Collection: Operations Specifications, Part 129 Application Published 05/03/2016 Document #: 2016-10346 Comments due 07/05/2016 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 a previously approved information collection. The FAA assesses the information collected and issues operations specifications to foreign air carriers. These operations specifications assure the foreign air carrier's ability to navigate and communicate safely within the U.S. National Airspace System.
Notice: Interim Guidance in the Preparation of FAA Form 7230-4 Published 05/02/2016 Document #: JO 7210.893 Effective date 06/06/2016 This notice amends FAA Order JO 7210.3, Facility Operation and Administration, to update transition issues and extend and revise interim guidance on the preparation of FAA Form 7230-4, Daily Record of Facility Operation. This notice continues to support a test and transition period for procedures created in the development of new quality assurance, quality control, and occurrence reporting processes and guidance.
May 4, 2016
Articles
FAA Air Traffic Report Thunderstorms off the Carolina coast, over Florida and the Gulf of Mexico likely will lead to delays from flights being rerouted around the severe weather. Cloud cover and some scattered showers may slow traffic in Boston (BOS), the New York area (EWR, JFK, LGA), Philadelphia (PHL), San Francisco (SFO) and the Washington, D.C., area (BWI, DCA, IAD) throughout the day today.
FAA Administrator Makes Two Major Drone Announcements Speaking today at the AUVSI annual conference in New Orleans, FAA Administrator Michael Huerta announced the agency is establishing a broad-based advisory committee that will provide advice on key unmanned aircraft integration issues. He also announced plans to make it easier for students to fly unmanned aircraft (PDF) as part of their coursework.
Rules
AD: Airbus Airplanes Published 05/04/2016 Docket #: FAA-2015-3990 Effective date 06/08/2016 The FAA is adopting a new AD for certain Airbus Model A320-214, -232, and -233 airplanes; and Airbus Model A321-211 and -231 airplanes. This AD requires identification of the affected PSUs, and depending on findings, doing applicable related investigative and corrective actions.
AD: Airbus Airplanes Published 05/04/2016 Docket #: FAA-2015-5811 Effective date 06/08/2016 The FAA is superseding AD 2004-19-11 for certain Airbus Model A320 series airplanes. AD 2004-19- 11 required modification of the inner rear spar web of the wing, cold expansion of the attachment holes of the forward pintle fitting and the actuating cylinder anchorage of the main landing gear (MLG), repetitive ultrasonic inspections for cracking of the rear spar of the wing, and corrective action if necessary. AD 2004-19-11 also provided optional terminating action for the repetitive inspections. This new AD retains the requirements of AD 2004-19-11, and requires the previously optional terminating action.
AD: The Boeing Company Airplanes Published 05/04/2016 Docket #: FAA-2016-6147 Effective date 05/19/2016 The FAA is adopting a new AD for certain The Boeing Company Model 747-8 series airplanes. This AD requires a detailed inspection for correct installation of the flex hose clamp of the occupant backup air supply and a general visual inspection for damage of the flex hose, and related investigative and corrective actions if necessary. The FAA is issuing this AD to detect and correct an incorrect clamp installation on the inboard end of the flex hose, which allows the flex hose to slowly become disconnected from the adjacent fiberglass duct, and damage to the hose. This condition, in conjunction with a cargo fire event, can potentially lead to decreased airflow to the main deck, possibly resulting in smoke and/or toxic fumes penetrating into the main deck passenger compartment, which could result in injury to the passengers or cabin crew.
AD: The Boeing Company Airplanes Published 05/04/2016 Docket #: FAA-2015-3982 Effective date 06/08/2016 The FAA is adopting a new AD for certain The Boeing Company Model 717-200 airplanes. This AD requires a detailed inspection for any distress of the vertical stabilizer leading edge skin, and related investigative and corrective actions if necessary. This AD also requires, for certain airplanes, repetitive detailed inspections of the spar cap for any loose and missing fasteners, repetitive eddy current testing high frequency (ETHF) and radiographic testing (RT) inspections of the spar cap for any crack, and related investigative and corrective actions if necessary.
AD: Turbomeca S.A. Turboshaft Engines Published 05/04/2016 Docket #: FAA-2015-7490 Effective date 06/08/2016 The FAA is adopting a new AD for certain Turbomeca S.A. Astazou XIV B and H turboshaft engines. This AD requires a one-time inspection of the front surface of the 3rd stage turbine for a groove.
Final Rule: Amendment of Class D and Class E Airspace; Walla Walla, WA Published 05/04/2016 Docket #: FAA-2015-3675 Effective date 07/21/2016 This action modifies Class D airspace, Class E surface area airspace, Class E surface area airspace designated as an extension, and Class E airspace extending upward from 700 feet above the surface at Walla Walla Regional Airport, Walla Walla, WA. After a review of the airspace, the FAA found it necessary to amend the airspace areas for the safety and management of Instrument Flight Rules (IFR) operations for arriving and departing aircraft at the airport. This action also updates the geographic coordinates of Walla Walla Regional Airport in the respective Class D and E airspace areas above.
Proposed Rule
NPRM AD: The Boeing Company Airplanes Published 05/04/2016 Docket #: FAA-2016-6141 Comments due 06/20/2016 The FAA proposes to adopt a new AD for certain The Boeing Model 767 airplanes. This proposed AD would require modifying the fuel quantity indicating system (FQIS) to prevent development of an ignition source inside the center fuel tank due to electrical fault conditions. This proposed AD would also provide optional actions for cargo airplanes.
NPRM AD: The Boeing Company Airplanes Published 05/04/2016 Docket #: FAA-2016-6140 Comments due 06/20/2016 The FAA proposes to adopt a new AD for certain The Boeing Company Model 777 airplanes. This proposed AD would require modifying the fuel quantity indicating system (FQIS) to prevent development of an ignition source inside the center fuel tank due to electrical fault conditions. This proposed AD would also provide alternative actions for cargo airplanes.
Legal Interpretations
Legal Interpretation: Educational Use of Unmanned Aircraft Systems (UAS) Issued 05/04/2016 Regulation/Order #: section 336 of the FAA Modernization and Reform Act of2012 (FMRA) This legal interpretation addresses the use of unmanned aircraft for hobby or recreational purposes at educational institutions and community-sponsored events; and the student use of unmanned aircraft in furtherance of receiving instruction at accredited educational institutions.
Special Conditions
SC: Gulfstream Aerospace Corporation Model GVII-G500 Airplane, Technical Criteria for Approving Side-Facing Seats Published 05/04/2016 Docket #: FAA-2016-1085 Effective date 05/04/2016 These special conditions are issued for the Gulfstream Aerospace Corporation (Gulfstream) Model GVII-G500 airplane. This airplane will have a novel or unusual design feature associated with side- facing seats. The applicable airworthiness regulations do not contain adequate or appropriate safety standards for this design feature. These special conditions contain the additional safety standards the Administrator considers necessary to establish a level of safety equivalent to that established by the existing airworthiness standards.
May 6, 2016
Articles
FAA Air Traffic Report Skies are clear east of the Rockies, except for parts of the East Coast, where cloud cover and rain could slow traffic in the New York area (EWR, JFK, LGA), Philadelphia (PHL) and the Washington, D.C., area (BWI, DCA, IAD). On the West Coast, low clouds and rain may delay flights in Los Angeles (LAX), San Diego (SAN) and San Francisco (SFO).
Rules
AD: Airbus Airplanes Published 05/06/2016 Docket #: FAA-2015-0250 Effective date 06/10/2016 The FAA is adopting a new AD for all Airbus Model A318, A319, A320, and A321 series airplanes. This AD was prompted by reports of airspeed indication discrepancies while flying at high altitudes in inclement weather. This AD requires replacing certain pitot probes on the captain, first officer, and standby sides with certain new pitot probes.
AD: Airbus Airplanes Published 05/06/2016 Docket #: FAA-2015-8427 Effective date 06/10/2016 The FAA is superseding AD 2007-10-10 R1 for all Airbus 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). AD 2007-10-10 R1 required revising the Airworthiness Limitations Section (ALS) of the Instructions for Continued Airworthiness to incorporate new limitations for fuel tank systems. This new AD requires revising the maintenance program or inspection program to incorporate revised fuel maintenance and inspection tasks.
AD: Airbus Helicopters (Type Certificate Previously Held by Eurocopter France) Published 05/06/2016 Docket #: FAA-2015-3741 Effective date 06/10/2016 The FAA is superseding AD 2013-08-17 for Airbus Helicopters Model SA-365N, SA-365N1, AS- 365N2, AS 365 N3, and SA-366G1 helicopters. AD 2013-08-17 required initial and recurring inspections of the 9-degree fuselage frame for a crack and repairing the frame if a crack exists. This new AD modifies the compliance times and expands the inspection area of the 9-inch frame.
AD: The Boeing Company Airplanes Published 05/06/2016 Docket #: FAA-2016-6149 Effective date 05/23/2016 The FAA is adopting a new AD for certain The Boeing Company Model 787-8 and 787-9 airplanes. This AD requires repetitive inspections of the bilge barriers located in the forward and aft cargo compartments for disengaged decompression panels, and reinstalling any disengaged panels.
Final Rule: Amendment of Class E Airspace; Ash Flat, AR Published 05/06/2016 Docket #: FAA-2016-4235 Effective date 07/21/2016 This action amends the airspace designation and airport name in Class E airspace by changing the designation from Cherokee Village Airport, AR, to Ash Flat, AR; and changing the airport name from Cherokee Village Airport to Sharp County Village Airport, Ash Flat, AR. These changes reflect the current information in the FAAs aeronautical database.
Proposed Rule
NPRM: Proposed Establishment of Class E Airspace; Harvey, ND Published 05/06/2016 Docket #: FAA-2016-5387 Comments due 06/20/2016 This action proposes to establish Class E en route domestic airspace in the Harvey Municipal Airport, Harvey, ND area, to facilitate vectoring of Instrument Flight Rules (IFR) aircraft under control of Minneapolis Air Route Traffic Control Center (ARTCC). The FAA is proposing this action to enhance the safety and efficiency of aircraft operations within the National Airspace System.
NPRM: Proposed Establishment of Class E Airspace; Linton, ND Published 05/06/2016 Docket #: FAA-2016-5456 Comments due 06/20/2016 This action proposes to establish Class E en route domestic airspace in the Linton Municipal Airport, Linton, ND area, to facilitate vectoring of Instrument Flight Rules (IFR) aircraft under control of Minneapolis Air Route Traffic Control Center (ARTCC). The FAA is proposing this action to enhance the safety and efficiency of aircraft operations within the National Airspace System (NAS).
NPRM: Proposed Establishment of Class E Airspace; Platte, SD Published 05/06/2016 Docket #: FAA-2016-5386 Comments due 06/20/2016 This action proposes to establish Class E en route domestic airspace in the Platte Municipal Airport, Platte, SD area, to facilitate vectoring of Instrument Flight Rules (IFR) aircraft under control of Minneapolis Air Route Traffic Control Center (ARTCC). The FAA is proposing this action to enhance the safety and efficiency of aircraft operations within the National Airspace System (NAS).
NPRM: Proposed Establishment of Class E Airspace; Slaton, TX Published 05/06/2016 Docket #: FAA-2016-3785 Comments due 06/20/2016 This action proposes to establish Class E airspace at Slaton, TX. Controlled airspace is necessary to accommodate new Standard Instrument Approach Procedures developed at Slaton Municipal Airport, for the safety and management of Instrument Flight Rules (IFR) operations at the airport.
Special Airworthiness Information Bulletins (SAIB)
SAIB: Inspections of the tailcone reinforcement for airplanes in “severe usage environments” with floats or skis Issued 05/04/2016 Document #: CE-16-16 This SAIB is to alert owners, operators, maintenance technicians, and inspectors of an airworthiness concern, specifically the potential for cracks and corrosion in the stabilizer hinge brackets and tailcone reinforcement brackets on Textron Aviation Inc. (Cessna) Models 180 and 185 airplanes that are equipped with floats or skis. Airplanes equipped with floats or skis are identified as “severe usage environments” in Cessna service manuals.
Notices
Notice: Opportunity to Comment on the Draft Advisory Circular 150/5360-14A, Access to Airports by Individuals With Disabilities Published 05/06/2016 Document #: FAA-4796 Comments due 06/06/2016 The FAA announces the availability of draft Advisory Circular, (AC) 150/5360-14A, Access to Airports by Individuals with Disabilities, for public review. This AC will provide guidance and recommendations for ensuring access to airports by individuals with disabilities. The draft AC substantially revises and incorporates regulatory updates and recommendations for Service Animal Relief Areas (SARA) at airports.
Notice: Opportunity to Comment on the Draft Advisory Circular 150/5360-14A, Access to Airports by Individuals With Disabilities Published 05/04/2016 Document #: JO 6480.85 This document's content can only be accessed from within the FAA network.
Notice: Guidance for DASI External Vent Port Location and Station Elevation Setting Published 05/05/2016 Document #: JO 6560.107 This document's content can only be accessed from within the FAA network.
Meeting: 2016 Meetings of the Equip 2020 Plenary and Working Groups Meeting date 06/22/2016; 09/14/2016; 12/13/2016 Meeting time 8:30am Time zone (EST/etc.) This notice announces the 2016 meetings of the Equip 2020 Plenary and Working Groups. Equip 2020 is a joint FAA and Industry group tasked with moving forward significantly on ADS-B Out implementation. Formed as a result of the Call to Action held October 28, 2014, Equip 2020 was given 32 tasks, reflecting barriers to implementation, which forms the basis of our agendas and discussions.
May 9, 2016
Articles
FAA Air Traffic Report Thunderstorms in the central part of the country could slow arrivals into North Texas (DFW, DAL) and increase travel time for cross-country flights as aircraft detour around the weather. Gusty winds could lead to delays in the Northeast, while cloud cover may slow flights into San Francisco (SFO).
Rules
AD: Airbus Airplanes Published 5/9/2016 Docket #: FAA-2015-4808 Effective date 6/13/2016 The FAA is adopting a new AD for certain Airbus Model A330-200, -200 Freighter, and -300 series airplanes; and Model A340-200 and -300 series airplanes. This AD requires removing fasteners, doing a rototest inspection of fastener holes, installing new fasteners, oversizing the holes and doing rototest inspections for cracks if necessary, and repairing any cracking that is found.
AD: The Boeing Company Airplanes Published 5/9/2016 Docket #: FAA-2015-0246 Effective date 6/13/2016 The FAA is adopting a new AD for certain The Boeing Company Model 737-300, -400, and -500 series airplanes. This AD also provides an optional preventive modification, which terminates the repetitive inspections at the modified location.
Proposed Rule
NPRM AD: Airbus Airplanes Published 5/9/2016 Docket #: FAA-2016-6418 Comments due 6/23/2016 The FAA proposes to adopt a new AD for all Airbus Model A330-200 Freighter, -200, and -300 series airplanes; and Airbus Model A340-200, -300, -500, and -600 series airplanes. This proposed AD would require an inspection of the fuel pumps to identify their part numbers and replacement of affected pumps.
May 10, 2016
Press Release
FAA Air Traffic Report Thunderstorms moving eastward across the Midwest could lead to some delays as flights are diverted around a line of severe weather that spawned tornadoes and large hail yesterday. Additional storm cells will slow traffic in the high-altitude airspace around Atlanta, Jacksonville, Indianapolis, Memphis and Cleveland. Low clouds in Chicago (MDW, ORD) and San Francisco (SFO) may contribute to delays in those cities today.
Proposed Rule
NPRM AD: General Electric Company Turbofan Engines Published 05/10/2016 Docket #: FAA-2016-5872 Comments due 07/11/2016 The FAA proposes to adopt a new airworthiness directive (AD) for all General Electric Company (GE) GEnx-1B64/P2, -1B67/P2, -1B70/P2, -1B70C/P2, -1B70/75/P2, and -1B74/75/P2 turbofan engines with engine assembly, part number (P/N) 2447M10G01 or P/N 2447M10G02, installed. This proposed AD was prompted by a report of a significant fan rub event. This proposed AD would require rework of the engine fan stator module assembly.
NPRM AD: The Boeing Company Airplanes Published 05/10/2016 Docket #: FAA-2016-6426 Comments due 06/24/2016 The FAA proposes to adopt a new airworthiness directive (AD) for all The Boeing Company Model 737-300, -400, and -500 series airplanes. This proposed AD was prompted by reports of intergranular cracks on the front spar chord lugs of the outboard horizontal stabilizer. This proposed AD would require repetitive inspections of the front spar chord lugs and lug bores of the horizontal stabilizer, and repair if necessary.
NPRM AD: The Boeing Company Airplanes Published 05/10/2016 Docket #: FAA-2016-6417 Comments due 06/24/2016 The FAA proposes to adopt a new airworthiness directive (AD) for all The Boeing Company Model DC-10-10 and DC-10-10F airplanes, Model DC-10-15 airplanes, Model DC-10-30 and DC-10-30F (KC- 10A and KDC-10) airplanes, Model DC-10-40 and DC-10-40F airplanes, Model MD-10-10F and MD- 10-30F airplanes, and Model MD-11 and MD-11F airplanes.
NPRM AD: Bombardier, Inc. Airplanes Published 05/10/2016 Docket #: FAA-2016-6414 Comments due 06/24/2016 The FAA proposes to adopt a new airworthiness directive (AD) for certain Bombardier, Inc. Model CL-600-2B19 (Regional Jet Series 100 & 440) airplanes. This proposed AD would require a revision of the airplane flight manual (AFM) emergency procedures section to provide procedures to guide the crew on how to stabilize the airplane airspeed and attitude for continued safe flight when a loss of all air data information has occurred in the flight deck.
NPRM AD: Bombardier, Inc. Airplanes Published 05/10/2016 Docket #: FAA-2016-6415 Comments due 06/24/2016 The FAA proposes to adopt a new AD for certain Bombardier, Inc. Model CL-600-2C10 (Regional Jet Series 700, 701, & 702) airplanes. This proposed AD would require a revision of the airplane flight manual (AFM) emergency procedures section to provide procedures to guide the crew on how to stabilize the airplane airspeed and attitude for continued safe flight when a loss of all air data information has occurred in the flight deck.
NPRM AD: Bell Helicopter Textron Helicopters Published 05/10/2016 Docket #: FAA-2016-6551 Comments due 07/11/2016 The FAA proposes to adopt a new airworthiness directive (AD) for certain Bell Helicopter Textron (Bell) Model 430 helicopters. This proposed AD would require establishing a life limit for a certain main rotor hub attachment bolt (bolt) and removing from service each bolt that has met or exceeded its life limit. The proposed actions are intended to establish a life limit for a certain part- numbered bolt to prevent failure of a bolt, failure of a main rotor hub, and subsequent loss of control of a helicopter.
Notices
Notice: Agency Information Collection Activities: Requests for Comments; Clearance of Renewed Approval of Information Collection: Application for Employment With the Federal Aviation Administration Published 05/10/2016 Document #: 2016-10976 Comments due: 07/11/2016 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 for a new information collection. The information collected is used to collect, process and report Unmanned Aircraft System (UAS) airborne and ground based observations by the public of drone behavior that they consider suspicious or illegal.
Notice: Agency Information Collection Activities: Requests for Comments; Clearance of Renewed Approval of Information Collection: Small Unmanned Aircraft Registration System (sUAS) Published 05/10/2016 Document #: 2016-10978 Comments due: 06/09/2016 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. Aircraft registration is necessary to ensure personal accountability among all users of the national airspace system. Aircraft registration also allows the FAA and law enforcement agencies to address non-compliance by providing the means by which to identify an aircraft's owner and operator.
Notice: Noise Exposure Map Notice for Harrisburg International Airport, Middletown, Pennsylvania Published 05/10/2016 Document #: 2016-10979 The Federal Aviation Administration (FAA) announces its determination that the noise exposure maps submitted by the Susquehanna Regional Airport Authority for Harrisburg International Airport under the provisions of 49 U.S.C. 47501 et seq. (Aviation Safety and Noise Abatement Act) and 14 CFR part 150 are in compliance with applicable requirements.
Notice: Noise Exposure Map Notice; Receipt of Noise Compatibility Program and Request for Review Boise Air Terminal (Gowen Field) Boise, ID Published 05/10/2016 Document #: 2016-10981 The Federal Aviation Administration (FAA) announces its determination that the noise exposure maps submitted by the City of Boise, ID for the Boise Air Terminal (Gowen Field), Boise, Idaho under the provisions of 40 U.S.C 47501 et seq. (Aviation Safety and Noise Abatement Act) and 14 CFR 150 are in compliance with applicable requirements.
Notice: Passenger Facility Charge (PFC) Program: Eligibility of Ground Access Projects Meeting Certain Criteria; Correction Issued 05/10/2016 Docket #: FAA-2016-6596 Comments due 06/02/2016 This action corrects the notice of proposed policy published on May 3, 2016. In that document, the FAA solicited comments on a proposal to amend its “Notice of Policy Regarding the Eligibility of Airport Ground Access Transportation Projects for Funding Under the Passenger Facility Charge (PFC) Program,” 1 regarding the requirements for PFC funding of on-airport, rail access projects. This document corrects errors in the docket number and contact information.
Notice: Waivers of Ship Protection Probability of Impact Requirement Issued 05/10/2016 Document #: 2016-09685 This notice concerns two petitions for waiver submitted to the FAA by Space Exploration Technologies Corp. (SpaceX): A petition to waive the requirement that a waiver request be submitted at least 60 days before the effective date of the waiver unless good cause for later submission is shown in the petition; and a petition to waive the requirements that exclude persons in waterborne vessels from the collective risk criteria and limit the probability of impact on waterborne vessels to 1 × 10 −5.
Notice: CHANGE TO FAA ORDER JO 7360.1, APPENDIX A, APPENDIX B, AND APPENDIX C, AIRCRAFT TYPE DESIGNATORS Issued 05/09/2016 Document #: JO 7360.1A REVISE LAHSO GROUP NUMBERS TO THE FOLLOWING AIRCRAFT: GULFSTREAM, ROCKWELL, NORTH AMERICAN ROCKWELL –TURBO COMMANDER (ALL MODELS) AC90: LAHSO GROUP 4 LEARJET 45 LJ45: LAHSO GROUP 6
May 11, 2016
Press Releases
FAA Air Traffic Report Foggy conditions and thunderstorms will likely result in flight delays from central Missouri to Minnesota today. Delays from low visibility are possible in Chicago (MDW, ORD), Minneapolis (MSP) and St. Louis (STL). Cross-country flights may need to be routed around the weather systems, resulting in delays. Stormy weather across the Appalachians is expected to intensify this afternoon and could reroute flights in the high-altitude airspace around Cleveland, Indianapolis and Washington, D.C. The D.C.-area airports (BWI, DCA, IAD) and Philadelphia (PHL) may experience delays due to low clouds this morning, with rain showers and possible thunderstorms developing later in the evening. Cloud cover is expected to slow flights this morning in San Francisco (SFO).
Rules
Final Rule: Viking Air Limited Airplanes Published 05/31/2016 Docket #: FAA-2016-6628 Effective date 05/31/2016 The FAA is adopting a new airworthiness directive (AD) for Viking Air Limited Model DHC-3 airplanes that are modified with the Baron Short Take Off and Landing (STOL) kit (Supplemental Type Certificate SA94-114 or SA 00287NY). This AD results from mandatory continuing airworthiness information (MCAI) issued by the aviation authority of another country to identify and correct an unsafe condition on an aviation product. The MCAI describes the unsafe condition as a center of gravity that is too far aft contributing to a stall during takeoff and loss of control during other phases of flight. We are issuing this AD to require actions to address the unsafe condition on these products.
Final Rule: M7 Aerospace LLC Airplanes Published 05/11/2016 Docket #: FAA-2016-4256 Effective date 06/15/2016 The FAA is adopting a new airworthiness directive (AD) for all M7 Aerospace LLC Models SA226-AT, SA226-T, SA226-T(B), SA226-TC, SA227-AC (C-26A), SA227-AT, SA227-BC (C-26A), SA227-CC, SA227- DC (C-26B), and SA227-TT airplanes. We received reports of failed elevator control rod ends due to corrosion and lack of lubrication. This AD requires initial and repetitive inspections and lubrication of the elevator control rod ends and bearings with replacement as necessary. We are issuing this AD to correct the unsafe condition on these products.
Final Rule: The Boeing Company Airplanes Published 05/11/2016 Docket #: FAA-2015-0247 Effective date 06/15/2016 The FAA is adopting a new airworthiness directive (AD) for certain The Boeing Company Model 777- 200 and -300 series airplanes equipped with Rolls-Royce Trent 800 series engines. This AD was prompted by reports of heat damage to the strut aft fairing heat shield primary seal, as well as heat and wear damage to the heat shield insulation blankets. This AD requires repetitive inspections for cracks and heat damage to the strut aft fairing lower spar web structure (a flammable fluid zone barrier), for wear to the heat shield primary seal, and, as applicable, for heat and wear damage to heat shield insulation blankets; and related investigative and corrective actions if necessary. This AD also provides optional terminating action for the repetitive inspections.
Final Rule: Establishment of Class E Airspace; Beach, ND Published 05/11/2016 Docket #: FAA-2015-5801 Effective date 07/21/16 This action establishes Class E airspace extending upward from 700 feet above the surface at Beach Airport, Beach, ND, to accommodate new Standard Instrument Approach Procedures for the safety and management of Instrument Flight Rules (IFR) operations at the airport.
Proposed Rules
NPRM AD: Airbus Airplanes Published 05/11/16 Docket #: FAA-2016-6431 Comments due 06/27/16 The FAA proposes to adopt a new airworthiness directive (AD) for certain Airbus Model A318-112 airplanes, A319-111, -112, -115, -132, and -133 airplanes, A320-214, -232, and -233 airplanes, and A321-211, -212, -213, -231, and -232 airplanes. This proposed AD would require a one-time eddy current conductivity measurement of certain cabin, cargo compartment, and frame structural parts to determine if aluminum alloy with inadequate heat treatment was used, and replacement if necessary.
NPRM: Airbus Airplanes Published 05/11/16 Docket #: FAA-2016-6429 Comments due 06/27/16 The FAA proposes to supersede Airworthiness Directive (AD) 2015-05-02, for certain Airbus Model A318, A319, A320, and A321 series airplanes. AD 2015-05-02 requires revising the maintenance or inspection program to incorporate new, more restrictive airworthiness limitations. Since we issued AD 2015-05-02, an evaluation by the design approval holder (DAH) indicates that principal structural elements and certain life limited parts are subject to widespread fatigue damage (WFD). This proposed AD would require revising the maintenance or inspection program, as applicable, to incorporate new or revised structural inspection requirements.
NPRM: Rosemount Aerospace, Inc. Pitot Probes Published 05/11/16 Docket #: FAA-2016-6116 Comments due 06/27/16 The FAA proposes to adopt a new airworthiness directive (AD) for Rosemount Aerospace Model 851AK pitot probes that were repaired by CSI Aerospace, Inc. that are installed on airplanes. This proposed AD was prompted by a report that certain pitot probes are indicating the wrong airspeed during flight in icing conditions. This proposed AD would require inspecting the airplane to determine the number of affected pitot probes installed and replacing the affected pitot probes. We are proposing this AD to correct the unsafe condition on these products.
NPRM: The Boeing Company Published 05/11/16 Docket #: FAA-2016-6427 Comments due 06/27/16 The FAA proposes to supersede Airworthiness Directive (AD) 2007-11-13, which applies to all The Boeing Company Model 717-200 airplanes. AD 2007-11-13 currently requires revising the Airworthiness Limitations Section (ALS) of the Instructions for Continued Airworthiness to incorporate new removal limits for certain components of the flap system and to reduce the inspection interval s for fatigue cracking of principal structural elements (PSE). Since we issued AD 2007-11-13, a new Airworthiness Limitations Instructions (ALI) revision was released that incorporates nondestructive inspection (NDI) techniques and reduced repetitive inspection intervals for three PSEs.
NPRM: The Boeing Company Airplanes Published 05/11/16 Docket #: FAA-2016-6428 Comments due 06/27/16 The FAA proposes to adopt a new airworthiness directive (AD) for certain The Boeing Company Model 787-8 airplanes. This proposed AD was prompted by reports indicating that certain wing side-of-body stringer fittings have been installed with faying surface mismatch beyond the allowed machining tolerance. This proposed AD would require inspection of certain stringer fittings for faying surface mismatch common to the side-of-body rib chord, replacement if necessary, and replacement of the clearance fit fasteners common to the side-of-body fittings and upper side-of- body rib chord with tapered sleeve bolts. We are proposing this AD to prevent an unacceptable reduction of the fatigue life in the upper side-of-body rib chord. Associated fatigue cracks can reduce the structural capability to a point where it cannot sustain limit load, which could adversely affect the structural integrity of the airplane.
NPRM: The Boeing Company Airplanes Published 05/11/16 Docket #: FAA-2016-6430 Comments due 06/27/16 The FAA proposes to supersede Airworthiness Directive (AD) 2005-13-30, which applies to all Boeing Model 737-100, -200, and -200C series airplanes. AD 2005-13-30 currently requires repetitive inspections to detect discrepancies of certain fuselage skin panels located just aft of the wheel well, and repair if necessary. Since we issued AD 2005-13-30, an evaluation by the design approval holder (DAH) indicates that the fuselage skin is subject to widespread fatigue damage (WFD), and we have received reports of cracks at the chem-milled steps in the fuselage skin. This proposed AD would add new fuselage skin inspections for cracking, inspections to detect missing or loose fasteners and any disbonding or cracking of bonded doublers, permanent repairs of time- limited repairs, related investigative and corrective actions if necessary, and skin panel replacement.
Notices
Notice: Public Notice for a Change in Use of Aeronautical Property and Long-Term Lease Approval at Harrisburg International Airport (MDT), Middletown, PA Published 5/11/2016 Document #: 2016-11118 Comments due 6/10/2016 The Federal Aviation Administration (FAA) is requesting public comment on the Susquehanna Area Regional Airport Authority's (SARAA) request to change 7.18 acres of airport property from aeronautical use to non-aeronautical use. The acreage in question is subject to the Provisions of the Federal Property and Administrative Services Act of 1949, and the Surplus Property Act of 1944 as amended. In accordance with 49 U.S.C. 47151(d), 47153(c), and 47107(h), this notice is required to be published in the Federal Register 30 days before waiving the condition that such land be used for aeronautical purposes.
Notice: Petition for Exemption; Summary of Petition Received; Drone Surveys and Reports Published 5/11/2016 Document #: 2016-11109 Comments due 5/31/2016 The petitioner is seeking relief from the requirements and limitations specified in exemption no. 10686, which stipulates that doors installed across the main aisle must open and close in a transverse direction. The petitioner seeks to install curved partition doors in Boeing Model 747-8 airplanes designated as private use, not for hire, not for common carriage.
Notice: Petition for Exemption; Summary of Petition Received; BNSF Railway Company Published 05/31/2016 Docket/Doc PE:2016-62 Comments due 5/31/2016 The petitioner is requesting to amend Exemption No. 11206 to allow changes to Condition and Limitations #5 and #6 (to allow operations within VLOS of either the PIC or the VO), #16 (to allow the PIC to possess an airline transport, commercial, private, recreational, or pilot certificate, as well as a current FAA airmen medical certificate or a valid U.S. driver's license), #18 (to allow operations at night), #20 (to allow operations during inclement weather and operations of UAS in Class G airspace applying the VFR limits in 14CFR 91.155), #29 (to allow operations from a moving vehicle), and #31 (to allow operations within 500 feet from non-participating vehicles).
Notice: Petition for Exemption; Summary of Petition Received; Drone Consultants LLC Published 05/11/2016 Docket/Doc PE:2016-63 Comments due 05/31/2016 The petitioner is requesting relief for the following: 1. Commercially Operate the DJI F550, DJI S- 800, DJIS-900 and DJI Phantom 3 for the aerial photography/videography/inspection, and conducting sUAS operator training, qualification and demonstrations. 2. Night operations of DJI Phantom 3 under VFR conditions up to 200 feet AGL without having to request permission to fly each time from the FAA FSDO closest to the proposed area of operations.
Notice: Petition for Exemption; Summary of Petition Received; Jackie E. Watson Published 05/31/16 Docket/Doc PE: 2016-57 Comments due 05/31/2016 Petitioner seeks to amend Exemption No. 12077 for relief from Condition and Limitation #13 regarding Pilot in Command requirements to operate an unmanned aircraft system (UAS) for aerial data collection.
Notice: Petition for Exemption; Summary of Petition Received Published 05/11/2016 Document #: 2016-11112 Comments due 05/31/2016 The petitioner seeks relief from the requirements and limitations specified in exemption no. 10686, which stipulates that doors installed across the main aisle must open and close in a transverse direction. The petitioner seeks to install curved partition doors in Boeing Model 747-8 airplanes designated as private use, not for hire, not for common carriage.
Notice: Petition for Exemption; Summary of Petition Received; The Boeing Company Published 05/11/2016 Document #: 2016-11113 Comments due 05/31/2016 The Boeing Company has requested an exemption from 14 CFR 25.810(c) for certain new production Model 737 series airplanes that will be delivered to completion centers for interior modification and exterior painting.
Notice: Submission Deadline for Schedule Information for Chicago O'Hare International Airport, John F. Kennedy International Airport, Los Angeles International Airport, Newark Liberty International Airport, and San Francisco International Airport for the Winter 2016 Scheduling Season Published 05/11/2016 Document #: 2016-11116 Comments due 05/19/16 The FAA announces the submission deadline of May 19, 2016, for winter 2016 flight schedules at Chicago O'Hare International Airport (ORD), John F. Kennedy International Airport (JFK), Los Angeles International Airport (LAX), Newark Liberty International Airport (EWR), and San Francisco International Airport (SFO) in accordance with the International Air Transport Association (IATA) Worldwide Slot Guidelines (WSG) and FAA airport level designations. The deadline coincides with the schedule submission deadline for the IATA Slot Conference for the winter 2016 scheduling season.
Notice: Notice of Intent To Rule on a Release Request for a Change in Designation of On-Airport Surplus Property From Aeronautical to Non-Aeronautical Use at the Harrisburg International Airport (MDT), Middletown, PA Published 05/11/2016 Docket/Doc #:2016-11117 Comments due 06/10/2016 The Federal Aviation Administration (FAA) is requesting public comment on the Susquehanna Area Regional Airport Authority's (SARAA) request to change 11.398 acres of airport property from aeronautical use to non-aeronautical use. The acreage in question is subject to the Provisions of the Federal Property and Administrative Services Act of 1949, and the Surplus Property Act of 1944 as amended. In accordance with 49 U.S.C. 47151(d), 47153(c), and 47107(h), this notice is required to be published in the Federal Register for 30 days before waiving the condition that such land be used for aeronautical purposes. The purpose of the release request is to enable SARAA to generate revenue from this property by taking action including, but not limited to, entering into a long-term lease with Shaner Hotel Holdings for the purpose of constructing and operating a four (4) story hotel consisting of 120 guest rooms, a meeting center and restaurant.
Flight Standards Information Management System (FSIMS)
FSIMS: Airbus A-350-900 Issued 05/12/2016 Revision 0 of the Airbus A350-900 Master Minimum Equipment List.
May 12, 2016
Press releases
Press Release – FAA Proposes $162,500 Civil Penalty Against Airbus Defence and Space for Alleged HazMat Violations The U.S. Department of Transportation’s Federal Aviation Administration (FAA) proposes a $162,500 civil penalty against Airbus Defence and Space of Madrid, Spain, for allegedly violating the Hazardous Materials Regulations.
FAA Regulations
FAA Proposed Rules
NPRM AD: ATR-GIE Avions de Transport Régional Airplanes Published Docket #: FAA-2016-0077 Comments due 06/27/2016 05/12/2016 We are revising an earlier proposed airworthiness directive (AD) for certain ATR—GIE Avions de Transport Régional Model ATR42-500 and Model ATR72-212A airplanes. The NPRM proposed to require measuring the gap between the Type III Emergency Exit doors and certain overhead stowage compartment fittings; removing certain fittings from the overhead stowage compartments and measuring the gap between the Type III Emergency Exit doors and the overhead stowage compartment hooks, if necessary; and re-installing or repairing, as applicable, the Type III Emergency Exit doors. The NPRM was prompted by a report indicating that interference occurred between a Type III Emergency Exit door and the surrounding passenger cabin furnishing during a production check. This action revises the NPRM by adding new proposed requirements for modifying the overhead stowage compartments. We are proposing this supplemental NPRM (SNPRM) to prevent interference between a Type III Emergency Exit door and the overhead stowage compartment fitting installed on the rail; which could result in obstructed opening of a Type III Emergency Exit door during an emergency evacuation. Since these actions impose an additional burden over those proposed in the NPRM, we are reopening the comment period to allow the public the chance to comment on these proposed changes.
NPRM AD: The Boeing Company Airplanes Published Docket #: FAA-2016-6670 Comments due 06/27/2016 05/12/2016 We propose to supersede Airworthiness Directive (AD) 2013-19-04, which applies to certain The Boeing Company Model 737-600, -700, -700C, -800, and -900 series airplanes. AD 2013-19-04 currently requires repetitive detailed and high frequency eddy current (HFEC) inspections for cracking of the skin around the eight fasteners common to the ends of the station (STA) 540 bulkhead chords between stringers S-22 and S-23, left and right sides; related investigative actions and corrective actions, if necessary; and provides an optional terminating modification. Since we issued AD 2013-19-04, we have received reports of additional cracks that are larger and initiated sooner than previously predicted. This proposed AD would reduce the inspection threshold and repetitive inspection intervals. We are proposing this AD to detect and correct fatigue cracking in the fuselage skin around the eight fasteners securing the STA 540 bulkhead chords. Such cracking can result in rapid decompression of the cabin.
NPRM AD: The Boeing Company Airplanes Published Docket #: FAA-2016-6669 Comments due 06/27/2016 05/12/2016 We propose to supersede Airworthiness Directive (AD) 2006-20-11, which applies to certain The Boeing Company Model 757-200, -200CB, and -200PF series airplanes. AD 2006-20-11 currently requires initial and repetitive detailed or high frequency eddy current (HFEC) inspections for cracks around the rivets at the upper fastener row of the skin lap splice of the fuselage, and repairing any crack found. Since we issued AD 2006-20-11, an evaluation done by the design approval holder (DAH) indicated that the fuselage skin lap splice is subject to widespread fatigue damage (WFD). This proposed AD would no longer allow the detailed inspections and would instead require repetitive external HFEC inspections for cracking of the skin lap splices of the fuselage, and repair if necessary. We are proposing this AD to detect and correct fatigue cracking at certain skin lap splice locations of the fuselage, which could result in reduced structural integrity and rapid decompression of the airplane.
NPRM: Aviation Training Devices; Pilot Certification, Training, and Pilot Schools; and Other Provisions Published Docket #: FAA-2016-6142 Comments due 08/10/2016 05/12/2016 This rulemaking would relieve burdens on pilots seeking to obtain aeronautical experience, training, and certification by increasing the allowed use of aviation training devices. These training devices have proven to be an effective, safe, and affordable means of obtaining pilot experience. This rulemaking also would address changing technologies by accommodating the use of technically advanced airplanes as an alternative to the use of older complex single engine airplanes for the commercial pilot training and testing requirements. Additionally, this rulemaking would broaden the opportunities for military instructors to obtain civilian ratings based on military experience, would expand opportunities for logging pilot time, and would remove a burden from sport pilot instructors by permitting them to serve as safety pilots. Finally, this rulemaking would include changes to some of the provisions established in an August 2009 final rule. These actions are necessary to bring the regulations in line with current needs and activities of the general aviation training community and pilots.
FAA Guidance Documents and Notices
FAA Final Policies
Final Policy: Deviation to FAA Order 8120.22A Production Approval Procedures Issued M/D/YYYY Policy #: AIR100_16-110-DM10 This memorandum authorizes a deviation to Order 8120.22A, Production Approval Procedures, paragraph 4-6(f) and Figure 4-4 which lists information to be included in a Parts Manufacturer Approval (PMA) Assist Letter. The Aircraft Certification Service (AIR) has been asked to clarify what is the minimum information required in a PMA Assist Letter. Notices
Notice: Aviation Rulemaking Advisory Committee-New Task Published Document #: 2016-11104 05/12/2016 The FAA has assigned the Aviation Rulemaking Advisory Committee (ARAC) a new task to provide recommendations regarding the certification of persons engaged in operations involving the loading of special cargo. Assignment of this task is in response to National Transportation Safety Board Recommendation A-15-014 which recommended that the FAA create a certification for personnel responsible for the loading, restraint, and documentation of special cargo loads on transport-category airplanes. This notice informs the public of the new ARAC activity and solicits membership for the new Loadmaster Certification Working Group.
May 13, 2016
FAA Proposed Rules
NPRM AD: Fokker Services B.V. Airplanes Published 05/13/2016 Docket #: FAA-2016-6665 Comments due 06/27/2016 The FAA proposes to adopt a new airworthiness directive (AD) for all Fokker Services B.V. Model F28 Mark 0070 and 0100 airplanes. This proposed AD was prompted by an aileron-wing flutter analysis finding that when a hydraulic aileron actuator is not powered, while at least one aileron flutter damper is inoperative (latent failure), the maximum speed currently defined in the airplane flight manual (AFM) is insufficient to meet the required safety margin. This proposed AD would require revising the AFM to include procedures to follow in the event of a hydraulic system failure and abnormal flight control behavior. We are proposing this AD to ensure that the flightcrew has procedures to follow in the event of a hydraulic system failure and abnormal flight control behavior. If not corrected, this condition could lead to aileron flutter and possible reduced control of the airplane.
NPRM AD: Saab AB, Saab Aeronautics (Type Certificate Previously Held by Saab AB, Saab Aerosystems) Airplanes Published 05/13/2016 Docket #: FAA-2016-6668 Comments due 06/27/2016 The FAA proposes to adopt a new airworthiness directive (AD) for certain Saab AB, Saab Aeronautics Model SAAB 2000 airplanes. This proposed AD was prompted by a report that on some airplanes, during the paint removal process for repainting the airplane, the basic corrosion protection (anodizing and primer) coating was sanded down to bare metal on the aluminum skin panels and the bare metal might not have been treated correctly for corrosion prevention. This proposed AD would require an inspection of structural components of the airplane for any damaged protective coating; inspections of those areas for pitting corrosion, if necessary; a thickness measurement to determine if there is reduced skin thickness, if necessary; and repair, if necessary. We are proposing this AD to detect and correct damaged protective coatings. This condition could result in pitting corrosion damage; and reduced metal thickness, which could result in reduced static and fatigue strength of the airplane's structural parts.
NPRM AD: Sikorsky Aircraft Corporation Helicopters Published 05/13/2016 Docket #: FAA-2016-6640 Comments due 07/12/2016 The FAA propses to adopt a new airworthiness directive (AD) for Sikorsky Aircraft Corporation (Sikorsky) Model S-92A helicopters. This proposed AD would require altering the fire bottle inertia switch wiring and performing a cartridge functional test of the fire extinguishing system. This proposed AD is prompted by the inadvertent tripping of inertia-switches that has led to unintentional discharging of the fire bottles, leaving the helicopter's auxiliary power unit and engines without fire protection. The proposed actions are intended to prevent unintentional and undetected fire bottle discharges and subsequent unavailability of fire suppression in case of a fire.
NPRM AD: The Boeing Company Airplanes Published 05/13/2016 Docket #: FAA-2016-6664 Comments due 06/27/2016 The FAA proposes to supersede Airworthiness Directive (AD) 2012-16-07, which applies to certain Boeing Model 737-500 series airplanes. AD 2012-16-07 currently requires inspections of the fuselage skin at the chem-milled steps, and repair if necessary. Since we issued AD 2012-16-07, an evaluation by the design approval holder (DAH) indicates that the fuselage skin is subject to widespread fatigue damage (WFD), and we have received reports of cracks at the chem-milled steps in the fuselage skin. This proposed AD would add new fuselage skin inspections for cracking, inspections to detect missing or loose fasteners and any disbonding or cracking of bonded doublers, permanent repairs of time-limited repairs, related investigative and corrective actions if necessary, and skin panel replacement. We are proposing this AD to detect and correct cracking on the aft lower lobe fuselage skins, which could result in rapid decompression of the airplane.
NPRM AD: The Boeing Company Airplanes Published 05/13/2016 Docket #: FAA-2016-6666 Comments due 06/27/2016 The FAA proposes to adopt a new airworthiness directive (AD) for certain Boeing Model 737-400 series airplanes. This proposed AD was prompted by an evaluation by the design approval holder (DAH) which indicates that the aft fuselage skin is subject to widespread fatigue damage (WFD) and reports of aft fuselage skin cracking. This proposed AD would require repetitive inspections to detect cracking of the aft fuselage skin, inspections to detect missing or loose fasteners and any disbonding or cracking of bonded doublers, permanent repairs of time-limited repairs, related investigative and corrective actions if necessary, and skin panel replacement. We are proposing this AD to detect and correct cracking in the aft fuselage skin along the longitudinal edges of the bonded skin doubler, which could result in possible rapid decompression and reduced structural integrity of the airplane.
NPRM AD: The Boeing Company Airplanes Published 05/13/2016 Docket #: FAA-2016-6667 Comments due 06/27/2016 We propose to supersede Airworthiness Directive (AD) 2009-21-01, which applies to certain Boeing Model 737-300 and 737-400 series airplanes. AD 2009-21-01 currently requires repetitive inspections to detect cracking of the aft fuselage skin, and related investigative and corrective actions if necessary. Since we issued AD 2009-21-01, an evaluation by the design approval holder (DAH) indicates that the aft fuselage skin is subject to widespread fatigue damage (WFD). This proposed AD would add new aft fuselage skin inspections for cracking, inspections to detect missing or loose fasteners and any disbonding or cracking of bonded doublers, permanent repairs of time-limited repairs, related investigative and corrective actions if necessary, and skin panel replacement. The proposed AD also removes Model 737-400 series airplanes from the applicability. We are proposing this AD to detect and correct cracking in the aft fuselage skin along the longitudinal edges of the bonded skin doubler, which could result in possible rapid decompression and reduced structural integrity of the airplane.
FAA Guidance Documents and Notices
Draft Technical Standards Orders
TSO: Traffic Alert and Collision Avoidance System (TCAS) Airborne Equipment, TCAS II with Hybrid Surveillance Updated 05/10/2016 Comments due 06/13/2016 This technical standard order (TSO) is for manufacturers applying for a TSO authorization (TSOA) or letter of design approval (LODA). In it, we (the Federal Aviation Administration or FAA) tell you what minimum performance standards (MPS) your traffic alert and collision avoidance system II (TCAS II) must first meet for approval and identification with the applicable TSO marking.
TSO: Airborne Selective Calling (SELCAL) Equipment Updated 05/10/2016 Comments due 06/06/2016 This technical standard order (TSO) is for manufacturers applying for a TSO authorization (TSOA) or letter of design approval (LODA). In it, we (the Federal Aviation Administration or FAA) tell you what minimum performance standards (MPS) your traffic alert and collision avoidance system II (TCAS II) must first meet for approval and identification with the applicable TSO marking.
Flight Standards Service Draft Advisory Circular
AC: 120-MFRM, Maintainer Fatigue Risk Management Updated 04/26/2016 Reference #: Title 14 Part xx-xx Comments due 05/31/2016 This advisory circular (AC) describes the basic concepts of human fatigue and how it relates to safety for aviation maintenance organizations and individual maintainers; provides information on Fatigue Risk Management (FRM) in terms of fatigue hazards and mitigation strategies specific to aviation maintainers; describes the benefits of implementing FRM methods within aviation maintenance organizations; and identifies methods for integrating FRM within a Safety Management System (SMS) (if applicable).
AC: 91-MPA, Maintaining Public Aircraft Updated 04/26/2016 Reference #: Title 14 Part xx-xx Comments due 05/22/2016 This advisory circular (AC) provides guidance for the owners and operators of public aircraft in developing inspection and maintenance programs. Government agencies can use this guidance if they choose to maintain their aircraft per Title 14 of the Code of Federal Regulations (14 CFR).
AC: 43-214A, Repairs and Alterations to Composite and Bonded Aircraft Structure Updated 04/26/2016 Reference #: Title 14 Part xx-xx Comments due 05/17/2016 This advisory circular (AC) provides guidance for the owners and operators of public aircraft in developing inspection and maintenance programs. Government agencies can use this guidance if they choose to maintain their aircraft per Title 14 of the Code of Federal Regulations (14 CFR).
Draft Master Minimum Equipment List
MMEL: Beechcraft-300 Rev 9, Beechcraft Updated 05/06/2016 Revision 19 Comments due 05/25/2016
MMEL: CL-600-2B19 Rev 19, Bombardier Updated 05/06/2016 Revision 9 Comments due 06/05/2017
Draft MMEL AEG Policy
MMEL: All Aircraft Evaluation Group Managers/ Policy Letter (PL)-98, Revision 1 Updated M/D/YYYY Revision 1 Draft 1 Comments due M/D/YYYY
May 16, 2016
FAA Final rules
Final Rule AD: The Boeing Company Airplanes Published 05/16/16 Docket #: FAA-2015-3141 Effective date 06/20/2016 We are adopting a new airworthiness directive (AD) for all The Boeing Company Model 757 airplanes. This AD was prompted by a report of cracking in the fuselage frame. This AD requires inspections for cracking in the fuselage frame, left and right sides, and repair if necessary. We are issuing this AD to detect and correct fuselage frame fatigue cracking. Such cracking could result in loss of structural integrity and the inability to sustain loading conditions.
Final Rule AD: The Boeing Company Airplanes Published 05/16/16 Docket #: FAA-2015-2462 Effective date 06/20/2016 We are adopting a new airworthiness directive (AD) for certain The Boeing Company Model 737- 100, -200, -200C, -300, -400, and -500 series airplanes. This AD was prompted by reports of cracked antenna support channels, skin cracking underneath the number 2 very high frequency (VHF) antenna, and cracking in the frames attached to the internal support structure. This AD requires repetitive inspections to determine the condition of the skin and the internal support structure, and follow-on actions including corrective action as necessary. We are issuing this AD to detect and correct skin cracking of the fuselage. Such cracking could result in separation of the number 2 VHF antenna from the airplane and rapid depressurization of the cabin.
FAA Proposed Rules
NPRM: Slot Management and Transparency for LaGuardia Airport, John F. Kennedy International Airport, and Newark Liberty International Airport Published 05/16/2016 Docket #: FAA-2014-1073 Withdrawn The DOT is withdrawing a previously published Notice of Proposed Rulemaking (NPRM) that would have replaced the Orders limiting scheduled operations at John F. Kennedy International Airport (JFK), Newark Liberty International Airport (EWR), and LaGuardia Airport (LGA) with longer-term limits on scheduled and unscheduled operations at JFK, EWR, and LGA, and requested comment on options to establish a secondary market for the purchase, sale, lease, or trade of slots at these airports, as well as procedures that would codify the review of slot transactions arising from the secondary market for public interest and anti-competitive effects.
FAA Special Conditions
SC: Cessna Aircraft Company, Models 208 and 208B, Caravan Airplanes; As Modified by Peregrine; Installation of Rechargeable Lithium Battery Published 05/16/16 Docket #: FAA-2016-6567 Effective date 05/16/16 These special conditions are issued for the Cessna Aircraft Company, Models 208 and 208B Caravan airplanes. This airplane, as modified by Peregrine, will have a novel or unusual design feature associated with the use of a replacement option of a lithium battery instead of nickel-cadmium (Ni- Cd) and lead-acid rechargeable batteries. 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.
FAA Guidance Documents and Notices
Notices
Notice: Noise Exposure Map Notice; Receipt of Noise Compatibility Program and Request for Review Boise Air Terminal (Gowen Field) Boise, ID; Correction Published 05/16/16 Document #: 2016-11503 Comments due 07/01/16 This action corrects the noise exposure map notice and receipt of noise compatibility program and request for review published on May 10, 2016. In that document, the FAA has determinied that the noise exposure maps submitted by the City of Boise, ID, for the Boise Air Terminal (Gowen Field), Boise, ID, are in compliance with applicable requirements, and that it is reviewing a proposed noise compatibility program that was submitted for Boise Air Terminal (Gowen Field) under part 150 in conjunction with the Noise Exposure Map, and that this program be approved or disapproved on or before October 29, 2016. This document corrects an error in the Supplementary Information showing Great Falls International Airport instead of Boise Air Terminal (Gowen Field).
Meeting: Sixth Meeting: RTCA Special Committee 233 Addressing Human Factors/Pilot Interface Issues for Avionics (SC-233) Meeting date 06/21/16 Meeting time 9:00am –5:00pm Time zone (EST/etc.) The FAA is issuing this notice to advise the public of the Sixth RTCA Special Committee 233 meeting.
Meeting: Tenth Meeting: RTCA Special Committee 231 (SC-231) Terrain Awareness Warning Systems (TAWS) Meeting date 07/10/16 Meeting time 9:00am –5:00pm Time zone (EST/etc.) The FAA is issuing this notice to advise the public of the Tenth RTCA Special Committee 231 meeting.
Meeting: Twenty-Third Meeting: RTCA Special Committee 222 (SC-222) AMS(R)S, Joint Meeting With EUROCAE WG-82 Meeting date 07/08/16 Meeting time 9:00am –5:00pm Time zone (EST/etc.) The FAA is issuing this notice to advise the public of the Tenth RTCA Special Committee 231 meeting.
Draft Technical Standards Orders
TSO: Airborne Selective Calling (SELCAL) Equipment Updated 05/10/16 Comments due 06/06/2016 This technical standard order (TSO) is for manufacturers applying for a TSO authorization (TSOA) or letter of design approval (LODA). In it, we (the Federal Aviation Administration, FAA) tell you what minimum performance standards (MPS) your Airborne Selective Calling (SELCAL) Equipment must first meet for approval and identification with the applicable TSO marking.
TSO: Traffic Alert and Collision Avoidance System (TCAS) Airborne Equipment, TCAS II with Hybrid Surveillance Updated 05/10/16 Comments due 06/13/2016 This technical standard order (TSO) is for manufacturers applying for a TSO authorization (TSOA) or letter of design approval (LODA). In it, we (the Federal Aviation Administration, FAA) tell you what minimum performance standards (MPS) your Airborne Selective Calling (SELCAL) Equipment must first meet for approval and identification with the applicable TSO marking.
Flight Standards Service Draft Advisory Circular
AC: AC 120-MFRM, Maintainer Fatigue Risk Management Updated 04/26/2016 Reference #: Title 14 Part 121 Comments due 05/31/2016 This advisory circular (AC) describes the basic concepts of human fatigue and how it relates to safety for aviation maintenance organizations and individual maintainers; provides information on Fatigue Risk Management (FRM) in terms of fatigue hazards and mitigation strategies specific to aviation maintainers; describes the benefits of implementing FRM methods within aviation maintenance organizations; and identifies methods for integrating FRM within a Safety Management System (SMS) (if applicable).
AC: AC 91-MPA, Maintaining Public Aircraft Updated 04/26/2016 Reference #: Title 14 Part 121 Comments due 05/22/2016 This advisory circular (AC) describes the basic concepts of human fatigue and how it relates to safety for aviation maintenance organizations and individual maintainers; provides information on Fatigue Risk Management (FRM) in terms of fatigue hazards and mitigation strategies specific to aviation maintainers; describes the benefits of implementing FRM methods within aviation maintenance organizations; and identifies methods for integrating FRM within a Safety Management System (SMS) (if applicable).
AC: AC 91-ENGO, Electronic News Gathering Operations Updated 04/26/2016 Reference #: Title 14 Part 121 Comments due 06/05/2016 This advisory circular (AC) provides best practices and guidelines for electronic news gathering (ENG) pilots and operators. It includes sample risk assessment tools as recommended by the National Transportation Safety Board (NTSB) safety recommendations A-09-002, A-09-003, and A- 09-008, as well as recommendations on electronic traffic advisory systems (TAS) and Automatic Dependent Surveillance Broadcast (ADS-B) installation.
AC: AC 43-214A, Repairs and Alterations to Composite and Bonded Aircraft Structure Updated 04/26/2016 Reference #: Title 14 Part 43 Comments due 05/16/2016 This advisory circular (AC) provides information and guidance concerning an acceptable means, but not the only means, of demonstrating compliance with the requirements of the applicable parts of Title 14 of the Code of Federal Regulations (14 CFR) regarding procedures and facilities for repairs and alterations of structures consisting of adhesively-bonded (including metal bond) and fiber- reinforced materials (e.g., carbon, aramid, and glass-reinforced polymeric materials mentioned in the current edition of AC 20-107, Composite Aircraft Structure). The information in this AC is applicable to repairs and alterations of bonded and composite structures, whether it is a damaged part that can be removed from the airplane for repairs, or repairs and alterations on the aircraft itself.
Draft Flight Standardization Board/Operational Suitability Report
FSB: Bombardier DHC-8-100, 200, 300, 400 Series, All Models Updated 05/13/2016 Revision 4 Comments due 05/19/2016
FSB: Draft FSB EMB-135-145 R8 Updated 05/13/2016 Revision 8 Comments due 05/20/2016
FSB: Draft FSB ATR42-72 R6 Updated 05/13/2016 Revision 6 Comments due 05/20/2016
FSB: Draft FSB BE-1900 REV5 Updated 05/13/2016 Revision 5 Comments due 06/16/2016
OSR: Bombardier DHC-8-100, 200, 300, 400 Series, All Models Updated M05/13/2016 Revision 4 Draft 1 Comments due 05/19/2016
OSR: Draft FSB EMB-135-145 R8 Updated M05/13/2016 Revision 8 Comments due 05/20/2016
OSR: Draft FSB ATR42-72 R6 Updated M05/13/2016 Revision 6 Comments due 05/20/2016
OSR: Draft FSB BE-1900 REV5 Updated M05/13/2016 Revision 5 Comments due 06/16/2016
Draft Master Minimum Equipment List
MMEL: MMEL Beechcraft-300 Rev 9, Beechcraft Updated 05/06/2016 Title 14 Part 91 Comments due 05/21/2016
MMEL: MMEL CL-600-2B19 Rev 19, Bombardier Updated 05/06/2016 Title 14 Part 91 Comments due 06/05/2016
Draft MMEL AEG Policy
MMEL: Draft MMEL Policy Letter 98 Revision 1 Updated 05/13/2016 Revision 1 Comments due 05/31/2016
May 17, 2016
FAA Guidance Documents and Notices
FAA Draft Advisory Circulars
AC: AC 21-46A, Technical Standard Program (TSO) Issued 04/22/2016 Document #: AC 21-46A Comment date 05/20/2016 Publish revision A to existing AC 21-46, TSO program. This revision provides the latest guidance for applicant to follow in participating in the TSO program.
AC: Alternate Methods of Compliance Issued 04/22/2016 Document #: AC 39-xx Comment date 05/30/2016 Advisory Circular 39-xx, Alternative Methods of Compliance (AMOC), has been created to provide guidance to persons seeking approval of an AMOC. This guidance was removed from FAA Order 8110.103A. The AC provides information regarding how to propose an AMOC, where to submit it, and has frequently asked questions about AMOCs.
AC: AC 33.15-3, Parts Manufacturer Approval (PMA) Metallic Part Material Compliance Using Comparative Test and Analysis Method for Turbine Engines or Auxiliary Power Units Issued 04/22/2016 Document #: AC 33.15-3 Comment date 07/20/2016 This advisory circular (AC) provides guidance to compare Parts Manufacturer Approval (PMA) materials with type design materials used in turbine engine parts or auxiliary power unit (APU) parts. The approach describes a comparative test and analysis method (CTAM) that can be used to demonstrate that the PMA part material is at least equivalent to the type design part material.
Notices
Notice: Agency Information Collection Activities: Requests for Comments; Clearance of Renewed Approval of Information Collection: Application for Employment With the Federal Aviation Administration; Withdrawal This action withdraws the Notice to collect information to process and report Unmanned Aircraft Systems (UAS) airborne and ground based observations by the public of drone behavior that they consider suspicious or illegal. The document contained errors, and needs further clarification.
Draft Technical Standards Orders
TSO: Airborne Selective Calling (SELCAL) Equipment Updated 05/10/2016 Comments due 06/6/2016 This technical standard order (TSO) is for manufacturers applying for a TSO authorization (TSOA) or letter of design approval (LODA). In it, we (the Federal Aviation Administration, FAA) tell you what minimum performance standards (MPS) your Airborne Selective Calling (SELCAL) Equipment must first meet for approval and identification with the applicable TSO marking.
TSO: Traffic Alert and Collision Avoidance System (TCAS) Airborne Equipment, TCAS II with Hybrid Surveillance Updated 05/10/2016 Comments due 06/13/2016 This technical standard order (TSO) is for manufacturers applying for a TSO authorization (TSOA) or letter of design approval (LODA). In it, we (the Federal Aviation Administration or FAA) tell you what minimum performance standards (MPS) your traffic alert and collision avoidance system II (TCAS II) must first meet for approval and identification with the applicable TSO marking.
Flight Standards Service Draft Advisory Circular
AC: AC 120-MFRM, Maintainer Fatigue Risk Management Updated 04/26/2016 Reference #: Title 14 Part 21 Comments due 05/31/2016 This advisory circular (AC) describes the basic concepts of human fatigue and how it relates to safety for aviation maintenance organizations and individual maintainers; provides information on Fatigue Risk Management (FRM) in terms of fatigue hazards and mitigation strategies specific to aviation maintainers; describes the benefits of implementing FRM methods within aviation maintenance organizations; and identifies methods for integrating FRM within a Safety Management System (SMS) (if applicable).
AC: AC 91-MPA, Maintaining Public Aircraft Updated 04/26/2016 Reference #: Title 14 Part 21 Comments due 05/22/2016 This advisory circular (AC) provides guidance for the owners and operators of public aircraft in developing inspection and maintenance programs. Government agencies can use this guidance if they choose to maintain their aircraft per Title 14 of the Code of Federal Regulations (14 CFR).
AC: AC 91-ENGO, Electronic News Gathering Operations Updated 04/26/2016 Reference #: Title 14 Part 21 Comments due 06/05/2016 This advisory circular (AC) provides best practices and guidelines for electronic news gathering (ENG) pilots and operators. It includes sample risk assessment tools as recommended by the National Transportation Safety Board (NTSB) safety recommendations A-09-002, A-09-003, and A- 09-008, as well as recommendations on electronic traffic advisory systems (TAS) and Automatic Dependent Surveillance Broadcast (ADS-B) installation.
Draft Flight Standardization Board/Operational Suitability Report
FSB: Draft FSB SF340 R2 Updated 05/13/2016 Revision 2 Comments due 05/13/2016
FSB: Draft FSB SF340 R2 Updated 05/13/2016 Revision 2 Comments due 05/13/2016 FSB: Bombardier DHC-8-100, 200, 300, 400 Series, All Models Updated 05/13/2016 Revision 4 Draft 1 Comments due 05/19/2016 FSB: Draft FSB EMB-135-145 R8 Updated 05/13/2016 Revision 8 Comments due 05/20/2016 FSB: Draft FSB BE-1900 REV5 Updated 05/13/2016 Revision 6 Comments due 05/20/2016
FSB: Draft FSB SF340 R2 Updated 05/13/2016 Revision 5 Comments due 06/16/2016
Draft Master Minimum Equipment List
MMEL: MMEL Beechcraft-300 Rev 9, Beechcraft Updated 05/03/2016 Revision 9 Comments due 05/25/2016
MMEL: MMEL CL-600-2B19 Rev 19, Bombardier Updated 05/03/2016 Revision 19 Comments due 06/05/2016
Draft MMEL AEG Policy
MMEL: Draft MMEL Policy Letter 98 Revision 1 Updated 05/13/2016 Revision 1 Comments due 05/31/2016
May 18, 2016
Press releases
City of Cleveland Agrees to Pay $200,000 and Enhance Compliance SystemsBrief The U.S. Department of Transportation’s Federal Aviation Administration (FAA) today announced a comprehensive settlement agreement with the City of Cleveland that resolves several pending enforcement cases.
FAA Legal Interpretations
Legal Interpretation: Oliver-Alpha Technologies - (2016) Legal Interpretation Issued 05/17/2016 Regulation/Order 61: 58 This is in response to your letter dated February 5, 2016, in which you sought clarification of 14 C.F.R. § 61.58(d)(2). You explained that you represent a part 91 aviation department that operates a Gulfstream G280 and a Gulfstream G 150. You recently sent one of your pilots who is already type rated in the G150 to Flight Safety where he successfully completed the initial G280 course thereby satisfying the PIC proficiency check requirements of§ 61.58(a)(l) and (2) for the G280 aircraft. You asked if, under§ 61.58(d), the PIC proficiency check requirements of§ 61.58(a)(l) and (a)(2) are also met for the G150 aircraft based on the pilot's satisfactory completion of the practical test for a type rating in the G280 aircraft.
Legal Interpretation: Ragland-Arizona Aero-Tech - (2016) Legal Interpretation Issued 05/17/2016 Regulation/Order 141: 63 This is in response to your letter dated February 5, 2016, in which you sought clarification of 14 C.F.R. § 61.58(d)(2). You explained that you represent a part 91 aviation department that operates a Gulfstream G280 and a Gulfstream G 150. You recently sent one of your pilots who is already type rated in the G150 to Flight Safety where he successfully completed the initial G280 course thereby satisfying the PIC proficiency check requirements of§ 61.58(a)(l) and (2) for the G280 aircraft. You asked if, under§ 61.58(d), the PIC proficiency check requirements of§ 61.58(a)(l) and (a)(2) are also met for the G150 aircraft based on the pilot's satisfactory completion of the practical test for a type rating in the G280 aircraft.
Special Airworthiness Information Bulletins (SAIB)
SAIB: Fuselage – Pilatus PC-9 Frame 11 Fittings – Inspection Issued 05/17/16 SAIB #: CE-16-17 This Special Airworthiness Information Bulletin is to alert owners, operators, maintenance technicians, and inspectors of an airworthiness concern on Pilatus Aircraft (Pilatus) Models PC-9, PC-9/A, PC-9/B, and PC-9/F airplanes with manufacturer’s serial numbers (MSN) 101 through MSN 248 and MSN 501 through MSN 567. Specifically, the concern is the possibility of stress corrosion cracking (SCC) on the main frame on the Frame (FR) 11 left fitting part number (P/N) 112.35.07.489 and right fitting P/N 112.35.07.490. This condition, if left uncorrected, could lead to potential loss of the horizontal stabilizer.
Orders
Order: JO 7110.122 - Wide Area Multilateration (WAM) Virtual Radar (VR) data for surveillance within the National Airspace System (NAS) Issued 05/17/16 Document JO: 7110-#122 Comments due M/D/YYYY This order prescribes guidance for the use of WAM-VR information for conducting ATC services using Standard Terminal Automation Replacement System (STARS) in Fusion Display Mode (FDM), Single Sensor Mode, and using Final Monitor Aid (FMA).
Notices
Meeting: Eighteenth Meeting: RTCA NextGen Advisory Committee (NAC) Meeting date 06/17/2016 Meeting time 9:00am – 3:00pm Time zone (EST/etc.) The FAA is issuing this notice to advise the public of the Eighteenth RTCA NextGen Advisory Committee meeting.
May 19, 2016
FAA Final rules AD: Bombardier, Inc. Airplanes Published 05/19/2016 Docket #: FAA-2015-8431 Effective date 06/23/2016 We are adopting a new airworthiness directive (AD) for certain Bombardier, Inc. Model BD-700- 1A10 and BD-700-1A11 airplanes. This AD was prompted by a determination that the network interface installed between the Information Management System (IMS) 6000 unit and the Cabin Entertainment System (CES) network could affect the Aircraft Control Domain (ACD), and result in the transmission of misleading navigational information to the flightcrew. This AD requires inspecting the network interface installation between the IMS and the CES, and disconnecting the installation, if necessary. We are issuing this AD to prevent the transmission of misleading navigational information, which could adversely affect the ability of the flightcrew to maintain the safe flight and landing of the airplane.
AD: Bombardier, Inc. Airplanes Published 05/19/2016 Docket #: FAA-2015-3634 Effective date 06/23/2016 We are superseding Airworthiness Directive (AD) 2014-20-01 for certain Bombardier, Inc. Model CL- 600-2B16 (CL-601-3A, CL-601-3R, and CL-604 Variants) airplanes. AD 2014-20-01 required repetitive inspections for any fuel leak in the right-hand landing lights compartment, and related investigative and corrective actions if necessary. AD 2014-20-01 also provides for an optional replacement of the connector of the fuel boost pump canister of the auxiliary power unit (APU), which terminates the repetitive inspections. This new AD requires replacing the connector of the fuel boost pump canister of the APU. This AD was prompted by the determination that a terminating action for the repetitive inspections is necessary. We are issuing this AD to detect and correct fuel leaks in the right-hand landing lights compartment, which, in combination with the heat generated by the taxi lights and landing lights on the ground reaching the auto-ignition temperature of the fuel, could result in ignition of any fuel or fumes present in the right-hand landing lights compartment.
AD: Bombardier, Inc. Airplanes Published 05/19/2016 Docket #: FAA-2013-#0703 Effective date 06/23/2016 We are adopting a new airworthiness directive (AD) for certain Bombardier, Inc. Model DHC-8-102, -103, -106, -201, -202, -301, -311, and -315 airplanes. This AD was prompted by a report of a pilot commanding an in-flight engine shut down in response to a low oil pressure warning indication. Further investigation revealed the mounting studs in the engine mounted alternating current (AC) generator mounting plate were pulled out of position and the threaded interface in the plate was corroded. This AD requires repetitive inspections for discrepancies on certain AC generator mounting adapters, and replacing discrepant adapters with serviceable ones. This AD also requires revising the maintenance program to incorporate a repetitive task specified in certain temporary revisions. We are issuing this AD to detect and correct corrosion in the AC generator mounting plate, which could result in a gap between the AC generator and the generator mounting plate, and cause loss of engine oil and consequent engine failure.
FAA Guidance Documents and Notices
Notices
Notice: Receipt of Noise Compatibility Program and Request for Review for Bob Hope Airport, Burbank, California Published 05/19/2016 Document #: 2016-11814 Comments due M/D/YYYY The Federal Aviation Administration (FAA) announces that it is reviewing a proposed noise compatibility program that was submitted for Bob Hope Airport under the provisions of 49 U.S.C. 47501 et seq. (the Aviation Safety and Noise Abatement Act, hereinafter referred to as “the Act”) and 14 Code of Federal Regulations (CFR) Part 150 by the Burbank-Glendale-Pasadena Airport Authority, Burbank, California. This program was submitted subsequent to a determination by FAA that associated noise exposure maps submitted under 14 CFR part 150 for Bob Hope Airport were in compliance with applicable requirements, effective October 10, 2013, 78 FR 64048-64049. The proposed noise compatibility program will be approved or disapproved on or before November 7, 2016.
Meeting: Twenty-Seventh Meeting: RTCA Special Committee 216 (SC-216) Aeronautical Systems Security Meeting date 06/17/2016 Meeting time 9:00am – 5:00pm Time zone (EST/etc.) The FAA is issuing this notice to advise the public of the Twenty-Seventh RTCA Special Committee 216 meeting.
May 20, 2016
FAA Final rules
AD: Airbus Airplanes Published Docket #: FAA-2014-0006 Effective date 06/24/2016 05/20/2016 We are adopting a new airworthiness directive (AD) for all Airbus Model A330-200 Freighter, A330- 200, A330-300, A340-200, A340-300, A340-500, and A340-600 series airplanes. This AD was prompted by the results of endurance qualification tests on the trimmable horizontal stabilizer actuator (THSA), which revealed a partial loss of the no-back brake (NBB) efficiency in specific load conditions. This AD requires inspecting certain THSAs to determine the number of total flight cycles the THSA has accumulated, and replacing the THSA if necessary. We are issuing this AD to detect and correct premature wear of the carbon friction disks on the NBB of the THSA. Such a condition could lead to reduced braking efficiency in certain load conditions and, in conjunction with the inability of the power gear train to keep the ball screw in its last commanded position, could result in uncommanded movements of the trimmable horizontal stabilizer (THS) and loss of control of the airplane.
AD: Airbus Airplanes Published Docket #: FAA-2015-6548 Effective date 06/24/2016 05/20/2016 We are adopting a new airworthiness directive (AD) for certain The Boeing Company Model 787-8 and 787-9 airplanes equipped with General Electric engines. This AD was prompted by reports of cracking in barrel nuts on a forward engine mount of Model 747-8 airplanes, which shares a similar design to the forward engine mount of Model 787-8 and 787-9 airplanes. This AD requires, for certain airplanes, replacement of the four barrel nuts of the forward engine mount on each engine. For certain other airplanes, this AD requires an inspection to determine if any forward engine mount barrel nut having a certain part number is installed; and related investigative and corrective actions if necessary. We are issuing this AD to detect and correct cracking of the forward engine mount barrel nuts. Such cracking could result in reduced load capacity of the forward engine mount and could result in separation of an engine from the airplane and consequent loss of control of the airplane.
Final Rule: Amendment of Class D and Class E Airspace for the following Tennessee Towns; Jackson, TN; Tri-Cities, TN Published Docket #: FAA-2016-0735 Effective date 05/26/2016 05/20/2016 This action corrects final rule published in the Federal Register of March 29, 2016, amending Class E Airspace designated as an extension at McKellar-Sipes Regional Airport, Jackson, TN, and Tri-Cities Regional Airport, Tri-Cities, TN. This action corrects the geographic coordinates for McKellar-Sipes Regional Airport. Also, the geographic coordinates for McKellar-Sipes Regional Airport in Class D airspace, Class E surface airspace, and Class E airspace extending upward from 700 feet above the surface, are updated to coincide with the FAA's aeronautical database. The airport name also is corrected in the Class E 700 feet airspace area. Additionally, Class D Airspace is added to the title.
Final Rule: Establishment of Class E Airspace; Harlan, KY Published Docket #: FAA-2016-3108 Effective date 07/21/2016 05/20/2016 This action establishes Class E Airspace at Harlan, KY, to accommodate new Area Navigation (RNAV) Global Positioning System (GPS) Standard Instrument Approach Procedures (SIAPs) serving Tucker- Guthrie Memorial Airport. Controlled airspace is necessary for the safety and management of instrument flight rules (IFR) operations at the airport. This action also updates the geographic coordinates of the airport.
Corrected Rule: Flight Simulation Training Device Qualification Standards for Extended Envelope and Adverse Weather Event Training Tasks Published Docket #: FAA-2014-0391 Effective date M/D/YYYY 05/20/2016 In FR Rule Doc. No. 2016-05860 beginning on page 18178 in the issue of March 30, 2016, make the following corrections: FAA Guidance Documents and Notices
Special Airworthiness Information Bulletins (SAIB)
SAIB: Fuel – Jet Fuel Containing Fatty Acid Methyl Ester (FAME)l Issued 05/19/2016 SAIB #: NE-09-56R2
SAIB: Engine Fuel and Control - Semi-Synthetic Jet Fuel Issued 05/19/2016 SAIB #: NE-11-56R2
Notices
Notice: Noise Exposure Map Notice for Charlotte Douglas International Airport (CLT), Charlotte, NC Published Document #: 2016-11953 Comments due M/D/YYYY 05/20/2016 The Federal Aviation Administration (FAA) announces its determination that the Noise Exposure Maps (NEMs) submitted by the City of Charlotte for Charlotte Douglas International Airport under the provisions of 49 U.S.C. 47501 et seq. (Aviation Safety and Noise Abatement Act (hereinafter referred to as “the Act”)) and 14 CFR part 150 (hereinafter referred to as “Part 150”) are in compliance with applicable requirements.
Notice: Passenger Facility Charge (PFC) Program: Eligibility of Ground Access Projects Meeting Certain Criteria Published Document #: 2016-6596 Comments due 06/17/2016 05/20/2016 The FAA is extending the comment period on its notice of proposed policy published on May 3, 2016, that proposes to amend its “Notice of Policy Regarding the Eligibility of Airport Ground Transportation Projects for Funding Under the Passenger Facility Charge (PFC) Program,” regarding the requirement for PFC funding of on-airport, rail access projects.
May 23, 2016
FAA Final rules
AD: Dassault Aviation Airplanes Published 05/23/2016 Docket #: FAA-2015-8426 Effective date 06/27/2016 The FAA is adopting a new airworthiness directive (AD) for certain Dassault Aviation Model MYSTERE-FALCON 900 airplanes, FALCON 900EX airplanes, and FALCON 2000EX airplanes. This AD was prompted by a report that during a test flight, it was found that the yaw damper on the takeoff roll can increase the Minimum Control Speed on Ground (Vmcg). This AD requires revising the airplane flight manual (AFM) to incorporate procedures for the flightcrew to check that the yaw damper is set to “off” before takeoff. We are issuing this AD to ensure that the flightcrew has procedures to set the yaw damper to “off” before takeoff, which, if activated, could result in reduced control of the airplane if one engine were to fail during takeoff.
FAA Proposed Rules
NPRM AD: Airbus Airplanes Published 05/23/2016 Docket #: FAA-2016-6671 Comments due 07/07/2016 The FAA proposes to adopt a new airworthiness directive (AD) for certain Airbus Model A300B4- 203 and A300B4-2C airplanes. This proposed AD was prompted by cracks found on pylon side panels (upper section) at rib 8. This proposed AD would require a detailed inspection for crack indications of the pylon side panels, a high frequency eddy current (HFEC) inspection to confirm any crack indications, modification of the pylon side panels, and repetitive inspections and repair if necessary. We are proposing this AD to detect and correct cracking of the pylon side panels. Such cracking could result in pylon structural failure and in-flight loss of an engine.
FAA Guidance Documents and Notices
Meeting: Forty-Fourth Meeting: RTCA Special Committee 206 (SC-206) Aeronautical Information and Meteorological Data Link Services Meeting date 05/23/2016 Meeting time 8:30am – 5:00pm Time zone (EST/etc.) The FAA is issuing this notice to advise the public of the Forty-Fourth RTCA Special Committee 206 meeting.
Meeting: Ninth Meeting: RTCA Special Committee 230 (SC-230) Airborne Weather Detection Systems (Joint With WG-95 Inflight Ice Long Range Awareness Systems' Fourth Meeting) Meeting date 05/23/2016 Meeting time 9:00am – 5:00pm Time zone (EST/etc.) The FAA is issuing this notice to advise the public of the Ninth RTCA Special Committee 230 meeting.
Meeting: Twenty-Third Meeting: RTCA Special Committee 225 (SC-225) Rechargeable Lithium Battery and Battery Systems Meeting date 05/23/2016 Meeting time 9:00am – 1:00pm Time zone (EST/etc.) The FAA is issuing this notice to advise the public of the Twenty-Third RTCA Special Committee 225 meeting.
May 24, 2016
FAA Final rules
Final Rule: Acceptance Criteria for Portable Oxygen Concentrators Used On Board Aircraft Published Docket #: FAA-2014-0554 Effective date 06/23/2016 05/24/2016 This final rule 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. This 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, this rulemaking will eliminate redundant operational requirements and paperwork requirements related to the physician's statement. As a result, this rulemaking will reduce burdens for POC manufacturers, passengers who use POCs while traveling, and affected aircraft operators. This final rule also makes 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.
Final Rule: Change of Newark Liberty International Airport (EWR) Designation; Notification of Availability of Final CATEX Declaration and Supporting Material Published Docket #: FAA-2008-0221 Effective date 05/24/2016 05/24/2016 This action announces the placement in the docket of the final documented categorical exclusion (the signed CATEX declaration and final Attachment A: Environmental Review of Proposed Change of Operating Authorization Requirement at Newark Liberty International Airport) for the redesignation of Newark Liberty International Airport (EWR) as a Level 2 schedule-facilitated airport.
Final Rule: Operating Limitations at John F. Kennedy International Airport Published Docket #: FAA-2007-29320 Effective date 05/24/2016 05/24/2016 This action extends the Order Limiting Operations at John F. Kennedy International Airport (JFK) published on January 18, 2008, and most recently extended March 26, 2014. The Order remains effective until October 27, 2018.
Final Rule: Standard Instrument Approach Procedures, and Takeoff Minimums and Obstacle Departure Procedures; Miscellaneous Amendments Published Docket #: FAA-2016-11956 Effective date 05/24/2016 05/24/2016 This rule amends, suspends, or removes Standard Instrument Approach Procedures (SIAPs) and associated Takeoff Minimums and Obstacle Departure Procedures for operations at certain airports. These regulatory actions are needed because of the adoption of new or revised criteria, or because of changes occurring in the National Airspace System, such as the commissioning of new navigational facilities, adding new obstacles, or changing air traffic requirements. These changes are designed to provide for the safe and efficient use of the navigable airspace and to promote safe flight operations under instrument flight rules at the affected airports.
Final Rule: Standard Instrument Approach Procedures, and Takeoff Minimums and Obstacle Departure Procedures; Miscellaneous Amendments Published Docket #: FAA-2016-11955 Effective date 05/24/2016 05/24/2016 This rule establishes, amends, suspends, or removes Standard Instrument Approach Procedures (SIAPs) and associated Takeoff Minimums and Obstacle Departure Procedures (ODPs) for operations at certain airports. These regulatory actions are needed because of the adoption of new or revised criteria, or because of changes occurring in the National Airspace System, such as the commissioning of new navigational facilities, adding new obstacles, or changing air traffic requirements. These changes are designed to provide safe and efficient use of the navigable airspace and to promote safe flight operations under instrument flight rules at the affected airports.
FAA Proposed Rules
NPRM: Proposed Establishment of Class E Airspace; Park River, ND Published Docket #: FAA-2016-5856 Comments due 07/08/2016 05/24/2016 This action proposes to establish Class E airspace extending upward from 700 feet above the surface at Park River Airport—WC Skjerven Field, Park River, ND. Controlled airspace is necessary to accommodate new Standard Instrument Approach Procedures developed at Park River Airport— WC Skjerven Field, for the safety and management of Instrument Flight Rules (IFR) operations at the airport. FAA Guidance Documents and Notices
Flight Standards Information Management System (FSIMS)
FSIMS: ED 4.6.1 135E AW Avionics Special Emphasis Programs Issued 05/20/2016 Determine if the CH will be able to; (1) Comply with regulations; (2) Provide aircraft maintenance program standards for avionics special emphasis programs.
FSIMS: EP 4.6.1 135C AW Avionics Special Emphasis Programs Issued 05/20/2016 Determine; (1) If the CH followed the accepted or approved process; (2) If the CH provided aircraft maintenance program standards for avionics special emphasis programs.
FSIMS: ED 4.6.1 135C AW Avionics Special Emphasis Programs Issued 05/20/2016 Determine if the CH will be able to; (1) Comply with regulations; (2) Provide aircraft maintenance program standards for avionics special emphasis programs.
FSIMS: ED 4.6.1 135B AW Avionics Special Emphasis Programs Issued 05/20/2016 Determine if the CH will be able to; (1) Comply with regulations; (2) Provide aircraft maintenance program standards for avionics special emphasis programs.
FSIMS: EP 4.6.1 121A AW Avionics Special Emphasis Programs Issued 05/20/2016 Determine; (1) If the CH followed the accepted or approved process; (2) If the CH provided aircraft maintenance program standards for avionics special emphasis programs.
FSIMS: EP 4.6.1 135B AW Avionics Special Emphasis Programs Issued 05/20/2016 Determine; (1) If the CH followed the accepted or approved process; (2) If the CH provided aircraft maintenance program standards for avionics special emphasis programs.
FSIMS: EP 4.6.1 135D AW Avionics Special Emphasis Programs Issued 05/20/2016 Determine; (1) If the CH followed the accepted or approved process; (2) If the CH provided aircraft maintenance program standards for avionics special emphasis programs.
FSIMS: ED 4.6.1 135D AW Avionics Special Emphasis Programs Issued 05/20/2016 Determine if the CH will be able to; (1) Comply with regulations; (2) Provide aircraft maintenance program standards for avionics special emphasis programs.
FSIMS: EP 4.6.2 121A AW Maintenance Special Emphasis Programs Issued 05/20/2016 Determine; (1) If the CH followed the accepted or approved process; (2) If the CH provided aircraft maintenance program standards for maintenance special emphasis programs.
FSIMS: ED 4.6.1 121A AW Avionics Special Emphasis Programs Issued 05/20/2016 Determine if the CH will be able to; (1) Comply with regulations; (2) Provide aircraft maintenance program standards for avionics special emphasis programs.
FSIMS: EP 4.6.1 135E AW Avionics Special Emphasis Programs Issued 05/20/2016 Determine; (1) If the CH followed the accepted or approved process; (2) If the CH provided aircraft maintenance program standards for avionics special emphasis programs.
Notices
Notice: Petition for Exemption; Summary of Petition Received; Columbia Helicopters, Inc. Published Document #: 2016-12128 Comments due 06/13/2016 05/24/2016 This notice contains a summary of a petition seeking relief from specified requirements of title 14 of the Code of Federal Regulations. The purpose of this notice is to improve the public's awareness of, and participation in, the FAA's exemption process. 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.
Meeting: Forty-First Meeting: RTCA Special Committee 224 (SC-224) Airport Security Access Control Systems Meeting date 06/16/2016 Meeting time 10:00am – 1:00pm Time zone (EST/etc.) The FAA is issuing this notice to advise the public of the Forty-First RTCA Special Committee 224 meeting.
Meeting: Fourteenth Meeting: RTCA Tactical Operations Committee (TOC) Meeting date 06/23/2016 Meeting time 9:00am – 4:00pm Time zone (EST/etc.) The FAA is issuing this notice to advise the public of the Fourteenth RTCA Tactical Operations Committee meeting.
Meeting: RTCA Program Management Committee (PMC) Meeting date 06/21/2016 Meeting time 8:30am – 4:30pm Time zone (EST/etc.) The FAA is issuing this notice to advise the public of the RTCA Program Management Committee meeting.
Meeting: Twenty-Sixth Meeting: RTCA Special Committee 217 (SC-217) Aeronautical Databases (Joint With EUROCAE WG-44 Aeronautical Databases) Meeting date 07/18/2016 Meeting time 9:00am – 5:00pm Time zone (EST/etc.) The FAA is issuing this notice to advise the public of the Twenty-Sixth RTCA Special Committee 217 meeting.
May 25, 2016
FAA Final rules
Final Rule: Operating Limitations at New York Laguardia Airport Published Docket #: FAA-2006-25755 Effective date 05/25/2016 05/25/2016 This action extends the Order Limiting Operations at New York LaGuardia Airport (LGA) published on December 27, 2006, and most recently extended March 27, 2014. The Order remains effective until October 27, 2018.
FAA Guidance Documents and Notices
FAA Final Policies
Final Policy: http://rgl.faa.gov/Regulatory_and_Guidance_Library/rgPolicy.nsf/0/16BC9DD85F8D41FD86257FBC0 05822FD?OpenDocument Issued 04/21/2016 Policy #: Air100_16-110-GM09 The purpose is to notify all aircraft certification field offices that we have created a generic FAA form 8110-31, Type Inspection Report (TIR).
Final Policy: Revised FAA Form 8110-26, Supplemental Type Inspection Report (STIR) Issued 04/21/2016 Policy #: Air100_16-110-GM10 This change transmits revised pages to order 8110.4C, Type Certification.
Final Policy: Revised Federal Aviation Administration (FAA) Form 8110-1, Type Inspection Authorization (TIA)*** Issued 05/19/2016 Policy #: Air100_16-110-GM10 The purpose is to notify all aircraft certification offices that we have revised FAA Form 8110-1, Type Inspection Authorization, (TIA).
Flight Standards Information Management System (FSIMS)
FSIMS: Douglas-DC-4, C54-DC, C54A-DC, C54B-DC, C54D-DC, D54E-DC, G54G-DC, Rev. 4 Date*** Issued 05/25/2016 Master Minumum Equipment List (MMEL) Orders
Order: Delegation of Authority – Office of Finance and Management*** Issued 05/25/2016 Document FN: 1100-168 Comments due M/D/YYYY This document's content can only be accessed from within the FAA network. The document's Office of Primary Responsibility (OPR) is AFN-1.
May 26, 2016 Press releases
FAA, NATCA ANNOUNCE TENTATIVE AGREEMENT ON NEW COLLECTIVE BARGAINING AGREEMENT The Federal Aviation Administration (FAA) and its largest union, the National Air Traffic Controllers Association, AFL-CIO (NATCA) announced today they have reached a tentative agreement on a new collective bargaining agreement (CBA) covering the air traffic control specialists assigned to the terminal and en route options, traffic management coordinators/specialists, air traffic controllers assigned to the flight service option, and Notice to Airmen specialists (NOTAMS).
FAA Regulations
FAA Final rules
AD: Airbus Airplanes Published Docket #: FAA-2015-7528 Effective date 06/30/2016 05/26/2016 We are adopting a new airworthiness directive (AD) for all Airbus 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); and Model A310 series airplanes. This AD was prompted by reports of premature aging of certain passenger chemical oxygen generators that resulted in the generators failing to activate. This AD requires an inspection to determine if certain passenger chemical oxygen generators are installed and replacement of affected passenger chemical oxygen generators. We are issuing this AD to prevent failure of the passenger chemical oxygen generator to activate and consequently not deliver oxygen during an emergency, possibly resulting in injury to airplane occupants.
AD: Airbus Airplanes Published 05/26/2016 Docket #: FAA-2015-4815 Effective date 06/30/2016 We are superseding Airworthiness Directive (AD) 2015-03-06 for all Airbus Model A330-200, A330- 200 Freighter, A330-300, A340-200, A340-300, A340-500, and A340-600 series airplanes. AD 2015- 03-06 required repetitive inspections of the left-hand (LH) and right-hand (RH) wing main landing gear (MLG) rib 6 aft bearing lugs (forward and aft) to detect any cracks on the two lugs, and replacement if necessary. This new AD requires reduction of certain compliance times. This AD was prompted by reports of additional cracking of the MLG rib 6 aft bearing lugs. We are issuing this AD to detect and correct cracking of the MLG rib 6 aft bearing lugs, which could result in collapse of the MLG upon landing.
AD: Bombardier, Inc. Airplanes Published 05/26/2016 Docket #: FAA-2016-6892 Effective date 06/10/2016 We are adopting a new airworthiness directive (AD) for all Bombardier, Inc. Model CL-600-2C10 (Regional Jet Series 700, 701, & 702) airplanes; Model CL-600-2D15 (Regional Jet Series 705) airplanes; Model CL-600-2D24 (Regional Jet Series 900) airplanes; and Model CL-600-2E25 (Regional Jet Series 1000) airplanes. This AD requires a detailed visual inspection of the upper and lower engine pylons for protruding, loose, or missing fasteners; and repair, including applicable related investigative and corrective actions, if necessary. This AD was prompted by reports of loose or missing Hi-Lite fasteners on the upper and lower engine pylon structure common to the upper and lower pylon skin panels and engine thrust fitting. We are issuing this AD to detect and correct protruding, loose, or missing fasteners, which could result in structural failure of the engine pylons.
AD: Bombardier, Inc. Airplanes Published 05/26/2016 Docket #: FAA-2015-2457 Effective date 06/30/2016 We are adopting a new airworthiness directive (AD) for certain Bombardier, Inc. Model CL-600- 2C10 (Regional Jet Series 700, 701, & 702) airplanes, Model CL-600-2D15 (Regional Jet Series 705) airplanes, and Model CL-600-2D24 (Regional Jet Series 900) airplanes. This AD was prompted by a report indicating that some operators have inadvertently removed the existing insulation blankets from the upper wing box area. This AD requires inspecting for and replacing missing insulation blankets in the upper wing box area. We are issuing this AD to detect and replace missing insulation blankets from the upper wing box area, which could result in inadequate thermal protection to prevent fuel ignition in the event of an undetected bleed-air leak due to a cracked or ruptured bleed-air duct.
AD: Fokker Services B.V. Airplanes Published 05/26/2015 Docket #: FAA-2015-8430 Effective date 06/30/2016 We are adopting a new airworthiness directive (AD) for all Fokker Services B.V. Model F.28 Mark 0070 and 0100 airplanes. This AD was prompted by accomplishment of a taxi-out checklist which revealed that the elevator movement was partially obstructed due to rotation of the flight control lock adjuster bracket. This AD requires a one-time inspection of the elevator tension control regulator for discrepancies, and corrective actions if necessary. We are issuing this AD to detect and correct discrepancies of the elevator tension control regulators. Such a condition could result in jamming of the elevator mechanism and consequent reduced controllability of the airplane.
FAA Proposed Rules
NPRM AD: Airbus Airplanes Published Docket #: FAA-2016-6883 Comments due 07/11/2016 05/26/2016 We propose to adopt a new airworthiness directive (AD) for certain Airbus Model A318-112 airplanes, A319-111, -112, -115, -132, and -133 airplanes, A320-214, -232, and -233 airplanes, and A321-211, -212, -213, -231, and -232 airplanes. This proposed AD was prompted by a quality control review on the final assembly line, which determined that the wrong aluminum alloy was used to manufacture several structural parts. This proposed AD would require a one-time eddy current conductivity measurements of certain cabin and cargo compartment structural parts to determine if an incorrect aluminum alloy was used, and replacement if necessary. We are proposing this AD to detect and replace structural parts made of incorrect aluminum alloy. This condition could result in reduced structural integrity of the airplane.
FAA Guidance Documents and Notices
FAA Final Advisory Circulars
AC: Portable Oxygen Concentrators Issued 05/24/2016 Document AFS: AC 120-95A This advisory circular (AC) explains Federal Aviation Administration (FAA) requirements for the use of portable oxygen concentrators (POC) on board aircraft. We intend for operators to use this AC as a resource during the development, implementation, and revision of standard operating procedures (SOP) and training programs regarding the use of POCs on board aircraft to increase the accessibility of air travel by passengers with disabilities.
Notice
Notice: Proposed Inlet Barrier Filter for Rotorcraft Policy Statement Published 05/26/2016 Docket #: FAA-2016-6691 Meeting date: 07/07/2016 The FAA is announcing a public meeting to gather additional technical input on the subject of installing an engine inlet barrier filter (IBF) on rotorcraft. Input gathered will aid in developing FAA guidance for evaluating engine IBFs installed on rotorcraft. Prior to the public meeting, the FAA previously sought public comments regarding the guidance online.
May 27, 2016 FAA Regulations
FAA Final rules
AD: Viking Air Limited Airplanes 05/27/2016 Docket #: FAA-2016-6628 Effective date 05/31/2016 The FAA is correcting an airworthiness directive (AD) that published in the Federal Register. That AD applies to Viking Air Limited Model DHC-3 airplanes that are modified with the Baron Short Take Off and Landing (STOL) kit (Supplemental Type Certificate SA94-114 or SA 00287NY). The Code of Federal Regulations reference for records maintenance cited in last sentence in paragraph (f) is incorrect. This document corrects that error. In all other respects, the original document remains the same; however we are publishing the entire rule in the Federal Register.
FAA Proposed Rules
NPRM AD: Robinson Helicopter Company Helicopters Published Docket #: FAA-2016-0733 Comments due 07/26/2016 05/27/2016 The FAA proposes to adopt a new airworthiness directive (AD) for Robinson Helicopter Company (Robinson) Model R44, R44 II, and R66 helicopters. This proposed AD would require a visual inspection of the main rotor blade (MRB) and either removing or altering it. This proposed AD is prompted by a report that a fatigue crack was found at an MRB's trailing edge and a determination that some MRBs may have reduced blade thickness due to blending out corrosion. The proposed actions are intended to prevent an MRB fatigue crack, which could lead to MRB failure and subsequent loss of helicopter control.
NPRM AD: The Boeing Company Airplanes Published Docket #: FAA-2013-0797 Comments due 07/11/2016 05/27/2016 The FAA is revising an earlier proposed airworthiness directive (AD) for certain The Boeing Company Model 767-300 and 767-300F series airplanes. The NPRM proposed to require modification and installation of components in the main equipment center. For certain other airplanes, the NPRM proposed to require modification, replacement, and installation of flight deck air relief system (FDARS) components. The NPRM was prompted by reports of malfunctions in the flight deck display units, which resulted in blanking, blurring, or loss of color on the display. This action revises the NPRM by revising the applicability; adding certain modifications; and clarifying certain requirements. We are proposing this supplemental NPRM (SNPRM) to prevent malfunctions of the flight deck display units, which could affect the ability of the flightcrew to read the displays for airplane attitude, altitude, or airspeed, and consequently reduce the ability of the flightcrew to maintain control of the airplane. Since these actions impose an additional burden over that proposed in the NPRM, we are reopening the comment period to allow the public the chance to comment on these proposed changes. FAA Proposed Special Conditions
SC: Bell Helicopter Textron, Inc. (BHTI), Model 525 Helicopters; Interaction of Systems and Structures Published M/D/YYYY Docket #: FAA-####-#### Effective date M/D/YYYY The FAA proposes special conditions for the BHTI Model 525 helicopter. This helicopter will have a novel or unusual design feature associated with fly-by-wire flight control system (FBW FCS) functions that affect the structural integrity of the rotorcraft. The applicable airworthiness regulations do not contain adequate or appropriate safety standards for this design feature. These proposed 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.
FAA Guidance Documents and Notices
Orders
Order: Location Identifiers Issued 05/26/2016 Document JO: 7350.9F The current identifiers and codes in the United States and Canada air traffic control systems are listed in this order. It contains guidelines for requesting location identifiers, name-codes, and procedure codes. Also, a brief explanation of assignment principles is included.
Notices
Notice: Notice of Request To Release Airport Property Published Document #: 2016-12635 Comments due 06/27/2016 05/27/2016 Notice Of Intent To Rule On Request To Release Airport Property At The Eastern Iowa Airport, Cedar Rapids, Iowa.
May 31, 2016
Press releases
FAA, NATCA ANNOUNCE TENTATIVE AGREEMENT ON NEW COLLECTIVE BARGAINING AGREEMENT The Federal Aviation Administration (FAA) and its largest union, the National Air Traffic Controllers Association, AFL-CIO (NATCA) announced today they have reached a tentative agreement on a new collective bargaining agreement (CBA) covering the air traffic control specialists assigned to the terminal and en route options, traffic management coordinators/specialists, air traffic controllers assigned to the flight service option, and Notice to Airmen specialists (NOTAMS).
FAA Regulations
FAA Final rules
AD: Turbomeca S.A. Turboshaft Engines Published 05/31/2016 Docket #: FAA-2016-2859 Effective date 07/05/2016 The FAA is adopting a new airworthiness directive (AD) for Turbomeca S.A. Arriel 1D and 1D1 turboshaft engines with a pre-modification (mod) TU357 gas generator module (M03), installed. This AD requires removing the pre-modification (mod) TU357 gas generator module (M03) and replacing with a part eligible for installation. This AD was prompted by reports of divergent rubbing between the piston shaft small diameter labyrinth and the rear bearing support. We are issuing this AD to prevent failure of the labyrinth seal and engine, in-flight shutdown, and loss of control of the helicopter.
Final Rule: Establishment of Class E Airspace; Lisbon, ND Published 05/31/2016 Docket #: FAA-2015-5800 Effective date 09/15/2016 This action establishes Class E airspace in Lisbon, ND. Controlled airspace is necessary to accommodate new Area Navigation (RNAV) Standard Instrument Approach Procedures at Lisbon Municipal Airport. The FAA is taking this action to enhance the safety and management of Instrument Flight Rule (IFR) operations at the airport.
FAA Proposed Rules
NPRM AD: Airbus Airplanes Published 05/31/2016 Docket #: FAA-2016-6894 Comments due 07/15/2016 The FAA proposes to adopt a new airworthiness directive (AD) for certain Airbus Model A300 F4- 600R series airplanes. This proposed AD was prompted by a report of two adjacent frame forks that were found cracked on the aft lower deck cargo door (LDCD) of two Model A300-600F4 airplanes during scheduled maintenance. This proposed AD would require repetitive high frequency eddy current (HFEC) inspections of the aft LDCD frame forks; a one-time check of the LDCD clearances; and a one-time detailed visual inspection of hooks, eccentric bushes, and x-stops; and corrective actions if necessary. We are proposing this AD to detect and correct cracked or ruptured aft LDCD frames, which could allow loads to be transferred to the remaining structural elements. This condition could lead to the rupture of one or more vertical aft LDCD frames, which could result in reduced structural integrity of the aft LDCD.
NPRM AD: Airbus Airplanes Published 05/31/2016 Docket #: FAA-2016-6896 Comments due 07/15/2016 The FAA proposes to adopt a new airworthiness directive (AD) for all Airbus Model A318-111, and - 112 airplanes, Model A319-111, -112, -113, -114, and -115 airplanes, Model A320-211, -212 and - 214 airplanes, and Model A321-111, -112, -211, -212, and -213 airplanes. This proposed AD was prompted by a report of a production quality deficiency on the inner retainer installed on link assemblies of the engine mount, which could result in failure of the retainer. This proposed AD would require an inspection for, and replacement of, all non-conforming aft engine mount retainers. We are proposing this AD to detect and correct non-conforming retainers of the aft engine mount. This condition could result in the loss of the locking feature of the nuts of the inner and outer pins; loss of the pins will result in the aft mount engine link no longer being secured to the aft engine mount, possibly resulting in damage to the airplane and injury to persons on the ground.
FAA Guidance Documents and Notices
FAA Legal Interpretations
Legal Interpretation: Nkugba - (2016) Legal Interpretation Issued 05/27/2016 Regulation/Order 14:91.205 This letter responds to a request for legal interpretation regarding the type of clock required while flying under Instrument Flight Rules (IFR).
Legal Interpretation: Tu-Civic Helicopters - (2016) Legal Interpretation Issued 05/27/2016 Regulation/Order 14 CFR:119.63 This letter responds to questions regarding compliance with Recency of Operations requirements.
Flight Standards Service Information for Operators (InFO)
InFO: InFO 16004, Datalink Communications (DLC) Recording Requirements – Clarification Issued 02/17/2016 InFO #: 16004 Comments due M/D/YYYY This clarifies how the FAA defines the phrase “install datalink communication (DLC) equipment” for the purposes of the DLC recording requirements.
Notices
Meeting: Air Traffic Procedures Advisory Committee Meeting date 05/31/2016 Meeting time 1:00pm – 4:00pm Time zone (EST/etc.) The FAA is issuing this notice to advise the public that a meeting of the Federal Aviation Administration Air Traffic Procedures Advisory Committee (ATPAC) will be held to review present air traffic control procedures and practices for standardization, revision, clarification, and upgrading of terminology and procedures.