Federal Aviation Administration 2016 – Federal Register Recent Federal Regulation Documents

Results 1,051 - 1,100 of 1,608
Airworthiness Directives; Schempp-Hirth Flugzeugbau GmbH Gliders
Document Number: 2016-09435
Type: Proposed Rule
Date: 2016-04-27
Agency: Federal Aviation Administration, Department of Transportation
We propose to adopt a new airworthiness directive (AD) for Schempp-Hirth Flugzeugbau GmbH Models Discus-2a, Discus-2b, Discus-2c, Discus 2cT, Ventus-2a, and Ventus-2b gliders. This proposed AD results from mandatory continuing airworthiness information (MCAI) originated 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 insufficient overlap of the airbrake panels. We are issuing this proposed AD to require actions to address the unsafe condition on these products.
Agency Information Collection Activities: Requests for Comments; Clearance of Renewed Approval of Information Collection: Aviation Maintenance Technical Schools
Document Number: 2016-09696
Type: Notice
Date: 2016-04-26
Agency: Federal Aviation Administration, Department of Transportation
In accordance with the Paperwork Reduction Act of 1995, FAA invites public comments about our intention to request the Office of Management and Budget (OMB) approval to renew an information collection. The information collected is needed to determine applicant eligibility and compliance for certification of Civil Aviation mechanics and operation of aviation mechanic schools.
Agency Information Collection Activities: Requests for Comments; Clearance of Renewed Approval of Information Collection: Human Space Flight Requirements for Crew and Space Flight Participants
Document Number: 2016-09693
Type: Notice
Date: 2016-04-26
Agency: Federal Aviation Administration, Department of Transportation
In accordance with the Paperwork Reduction Act of 1995, FAA invites public comments about our intention to request the Office of Management and Budget (OMB) approval to renew an information collection. The FAA uses the information collected related to public safety to ensure that a launch or reentry operation involving a human on board a vehicle will meet the risk criteria and requirements with regard to ensuring public safety.
Membership in the National Parks Overflights Advisory Group Aviation Rulemaking Committee
Document Number: 2016-09690
Type: Notice
Date: 2016-04-26
Agency: Federal Aviation Administration, Department of Transportation
By Federal Register notice (See 81 FR 290, January 5, 2016) the National Park Service (NPS) and the Federal Aviation Administration (FAA) invited interested persons to apply to fill two upcoming openings on the National Parks Overflights Advisory Group (NPOAG) Aviation Rulemaking Committee (ARC). The notice invited interested persons to apply to fill future openings to represent air tour operator concerns and environmental interests. This notice informs the public of the person selected to fill the air tour operator future vacancy. No selection has been made for the vacancy representing environmental interests so this notice also invites persons interested in serving on the ARC to apply for the upcoming opening for this seat.
Delegation of Authority
Document Number: 2016-09656
Type: Notice
Date: 2016-04-26
Agency: Federal Aviation Administration, Department of Transportation
The FAA is giving notice of a new delegation of authority from the Administrator to the Chief Counsel and to the Director of the Office of Adjudication regarding civil penalty actions under 14 CFR part 13 subpart G. The delegation was set forth in a memorandum signed by the Administrator dated March 28, 2016. The FAA is publishing the text of the delegation, so that it is available to interested parties. This delegation supersedes and replaces a previous delegation of authority by the Administrator by memorandum issued on October 27, 1992 and published in the Federal Register on December 9, 1992. 57 FR 58280; December 9, 1992.
Airworthiness Directives; Dassault Aviation
Document Number: 2016-08952
Type: Rule
Date: 2016-04-26
Agency: Federal Aviation Administration, Department of Transportation
We are adopting a new airworthiness directive (AD) for all Dassault Aviation Model FALCON 7X airplanes. This AD was prompted by reports of multiple cases of ram air turbine (RAT) blade damage. This AD requires deployment of the RAT, replacement of the RAT placard with a new RAT placard, and re-identification of the RAT. We are issuing this AD to prevent blade damage to the RAT, which could prevent RAT deployment in flight during an emergency, possibly resulting in reduced control of the airplane.
Airworthiness Directives; Airbus Airplanes
Document Number: 2016-08951
Type: Rule
Date: 2016-04-26
Agency: Federal Aviation Administration, Department of Transportation
We are superseding Airworthiness Directive (AD) 2014-03-14 for all Airbus Model A330-200 and -300 series airplanes, and Model A340- 200, -300, -500, and -600 series airplanes. AD 2014-03-14 required removing bulb-type maintenance lights; installing a drain mast on certain airplanes; and installing muffs on connecting bleed elements on certain airplanes. For certain Model A340-200 and -300 series airplanes, this new AD also requires replacing certain insulation sleeves with new insulation sleeves. This AD results from fuel system reviews conducted by the airplane manufacturer. We are issuing this AD to prevent ignition sources inside fuel tanks, which, in combination with flammable fuel vapors, could result in fuel tank explosions and consequent loss of the airplane.
Airworthiness Directives; Kaman Aerospace Corporation
Document Number: 2016-09434
Type: Rule
Date: 2016-04-25
Agency: Federal Aviation Administration, Department of Transportation
We are adopting a new airworthiness directive (AD) for Kaman Aerospace Corporation (Kaman) Model K-1200 helicopters. This AD requires revising the ``Flight LimitationsNO LOAD'' and ``Flight Limitations LOAD'' sections of the rotorcraft flight manual (RFM). This AD was prompted by a report of certain flight maneuvers that may lead to main rotor (M/R) blade to opposing hub contact. These actions are intended to prevent damage to the M/R flight controls and subsequent loss of control of the helicopter.
Airworthiness Directives; Bell Helicopter Textron Canada Helicopters
Document Number: 2016-09236
Type: Rule
Date: 2016-04-25
Agency: Federal Aviation Administration, Department of Transportation
We are superseding Airworthiness Directive (AD) 2010-19-51 for Bell Helicopter Textron Canada (Bell) Model 222, 222B, 222U, 230, and 430 helicopters. AD 2010-19-51 required inspecting parts of the main rotor hydraulic servo actuator (servo actuator) for certain conditions and replacing any unairworthy parts before further flight. This new AD requires installing a servo actuator with a new stainless steel piston rod. This AD was prompted by a collective servo actuator malfunction. We are issuing this AD to detect corrosion on a piston rod, which could result in failure of the servo actuator and consequent loss of helicopter control.
Notice of Opportunity for Public Comment on a Property Swap at Augusta State Airport in Augusta, ME
Document Number: 2016-09428
Type: Notice
Date: 2016-04-22
Agency: Federal Aviation Administration, Department of Transportation
Under the provisions of Title 49, U.S.C. Section 47153(d), notice is being given that the FAA is considering a property swap at Augusta State Airport in Augusta, ME. The purpose of the land swap between the State of Maine (Airport Sponsor) and Dragon Products Company, Inc., to resolve a compliance issue. The 13 acre parcel is at the bottom of the slope on the departure end of RW 35, and lies approximately 300' below the elevation of the end of the Runway. This portion of land is not considered useable for aeronautical purposes based upon its location and elevation. The parcel currently contains a pile of hardened concrete spoils placed there by Dragon Products Company, Inc. The solutions to mitigate this situation include removal of the spoils pile, which would be cost prohibitive, or release the land to Dragon Products Company, Inc. as part of an equal value parcel exchange. The State of Maine determined the parcel exchange as the best alternative. The parcel that Dragon has offered for exchange abuts the Augusta State Airport property on one side and City of Augusta property on another. The Offered Parcel would be advantageous to the State of Maine for potential non-aeronautical airport revenue generating purposes. The State of Maine would retain all avigation rights over both parcels.
Special Conditions: Bombardier Inc. Model BD-700-2A12 and BD-700-2A13 Airplanes; Airplane Electronic System Security Protection From Unauthorized External Access
Document Number: 2016-09336
Type: Rule
Date: 2016-04-22
Agency: Federal Aviation Administration, Department of Transportation
These special conditions are issued for the Bombardier Inc. Model BD-700-2A12 and BD-700-2A13 airplanes. These airplanes will have a digital-systems network architecture composed of several connected networks that may allow access to or by external computer systems and networks, and may result in airplane systems-security vulnerabilities. The applicable airworthiness regulations do not contain adequate or appropriate safety standards for this design feature. These special conditions contain the additional safety standards that the Administrator considers necessary to establish a level of safety equivalent to that established by the existing airworthiness standards.
Special Conditions: Gulfstream Aerospace Corporation Model GVII-G500 Airplanes; Airplane Electronic System Security Protection From Unauthorized External Access
Document Number: 2016-09335
Type: Rule
Date: 2016-04-22
Agency: Federal Aviation Administration, Department of Transportation
These special conditions are issued for the Gulfstream Aerospace Corporation (Gulfstream) Model GVII-G500 airplane. These airplanes will have a digital-systems network architecture composed of several connected networks that may allow access to or by external computer systems and networks, and may result in airplane electronic system- security vulnerabilities. The applicable airworthiness regulations do not contain adequate or appropriate safety standards for this design feature. These special conditions contain the additional safety standards that the Administrator considers necessary to establish a level of safety equivalent to that established by the existing airworthiness standards.
Special Conditions: Gulfstream Aerospace Corporation Model GVII-G500 Airplanes, Pilot Compartment View Requirements With an Enhanced Flight Vision System
Document Number: 2016-09334
Type: Rule
Date: 2016-04-22
Agency: Federal Aviation Administration, Department of Transportation
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 when compared to the state of technology envisioned in the airworthiness standards for transport category airplanes. This design feature is an enhanced flight vision system (EFVS) that includes a head-up display (HUD) capable of displaying forward-looking infrared (FLIR) imagery, intended to be used for instrument approaches under provisions of Title 14, Code of Federal Regulations (14 CFR) 91.175(l) and (m). The applicable airworthiness regulations do not contain adequate or appropriate safety standards for this design feature. These special conditions contain the additional safety standards that the Administrator considers necessary to establish a level of safety equivalent to that established by the existing airworthiness standards.
Special Conditions: Dassault Aviation Model Falcon 5X Airplane; Use of Automatic Power Reserve (APR), an Automatic Takeoff Thrust Control System (ATTCS) for Go-Around Performance Credit
Document Number: 2016-09333
Type: Rule
Date: 2016-04-22
Agency: Federal Aviation Administration, Department of Transportation
These special conditions are issued for the Dassault Aviation (Dassault) Model Falcon 5X airplane. This airplane will have a novel or unusual design feature associated with go-around performance credit when using an automatic takeoff thrust-control system. The applicable airworthiness regulations do not contain adequate or appropriate safety standards for this design feature. These special conditions contain the additional safety standards that the Administrator considers necessary to establish a level of safety equivalent to that established by the existing airworthiness standards.
Petition for Exemption; Summary of Petition Received; Precisionhawk
Document Number: 2016-09332
Type: Notice
Date: 2016-04-22
Agency: Federal Aviation Administration, Department of Transportation
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.
Petition for Exemption; Summary of Petition Received; Rotorcraft Leasing Co.
Document Number: 2016-09331
Type: Notice
Date: 2016-04-22
Agency: Federal Aviation Administration, Department of Transportation
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.
Petition for Exemption; Summary of Petition Received; Delta Air Lines Inc.
Document Number: 2016-09330
Type: Notice
Date: 2016-04-22
Agency: Federal Aviation Administration, Department of Transportation
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.
Petition for Exemption; Summary of Petition Received; William Nelson
Document Number: 2016-09329
Type: Notice
Date: 2016-04-22
Agency: Federal Aviation Administration, Department of Transportation
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.
Petition for Exemption; Summary of Petition Received; Airlines for America
Document Number: 2016-09327
Type: Notice
Date: 2016-04-22
Agency: Federal Aviation Administration, Department of Transportation
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.
Petition for Exemption; Summary of Petition Received; Delta Air Lines, Inc.
Document Number: 2016-09325
Type: Notice
Date: 2016-04-22
Agency: Federal Aviation Administration, Department of Transportation
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.
Special Conditions: Gulfstream Aerospace Corporation, Gulfstream GVI Airplane; Non-Rechargeable Lithium Battery Installations
Document Number: 2016-09311
Type: Rule
Date: 2016-04-22
Agency: Federal Aviation Administration, Department of Transportation
These special conditions are issued for the Gulfstream Aerospace Corporation (Gulfstream) GVI airplane. This airplane will have a novel or unusual design feature when compared to the state of technology envisioned in the airworthiness standards for transport- category airplanes. This design feature is non-rechargeable lithium 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.
Proposed Amendment of Class E Airspace, Truckee, CA
Document Number: 2016-09300
Type: Proposed Rule
Date: 2016-04-22
Agency: Federal Aviation Administration, Department of Transportation
This supplemental notice of proposed rulemaking would establish Class E surface area airspace within a 4.2-mile radius of Truckee-Tahoe Airport, Truckee, CA, to increase safety and enhance existing instrument flight rules (IFR) procedures in the immediate vicinity of Truckee-Tahoe Airport, Truckee, CA. In an NPRM published in the Federal Register on December 18, 2015, the FAA proposed to amend Class E airspace extending upward from 700 feet above the surface at Truckee-Tahoe Airport. The FAA concurs with a comment received regarding the proposal, and finds establishing Class E surface area airspace along with the proposed Class E airspace modification is warranted for the safety and management of IFR operations.
Airworthiness Directives; Airbus Helicopters Deutschland GmbH Helicopters
Document Number: 2016-09237
Type: Proposed Rule
Date: 2016-04-22
Agency: Federal Aviation Administration, Department of Transportation
We propose to adopt a new airworthiness directive (AD) for certain Airbus Helicopters Deutschland GmbH (Airbus Helicopters) Model MBB-BK 117 C-2 helicopters. This proposed AD would require inspecting each terminal lug and replacing any lug that has discoloration, corrosion, incorrect crimping, or incorrect installation. This proposed AD is prompted by the discovery that terminal lugs with incorrect crimping may have been installed on these helicopters. The proposed actions are intended to detect incorrectly installed or crimped terminal lugs and prevent contact resistance and reduced gastightness between the wire and terminal lug, subsequent loss of electrical power, and an electrical fire.
Establishment of Class E Airspace; Coldwater, KS
Document Number: 2016-09158
Type: Rule
Date: 2016-04-22
Agency: Federal Aviation Administration, Department of Transportation
This action establishes Class E airspace in Coldwater, KS. Controlled airspace is necessary to accommodate new Standard Instrument Approach Procedures (SIAPs) at Comanche County Airport. The FAA is taking this action to enhance the safety and management of Instrument Flight Rule (IFR) operations at the airport. Additionally, to this action corrects the spelling of the airport name to Comanche County Airport, inadvertently misspelled in the proposal.
Airworthiness Directives; The Boeing Company Airplanes
Document Number: 2016-09000
Type: Rule
Date: 2016-04-22
Agency: Federal Aviation Administration, Department of Transportation
We are adopting a new airworthiness directive (AD) for The Boeing Company Model 787-8 and 787-9 airplanes powered by General Electric (GE) GEnx-1B engines. This AD requires revising the airplane flight manual (AFM) to provide the flight crew a revised fan ice removal procedure and a new associated mandatory flight crew briefing to reduce the likelihood of engine damage due to fan ice shedding. This AD also removes certain dispatch relief. For airplanes with certain engines, this AD also requires reworking or replacing at least one engine. This AD was prompted by a recent engine fan blade rub event that caused an in-flight non-restartable power loss. We are issuing this AD to prevent susceptibility to heavy fan blade rubs, which could result in engine damage and a possible in-flight non-restartable power loss of one or both engines.
Proposed Revocation of Class E Airspace; Lake Providence, LA
Document Number: 2016-08770
Type: Proposed Rule
Date: 2016-04-22
Agency: Federal Aviation Administration, Department of Transportation
This action proposes to remove Class E airspace extending upward from 700 feet above the surface at Byerley Airport, Lake Providence, LA. The decommissioning of non-directional radio beacons (NDB) and cancellation of Standard Instrument Approach Procedures (SIAPs) have made this action necessary for continued safety and management within the National Airspace System.
Establishment of Class E Airspace; Danville AR
Document Number: 2016-08765
Type: Rule
Date: 2016-04-22
Agency: Federal Aviation Administration, Department of Transportation
This action establishes Class E airspace extending upward from 700 feet above the surface at Danville Municipal Airport, Danville, AR, to accommodate new Standard Instrument Approach Procedures (SIAPs) for the safety and management of Instrument flight Rules (IFR) operations at the airport.
Establishment of Class E Airspace; Moriarty, NM
Document Number: 2016-08758
Type: Rule
Date: 2016-04-22
Agency: Federal Aviation Administration, Department of Transportation
This action establishes Class E airspace in Moriarty, NM. Controlled airspace is necessary to accommodate new Area Navigation (RNAV) Standard Instrument Approach Procedures at Moriarty Airport. The FAA is taking this action to enhance the safety and management of Instrument Flight Rule (IFR) operations at the airport.
Standard Instrument Approach Procedures, and Takeoff Minimums and Obstacle Departure Procedures; Miscellaneous Amendments
Document Number: 2016-08756
Type: Rule
Date: 2016-04-22
Agency: Federal Aviation Administration, Department of Transportation
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.
Standard Instrument Approach Procedures, and Takeoff Minimums and Obstacle Departure Procedures; Miscellaneous Amendments
Document Number: 2016-08754
Type: Rule
Date: 2016-04-22
Agency: Federal Aviation Administration, Department of Transportation
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.
Standard Instrument Approach Procedures, and Takeoff Minimums and Obstacle Departure Procedures; Miscellaneous Amendments
Document Number: 2016-08753
Type: Rule
Date: 2016-04-22
Agency: Federal Aviation Administration, Department of Transportation
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.
Standard Instrument Approach Procedures, and Takeoff Minimums and Obstacle Departure Procedures; Miscellaneous Amendments
Document Number: 2016-08751
Type: Rule
Date: 2016-04-22
Agency: Federal Aviation Administration, Department of Transportation
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.
Airworthiness Directives; The Boeing Company Airplanes
Document Number: 2016-08539
Type: Rule
Date: 2016-04-22
Agency: Federal Aviation Administration, Department of Transportation
We are superseding Airworthiness Directive (AD) 2012-17-13, which applied to certain The Boeing Company Model 707 airplanes, and Model 720 and 720B series airplanes. For certain airplanes, AD 2012-17- 13 required using redefined flight cycle counts; determining the type of material of the horizontal stabilizer, rear spar, and upper and lower chords on the inboard and outboard ends of the rear spar; repetitively inspecting for cracking of the horizontal stabilizer components; and repairing or replacing the chord, or modifying chord segments made of 7079 aluminum, if necessary. For all airplanes, AD 2012-17-13 required inspecting certain structurally significant items, and repairing discrepancies if necessary. This new AD adds a requirement to replace all chord segments made of 7079 aluminum with new, improved chord segments made of 7075 aluminum. This AD was prompted by a determination that all chord segments made of 7079 aluminum must be replaced with new, improved chord segments made of 7075 aluminum. We are issuing this AD to detect and correct stress corrosion and potential early fatigue cracking in the horizontal stabilizer, which could result in reduced structural integrity of the horizontal stabilizer.
Special Conditions: Gulfstream Aerospace Corporation Model GVII-G500 Airplanes, Design Roll Maneuver Requirement
Document Number: 2016-09326
Type: Rule
Date: 2016-04-21
Agency: Federal Aviation Administration, Department of Transportation
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 when compared to the state of technology envisioned in the airworthiness standards for transport category airplanes. This design feature is electronic flight controls that affect maneuvering. 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.
Notice of Request To Release Airport Property
Document Number: 2016-09307
Type: Notice
Date: 2016-04-21
Agency: Federal Aviation Administration, Department of Transportation
The FAA proposes to rule and invites public comment on the release of land at Strother Field (WLD), Winfield, Kansas, under the provisions of 49 U.S.C. 47107(h)(2).
Registration of Small Unmanned Aircraft Systems Operated Under Exemptions Issued by the FAA
Document Number: 2016-09199
Type: Notice
Date: 2016-04-21
Agency: Federal Aviation Administration, Department of Transportation
The FAA is issuing this notice to advise owners of small unmanned aircraft systems (sUAS) used for purposes other than as model aircraft under the authority of an exemption issued by the FAA that they may register their sUAS using the web-based aircraft registration system. It also provides specific information pertaining to any exemptions that include conditions relating to the registration of small UAS.
Airworthiness Directives; Pratt & Whitney Division Turbofan Engines
Document Number: 2016-09122
Type: Proposed Rule
Date: 2016-04-20
Agency: Federal Aviation Administration, Department of Transportation
We propose to adopt a new airworthiness directive (AD) for certain Pratt & Whitney (PW) PW4164, PW4164-1D, PW4168, PW4168-1D, PW4168A, PW4168A-1D, and PW4170 turbofan engines. This proposed AD was prompted by several instances of fuel leaks on PW engines installed with the Talon IIB combustion chamber configuration. This proposed AD would require initial and repetitive inspections of the affected fuel nozzles and their replacement with parts eligible for installation. We are proposing this AD to prevent failure of the fuel nozzles, which could lead to engine fire and damage to the airplane.
Airworthiness Directives; Turbomeca S.A. Turboshaft Engines
Document Number: 2016-09121
Type: Rule
Date: 2016-04-20
Agency: Federal Aviation Administration, Department of Transportation
We are adopting a new airworthiness directive (AD) for all Turbomeca S.A. Arriel 2E turboshaft engines. This AD requires removing the pre-TU 193 adjusted high-pressure/low-pressure pump and metering valve assembly and replacing it with a part that is eligible for installation. This AD also requires replacing the constant delta- pressure (delta-P) diaphragm of the fuel metering valve. This AD was prompted by reports of fuel flow non-conformities found during acceptance tests of Arriel 2E hydro-mechanical metering units (HMUs). We are issuing this AD to prevent failure of the delta-P diaphragm, which could result in an uncommanded in-flight shutdown and damage to the helicopter.
Notice of Policy Clarification for Acceptance of Documents With Digital Signatures by the Federal Aviation Administration Aircraft Registry
Document Number: 2016-09069
Type: Notice
Date: 2016-04-20
Agency: Federal Aviation Administration, Department of Transportation
Notice is hereby given of the FAA's clarification of its policy regarding the acceptance of documents submitted to the FAA Aircraft Registry with digital signatures in support of aircraft registration under 14 CFR 47.13 and conveyances or security documents submitted to the FAA Aircraft Registry regarding claims and interests under 14 CFR 49.13.
Airworthiness Directives; Dassault Aviation Airplanes
Document Number: 2016-09005
Type: Proposed Rule
Date: 2016-04-20
Agency: Federal Aviation Administration, Department of Transportation
We propose to supersede Airworthiness Directive (AD) 2011-10- 01, for all Dassault Aviation Model FALCON 7X airplanes. AD 2011-10-01 currently requires repetitive functional tests of the ram air turbine (RAT) heater and repair if necessary. Since we issued AD 2011-10-01, we received a revision of an airworthiness limitations items (ALI) document, which introduces new and more restrictive maintenance requirements and airworthiness limitations for airplane structures and systems. This proposed AD would require revising the maintenance or inspection program to incorporate new maintenance requirements and airworthiness limitations. We are proposing this AD to prevent reduced structural integrity and reduced control of these airplanes due to the failure of system components.
Airworthiness Directives; Zodiac Seats California LLC Seating Systems
Document Number: 2016-09004
Type: Proposed Rule
Date: 2016-04-20
Agency: Federal Aviation Administration, Department of Transportation
We propose to adopt a new airworthiness directive (AD) for certain Zodiac Seats California LLC seating systems. This proposed AD was prompted by a determination that the affected seating systems may cause serious injury to the occupant during forward impacts when subjected to certain inertia forces. This proposed AD would require removing affected seating systems. We are proposing this AD to prevent serious injury to the occupant during forward impacts in emergency landing conditions.
Airworthiness Directives; Dassault Aviation Airplanes
Document Number: 2016-09003
Type: Proposed Rule
Date: 2016-04-20
Agency: Federal Aviation Administration, Department of Transportation
We propose to adopt a new airworthiness directive (AD) for all Dassault Aviation Model FALCON 900EX and FALCON 2000EX airplanes. This proposed AD was prompted by a review that identified a nonconformity between the torque value applied to the screw-nuts of aileron servo actuators, and the torque value specified by the type design. This proposed AD would require replacing certain aileron servo actuators with serviceable servo actuators. We are proposing this AD to prevent desynchronization between two servo actuator barrels, which could lead to reduced control of the airplane during roll maneuvers at low altitude.
Airworthiness Directives; Bombardier, Inc. Airplanes
Document Number: 2016-08960
Type: Proposed Rule
Date: 2016-04-20
Agency: Federal Aviation Administration, Department of Transportation
We propose to supersede Airworthiness Directive (AD) 2015-02- 23, for certain Bombardier, Inc. Model CL-600-1A11 (CL-600), CL-600- 2A12 (CL-601), and CL-600-2B16 (CL-601-3A, and CL-601-3R Variants) airplanes. AD 2015-02-23 currently requires repetitive inspections for fractured or incorrectly oriented fasteners on the inboard flap hinge- box forward fittings on both wings, and replacement of all fasteners if necessary. The preamble to AD 2015-02-23 explains that we consider the requirements interim action and are considering further rulemaking. We now have determined that further rulemaking is indeed necessary, and that replacement of the fasteners is necessary. This proposed AD would require terminating action to replace the fasteners on the inboard flap hinge-box forward fittings on both wings. We are proposing this AD to detect and correct incorrectly oriented or fractured fasteners, which could result in detachment of the flap hinge-box and the flap surface, and consequent reduced controllability of the airplane.
Airworthiness Directives; BAE SYSTEMS (Operations) Limited Airplanes
Document Number: 2016-08957
Type: Proposed Rule
Date: 2016-04-20
Agency: Federal Aviation Administration, Department of Transportation
We propose to supersede Airworthiness Directive (AD) 2010-10- 13, for all BAE SYSTEMS (Operations) Limited Model BAe 146 and Avro 146 series airplanes. AD 2010-10-13 currently requires repetitive inspections of the wing fixed leading edge and front spar structure for corrosion and cracking, and repair if necessary. Since we issued AD 2010-10-13, the Design Approval Holder (DAH) has issued revised inspection procedures that eliminate a previously approved inspection procedure. This proposed AD would require revised inspection procedures. We are proposing this AD to detect and correct corrosion and cracking of the wing fixed leading edge and front spar structure, which could result in reduced structural integrity of the wing.
Airworthiness Directives; Airbus Airplanes
Document Number: 2016-08953
Type: Proposed Rule
Date: 2016-04-20
Agency: Federal Aviation Administration, Department of Transportation
We propose to supersede Airworthiness Directive (AD) 2005-15- 07, for certain Airbus Model A320-111 airplanes and Model A320-200 series airplanes. AD 2005-15-07 currently requires installing insulator and cable ties to the electrical cables of the S routes at the gaps in the raceway in the wing trailing edge and the wing tip and wing root areas. Since we issued AD 2005-15-07, we have received reports of wire chafing in the left-hand wing trailing edge. This proposed AD would require additional modifications in the trailing edges of both wings. This proposed AD would also remove airplanes from the applicability. We are proposing this AD to prevent wire chafing in the trailing edge of the wings, which could result in a short circuit in the vicinity of the fuel tanks, consequently resulting in a potential source of ignition in a fuel tank vapor space and consequent fuel tank explosion.
Notice of Intent To Release Airport Property From Quitclaim Deed; North Perry Airport, Hollywood, FL
Document Number: 2016-09079
Type: Notice
Date: 2016-04-19
Agency: Federal Aviation Administration, Department of Transportation
The FAA hereby provides notice of intent to release approximately 0.07 acres of airport property at North Perry Airport, Hollywood, FL, from the conditions, reservations, and restrictions as contained in a Quitclaim Deed agreement between the FAA and Broward County, FL, dated October 11, 1957. The release of property will allow Broward County to dispose of the property for other than aeronautical purposes. The property is located at the intersection of Pembroke Road (State Road 824) and Airport Drive South, Hollywood, Florida. The parcel is currently designated as non-aeronautical land use. The property will be released of its federal obligations in order for the FDOT to use the property for installation and maintenance of a traffic signal device and associated highway improvements. The fair market value of these parcels has been determined to be $53,900.
Notice of Request To Release Airport Property
Document Number: 2016-08902
Type: Notice
Date: 2016-04-18
Agency: Federal Aviation Administration, Department of Transportation
The FAA proposes to rule and invites public comment on the release of land at the Hebron Municipal Airport (HJH), Hebron, Nebraska, under the provisions of 49 U.S.C. 47107(h)(2).
Deadline for Notification of Intent To Use the Airport Improvement Program (AIP) Primary, Cargo, and Nonprimary Entitlement Funds Available to Date for Fiscal Year 2016
Document Number: 2016-08766
Type: Notice
Date: 2016-04-15
Agency: Federal Aviation Administration, Department of Transportation
The Federal Aviation Administration (FAA) announces May 2, 2016, as the deadline for each airport sponsor to notify the FAA whether or not it will use its fiscal year 2016 entitlement funds available under Section 47114 of Title 49, United States Code, to accomplish Airport Improvement Program (AIP) eligible projects that the airport sponsor previously identified through the Airports Capital Improvement Plan (ACIP) process during the preceding year. The airport sponsor's notification must address all entitlement funds available to date for fiscal year 2016, as well as any entitlement funds not obligated from prior years. After Friday, July 1, 2016, the FAA will carry-over the remainder of currently available entitlement funds, and these funds will not be available again until at least the beginning of fiscal year 2017. Currently, the AIP has 79 percent of the entitlements available through July 15, 2016. If congressional action is taken on future extensions which provide for additional current year and protected entitlements (the remaining 21 percent), the FAA will then work with airport sponsors to adjust accordingly. This notification requirement does not apply to non- primary airports covered by the block-grant program.
Office of Commercial Space Transportation; Notice of Availability of the Final Environmental Assessment (Final EA), Finding of No Significant Impact (FONSI)/Record of Decision (ROD) for the Kodiak Launch Complex Launch Pad 3, Kodiak Island, Alaska
Document Number: 2016-08746
Type: Notice
Date: 2016-04-15
Agency: Federal Aviation Administration, Department of Transportation
In accordance with the National Environmental Policy Act of 1969, as amended (NEPA; 42 United States Code 4321 et seq.), Council on Environmental Quality NEPA implementing regulations (40 CFR parts 1500 to 1508), and FAA Order 1050.1E, Change 1, Environmental Impacts: Policies and Procedures, the FAA is announcing the availability of the Final EA and FONSI/ROD for the Kodiak Launch Complex Launch Pad 3.
Airworthiness Directives; Bombardier Inc. Airplanes
Document Number: 2016-08533
Type: Proposed Rule
Date: 2016-04-14
Agency: Federal Aviation Administration, Department of Transportation
We propose to adopt a new airworthiness directive (AD) for certain Bombardier, Inc. Model CL-600-2B19 (Regional Jet Series 100 & 440), CL-600-2C10 (Regional Jet Series 700, 701, & 702), CL-600-2D15 (Regional Jet Series 705), CL-600-2D24 (Regional Jet Series 900), and CL-600-2E25 (Regional Jet Series 1000) airplanes. This proposed AD was prompted by reports of undesirable changes in the Reference Airspeed (RAS) Bug, occurring during flight without pilot input. This proposed AD would require replacing the flight control computer (FCC). We are proposing this AD to prevent uncommanded pitch changes, which could result in deviation from a safe flight path.
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