Federal Aviation Administration May 2018 – Federal Register Recent Federal Regulation Documents
Results 101 - 150 of 159
Airworthiness Directives; Airbus Airplanes
We are superseding Airworthiness Directive (AD) 2015-15-13, which applied to certain Airbus Model A319 series airplanes; Model A320-211, -212, -214, -231, -232, and -233 airplanes; and Model A321- 111, -112, -131, -211, -212, -213, -231, and -232 airplanes. AD 2015- 15-13 required a modification of the potable water service panel and waste water service panel, including doing applicable related investigative and corrective actions. This AD requires a modification of the waste water and potable water service panels with new compliance times. This AD also removes certain airplanes from the applicability and adds Model A320-216 airplanes to the applicability. This AD was prompted by an evaluation by the design approval holder (DAH) indicating that the potable water and waste water service panel areas are subject to widespread fatigue damage (WFD). We are issuing this AD to address the unsafe condition on these products.
Airworthiness Directives; Airbus Airplanes
We are adopting a new airworthiness directive (AD) for certain Airbus Model A330-301, -321, -322, -341, and -342 airplanes; Model A340-200 series airplanes; and Model A340-300 series airplanes. This AD requires contacting the FAA to obtain instructions for addressing the unsafe condition on these products, and doing the actions specified in those instructions. This AD was prompted by reports of cracks on both left-hand (LH) and right-hand (RH) sides on certain frame (FR) locations. We are issuing this AD to address the unsafe condition on these products.
Airworthiness Directives; Airbus Airplanes
We propose to adopt a new airworthiness directive (AD) for all Airbus Model A300 series airplanes. This proposed AD was prompted by a revision of an airworthiness limitation items (ALI) document. This proposed AD would require revising the maintenance or inspection program, as applicable, to incorporate the specified maintenance requirements and airworthiness limitations. We are proposing this AD to address the unsafe condition on these products.
Airworthiness Directives; Bombardier, Inc., Airplanes
We propose to supersede Airworthiness Directive (AD) 2015-17- 04, which applies to certain Bombardier, Inc., Model CL-600-2C10 (Regional Jet Series 700, 701, & 702), Model CL-600-2D15 (Regional Jet Series 705), and Model CL-600-2D24 (Regional Jet Series 900) airplanes. AD 2015-17-04 requires replacement of left and right fixed control rods and lever assemblies of the elevator control system. Since we issued AD 2015-17-04, we have received a report indicating that certain revisions of the service information were missing instructions. This proposed AD would require a detailed visual inspection of the key washers and self- locking nuts of the elevator control linkages and corrective actions if necessary. We are proposing this AD to address the unsafe condition on these products.
Airworthiness Directives; The Boeing Company Airplanes
We are adopting a new airworthiness directive (AD) for all The Boeing Company Model 787-8 airplanes. This AD requires inspecting the part number of the occupant restraint system on the standard attendant seats, and doing additional inspections and corrective actions if necessary. This AD was prompted by a report of loose attachment bolts on the occupant restraint system on a standard attendant seat due to the bolts being over-torqued during production. We are issuing this AD to address the unsafe condition on these products.
Airworthiness Directives; Bombardier, Inc., Airplanes
We are superseding Airworthiness Directive (AD) 2016-25-18, which applied to certain Bombardier, Inc., Model BD-700-1A10 and BD- 700-1A11 airplanes. AD 2016-25-18 required an inspection for discrepancies of the attachment points of the links between the engine rear mount assemblies, and corrective actions if necessary. This AD requires an inspection of certain attachment points, corrective action if necessary, and replacement of certain bolts and nuts in the engine rear mount assemblies. This AD also adds airplanes to the applicability. This AD was prompted by the determination that replacement of certain nuts and bolts in the engine rear mount assemblies is necessary. We are issuing this AD to address the unsafe condition on these products.
Fifty First RTCA SC-206 Aeronautical Information and Meteorological Data Link Services (AIS) Plenary
The FAA is issuing this notice to advise the public of a meeting of Fifty First RTCA SC-206 Aeronautical Information and Meteorological Data Link Services (AIS) Plenary.
Airworthiness Directives; Rolls-Royce plc Turbojet Engines
We are adopting a new airworthiness directive (AD) for Rolls- Royce plc (RR) Viper Mk. 601-22 turbojet engines. This AD requires removing the oil pump assembly, part number (P/N) V112027, and oil pressure filter, P/N V21264, from service and replacing them with parts eligible for installation. This AD was prompted by a report of an engine failure caused by installation of an incorrect oil filter. We are issuing this AD to correct the unsafe condition on these products.
Notice of 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 2018/2019 Scheduling Season
Under this notice, the FAA announces the submission deadline of May 17, 2018, for winter 2018/2019 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). The deadline coincides with the schedule submission deadline for the International Air Transport Association (IATA) Slot Conference for the winter 2018/2019 scheduling season.
RTCA PMC Program Management Committee Plenary
The FAA is issuing this notice to advise the public of a meeting of RTCA PMC Program Management Committee Plenary.
Airworthiness Directives; ATR-GIE Avions de Transport Régional Airplanes
We propose to adopt a new airworthiness directive (AD) for certain ATR-GIE Avions de Transport R[eacute]gional Model ATR42-200, - 300, and -320 airplanes. This proposed AD was prompted by a determination that more restrictive maintenance requirements and airworthiness limitations are necessary. This proposed AD would require updating the maintenance or inspection program, as applicable, to incorporate new or more restrictive maintenance requirements and airworthiness limitations. We are proposing this AD to address the unsafe condition on these products.
Airworthiness Directives; Airbus Airplanes
We propose to adopt a new airworthiness directive (AD) for all Airbus Model A330-200 Freighter series airplanes, Model A330-200 series airplanes, Model A330-300 series airplanes, Model A340-200 series airplanes, Model A340-300 series airplanes, Model A340-500 series airplanes, and Model A340-600 series airplanes. This proposed AD was prompted by a report of deficient fatigue performance of high strength steel used in forgings. Components made from the affected high strength steel are installed on the main landing gear (MLG), nose landing gear (NLG), and center landing gear (CLG). This proposed AD would require identifying the part number and serial number of certain components installed on the MLG, NLG, and CLG; replacing affected parts; identifying the airplane's weight variant; and determining the applicable life limit for certain components installed on the MLG, NLG, and CLG. We are proposing this AD to address the unsafe condition on these products.
Airworthiness Directives; Airbus Helicopters
We propose to adopt a new airworthiness directive (AD) for Airbus Helicopters Model AS-365N2, AS 365 N3, EC 155B, EC155B1, SA- 365N1, and SA-366G1 helicopters. This proposed AD would require repetitive inspections of the aft fuselage outer skin. This proposed AD is prompted by several reports of aft fuselage outer skin disbonding. The actions of this proposed AD are intended to address an unsafe condition on these products.
Airworthiness Directives; SOCATA Airplanes
We propose to supersede Airworthiness Directive (AD) 98-16-03 for SOCATA Models TB 9 and TB 10 airplanes. 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 fatigue cracking of the wing front attachments on the wing and fuselage sides. We are issuing this proposed AD to require actions to address the unsafe condition on these products.
Thirty Sixth RTCA SC-214 Standards for Air Traffic Data Communications Services Plenary
The FAA is issuing this notice to advise the public of a meeting of Thirty Sixth RTCA SC-214 Standards for Air Traffic Data Communications Services Plenary.
Eighty Eighth RTCA SC-147 Plenary Session Joint With EUROCAE WG-75
The FAA is issuing this notice to advise the public of a meeting of Eighty Eighth RTCA SC-147 Plenary Session Joint with EUROCAE WG-75.
Airworthiness Directives; Airbus Helicopters
We propose to adopt a new airworthiness directive (AD) for Airbus Helicopters Model AS332C, AS332C1, AS332L, and AS332L1 helicopters. This proposed AD would require inspecting the jettisoning mechanism of the left-hand (LH) and right-hand (RH) cabin sliding plug doors. This proposed AD is prompted by a report that during a scheduled inspection a cabin door failed to jettison. The actions of this proposed AD are intended to correct an unsafe condition on these products.
Airworthiness Directives; ATR-GIE Avions de Transport Régional Airplanes
We propose to adopt a new airworthiness directive (AD) for all ATR-GIE Avions de Transport R[eacute]gional Model ATR42-500 airplanes. This proposed AD was prompted by a determination that more restrictive maintenance requirements and airworthiness limitations are necessary. This proposed AD would require revising the maintenance or inspection program, as applicable, to incorporate new and/or more restrictive maintenance requirements and airworthiness limitations. We are proposing this AD to address the unsafe condition on these products.
Airworthiness Directives; Bombardier, Inc., Airplanes
We propose to adopt a new airworthiness directive (AD) for certain Bombardier, Inc., Model BD-700-1A10 and BD-700-1A11 airplanes. This proposed AD was prompted by a report of cracking at the fastener holes of the left-hand-side support bracket of the elevator bell crank for the control linkage in the vertical stabilizer. This proposed AD would require an eddy current inspection on certain support brackets of the elevator bell crank for any cracking at the fastener holes, a measurement to confirm that the fastener hole diameters are within tolerance, and replacement with a new support bracket of the elevator bell crank if necessary. We are proposing this AD to address the unsafe condition on these products.
Airworthiness Directives; Airbus Airplanes
We propose to adopt 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 proposed AD was prompted by a determination that new or more restrictive maintenance requirements and airworthiness limitations are necessary. This proposed AD would require revising the maintenance or inspection program, as applicable, to incorporate new or more restrictive maintenance requirements and airworthiness limitations. We are proposing this AD to address the unsafe condition on these products.
Airworthiness Directives; Textron Aviation Inc. Airplanes
We are revising Airworthiness Directive (AD) 2018-03-03 for certain Textron Aviation Inc. Models 401, 401A, 401B, 402, 402A, 402B, 402C, 411, 411A, 414, 414A, 421, 421A, 421B, 421C, and 425 airplanes. AD 2018-03-03 required repetitively inspecting the left and the right forward lower carry through spar cap for cracks and replacing the carry through spar cap if cracks were found. This AD addresses the same unsafe condition and requires the same actions as AD 2018-03-03, but clarifies the compliance times for the initial inspection of the carry through spar cap. This AD was prompted by several reports of confusion in interpreting the compliance times for the initial inspection of the carry through spar cap. We are issuing this AD to eliminate confusion in interpreting the compliance times for this inspection.
Airworthiness Directives; Learjet, Inc. Airplanes
We propose to adopt a new airworthiness directive (AD) for certain Learjet, Inc. Models 28, 29, 31, 31A, 35, 35A, 36, 36A, 55, 55B, 55C, and 60 airplanes. This proposed AD was prompted by fatigue cracks initiating in the flap support structure due to repetitive flap loads, which has caused flap nose roller support bracket failure. This proposed AD would require replacement of the flap nose roller fitting, nose roller support bracket, and adjacent rib support structure with more robust components. We are proposing this AD to address the unsafe condition on these products.
Standard Instrument Approach Procedures, and Takeoff Minimums and Obstacle Departure Procedures; Miscellaneous Amendments
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
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.
Commercial Space Transportation Advisory Committee-Open Meeting
Pursuant to Section 10(a)(2) of the Federal Advisory Committee Act, notice is hereby given of a meeting of the Commercial Space Transportation Advisory Committee (COMSTAC).
Petition for Exemption; Summary of Petition Received; Ameriflight
This notice contains a summary of a petition seeking relief from specified requirements of Federal Aviation 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.
Amendment of Class E Airspace; Charlotte, MI
This action modifies Class E airspace extending upward from 700 feet above the surface at Fitch H. Beach Airport, Charlotte, MI, due to the decommissioning of the Lansing VHF omnidirectional range (VOR) and collocated tactical air navigation (TACAN) which provided navigation guidance for the instrument procedures to this airport. The Lansing VOR/TACAN is being decommissioned as part of the VOR Minimum Operational Network (MON) Program. This action enhances safety and management of instrument flight rules (IFR) operations at this airport. Additionally, the geographic coordinates of the airport are being adjusted to coincide with the FAA's aeronautical database. An editorial change is also being made removing the city associated with the airport name in the airspace legal designation.
Amendment of Class E Airspace; Milwaukee, WI
This action modifies Class E airspace extending upward from 700 feet above the surface at Batten International Airport, Racine, WI, contained within the Milwaukee, WI, airspace description. This action is required due to the decommissioning of the Horlick VHF omnidirectional range (VOR) which provided navigation guidance for the standard instrument approach procedures to this airport. The Horlick VOR is being decommissioned as part of the VOR Minimum Operational Network (MON) Program. This action enhances the safety and management of instrument flight rules (IFR) operations at the airport.
Proposed Amendment of Class D and Class E Airspace and Proposed Revocation of Class E Airspace; Jackson, MI
This action proposes to modify Class D airspace, Class E airspace designated as a surface area, and Class E airspace extending upward from 700 feet above the surface, and remove Class E airspace designated as an extension to Class D or Class E surface area at Jackson County Airport-Reynolds Field, Jackson MI. The FAA is proposing this action due to the decommissioning of the Jackson VHF omnidirectional range (VOR) which provided navigation guidance for the instrument procedures to this airport. The VOR is being decommissioned as part of the VOR Minimum Operational Network (MON) Program. The name and the geographic coordinates of the airport would also be updated to coincide with the FAA's aeronautical database. Additionally, this action would replace the outdated term ``Airport/Facility Directory'' with the term ``Chart Supplement'' in the associated airspace legal descriptions.
Airworthiness Directives; Safran Helicopter Engines, S.A., Turboshaft Engines
We are adopting a new airworthiness directive (AD) for all Safran Helicopter Engines, S.A., Arriel 2E turboshaft engines. This AD was prompted by reports of ruptured front support pins on the accessory gearbox front support. This AD requires replacement of the accessory gearbox front support. We are issuing this AD to address the unsafe condition on these products.
Amendment of Class E Airspace; Muscatine, IA
This action modifies Class E airspace designated as a surface area and Class E airspace extending upward from 700 feet above the surface at Muscatine Municipal Airport, Muscatine, IA. This action is required due to the decommissioning of the Port City VHF omnidirectional range (VOR) facility, which provided navigation guidance for the instrument procedures to this airport. The VOR has been decommissioned as part of the VOR Minimum Operational Network (MON) Program.
Proposed Revocation of Class E Airspace; Springfield, OH
This action proposes to remove Class E airspace areas designated as an extension to a Class D surface area at Springfield- Beckley Municipal Airport, Springfield, OH. The FAA is proposing this action as a result of an airspace review, which inadvertently overlooked the removal of the associated Class E airspace extensions when the Class D airspace was removed.
Airworthiness Directives; Airbus Airplanes
We are adopting a new airworthiness directive (AD) for certain Airbus Model A318 series airplanes and Model A319 series airplanes; all Model A320-211, -212, -214, -216, -231, -232, and -233 airplanes; and all Model A321-111, -112, -131, -211, -212, -213, -231, and -232 airplanes. This AD was prompted by an evaluation by the design approval holder (DAH) indicating that the holes of the upper cleat to upper stringer attachments at certain areas of the left- and right-hand wings are subject to widespread fatigue damage (WFD). This AD requires modifying the holes of the upper cleat to upper stringer attachments at certain areas of the left- and right-hand wings. We are issuing this AD to address the unsafe condition on these products.
Airworthiness Directives; Gulfstream Aerospace Corporation Airplanes
We are adopting a new airworthiness directive (AD) for certain Gulfstream Aerospace Corporation Models G-IV and GIV-X airplanes. This AD was prompted by the potential for fatigue cracks developing in the main landing gear actuator attachment fitting that had a certain repair incorporated. This AD requires incorporating new revisions into the Instructions for Continued Airworthiness of the Limitations section of the FAA-approved maintenance program (e.g., maintenance manual) that establish an inspection cycle for the repaired MLG side brace actuator fittings. We are issuing this AD to address the unsafe condition on these products.
Airworthiness Directives; Viking Air Limited Airplanes
We are revising an earlier proposal for all Viking Air Limited Models DHC-2 Mk. I, DHC-2 Mk. II, and DHC-2 Mk. III airplanes. This proposed airworthiness directive (AD) results from mandatory continuing airworthiness information (MCAI) originated by an aviation authority of another country to identify and address an unsafe condition on an aviation product. The MCAI describes the unsafe condition as cracking found in the wing rear spar web at the wing station where the flap outboard hinge is attached. This action revises the proposal by issuing an SNPRM that changes the compliance times to more closely match the compliance times in the MCAI. We are proposing this AD to address the unsafe condition on these products. Since these actions may impose an additional burden over those in the notice of proposed rulemaking (NPRM), we are reopening the comment period to allow the public the opportunity to comment on these changes.
Twenty Seventh RTCA SC-223 IPS and AeroMACS Joint Plenary With WG-108
The FAA is issuing this notice to advise the public of a meeting of Twenty Seventh RTCA SC-223 IPS and AeroMACS Joint Plenary with WG-108.
Airworthiness Directives; Airbus Airplanes
We propose to adopt a new airworthiness directive (AD) for certain Airbus Model A319-131, A319-132, A319-133, A320-231, A320-232, A320-233, A321-131, A321-231, and A321-232 airplanes. This proposed AD was prompted by reports of fan cowl door (FCD) losses during take-off. This proposed AD would require modification and re-identification, or replacement, of certain FCDs, and installation of a placard in the flight deck. We are proposing this AD to address the unsafe condition on these products.
Airworthiness Directives; The Boeing Company Airplanes
We are adopting a new airworthiness directive (AD) for certain The Boeing Company Model 737-200, -300, -400, and -500 series airplanes. This AD was prompted by reports of cracks in the frame web common to the stringer ties adjacent to the air-conditioning support brackets. This AD requires an inspection of the frame for any air- conditioning bracket assembly or intercostal, and, depending on the results, repetitive inspections of the frame web for cracking of certain locations, and applicable on-condition actions. We are issuing this AD to address the unsafe condition on these products.
Proposed Establishment of Class E Airspace; Hoonah, AK
This action proposes to establish Class E airspace extending upward from 700 feet above the surface, at Hoonah Airport, Hoonah, AK, to accommodate area navigation (RNAV) procedures at the airport. This action would ensure the safety and management of instrument flight rules (IFR) operations within the National Airspace System.
Amendment of Class D and E Airspace and Revocation of Class E Airspace; Pocatello, ID
This action amends controlled airspace at Pocatello Regional Airport, Pocatello, ID, by amending Class D airspace and Class E airspace designated as a surface area; removing Class E airspace designated as an extension to a Class D or E surface area; and amending Class E airspace extending upward from 700 feet above the surface. Also, this action updates the airport's geographic coordinates for the associated Class D and E airspace areas to reflect the FAA's current aeronautical database. Additionally, reference to the Pocatello VHF Omnidirectional Range/Tactical Air Navigation (VORTAC) is removed from the Class E airspace extending upward from 700 feet above the surface description. This action enhances the safety and management of instrument flight rules (IFR) operations at the airport.
Proposed Amendment of Class D and Class E Airspace, and Revocation of Class E Airspace; Juneau, AK
This action proposes to amend Class D airspace, Class E surface area airspace, Class E airspace extending upward from 700 feet above the surface, and remove Class E airspace designated as an extension at Juneau International Airport, Juneau, AK. Airspace redesign is necessary as the FAA transitions from ground-based to satellite-based navigation for the safety and management of instrument flight rules (IFR) operations at the airport. This proposal would also update the airport's geographic coordinates to match the FAA's aeronautical database for the associated Class D and E airspace areas, and would make an editorial change to the Class D airspace legal description replacing Airport/Facility Directory with the term Chart Supplement.
Proposed Amendment of Class D and Class E Airspace; Moses Lake, WA
This action proposes to modify Class D airspace, Class E surface area airspace, Class E airspace designated as an extension, and Class E airspace extending upward from 700 and 1,200 feet above the surface at Grant County International Airport (formerly Grant County Airport), Moses Lake, WA. This action also proposes to remove the Notice to Airmen (NOTAM) part-time status of Class E airspace designated as an extension, and update the airport name and geographic coordinates for the airport in the associated Class D and E airspace areas to match the FAA's aeronautical database. These changes are necessary to accommodate airspace redesign for the safety and management of instrument flight rules (IFR) operations at the airport. Also, an editorial change would be made to the Class D and Class E airspace legal descriptions replacing ``Airport/Facility Directory'' with the term ``Chart Supplement''.
Special Conditions: St. Louis Helicopter, LLC; Textron Aviation B300, B300C, B300C (MC-12W), and B300C (UC-12W) Airplanes; Installation of Rechargeable Lithium Batteries
These special conditions are issued for the Textron Aviation models B300, B300C, B300C (MC-12W), and B300C (UC-12W) series airplanes. The airplane, as modified by St. Louis Helicopter LLC, will have a novel or unusual design feature associated with the installation of a rechargeable lithium battery. The applicable airworthiness regulations do not contain adequate or appropriate safety standards for this design feature. These special conditions contain the additional safety standards 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; Gustavus, AK
This action proposes to amend Class E airspace extending upward from 700 feet above the surface at Gustavus Airport, Gustavus, AK. Airspace redesign is necessary as the FAA transitions from ground- based to satellite-based navigation for the safety and management of instrument flight rules (IFR) operations at this airport.
Proposed Amendment of Class D Airspace, Removal of Class E Airspace, and Establishment of Class E Airspace; Olive Branch, MS
This action proposes to amend Class D airspace, remove Class E airspace designated as an extension, and establish Class E airspace extending upward from 700 feet or more above the surface at Olive Branch Airport, Olive Branch, MS. The Olive Branch non-directional radio beacon (NDB) has been decommissioned, requiring the redesign of the airspace. This proposal would replace the outdated term Airport/ Facility Directory with the term Chart Supplement in the Class D legal description.
Proposed Amendment of Class E Airspace, Memphis, TN
This action proposes to amend Class E airspace extending upward from 700 feet above the surface at Memphis International Airport, Memphis, TN. Airspace reconfiguration is necessary due to the decommissioning of the Elvis non-directional radio beacon (NDB), and for the safety and management of instrument flight rules (IFR) operations at this airport. Olive Branch Airport, Olive Branch, MS, would be removed from the airspace description to be reestablished in a separate rulemaking.
Proposed Amendment of Class E Airspace, Knoxville, TN
This action proposes to amend Class E surface airspace at Knoxville Downtown Island Airport, Knoxville, TN, by adding to the airspace description the exclusion of a 1-mile radius around University of Tennessee Medical Center Heliport, to allow helicopters departing from the heliport to no longer require a clearance. Also, the BENFI non-directional beacon (NDB) has been decommissioned, requiring redesign of Class E airspace extending upward from 700 feet above the surface at McGhee-Tyson Airport. Controlled airspace is necessary for the safety and management of instrument flight rules (IFR) operations at these airports. This action also would update the geographic coordinates of Knoxville Downtown Island Airport, McGhee Tyson Airport, and Gatlinburg-Pigeon Forge Airport in the associated Class E airspace areas to coincide with the FAA's aeronautical database.
Airworthiness Directives; Airbus Airplanes
We propose to adopt a new airworthiness directive (AD) for certain Airbus Model A318, A319, and A320 series airplanes, and Model A321-111, -112, -131, -211, -212, -213, -231, -232, -251N, -253N, and - 271N airplanes. This proposed AD was prompted by a determination that more restrictive maintenance requirements and airworthiness limitations are necessary. This proposed AD would require revising the maintenance or inspection program, as applicable, to incorporate the specified maintenance requirements and airworthiness limitations. We are proposing this AD to address the unsafe condition on these products.
Airworthiness Directives; CFM International S.A. Turbofan Engines
We are adopting a new airworthiness directive (AD) for all CFM International S.A. (CFM) Model CFM56-7B engines. This AD requires initial and repetitive inspections of the concave and convex sides of the fan blade dovetail to detect cracking and replacement of any blades found cracked. This AD was prompted by a recent engine failure due to a fractured fan blade, that resulted in the engine inlet cowl disintegrating and debris penetrating the fuselage, causing a loss of pressurization, and prompting an emergency descent. We are issuing this AD to address the unsafe condition on these products.
Special Conditions: VT DRB Aviation Consultants, Boeing Model 777-200 Airplanes; Installation of an Airbag System in Shoulder Belts
This document corrects an error that appeared in docket no. FAA-2017-0126, Special Conditions No. 25-654-SC, which was published in the Federal Register on April 7, 2017. The error occurs in the docket number of the final special conditions document.
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