Federal Aviation Administration February 12, 2019 – Federal Register Recent Federal Regulation Documents

Amendment of Restricted Areas R-5502A and R-5502B; Lacarne, OH
Document Number: 2019-02065
Type: Rule
Date: 2019-02-12
Agency: Federal Aviation Administration, Department of Transportation
This action updates the using agency information for restricted areas R-5502A and R-5502B; Lacarne, OH, and updates the controlling agency information for R-5502A. Additionally, this action adds exclusion language to the R-5502B boundaries information to overcome potential controlling agency confusion caused when both restricted areas are active in the same volume of airspace. These are administrative changes to reflect the current organizations tasked with using agency and controlling agency responsibilities for the restricted areas. It does not affect the overall R-5502 restricted area complex boundaries, designated altitudes, time of designation, or activities conducted within the restricted areas.
Proposed Modification of the Miami, FL, Class B Airspace; and the Fort Lauderdale, FL, Class C Airspace Areas; Public Meeting Postponement
Document Number: 2019-02058
Type: Proposed Rule
Date: 2019-02-12
Agency: Federal Aviation Administration, Department of Transportation
This notice announces the postponement of a fact-finding informal airspace meeting regarding a plan to modify the Miami, FL, Class B Airspace, and the Fort Lauderdale, FL, Class C Airspace areas. The meeting was previously scheduled for February 27, 2019.
Airworthiness Directives; Pacific Aerospace Ltd. Airplanes
Document Number: 2019-01541
Type: Rule
Date: 2019-02-12
Agency: Federal Aviation Administration, Department of Transportation
We are adopting a new airworthiness directive (AD) for all Pacific Aerospace Ltd. Model FBA-2C1, FBA-2C2, FBA-2C3, and FBA-2C4 airplanes. This AD was prompted by a report of corrosion found in the external and internal surfaces of an elevator push-pull rod. This AD requires an inspection for corrosion of the elevator push-pull rod assembly, and corrective actions if necessary. We are issuing this AD to address the unsafe condition on these products.
Airworthiness Directives; Airbus SAS Airplanes
Document Number: 2019-01522
Type: Rule
Date: 2019-02-12
Agency: Federal Aviation Administration, Department of Transportation
We are adopting a new airworthiness directive (AD) for certain Airbus SAS Model A321-111, -112, -131, -211, -212, -213, -231, and -232 airplanes. This AD was prompted by a report that during removal of left-hand (LH) gear rib 5, four failed fasteners were discovered. This AD requires a one-time ultrasonic inspection of the LH and right-hand (RH) wing rib 5-to-rear spar attachments for cracked or failed fasteners, and if necessary, a detailed inspection of the gear rib 5 and spar web for cracks and damage; a rotating probe test of the gear rib and spar web bolt holes for cracks and damage; reaming the gear rib and the spar web bolt holes; and replacement of cracked or failed fasteners. We are issuing this AD to address the unsafe condition on these products.
Airworthiness Directives; The Boeing Company Airplanes
Document Number: 2019-01520
Type: Rule
Date: 2019-02-12
Agency: Federal Aviation Administration, Department of Transportation
We are adopting a new airworthiness directive (AD) for all The Boeing Company Model 737-100, -200, -200C, -300, -400, and -500 series airplanes. This AD was prompted by a report of cracks in a certain body station (STA) frame web and doubler at fastener holes common to the stop fitting at a certain stringer. This AD requires repetitive surface high frequency eddy current (HFEC) inspections for cracking of the frame web and doubler at the stop fitting at a certain stringer, and applicable on-condition actions. We are issuing this AD to address the unsafe condition on these products.
Airworthiness Directives; the Boeing Company Airplanes
Document Number: 2019-01518
Type: Rule
Date: 2019-02-12
Agency: Federal Aviation Administration, Department of Transportation
We are superseding Airworthiness Directive (AD) 2016-18-01, which applied to certain The Boeing Company Model 737-600, -700, -700C, -800, -900, and -900ER series airplanes. AD 2016-18-01 required repetitive lubrication of the forward and aft trunnion pin assemblies of the right and left main landing gears (MLGs); repetitive inspection of these assemblies for corrosion and chrome damage, and related investigative and corrective actions if necessary; and installation of new or modified trunnion pin assembly components, which terminated the repetitive lubrication and repetitive inspections. Since we issued AD 2016-18-01, we have determined that rotable parts were not addressed in that AD, and it is therefore necessary to include all airplanes of the affected models in the applicability. This AD retains the requirements of AD 2016-18-01, adds airplanes to the applicability, and prohibits the installation of a MLG or MLG trunnion pin assembly under certain conditions. We are issuing this AD to address the unsafe condition on these products.
Update to Investigative and Enforcement Procedures
Document Number: 2019-00771
Type: Proposed Rule
Date: 2019-02-12
Agency: Federal Aviation Administration, Department of Transportation
The FAA proposes to revise the procedural rules governing Federal Aviation Administration investigations and enforcement actions. The proposed revisions include updates to statutory and regulatory references, updates to agency organizational structure, elimination of inconsistencies, clarification of ambiguity, increases in efficiency, and improved readability.
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