Federal Aviation Administration August 12, 2009 – Federal Register Recent Federal Regulation Documents

Airworthiness Directives; McDonnell Douglas Model DC-9-30, DC-9-40, and DC-9-50 Series Airplanes
Document Number: E9-19265
Type: Proposed Rule
Date: 2009-08-12
Agency: Federal Aviation Administration, Department of Transportation
We propose to adopt a new airworthiness directive (AD) for certain McDonnell Douglas Model DC-9-30, DC-9-40, and DC-9-50 series airplanes. This proposed AD would require inspecting to determine the part numbers of the forward and aft auxiliary tank fuel boost and transfer pump conduit/conduit assembly and conduit assembly electrical connector, as applicable, and corrective actions if necessary. This proposed AD results from fuel system reviews conducted by the manufacturer. We are proposing this AD to detect and correct the potential for an arc/spark condition to occur within the fuel boost or transfer pump conduit assembly connectors and propagate into the forward and aft auxiliary fuel tanks, which could result in a fire or explosion.
Airworthiness Directives; Boeing Model 747-200C and -200F Series Airplanes
Document Number: E9-19262
Type: Proposed Rule
Date: 2009-08-12
Agency: Federal Aviation Administration, Department of Transportation
The FAA proposes to supersede an existing airworthiness directive (AD) that applies to certain Boeing Model 747-200C and -200F series airplanes. The existing AD currently requires repetitive inspections to find fatigue cracking in the floor panel attachment fastener holes of the upper chord of certain upper deck floor beams in Section 41 (i.e., body station 520 and forward), and repair if necessary. The existing AD also provides optional modifications, which extend the threshold for the initiation of certain repetitive inspections. This proposed AD would add repetitive inspections to find fatigue cracking in the floor panel attachment fastener holes of the upper chord of certain other upper deck floor beams in Section 41 and Section 42 (i.e., aft of body station 520); repetitive inspections to find fatigue cracking in the permanent fastener holes of the upper chord of certain upper deck floor beams in Section 41; and related investigative and corrective actions. This proposed AD would also provide a new optional modification, which would terminate certain repetitive inspections. This proposed AD results from new reports of cracking in the upper chord of the upper deck floor beams in Sections 41 and 42, and new analysis that shows the permanent fastener holes of the upper chord of certain upper deck floor beams in Section 41 are also susceptible to fatigue cracking. We are proposing this AD to detect and correct cracking in the upper chord of the upper deck floor beams. Such cracking could extend and sever the floor beams, which could result in rapid decompression and loss of controllability of the airplane.
Airworthiness Directives; Saab AB, Saab Aerosystems Model SAAB 340A (SAAB/SF340A) and SAAB 340B Airplanes
Document Number: E9-19261
Type: Proposed Rule
Date: 2009-08-12
Agency: Federal Aviation Administration, Department of Transportation
We are revising an earlier NPRM for the products listed above. This action revises the earlier NPRM by expanding the scope. 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:
Proposed Amendment of Class E Airspace; Midlothian-Waxahachie, TX
Document Number: E9-19251
Type: Proposed Rule
Date: 2009-08-12
Agency: Federal Aviation Administration, Department of Transportation
This action proposes to amend Class E airspace at Midlothian- Waxahachie, TX. Additional controlled airspace is necessary to accommodate new Standard Instrument Approach Procedures (SIAPs) at Mid- Way Regional Airport, Midlothian-Waxahachie, TX. This action would also reflect the name change to Mid-Way Regional Airport and update the geographic coordinates. The FAA is taking this action to enhance the safety and management of Instrument Flight Rules (IFR) operations for SIAPs at Mid-Way Regional Airport.
Proposed Revision of Class E Airspace; Noorvik, AK
Document Number: E9-19250
Type: Proposed Rule
Date: 2009-08-12
Agency: Federal Aviation Administration, Department of Transportation
This action proposes to establish Class E airspace at the Robert (Bob) Curtis Memorial Airport at Noorvik, AK. Two Standard Instrument Approach Procedures (SIAPs) are being developed for the Robert (Bob) Curtis Memorial Airport at Noorvik, AK. Additionally, one textual Obstacle Departure Procedure (ODP) is being developed. Adoption of this proposal would result in establishing Class E airspace upward from 700 feet (ft.) above the surface at the Robert (Bob) Curtis Memorial Airport at Noorvik, AK.
Special Conditions: Boeing Model 747-8/-8F Airplanes; Additional Airframe Structural Design Requirements Related to Sudden Engine Stoppage Due to Fan Blade Failures
Document Number: E9-19249
Type: Rule
Date: 2009-08-12
Agency: Federal Aviation Administration, Department of Transportation
These special conditions are issued for Boeing Model 747-8/-8F airplanes. These airplanes will have a novel or unusual design feature(s) associated with an increased engine size when compared to previous model airplanes. These larger engines with larger bypass fans are capable of producing higher and more complex dynamic loads than previously experienced in older designs. 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: Boeing Model 747-8/-8F Airplanes; Interaction of Systems and Structures
Document Number: E9-19246
Type: Rule
Date: 2009-08-12
Agency: Federal Aviation Administration, Department of Transportation
These special conditions are issued for the Boeing Model 747- 8/-8F airplanes. These airplanes will have a novel or unusual design feature(s) that will affect structural performance. 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.
Airworthiness Directives; Short Brothers Model SD3-60 Airplanes
Document Number: E9-19181
Type: Rule
Date: 2009-08-12
Agency: Federal Aviation Administration, Department of Transportation
We are revising an existing airworthiness directive (AD) for the products listed above. This 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:
Notice of Intent To Rule on Request To Release Airport Property at the Seattle-Tacoma International Airport, Seattle, WA
Document Number: E9-19055
Type: Notice
Date: 2009-08-12
Agency: Federal Aviation Administration, Department of Transportation
The FAA proposes to rule and invite public comment on the release of land at the Seattle-Tacoma International Airport under the provisions of section 125 of the Wendell H. Ford Aviation Investment Reform Act for the 21st Century (AIR 21).
IFR Altitudes; Miscellaneous Amendments
Document Number: E9-18851
Type: Rule
Date: 2009-08-12
Agency: Federal Aviation Administration, Department of Transportation
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.
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