Federal Register Proposed Rules, Rules and Notices for June 4,2013

June 4,2013

PROPOSED RULES

Proposed Amendment of Class D and Class E Airspace; San Marcos, TX [FR DOC# 2013-13016] SUMMARY: This action proposes to amend Class D and Class E airspace at San Marcos, TX. Additional controlled airspace is necessary to accommodate new Standard Instrument Approach Procedures (SIAP) at San Marcos Municipal Airport and the decommissioning of the Garys Locator Outer Marker (LOM). The FAA is taking this action to enhance the safety and management of Instrument Flight Rules (IFR) operations for SIAPs at the airport. Adjustments to the geographic coordinates also would be made.

Proposed Establishment of Class E Airspace; Umatilla, FL [FR DOC# 2013-13020] SUMMARY: This action proposes to establish Class E Airspace at Umatilla, FL, to accommodate the Area Navigation (RNAV) Global Positioning System (GPS) Standard Instrument Approach Procedures at Umatilla Municipal Airport. This action would enhance the safety and airspace management of Instrument Flight Rules (IFR) operations at the airport.

 
RULES

Airworthiness Directives; The Boeing Company Airplanes [FR DOC# 2013-12717] SUMMARY: We are adopting a new airworthiness directive (AD) for certain The Boeing Company Model 747- 100, 747-100B, 747-100B SUD, 747-200B, 747-200F, 747-300, 747-400, 747-400D, 747-400F, 747SR, and 747SP series airplanes; Model 767-200, -300, -300F, and -400ER series airplanes; and Model 777-200, -200LR, -300, and -300ER series airplanes. This AD was prompted by operator or in-service reports of burned Boeing Material Specification (BMS) 8-39 urethane foam, and a report from the airplane manufacturer indicating that airplanes were assembled, throughout various areas of the airplane (including flight deck and cargo compartments), with seals made of BMS 8-39 urethane foam, a material with fire-retardant properties that deteriorate with age. This AD requires replacing certain seals made of BMS 8-39 urethane foam. We are issuing this AD to prevent the failure of urethane seals to maintain sufficient Halon concentrations in the cargo compartments to extinguish or contain fire or smoke, and to prevent penetration of fire or smoke in areas of the airplane that are difficult to access for fire and smoke detection or suppression.

Airworthiness Directives; Iniziative Industriali Italiane S.p.A. Airplanes [FR DOC# 2013-
12516] SUMMARY: We are adopting a new airworthiness directive (AD) for Iniziative
Industriali Italiane S.p.A. Models Sky Arrow 650 TC, Sky Arrow 650 TCN, Sky Arrow 650TCS, and Sky Arrow 650TCNS airplanes. 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 improper installation of the spherical bearing on the central hinge lever and a crack on the weld length of the horizontal tail/elevator plane hinge assembly. We are
issuing this AD to require actions to address the unsafe condition on these products.

Airworthiness Directives; Dassault Aviation Airplanes [FR DOC# 2013-12722] SUMMARY: We are adopting a new airworthiness directive (AD) for certain Dassault Aviation Model Mystere- Falcon 900 and Falcon 900EX airplanes. This AD was prompted by reports of chafing between the tail strobe power supply and a hydraulic line. This AD requires modifying the tail strobe power supply wire routing. We are issuing this AD to prevent chafing between the tail strobe power supply and a hydraulic line, which could result in hydraulic fluid leakage and possible fire due to arcing, and consequent loss of control of the airplane due to structural failure of the tail.

Airworthiness Directives; Embraer S.A. Airplanes [FR DOC# 2013-12900] SUMMARY: We are adopting a new airworthiness directive (AD) for certain Embraer S.A. Model ERJ 190 airplanes. This AD was prompted by reports of cracks on the side stay of the main landing gear (MLG). This AD requires repetitive measurements of the left-hand (LH) and right-hand (RH) MLG side stay support fitting to detect bushing migration, and eventual replacement of the bushing; and a detailed inspection for damage on the LH and RH MLG side stay support assembly, and related investigative and corrective actions if necessary. We are issuing this AD to prevent excessive bearing friction, which might compromise the MLG free fall extension and cause fatigue cracking on the MLG side stay and on its support
assembly, resulting in reduced structural integrity of the MLG.

Airworthiness Directives; Bell Helicopter Textron, Inc. (Bell) Helicopters [FR DOC# 2013-
12720] SUMMARY: We are adopting a new airworthiness directive (AD) for Bell Model 214B, 214B-1, and 214ST helicopters with a certain tail rotor hanger bearing (bearing)
installed. This AD requires inspecting the bearing to determine whether an incorrectly
manufactured seal material is installed on the bearing. This AD is prompted by a report
that certain bearings were manufactured with an incorrect seal material that does not meet Bell specifications. The actions specified by this AD are intended to prevent loss of
bearing grease, failure of the bearing, and subsequent loss of control of the helicopter.

Airworthiness Directives; Bombardier, Inc. Airplanes [FR DOC# 2013-12898] SUMMARY: We are adopting a new airworthiness directive (AD) for certain Bombardier, Inc. Model BD-100-1A10 (Challenger 300) airplanes. This AD was prompted by reports of failure of a screw cap or end cap of the hydraulic system accumulator while on the ground, which resulted in loss of use of that hydraulic system and high-energy impact damage to adjacent systems and structures. This AD would require inspecting for the correct serial number of a certain hydraulic system accumulator, and replacing affected hydraulic system accumulators with new or serviceable accumulators. We are issuing this AD to prevent failure of a screw cap or end cap and loss of the related hydraulic system, which could result in damage to airplane structure and consequent reduced controllability of the airplane.

 

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