Department of Transportation March 26, 2008 – Federal Register Recent Federal Regulation Documents
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Reports, Forms, and Recordkeeping Requirements Agency Information Collection Activity Under OMB Review
In compliance with the Paperwork Reduction Act of 1995 (44 U.S.C. 3501 et seq.), this notice announces that the Information Collection Request (ICR) abstracted below has been forwarded to the Office of Management and Budget (OMB) for review and comment. The ICR describes the nature of the information collections and their expected burden. The Federal Register Notice with a 60-day comment period was published on January 22, 2008, Volume 73, Number 14, Page Numbers 3800 and 3801. This document describes two collections of information for which NHTSA intends to seek OMB approval.
Pipeline Safety: Issues Related to Mechanical Couplings Used in Natural Gas Distribution Systems
PHMSA published a document in the Federal Register of March 4, 2008, issuing an advisory bulletin concerning failures of mechanical couplings and related appurtenances in natural gas distribution systems. The document described certain affected pipe incorrectly and did not clearly identify the State involved in certain data.
Airworthiness Standards; Aircraft Engine Standards Overtorque Limits
The FAA proposes to amend the certification standards for aircraft engines to introduce requirements for approval of maximum engine overtorque. This action would add a new engine overtorque test, amend engine ratings and operating limitations, and define maximum engine overtorque for certain turbopropeller and turboshaft engines. The proposed rule is intended to harmonize applicable U.S. and European standards and simplify airworthiness approvals for import and export of aircraft engines.
Petition for Exemption; Summary of Petition Received
This notice contains a summary of a petition seeking relief from specified requirements of 14 CFR. The purpose of this notice is to improve the public's awareness of, and participation in, this aspect of FAA's regulatory activities. 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.
Airworthiness Directives; Boeing Model 737-300, -400, and -500 Series Airplanes
We propose to adopt a new airworthiness directive (AD) for all Boeing Model 737-300, -400, and -500 series airplanes. This proposed AD would require repetitive inspections for discrepancies of the fuse pins of the inboard and outboard midspar fittings of the nacelle strut, and corrective actions if necessary. This proposed AD results from a report of corrosion damage of the chrome runout on the head side found on all four midspar fuse pins of the nacelle strut. Additionally, a large portion of the chrome plate was missing from the corroded area of the shank. We are proposing this AD to detect and correct discrepancies of the fuse pins of the inboard and outboard midspar fittings of the nacelle strut, which could result in reduced structural integrity of the fuse pins and consequent loss of the strut and separation of the engine from the airplane.
Airworthiness Directives; Boeing Model 727-200 Series Airplanes Equipped with an Auxiliary Fuel Tank System Installed in Accordance with Supplemental Type Certificate SA1350NM
We are adopting a new airworthiness directive (AD) for certain Boeing Model 727-200 series airplanes. This AD requires deactivating auxiliary fuel tank systems installed in accordance with Supplemental Type Certificate (STC) SA1350NM. This AD results from fuel tank system reviews conducted by the manufacturer that identified potential unsafe conditions for which the manufacturer has not provided corrective actions. We are issuing this AD to prevent the potential of 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; Saab Model SAAB-Fairchild SF340A (SAAB/SF340A) and SAAB 340B Airplanes
We are adopting a new 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:
Airworthiness Directives; MORAVAN a.s. Model Z-143L Airplanes
We are adopting a new airworthiness directive (AD) for the products listed above. 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:
Airworthiness Directives; Pacific Aerospace Limited Model 750XL Airplanes
We are adopting a new airworthiness directive (AD) for the products listed above. This AD results from mandatory continuing airworthiness information (MCAI) issued 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 \1/8\-inch rivets installed in place of the correct \5/32\-inch rivets that secure the horizontal tail surface load transfer angles to the rearmost fuselage frame at Station 384.62. We are issuing this AD to require actions to correct the unsafe condition on these products.
Airworthiness Directives; APEX Aircraft Model CAP 10 B Airplanes
We are adopting a new airworthiness directive (AD) for the products listed above. This AD results from mandatory continuing airworthiness information (MCAI) issued 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:
Airworthiness Directives; Pacific Aerospace Corporation, Ltd. Models FU24-954 and FU24A-954 Airplanes
We are adopting a new airworthiness directive (AD) for the products listed above. This AD results from mandatory continuing airworthiness information (MCAI) issued 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:
Airworthiness Directives; APEX Aircraft Model CA 10B Airplanes
We are adopting a new airworthiness directive (AD) for the products listed above. This AD results from mandatory continuing airworthiness information (MCAI) issued 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:
Agency Information Collection Activity Seeking OMB Approval
The FAA invites public comments about our intention to request the Office of Management and Budget's (OMB) revision of a current information collection. The Federal Register Notice with a 60-day comment period soliciting comments on the following collection of information was published on December 6, 2007, vol. 72, no. 234, page 68949. This collection maintains a reservation reporting system for unscheduled instrument flight rule (IFR) arrivals at Chicago's O'Hare International Airport.
Establishment of Class E Airspace; Hinton, OK
This action established Class E airspace at Hinton, OK. New Area Navigation (RNAV) Global Positioning System (GPS) Standard Instrument Approach Procedures (SIAPs) at Hinton Muni Airport has made this action necessary. The FAA is proposing this action to enhance the safety and management of Instrument Flight Rules (IFR) aircraft operations at Hinton Muni Airport, OK.
Agency Information Collection Activity Seeking OMB Approval
The FAA invites public comments about our intention to request the Office of Management and Budget's (OMB) revision of a current information collection. The Federal Register Notice with a 60-day comment period soliciting comments on the following collection of information was published on December 6, 2007, vol. 72, no. 234, page 68950. The respondents supply information to the FAA Civil Aviation Registry's Aircraft Registration Branch in order to obtain an authorization code for access to the International Registry.
Airworthiness Directives; Turbomeca Arriel 1B, 1D, 1D1, and 1S1 Turboshaft Engines
The FAA is superseding an existing airworthiness directive (AD) for certain Turbomeca Arriel 1B, 1D, 1D1, and 1S1 turboshaft engines. That AD currently requires initial and repetitive position checks of the gas generator 2nd stage turbine blades on all Turbomeca Arriel 1B, 1D, 1D1, and 1S1 turboshaft engines. That AD also currently requires initial and repetitive replacements of 2nd stage turbines on 1B, 1D, and 1D1 engines only. This AD requires adding a 3,000 hour life limit to Arriel 1B 2nd stage turbine blades. This AD results from reports of failures of second stage turbine blades. We are issuing this AD to prevent failures of the 2nd stage turbine blades, which could result in uncommanded in-flight engine shutdown, and subsequent forced autorotation landing or accident.
Airworthiness Directives; Avidyne Corporation Primary Flight Displays (Part Numbers 700-00006-000, -001, -002, -003, and -100)
The FAA is adopting a new airworthiness directive (AD) for certain Avidyne Corporation (Avidyne) Primary Flight Displays (PFDs) (Part Numbers (P/Ns) 700-00006-000, -001, -002, -003, and -100) that are installed on airplanes. This AD requires a check of the maintenance records and inspection of the PFD (if necessary) to determine if an affected serial number PFD is installed. If an affected serial number PFD is installed, this AD requires you to incorporate information that limits operation when certain conditions for the PFD or backup instruments exist. This AD results from several field reports of PFDs displaying incorrect altitude and airspeed information. We are issuing this AD to prevent certain conditions from existing when PFDs display incorrect attitude, altitude, and airspeed information. This could result in airspeed/altitude mismanagement or spatial disorientation of the pilot with consequent loss of airplane control, inadequate traffic separation, or controlled flight into terrain.
Federal Motor Vehicle Safety Standards, Child Restraint Systems; Anthropomorphic Test Devices
This document reopens the comment period on a supplemental notice of proposed rulemaking (SNPRM) to amend Federal Motor Vehicle Safety Standard (FMVSS) No. 213, ``Child Restraint Systems.'' Among other things, the SNPRM proposed to specify procedures the agency would use to position a Hybrid III 10-year-old child dummy and a Hybrid III 6-year-old child dummy in booster seats when conducting FMVSS No. 213 compliance tests. Comments on the SNPRM were due March 24, 2008. The Juvenile Products Manufacturers Association (JPMA) petitioned NHTSA to extend the comment period by a minimum of 60 days to appropriately respond with comments to the notice. We have granted the request to extend the comment period and are reopening the comment period for 45 days.
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