Federal Aviation Administration August 7, 2008 – Federal Register Recent Federal Regulation Documents
Results 1 - 12 of 12
Newark Liberty International Airport Slots; Request for Bids
The FAA plans to auction a lease for a package of slots at Newark Liberty International Airport on September 3, 2008. If you are interested in participating in the auction, commenting on the planned auction procedures or draft lease terms, you will be able to find additional information and procedures for providing comments at https:// faaco.faa.gov.
Robinson R-22/R-44 Special Training and Experience Requirements
This action proposes to continue the existing special training and experience requirements in Special Federal Aviation Regulation (SFAR) No. 73 and eliminate the termination date for SFAR 73. Currently, SFAR No. 73 is a final rule that will expire on June 30, 2009. Since 1998, the FAA has extended SFAR 73 for two 5-year periods. The FAA recently re-issued SFAR No. 73 and extended the rule's expiration date to June 30, 2009. SFAR No. 73 requires special training and experience for pilots operating the Robinson model R-22 or R-44 helicopters in order to maintain the safe operation of Robinson helicopters. It also requires special training and experience for certified flight instructors conducting student instruction or flight reviews in R-22 or R-44 helicopters.
Airworthiness Directives; Cessna Aircraft Company (Type Certificate Previously Held by Columbia Aircraft Manufacturing) Models LC40-550FG, LC41-550FG, and LC42-550FG Airplanes
We propose to revise Airworthiness Directive (AD) 2007-07- 06, which applies to certain Cessna Aircraft Company (type certificate previously held by Columbia Aircraft Manufacturing) (Cessna) Models LC40-550FG, LC41-550FG, and LC42-550FG airplanes. AD 2007-07-06 currently requires the following: adding information to the limitations section of the airplane flight manual (AFM); repetitively inspecting the aileron and the elevator linear bearings and control rods for foreign object debris, scarring, or damage; and taking all necessary corrective actions. Since we issued AD 2007-07-06, Cessna has issued a new service bulletin that contains procedures for installing an access panel to facilitate the required inspections. Consequently, this proposed AD would retain the actions currently required in AD 2007-07- 06; allow installing access panels; and change the serial number applicability. We are proposing this AD to prevent jamming in the aileron and elevator control systems, which could result in failure. This failure could lead to loss of control.
Airworthiness Directives; Allied Ag Cat Productions, Inc. G-164 Series Airplanes
We propose to supersede Airworthiness Directive (AD) 78-08-09, which applies to certain Allied Ag Cat Productions, Inc. (formerly Grumman-American) Models G-164, G-164A, and G-164B airplanes. AD 78-08- 09 currently requires repetitively inspecting the interior and the exterior of the main tubular spar of the rudder assembly for corrosion, taking necessary corrective action if corrosion is found, and applying corrosion protection. Since we issued AD 78-08-09, the rudder main tubular spar failed on a later production airplane. Consequently, this proposed AD would retain the actions required in AD 78-08-09 and expand the applicability to include all G-164 series airplanes. We are proposing this AD to detect and correct corrosion in the rudder main tubular spar, which could result in failure of the weld to the main spar tube. This failure could lead to loss of directional control.
Airworthiness Directives; Fokker Model F.28 Mark 0100 Airplanes
We propose to adopt a new airworthiness directive (AD) for the products listed above that would supersede an existing AD. 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: * * * * *
Airworthiness Directives; Boeing Model 757-200, 757-200PF, and 757-300 Series Airplanes
We propose to adopt a new airworthiness directive (AD) for certain Boeing Model 757-200, 757-200PF, and 757-300 series airplanes. This proposed AD would require, for certain airplanes, measuring the electrical bond resistance at certain stations and doing any applicable repair; installing support brackets for the hot short protector and new support clamps for the wire bundles; installing the equipment of the hot short protector; and modifying an existing wire bundle and installing a new wire bundle. This proposed AD would also require, for certain other airplanes, measuring the electrical bond resistance at certain stations, measuring the electrical bonding resistance between the hot short protector and rear spar web, and doing any applicable repair. This proposed AD also would require revising the Airworthiness Limitations section of the Instructions for Continued Airworthiness. This proposed AD results from fuel system reviews conducted by the manufacturer. We are proposing this AD to prevent the center fuel tank densitometer from overheating and becoming a potential ignition source inside the fuel tank, which, in combination with flammable fuel vapors, could result in a center fuel tank explosion and consequent loss of the airplane.
Airworthiness Directives; Boeing Model 777 Airplanes
We propose to adopt a new airworthiness directive (AD) for certain Boeing Model 777 airplanes. This proposed AD would require doing an inspection of the motor operated valve (MOV) actuators of the main and center fuel tanks for a certain part number; replacing the MOV actuator with a new MOV actuator if necessary; and measuring the electrical resistance of the bond from the adapter plate to the airplane structure, and corrective actions if necessary. This proposed AD would also require revising the Airworthiness Limitations section of the Instructions for Continued Airworthiness. This proposed AD results from fuel system reviews conducted by the manufacturer. We are proposing this AD to prevent electrical current from flowing through a MOV actuator into a fuel tank, which could create a potential ignition source inside the fuel tank. This condition, in combination with flammable fuel vapors, could result in a fuel tank explosion and consequent loss of the airplane.
Airworthiness Directives; Airbus Model A310 Series Airplanes
We propose to adopt a new airworthiness directive (AD) for the products listed above. 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: Two operators of A300 aircraft fitted with General Electric (GE) CF6-50 engine series have reported cracks on the lower side of Rib 5 in the pylon box. Investigations disclosed that these cracks are due to the stresses resulting from the pressure applied by the thrust reverser cowl bumpers. Cracking of the engine pylons could result in reduced structural integrity of the engine support structure. The proposed AD would require actions that are intended to address the unsafe condition described in the MCAI.
Airworthiness Directives; Saab Model SAAB 2000 Airplanes
We propose to adopt a new airworthiness directive (AD) for the products listed above. 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:
Special Conditions: Airbus A318, A319, A320, and A321 Series Airplanes; Astronautics Electronic Flight Bags With Lithium Battery Installations
This action proposes special conditions for the Airbus A318, A319, A320, and A321 series airplanes. These airplanes, as modified by L2 Consulting Services, will have a novel or unusual design feature associated with Astronautics electronic flight bags which use lithium battery technology. The applicable airworthiness regulations do not contain adequate or appropriate safety standards for this design feature. These proposed 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; Eclipse Aviation Corporation Model EA500 Airplanes
The FAA is superseding emergency Airworthiness Directive (AD) 2008-13-51, which currently applies to all owners/operators of Eclipse Aviation Corporation (Eclipse) Model EA500 airplanes that received the emergency AD by letter issued June 12, 2008. Emergency AD 2008-13-51 requires owner/operators to insert temporary revisions into the emergency and normal procedures sections of the airplane flight manual (AFM), do a pilot evaluation of the throttles with replacement as necessary, and report the evaluation results to the FAA. Emergency AD 2008-13-51 was the result of the throttle position exceeding its maximum range. Since issuing that AD, Eclipse developed an FAA-approved test procedure and issued Eclipse Aviation Alert Service Bulletin SB 500-76-001, REV B, dated July 22, 2008. The service bulletin provides a standardized procedure for testing and modifying (as applicable) the throttle lever with replacement as necessary. We are issuing this AD to mandate the actions in this service bulletin to be done by a person authorized to perform maintenance and reduce the likelihood of the throttle position signal exceeding its maximum range, which could cause loss of left and right engine control. This condition could result in the inability to maintain desired airspeed and/or altitude with consequent loss of control.
Standard Instrument Approach Procedures, and Takeoff Minimums and Obstacle Departure Procedures; Miscellaneous Amendments
This Rule establishes, amends, suspends, or revokes 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 safe and efficient use of the navigable airspace and to promote safe flight operations under instrument flight rules at the affected airports.
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