The Federal Register http://thefederalregister.com/b.p/department/DEPARTMENT_OF_TRANSPORTATION/2003-12-23/ Daily Publications of Meetings and Rules Changes for the Federal Government Mon, Dec 1 2008 11:00:00 GMT Mon, Dec 1 2008 11:00:00 GMT info@thefederalregister.com <![CDATA[ Airworthiness Directives; Airbus Model A319, A320, and A321 Series Airplanes]]> http://thefederalregister.com/d.p/2003-12-23-03-31063 ]]> http://thefederalregister.com/d.p/2003-12-23-03-31063 Tue, Dec 23 2003 11:00:00 GMT <![CDATA[ Airworthiness Directives; Airbus Model A300 B4-600 Series Airplanes, Model A300 B4-600R Series Airplanes, Model A300]]> http://thefederalregister.com/d.p/2003-12-23-03-31191 ]]> http://thefederalregister.com/d.p/2003-12-23-03-31191 Tue, Dec 23 2003 11:00:00 GMT <![CDATA[ Airworthiness Directives; Airbus Model A319, A320, and A321 Series Airplanes Equipped With Certain Litton Air Data]]> http://thefederalregister.com/d.p/2003-12-23-03-31270 ]]> http://thefederalregister.com/d.p/2003-12-23-03-31270 Tue, Dec 23 2003 11:00:00 GMT <![CDATA[ Airworthiness Directives; Airbus Model A319-113 and -114 Series Airplanes; and Model A320-111, -211, and -212 Series]]> http://thefederalregister.com/d.p/2003-12-23-03-31271 ]]> http://thefederalregister.com/d.p/2003-12-23-03-31271 Tue, Dec 23 2003 11:00:00 GMT <![CDATA[ Airworthiness Directives; Boeing Model 747-100, 747-100B, 747- 100B SUD, 747-200B, 747-200C, 747-200F, 747-300,]]> http://thefederalregister.com/d.p/2003-12-23-03-31195 ]]> http://thefederalregister.com/d.p/2003-12-23-03-31195 Tue, Dec 23 2003 11:00:00 GMT <![CDATA[ Airworthiness Directives; Boeing Model 737-100, -200, -200C, - 300, -400, and -500 Series Airplanes]]> http://thefederalregister.com/d.p/2003-12-23-03-31273 [[Page 74174]]
onetime general visual inspection to identify the material of the rudder assembly, and corrective actions, if necessary. For airplanes with a graphite assembly, this action requires repetitive general visual inspections of the flange bolts of the rudder front spar for any loose bolts, and corrective actions, if necessary. This action is necessary to detect and correct loose bolts common to the flange of the rudder front spar and main thrust hinge and actuator assembly, as well as the auxiliary actuator support fitting, which could cause the rudder actuator to separate from the rudder during certain flight conditions, resulting in loss of rudder control and consequent loss of control of the airplane. This action is intended to address the identified unsafe condition. ]]> http://thefederalregister.com/d.p/2003-12-23-03-31273 Tue, Dec 23 2003 11:00:00 GMT <![CDATA[ Airworthiness Directives; Dassault Model Falcon 900 EX and Mystere-Falcon 900 Series Airplanes]]> http://thefederalregister.com/d.p/2003-12-23-03-31192 ]]> http://thefederalregister.com/d.p/2003-12-23-03-31192 Tue, Dec 23 2003 11:00:00 GMT <![CDATA[ Airworthiness Directives; McDonnell Douglas Model DC-10-10, DC- 10-10F, DC-10-15, DC-10-30, DC-10-30F, DC-10-30F]]> http://thefederalregister.com/d.p/2003-12-23-03-31193 ]]> http://thefederalregister.com/d.p/2003-12-23-03-31193 Tue, Dec 23 2003 11:00:00 GMT <![CDATA[ Airworthiness Directives; McDonnell Douglas Model MD-11 and -11F Airplanes]]> http://thefederalregister.com/d.p/2003-12-23-03-31196 ]]> http://thefederalregister.com/d.p/2003-12-23-03-31196 Tue, Dec 23 2003 11:00:00 GMT <![CDATA[ Airworthiness Directives; McDonnell Douglas Model MD-90-30 Airplanes]]> http://thefederalregister.com/d.p/2003-12-23-03-31439 ]]> http://thefederalregister.com/d.p/2003-12-23-03-31439 Tue, Dec 23 2003 11:00:00 GMT <![CDATA[ Safety Auditor Certification; Notice of Statutory Compliance Date]]> http://thefederalregister.com/d.p/2003-12-23-03-31597 ]]> http://thefederalregister.com/d.p/2003-12-23-03-31597 Tue, Dec 23 2003 11:00:00 GMT <![CDATA[ Pipeline Safety: Potential Service Disruptions in Supervisory Control and Data Acquisition Systems]]> http://thefederalregister.com/d.p/2003-12-23-03-31574 ]]> http://thefederalregister.com/d.p/2003-12-23-03-31574 Tue, Dec 23 2003 11:00:00 GMT