Federal Aviation Administration June 20, 2005 – Federal Register Recent Federal Regulation Documents

Treatments for Fruits and Vegetables
Document Number: C5-11460
Type: Proposed Rule
Date: 2005-06-20
Agency: Department of Agriculture, Animal and Plant Health Inspection Service, Federal Aviation Administration, Department of Transportation
Amendment of Class E Airspace; Harrisburg, PA
Document Number: C5-11329
Type: Rule
Date: 2005-06-20
Agency: Federal Aviation Administration, Department of Transportation
Airworthiness Directives; Raytheon Aircraft Company Model 390 Airplanes
Document Number: 05-12060
Type: Proposed Rule
Date: 2005-06-20
Agency: Federal Aviation Administration, Department of Transportation
The FAA proposes to adopt a new airworthiness directive (AD) for certain Raytheon Aircraft Company (Raytheon) Model 390 airplanes. This proposed AD would require you to replace the rudder pedal arm assemblies used in the rudder control system with parts of improved design. This proposed AD results from reports of cracks found on the rudder pedal arm assemblies. We are issuing this proposed AD to prevent failure of the rudder pedal arm assemblies caused by fatigue cracks. This failure could lead to loss of rudder control, loss of nose gear steering, and loss of toe brakes on the side on which the failure occurs.
Airworthiness Directives; The Lancair Company Model LC41-550FG Airplanes
Document Number: 05-11880
Type: Rule
Date: 2005-06-20
Agency: Federal Aviation Administration, Department of Transportation
The FAA is adopting a new airworthiness directive (AD) for certain The Lancair Company (Lancair) Model LC41-550FG airplanes. This AD requires both visual and dye penetrant inspections of the elevator torque tube assembly for cracks. If a crack is found, this AD requires replacement with a modified assembly that incorporates a steel doubler. This AD also requires replacement of the modified elevator torque tube assembly every 300 hours time-in-service or 18 months (whichever occurs first). This AD results from cracks found in the weld area of the elevator torque tube assembly. We are issuing this AD to detect and correct cracks in the elevator torque tube assembly, which could result in failure of the elevator torque tube assembly and subsequent loss of control of the airplane.