Federal Aviation Administration June 20, 2008 – Federal Register Recent Federal Regulation Documents

Hawaii Air Tour Common Procedures Manual, FAA AWP13-136A
Document Number: E8-14014
Type: Notice
Date: 2008-06-20
Agency: Federal Aviation Administration, Department of Transportation
This notice announces the availability of and requests comments on the proposed draft for the Hawaii Air Tour Common Procedures Manual, draft AWP13-136A.
Airworthiness Directives; Boeing Model 707 Airplanes and Model 720 and 720B Series Airplanes
Document Number: E8-13925
Type: Proposed Rule
Date: 2008-06-20
Agency: Federal Aviation Administration, Department of Transportation
We propose to adopt a new airworthiness directive (AD) for all Boeing Model 707 airplanes and Model 720 and 720B series airplanes. This proposed AD would require performing an operational test of the engine fuel suction feed of the fuel system, and other related testing if necessary. This proposed AD results from a report of in-service occurrences of loss of fuel system suction feed capability, followed by total loss of pressure of the fuel feed system. We are proposing this AD to detect and correct failure of the engine fuel suction feed of the fuel system, which could result in multi-engine flameout, inability to restart the engines, and consequent forced landing of the airplane.
Airworthiness Directives; Empresa Brasileira de Aeronautica S.A. (EMBRAER) Model EMB-135 Airplanes, and Model EMB-145, -145ER, -145MR, -145LR, -145XR, -145MP, and -145EP Airplanes
Document Number: E8-13923
Type: Proposed Rule
Date: 2008-06-20
Agency: Federal Aviation Administration, Department of Transportation
The FAA proposes to supersede an existing airworthiness directive (AD) that applies to all EMBRAER Model EMB-135 airplanes and Model EMB-145, -145ER, -145MR, -145LR, -145XR, -145MP, and -145EP airplanes. The existing AD currently requires replacing the metallic tubes enclosing the vent and pilot valve wires in the left- and right- hand wing fuel tanks with non-conductive hoses. This proposed AD would add airplanes to the applicability of the existing AD. This proposed AD results from fuel system reviews conducted by the manufacturer. We are proposing this AD to prevent an ignition source inside the fuel tank that could ignite fuel vapor and cause a fuel tank explosion and loss of the airplane.
Airworthiness Directives; Bombardier Model CL-600-2B19 (Regional Jet Series 100 and 440) Airplanes
Document Number: E8-13922
Type: Proposed Rule
Date: 2008-06-20
Agency: Federal Aviation Administration, Department of Transportation
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 727 Airplanes
Document Number: E8-13920
Type: Proposed Rule
Date: 2008-06-20
Agency: Federal Aviation Administration, Department of Transportation
We propose to adopt a new airworthiness directive (AD) for certain Boeing Model 727 airplanes. This proposed AD would require performing an operational test of the engine fuel suction feed of the fuel system, and other related testing if necessary. This proposed AD results from a report of in-service occurrences of loss of fuel system suction feed capability, followed by total loss of pressure of the fuel feed system. We are proposing this AD to detect and correct failure of the engine fuel suction feed of the fuel system, which could result in multi-engine flameout, inability to restart the engines, and consequent forced landing of the airplane.
Airworthiness Directives; BAE Systems (Operations) Limited (Jetstream) Model 4101 Airplanes
Document Number: E8-13919
Type: Proposed Rule
Date: 2008-06-20
Agency: Federal Aviation Administration, Department of Transportation
The FAA proposes to supersede an existing airworthiness directive (AD) that applies to all BAE Systems (Operations) Limited (Jetstream) Model 4101 airplanes. The existing AD currently requires repetitive tests for free movement of the capsule/bearing of the nose landing gear (NLG), and related investigative and corrective actions. This proposed AD would require a modified test for free movement of the capsule/bearing of the NLG at reduced repeat intervals, and replacement of the NLG assembly with a modified assembly. This proposed AD results from additional reports of the NLG failing to extend fully on an airplane that had been inspected in accordance with AD 2004-14-07. We are proposing this AD to prevent failure of the NLG to extend fully, which could result in reduced controllability of the airplane during landing.
Miscellaneous Markings and Placards
Document Number: E8-13900
Type: Rule
Date: 2008-06-20
Agency: Federal Aviation Administration, Department of Transportation
This action corrects a typographical error that appeared in a final rule, which the FAA published in the Federal Register. In that final rule, the FAA inadvertently changed a word. The intent of this action is to correct the error in the regulation to ensure the requirement is clear and accurate.
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