Summary
The FAA is adopting a new airworthiness directive (AD) for certain Boeing airplanes, identified above. This AD requires inspecting to determine if certain motor-operated shutoff valve actuators for the fuel tanks are installed, and related investigative and corrective actions if necessary. This AD also requires revising the Airworthiness Limitations (AWLs) section of the Instructions for Continued Airworthiness to incorporate AWL No. 28-AWL-21, No. 28-AWL-22, and No. 28-AWL-24 (for Model 737-600, -700, -700C, -800 and -900 series airplanes); and No. 28-AWL-23, No. 28-AWL-24, and No. 28-AWL-25 (for Model 757-200, -200PF, -200CB, and -300 series airplanes). This AD results from a design review of the fuel tank systems. We are issuing this AD to prevent electrical energy from lightning, hot shorts, or fault current from entering the fuel tank through the actuator shaft, which could result in fuel tank explosions and consequent loss of the airplane.
Directive Details
AD Number
FAA-2007-28662
Document Number
E8-4486
Type
Rule
Publication Date
March 12, 2008
Effective Date
April 16, 2008
Affected Manufacturer
Boeing Model 737-600, -700, -700C, -800 and -900 Series
Criticality
important
Emergency
No
Docket ID
Docket No. FAA-2007-28662
Topics
Official Documents
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