Airworthiness Directives; Airbus Model A310 and A300-600 Series Airplanes
airworthiness · Rule · Final rule. · Published 1997-04-10 · Effective 1997-05-15 · 62 FR 17536
Document
Document number
97-9011
Federal Register citation
62 FR 17536
Type
Rule
Action
Final rule.
Category
airworthiness
Manufacturer
Airbus Model A310 and A300-600 Series
Publication date
1997-04-10
Effective date
1997-05-15
FAA docket
Docket No. 94-NM-196-AD
Abstract
This amendment adopts a new airworthiness directive (AD), applicable to certain Airbus Model A310 and A300-600 series airplanes, that requires a functional flow test and leak test to verify if the pressure reducing valve in the cargo fire extinguishing system is in a serviceable condition, and replacement of any faulty valve with a new valve prior to extended range twin-engine operations of the airplane. This amendment is prompted by a report that, during a scheduled maintenance check, an inoperative pressure reducing valve was found in the cargo fire extinguishing system. The actions specified by this AD are intended to ensure that a faulty pressure reducing valve is not installed, which could result in reduced fire protection of the cargo compartment of the airplane.