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AD 96-17-02 SUPERSEDED

Fuel Shutoff Valves
WARNING: This AD has been superseded and is no longer active. Replaced by: 98-26-04. Refer to the superseding AD(s) for current requirements.
Key Information
AD Number 96-17-02 Status Superseded
Effective Date August 28, 1996 Issue Date Not specified
Docket Number 96-NM-195-AD Amendment 39-9710
Product Type ["Aircraft"] Product Subtype ["Large Airplane"]
CFR Part --- - Part 39 CFR Section N/A
Citation This information is not available.
Applicability
Manufacturer(s) The Boeing Company
Model(s) 757 Series (all)
Related Airworthiness Directives
Superseded By 98-26-04
Regulatory Text

96-17-02 BOEING : Amendment 39-9710. Docket 96-NM-195-AD.\n\n Applicability: Model 757 series airplanes, line positions 478 through 699 inclusive; certificated in any category.\n\n NOTE 1: This AD applies to each airplane identified in the preceding applicability provision, regardless of whether it has been modified, altered, or repaired in the area subject to the requirements of this AD. For airplanes that have been modified, altered, or repaired so that the performance of the requirements of this AD is affected, the owner/operator must request approval for an alternative method of compliance in accordance with paragraph (b) of this AD. The request should include an assessment of the effect of the modification, alteration, or repair on the unsafe condition addressed by this AD; and, if the unsafe condition has not been eliminated, the request should include specific proposed actions to address it.\n\n Compliance: Required as indicated, unless accomplished previously. \n\n To prevent uncommanded fuel flow from the fuel tanks to the engine nacelle in the event of a leak in the engine fuel line or a fire in the engine nacelle, accomplish the following:\n\n (a) Within 60 days after the effective date of this AD, perform an inspection to detect leakage of the fuel shutoff (spar) valves and verify that the valves do not leak when commanded to close, in accordance with Boeing Alert Service Bulletin 757-28A0045, dated July 30, 1996.\n\n (l) If both fuel shutoff valves pass the inspection for leakage and the valves close when commanded, no further action is required by this AD.\n\n (2) If either or both of the fuel shutoff valves do not pass the inspection for leakage: Prior to further flight, adjust the engine fuel shutoff valve(s) in accordance with Part III of the alert service bulletin and repeat the requirements of paragraph (a) of this AD.\n\n (b) An alternative method of compliance or adjustment of the compliance time that provides an acceptable level of safety may be used if approved by the Manager, Seattle Aircraft Certification Office (ACO), FAA, Transport Airplane Directorate. Operators shall submit their requests through an appropriate FAA Principal Maintenance Inspector, who may add comments and then send it to the Manager, Seattle ACO.\n\n NOTE 2: Information concerning the existence of approved alternative methods of compliance with this AD, if any, may be obtained from the Seattle ACO.\n \n (c) The actions shall be done in accordance with Boeing Alert Service Bulletin 757-28A0045, dated July 30, 1996. This incorporation by reference was approved by the Director of the Federal Register in accordance with 5 U.S.C. 552(a) and 1 CFR part 51. Copies may be obtained from Boeing Commercial Airplane Group, P.O. Box 3707, Seattle, Washington 98124-2207. Copies may be inspected at the FAA, Transport Airplane Directorate, 1601 Lind Avenue, SW., Renton, Washington; or at the Office of the Federal Register, 800 North Capitol Street, NW., suite 700, Washington, DC.\n\n (d) This amendment becomes effective on August 28, 1996.

For Further Information Contact

Bernie Gonzalez, Aerospace Engineer, Propulsion Branch, ANM-140S, FAA, Seattle Aircraft Certification Office, 1601 Lind Avenue, SW., Renton, Washington; telephone (206) 227-2682; fax (206) 227-1181.