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AD 88-21-03 R1 ACTIVE

Fuel Crossfeed Valve
Key Information
AD Number 88-21-03 R1 Status Active
Effective Date November 18, 1988 Issue Date Not specified
Docket Number Unknown Amendment 39-6077
Product Type ["Aircraft"] Product Subtype ["Large Airplane"]
CFR Part --- - Part 39 CFR Section N/A
Citation This information is not available.
Applicability
Manufacturer(s) Airbus The Boeing Company
Model(s) A300 B2-1A A300 B2-1C A300 B2-203 A300 B2K-3C A300 B4-103 A300 B4-203 A300 B4-2C A310-203 A310-221 A310-222 737-200 Series 737-300 Series 757-200 Series 767-200 Series 767-300 Series
Regulatory Text

88-21-03 R1 AIRBUS INDUSTRIE AND BOEING: Amendment 39-6045 as amended by Amendment 39-6077. Applies to all Airbus Model A300 and A310-200 series airplanes, and Boeing Models 737-200, 737-300, 757-200, 767-200, and 767-300 series airplanes, certificated in any category, which are approved for operations over a route that contains a point farther than one hour flying time at the normal one-engine inoperative cruise speed (in still air) from an adequate airport in deviation from Section 121.161 of the Federal Aviation Regulations, referred to as "extended range," "EROP," or "ETOP" operations. Compliance required within 30 days after the effective date of the AD, unless previously accomplished. \n\n\tTo prevent failure of the fuel crossfeed valve during a single engine diversion on an extended range flight, which could result in the inability of the airplane to stay within the airplane lateral imbalance limit or in fuel starvation in the operating engine before the airplane is ableto reach the diversion airport, accomplish the following: \n\n\tA.\tRevise the LIMITATIONS SECTION of the FAA-approved Airplane Flight Manual (AFM) or Flight Manual Appendix, as appropriate, by adding the following instructions. This may be accomplished by inserting a copy of this AD in the AFM. \n\n\t\tFuel Crossfeed Valve. \n\n\t\tPerform an operational check of the fuel crossfeed valve during the last hour of \n\t\tcruise flight during each extended range operation. Enter valve failure conditions\n\t\tresulting from the operational check in the airplane log. \n\n\tB.\tRepair or replace, prior to next flight, any fuel crossfeed valve system component not exhibiting proper operation. \n\n\tC.\tAn alternate means of compliance or adjustment of the compliance time, which provides an acceptable level of safety and which has the concurrence of an FAA Principal Operations Inspector, may be used when approved by the Manager, Seattle Aircraft Certification Office, FAA, Northwest Mountain Region. \n\n\t\tNOTE: The request should be forwarded through an FAA Principal Operations Inspector (POI), who may add any comments and then send it to the Manager, Seattle Aircraft Certification Office. \n\n\tThis amendment revises AD 88-21-03, Amendment 39-6045, effective October 24, 1988. \n\tThis amendment, 39-6077, becomes effective November 18, 1988.