AD 91-05-11

Active

AFM Changes - Extended Range

Key Information
91-05-11
Active
March 26, 1991
Not specified
90-NM-196-AD
39-6909
Applicability
["Aircraft"]
["Large Airplane"]
The Boeing Company
737-300 Series
Regulatory Text

91-05-11 BOEING: Amendment 39-6909. Docket No. 90-NM-196-AD. \n\n\tApplicability: Model 737-300 series airplanes, equipped with CFM56-3 series engines, certificated in any category. \n\n\tCompliance: Required as indicated, unless previously accomplished. \n\n\tTo reduce the risk of total engine thrust loss due to unavoidable severe weather penetration during an ETOPS single engine diversion, accomplish the following: \n\n\tA.\tWithin the next 30 days after June 12, 1989 (the effective date of Amendment 39-6247), delete from the FAA-approved Airplane Flight Manual (AFM) any reference to approval or suitability of the Model 737-300 airplane for use in extended range operation. This may be accomplished by replacing the existing AFM page(s) containing the Extended Range Operations suitability statement with a page(s) which has that statement deleted. If the existing AFM does not contain such a statement, then no action is necessary. \n\n\tB.\tA new AFM ETOPS suitability statement, outlined below, may be inserted into the FAA-approved AFM when the airplane has been configured in accordance with Boeing Document D6-38123, Revision A, dated September 14, 1990, "Configuration, Maintenance and Procedures for Extended Range Operation" (CMP): \n\n\t\t\t\tEXTENDED RANGE OPERATIONS \n\n\tThe type design reliability and performance of this airplane/engine combination has been evaluated in accordance with FAA Advisory Circular 120-42A and found suitable for extended range operations when configured in accordance with FAA-approved Boeing Document D6- 38123, Revision A, dated September 14, 1990, "Configuration, Maintenance and Procedures for Extended Range (ER) Operation." This finding does not constitute approval to conduct extended range operations. \n\n\tC.\tAn alternate means of compliance or adjustment of the compliance time, which provides an acceptable level of safety, may be used when approved by the Manager, Seattle Aircraft Certification Office (ACO), FAA, Transport Airplane Directorate. \n\n\tNOTE: The request should be submitted directly to the Manager, Seattle ACO, and a copy sent to the cognizant FAA Principal Inspector (PI). The PI will then forward comments or concurrence to the Seattle ACO. \n\n\tD.\tSpecial flight permits may be issued in accordance with FAR 21.197 and 21.199 to operate airplanes to a base in order to comply with the requirements of this AD. \n\n\tAll persons affected by this directive who have not already received the appropriate service documents from the manufacturer may obtain copies upon request to Boeing Commercial Airplane Group, P.O. Box 3707, Seattle, Washington 98124. These documents may be examined at the FAA, Northwest Mountain Region, Transport Airplane Directorate, 1601 Lind Avenue SW., Renton, Washington. \n\n\tAirworthiness Directive 91-05-11 supersedes AD 89-13-06, Amendment 39-6247. \n\tThis amendment (39-6909, AD 91-05-11) becomes effective on March 26, 1991.

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References
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--- - Part 39
FAA Documents