AD 89-13-04

Active

Takeoff Configuration Warning Systems

Key Information
89-13-04
Active
July 24, 1989
Not specified
Unknown
39-6238
Applicability
["Aircraft"]
["Large Airplane"]
The Boeing Company
757-200 Series 757-200CB Series 757-200PF Series 757-300 Series
Regulatory Text

89-13-04 BOEING: Amendment 39-6238. \n\tApplicability: Model 757 series airplanes specified in Boeing Alert Service Bulletin 757- 27A0063, Revision 1, dated May 17, 1985, certificated in any category. \n\n\tCompliance: Required within the next 12 months after the effective date of this AD, unless previously accomplished. \n\n\tTo prevent the occurrence of takeoff configuration false warnings, accomplish the following: \n\n\tA.\tModify the circuitry of the Takeoff Configuration Warning Systems (TOCWS) in accordance with Boeing Alert Service Bulletin 757-27A0063, Revision 1, dated May 17, 1985. \n\n\tB.\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, FAA, Northwest Mountain Region. \n\n\tNOTE: The request should be forwarded through an FAA Principal Maintenance Inspector (PMI), who will either concur or comment and then send it to the Manager, Seattle Aircraft Certification Office. \n\n\tC.\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 Airplanes, P.O. Box 3707, Seattle, Washington 98124. These documents may be examined at the FAA, Northwest Mountain Region, Transport Airplane Directorate, 17900 Pacific Highway South, Seattle, Washington, or Seattle Aircraft Certification Office, 9010 East Marginal Way South, Seattle, Washington. \n\n\tThis amendment (39-6238, AD 89-13-04) becomes effective on July 24, 1989.

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References
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--- - Part 39
FAA Documents