AD 89-03-10

Active

Spoiler Wheel Command Units

Key Information
89-03-10
Active
March 15, 1989
Not specified
Unknown
39-6137
Applicability
["Aircraft"]
["Large Airplane"]
The Boeing Company
757-200 Series 757-200CB Series 757-200PF Series 757-300 Series
Regulatory Text

89-03-10 BOEING: Amendment 39-6137.\n\tApplicability: Model 757 series airplanes, as listed in Boeing Service Bulletin 757-27-0076, dated May 19, 1988, certificated in any category.\n\n\tCompliance: Required within the next 24 months after the effective date of this AD, unless previously accomplished.\n\n\tTo prevent uncommanded extension of three flight spoilers on one wing, due to failure of a spoiler wheel command unit, accomplish the following:\n\n\tA.\tReplace both spoiler wheel command units, in accordance with Boeing Service Bulletin 757-27-0076, dated May 19, 1988.\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 may add any comments 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 for the accomplishment of the inspections required by 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, 17900 Pacific Highway South, Seattle, Washington, or Seattle Aircraft Certification Office, FAA, Northwest Mountain Region, 9010 East Marginal Way South, Seattle, Washington.\n\n\tThis amendment (39-6137, AD 89-03-10) becomes effective March 15, 1989.

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References
This information is not available.
--- - Part 39
FAA Documents