AD 78-04-02

Active

Attach Bolt Replacement

Key Information
78-04-02
Active
August 16, 1978
Not specified
Unknown
39-3267
Applicability
["Aircraft"]
["Large Airplane"]
The Boeing Company
737-100 Series 737-200 Series 737-200C Series
Regulatory Text

78-04-02\tBOEING: Amendment 39-3140 as amended by Amendment 39-3267. Applies to all Boeing Model 737-100/200/200C/T43A series airplanes, listed in Boeing Service Bulletin No. 737-53-1048 which have not had the bolt replacement accomplished per figure 1 of that service bulletin, certificated in all categories. \n\tA.\tWithin the next 75 flight hours time-in-service after January 16, 1978, unless accomplished within the last 3,000 flight hours time-in-service, accomplish paragraph B below. \n\tB.\tRemove panels 9126 L.H. and 9226 R.H. and check all attach bolts (16 per side) of the two horizontal stabilizer hinge outboard fittings for looseness. If found loose, before further flight, tighten bolt(s) to 65-80 in.-lbs. or accomplish the bolt replacement of figure 1 of Boeing Service Bulletin No. 737-53-1048, or later FAA approved revisions, or equivalent approved by the Chief, Engineering and Manufacturing Branch, FAA Northwest Region. In the event it is impracticable to perform the inspection within 75 flight hours time-in-service after January 16, 1978, permission to ferry an airplane to a location where the inspection can be accomplished, may be obtained by contacting the Chief, Engineering and Manufacturing Branch, FAA Northwest Region. \n\tC.\tWithin the next 3,000 flight hours time-in-service after the inspection accomplished per paragraph A of this AD, and thereafter at intervals not to exceed 3,000 flight hours time-in- service, accomplish the inspection of paragraph B. \n\tD.\tTerminating action to this AD consists of replacement of the attach bolts of the horizontal stabilizer hinge outboard fittings in accordance with Figure 1 of Boeing Service Bulletin No. 737-53-1048, or later FAA approved revisions, or in a manner approved by the Chief, Engineering and Manufacturing Branch, FAA Northwest Region. \n\tThe manufacturer's specifications and procedures identified and described in this directive are incorporated herein and made a part hereof pursuant to 5 U.S.C. 552(a)(1). \n\tAll persons affected by this directive who have not already received these documents from the manufacturer, may obtain copies upon request to Boeing Commercial Airplane Company, P.O. Box 3707, Seattle, Washington 98124. These documents may also be examined at FAA, Northwest Region, 9010 East Marginal Way South, Seattle, Washington 98108. \n\tAmendment 39-3140 became effective February 14, 1978. \n\tThis amendment 39-3267 becomes effective August 16, 1978.

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