AD 87-06-11

Active

Cargo Restraints

Key Information
87-06-11
Active
April 13, 1987
Not specified
Unknown
39-5576
Applicability
["Aircraft"]
["Large Airplane"]
The Boeing Company
747-100 Series 747-100B Series 747-100B SUD Series 747-200B Series 747-200C Series 747-200F Series 747-300 Series 747-400 Series 747-400D Series 747-400F Series 747SP Series 747SR Series
Regulatory Text

87-06-11 BOEING: Amendment 39-5576. Applies to Model 747 convertible and freighter series airplanes listed in Boeing Alert Service Bulletin 747-53A2273, dated July 29, 1986, certificated in any category. \n\n\tTo prevent inadvertent in-flight movement of main deck cargo on freighter or convertible airplanes, accomplish the following, unless already accomplished: \n\n\tA.\tWithin 10 landings after the effective date of this AD, or immediately after the replacement or reinstallation of the restraint hardware, unless the requirements of paragraph B., for removal of placards, decals, or stencils, are accomplished, install suitable placards, decals, or stencils at all restraints along both left and right buttock lines (BL) 98.2, 9.8, and 1.8, between body stations (BS) 980 and 1500, that state the following: \n\n\t\t"This restraint is inoperative. Cargo must be tied down per FAA-approved procedures." \n\n\tB.\tPlacards, decals, or stencils installed in accordance with the provisions of paragraph A., above, may be removed at each location where a determination is made in accordance with Boeing Service Bulletin 747-53A2273, dated July 29, 1986, or later FAA- approved revisions, that the restraint lip overlap meets or exceeds the minimum value specified therein, or if terminating action defined in paragraph C., below, is accomplished. \n\n\tC.\tTerminating action for this amendment consists of the inspection of the seat track alignment and, if necessary, modification of the floor beams between body station 980 and 1480 in accordance with Section III., Part II of the Boeing Service Bulletin 747-53A2273, dated July 29, 1986, or later FAA-approved revisions. \n\n\tD.\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 Maintenance Inspector, may be used when approved by the Manager, Seattle Aircraft Certification Office, FAA, Northwest Mountain Region. \n\n\tE.\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 inspections and/or modifications required by this AD. \n\n\tAll persons affected by this directive who have not already received the applicable service bulletin from the manufacturer may obtain copies upon request to the Boeing Commercial Airplane Company, P.O. Box 3707, Seattle, Washington 98124-2207. This information may be examined at the FAA, Northwest Mountain Region, 17900 Pacific Highway South, Seattle, Washington, or the Seattle Aircraft Certification Office, 9010 East Marginal Way South, Seattle, Washington. \n\n\tThis Amendment becomes effective April 13, 1987.

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