74-23-03 BOEING: Amendment 39-2003. Applies to all Model 727 Series Airplanes certificated in all categories and equipped with the Auto Pack Trip System. \n\tCompliance required as indicated unless already accomplished. \n\tTo prevent the inadvertent trip of both air conditioning packs and the subsequent rapid loss of cabin pressurization, accomplish the following: \n\t(A)\tWithin one calendar day after the effective date of this AD, as an interim action, during the first flight and on all subsequent flights until the action specified in paragraph (B) and (C) of this AD has been accomplished, control the Auto Pack Trip System in accordance with the information and procedures contained in Boeing 727 "Operations Manual Bulletin" Number 74-7 dated September 5, 1974; and \n\t(B)\tWithin 100 hours time in service after the effective date of this AD, unless paragraph (C) is already accomplished, collar the Auto Pack Trip circuit breaker on the P6 panel and install one placard adjacent to thecircuit breaker and one adjacent to the Auto Pack Trip Switch which reads, "Auto Pack Trip Inoperative". \n\t(C)\tAs terminating action of this AD, within the next 900 hours time in service after the effective date of this AD, modify the Auto Pack Trip System in accordance with the information contained in the following documents as applicable, or a method approved by the Chief, Engineering and Manufacturing Branch, FAA Northwest Region: \n\t\t(1)\tBoeing Alert Service Bulletin 727-36-21 dated September 20, 1974, or later FAA approved revisions, applies to 727-200 series airplanes. \n\t\t(2)\tBoeing Service Bulletin 727-36-17, Revision 2, dated October 4, 1974, or later FAA approved revisions, applies to the following 727-100 series airplanes if Boeing Service Bulletin 727-36-17 original issue and Revision 1 have been incorporated: \n\n\t727-116\tS/N 19811 \n\t727-116C \tS/N 19813 and 19814 \n\t727-21\t\tS/N 18992 thru 18999 \n\t727-21\t\tS/N 19005 thru 19007 \n\t727-21\t\tS/N 19035 thru 19038 \n\t727-21\t\tS/N 19257 thru 19262 \n\t727-21C \tS/N 19134 thru 19137 \n\n\t\t(3)\tBoeing Service Bulletin 727-36-18, Revision 1, dated October 4, 1974, or later FAA approved revisions, applies to the following 727-100 series airplanes if Boeing Service Bulletin 727-36-18 has been incorporated: \n\n\t727-155C \tS/N 19619 \n\n\t\t(4)\tBoeing Service Bulletin 727-36-22 dated October 4, 1974, or later FAA approved revisions, applies to the following 727-100 series airplanes: \n\n\t727-17\t\tS/N 20327 and 20328; \n\t\t\tS/N 20512 and 20513 \n\t727-41\t\tS/N 20422 thru 20426 \n\t727-113C \tS/N 20343 \n\t727-1H2 \tS/N 20533 \n\t727-1F8\tS/N 20421 \n\t727-C3\t\tS/N 20418 thru 20420 \n\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). All persons affected by this Directive who have not already received these documents from the manufacturer, may obtain copies upon request to the Boeing Commercial Airplane Company,P. O. Box 3707, Seattle, Washington 98124. These documents may be examined at FAA Northwest Region, 9010 East Marginal Way, Seattle, Washington 98108. \n\n\tThis amendment becomes effective November 8, 1974.