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AD 2001-12-08 R1 ACTIVE

Escape Ropes
Key Information
AD Number 2001-12-08 R1 Status Active
Effective Date July 20, 2001 Issue Date October 18, 2001
Docket Number 2000-NM-116-AD Amendment 39-12480
Product Type ["Aircraft"] Product Subtype ["Large Airplane"]
CFR Part --- - Part 39 CFR Section N/A
Citation (Federal Register: October 26, 2001 (Volume 66, Number 208))
Applicability
Manufacturer(s) The Boeing Company
Model(s) 767-200 Series 767-300 Series 767-300F Series 767-400ER Series
Related Airworthiness Directives
Supersedes 2001-12-08
Summary

This amendment corrects and clarifies information in an existing airworthiness directive (AD) that applies to certain Boeing Model 767 series airplanes. That AD currently requires removing the two existing escape ropes in the flight compartment; installing new escape ropes, bags, and placards; and replacing the nylon straps with new straps; as applicable. This document clarifies and corrects the affected airplane line numbers. This correction is necessary to ensure that operators do not misinterpret which airplanes are subject to the requirements of this AD. \n\n\tThe incorporation by reference of certain publications listed in the regulations was approved previously by the Director of the Federal Register as of July 20, 2001 (66 FR 32531, June 15, 2001).

Action Required

Final rule; correction

Regulatory Text

2001-12-08 R1 Boeing: Amendment 39-12480. Docket 2000-NM-116-AD. Revises AD 2001-12-08, Amendment 39-12263.\n\n\tApplicability: Model 767 series airplanes, line numbers 1 through 334, certificated in any category; excluding those airplanes having line numbers 265, 281, 284, 286, 288, 293, and 298.\n\n\tNote 1: This AD applies to each airplane identified in the preceding applicability provision, regardless of whether it has been modified, altered, or repaired in the area subject to the requirements of this AD. For airplanes that have been modified, altered, or repaired so that the performance of the requirements of this AD is affected, the owner/operator must request approval for an alternative method of compliance in accordance with paragraph (b) of this AD. The request should include an assessment of the effect of the modification, alteration, or repair on the unsafe condition addressed by this AD; and, if the unsafe condition has not been eliminated, the request should include specific proposed actions to address it.\n\n\tCompliance: Required as indicated, unless accomplished previously.\n\n\tTo ensure that flight crew members safely reach the ground from a flight compartment window in the event of an emergency evacuation, accomplish the following:\n\nReplacement\n\n\t(a) Within 18 months after the effective date of this AD, do the actions specified in paragraphs (a)(1) and (a)(2) of this AD, as applicable, per Boeing Alert Service Bulletin 767-25A0265, dated May 27, 1999.\n\n\t\t(1) For all airplanes: Remove the two existing escape ropes and install new escape ropes, bags, and placards, as applicable, in the flight compartment.\n\n\t\t(2) For airplanes having line numbers 1 through 107 inclusive; on which Boeing Service Bulletin 767-25-0149, dated March 7, 1991, has been accomplished; or on which neither Boeing Service Bulletin 767-25-0149, dated March 7, 1991, nor 767-25A0242, dated October 31, 1996, has been accomplished: Replace the nylon straps with new straps.\n\nAlternative Methods of Compliance\n\n\t(b) An alternative method of compliance or adjustment of the compliance time that provides an acceptable level of safety may be used if approved by the Manager, Seattle Aircraft Certification Office (ACO), FAA. Operators shall submit their requests through an appropriate FAA Principal Maintenance Inspector, who may add comments and then send it to the Manager, Seattle ACO.\n\n\tNote 2: Information concerning the existence of approved alternative methods of compliance with this AD, if any, may be obtained from the Seattle ACO.\n\nSpecial Flight Permits\n\n\t(c) Special flight permits may be issued in accordance with sections 21.197 and 21.199 of the Federal Aviation Regulations (14 CFR 21.197 and 21.199) to operate the airplane to a location where the requirements of this AD can be accomplished.\n\nIncorporation by Reference\n\n\t(d) The actions shall be done in accordance with Boeing Alert Service Bulletin 767-25A0265, dated May 27, 1999. This incorporation by reference was approved previously by the Director of the Federal Register as of July 20, 2001 (66 FR 32531, June 15, 2001). Copies may be obtained from Boeing Commercial Airplane Group, P.O. Box 3707, Seattle, Washington 98124-2207. Copies may be inspected at the FAA, Transport Airplane Directorate, 1601 Lind Avenue, SW., Renton, Washington; or at the Office of the Federal Register, 800 North Capitol Street, NW., suite 700, Washington, DC.\n\nEffective Date\n\n\t(e) The effective date of this amendment remains July 20, 2001.

Supplementary Information

On June 6, 2001, the Federal Aviation Administration (FAA) issued AD 2001-12-08, amendment 39-12263 (66 FR 32531, June 15, 2001), which applies to certain Boeing Model 767 series \nairplanes. That AD requires removing the two existing escape ropes in the flight compartment; installing new escape ropes, bags, and placards; and replacing the nylon straps with new straps; as applicable. That action was necessary to ensure that flight crew members safely reach the ground from a flight compartment window in the event of an emergency evacuation. That action is intended to address the identified unsafe condition.\n\nNeed for the Correction\n\n\tInformation obtained recently by the FAA indicates that the applicability of AD 2001-12-08 and the applicability of paragraph (a)(2) of that AD need to be clarified and corrected.\n\n\tAs published, the applicability of the AD references Boeing Alert Service Bulletin 767-25A0265, dated May 27, 1999, as the appropriate source ofservice information for determining the affected Model 767 series airplanes. The service bulletin references Service Bulletin Index Document D624T001, Part 3, for airplane variable number, line number, and serial number data. Because some operators may not readily have access to this secondary source of service information, the FAA has determined that the applicability of the AD should specify the affected airplane line numbers (i.e., line numbers 1 through 334, excluding line numbers 265, 281, 284, 286, 288, 293, and 298), which were identified in the Summary of Boeing Alert Service Bulletin 767-25A0265.\n\n\tParagraph (a)(2) of AD 2001-12-08 affects airplanes having "serial numbers 1 through 107 inclusive." However, the reference to "serial numbers" is incorrect. The FAA's intent was to list "line numbers 1 through 107 inclusive," as indicated in the referenced Boeing Alert Service Bulletin 767-25A0265, dated May 27, 1999.\n\n\tThe FAA has determined that a correction to AD 2001-12-08 is necessary. The correction will clarify and correct the affected airplane line numbers.\n\nCorrection of Publication\n\n\tThis document corrects and clarifies the errors of AD 2001-12-08 and correctly adds the AD as an amendment to section 39.13 of the Federal Aviation Regulations (14 CFR 39.13).\n\n\tThe AD is reprinted in its entirety for the convenience of affected operators. The effective date of the AD remains July 20, 2001.\n\n\tSince this action only clarifies and corrects a current requirement, it has no adverse economic impact and imposes no additional burden on any person. Therefore, the FAA has determined that notice and public procedures are unnecessary.\n\nList of Subject in 14 CFR Part 39\n\n\tAir transportation, Aircraft, Aviation safety, Incorporation by reference, Safety.\n\nAdoption of the Correction\n\n\tAccordingly, pursuant to the authority delegated to me by the Administrator, the Federal Aviation Administration amends part 39 of the Federal Aviation Regulations (14 CFR part 39) as follows:\n\nPART 39--AIRWORTHINESS DIRECTIVES\n\n\t1. The authority citation for part 39 continues to read as follows:\n\n\tAuthority: 49 U.S.C. 106(g), 40113, 44701.\n\nSec. 39.13 (Amended)\n\n\t2. Section 39.13 is amended by removing amendment 39-12263 (66 FR 32531, June 15, 2001), and by adding a new airworthiness directive (AD), amendment 39-12480, to read as follows:

For Further Information Contact

John Picolla, Aerospace Engineer, Airframe Branch, ANM-120S, FAA, Seattle Aircraft Certification Office, 1601 Lind Avenue, SW., Renton, Washington 98055-4056; telephone (425)\n227-1509; fax (425) 227-1181.