Airworthiness directives › 95-14-04
AD 95-14-04 Airworthiness Directives; British Aerospace Model BAC 1-11 200 and 400 Airplanes
Models named: BAC 1-11 200, 400. Read the applicability below — it usually turns on serial or part numbers too.
Applicability*9
Model BAC 1-11 200 and 400 airplanes, certificated in any category. Note 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 [[Page 35323]] owner/operator must use the authority provided in paragraph (c) of this AD to request approval from the FAA. This approval may address either no action, if the current configuration eliminates the unsafe condition; or different actions necessary to address the unsafe condition described in this AD. Such a request should include an assessment of the effect of the changed configuration on the unsafe condition addressed by this AD. In no case does the presence of any modification, alteration, or repair remove any airplane from the applicability of this AD.
Compliance
Required as indicated, unless accomplished previously. To prevent reduced structural integrity of the airplane, accomplish the following: (a) Prior to reaching the ``Not Exceed Time'' interval specified in Table 1 of British Aerospace Alert Service Bulletin 5-A-PM5995, Issue 3, dated March 19, 1993; or within 15 months after the effective date of this AD; whichever occurs later: Install the structural modification listed in each Item in Table 1 of the alert service bulletin, except for Items 6, 11, 13, and 14. The modifications shall be done in accordance with the appropriate service bulletin specified for each Item in Table 1, listed under ``Service Bulletin No.'' Note 2: Items 6, 11, 13, and 14 in Table 1 of British Aerospace Alert Service Bulletin 5-A-PM5995, Issue 3, are not included in the requirements of this AD since those items are addressed by separate rulemaking actions. (b) Accomplishment of the modifications required by paragraph (a) of this AD constitutes terminating action for the repetitive inspections required by the following AD's: ------------------------------------------------------------------------ Amendment Federal Register AD No. No. citation Date of publication ------------------------------------------------------------------------ 67-30-02....... 39-0507 32 FR 15421 November 4, 1967. 87-21-06....... 39-5744 52 FR 38396 October 16, 1987. 82-01-02 R1.... 39-4824 49 FR 9412 March 13, 1984. 83-20-02....... 39-4735 48 FR 44462 September 29, 1983. 88-11-09....... 39-5891 53 FR 17918 May 19, 1988. 72-06-01....... 39-1406 37 FR 4900 March 7, 1972. 71-25-02....... 39-1349 36 FR 22363 November 25, 1971. ------------------------------------------------------------------------ (c) 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, Standardization Branch, ANM-113, FAA, Transport Airplane Directorate. Operators shall submit their requests through an appropriate FAA Principal Maintenance Inspector, who may add comments and then send it to the Manager, Standardization Branch, ANM-113. Note 3: Information concerning the existence of approved alternative methods of compliance with this AD, if any, may be obtained from the Standardization Branch, ANM-113. (d) 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. (e) The installation shall be done in accordance with British Aerospace Alert Service Bulletin 5-A-PM5995, Issue 3, dated March 19, 1993. This incorporation by reference was approved by the Director of the Federal Register in accordance with 5 U.S.C. 552(a) and 1 CFR part 51. Copies may be obtained from British Aerospace, Airbus Limited, P.O. Box 77, Bristol BS99 7AR, England. 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. (f) This amendment becomes effective on August 7, 1995. Issued in Renton, Washington, on June 23, 1995. James V. Devany, Acting Manager, Transport Airplane Directorate, Aircraft Certification Service. [FR Doc. 95-15995 Filed 7-6-95; 8:45 am] BILLING CODE 4910-13-U
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The directive text above is reproduced from the Federal Register, a work of the United States government and in the public domain. The separation into applicability, compliance and required actions is TrackAD's.*1