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Airworthiness directives › 2008-17-04

AD 2008-17-04 Airworthiness Directives; BAE Systems (Operations) Limited (Jetstream) Model 4101 Airplanes

2008-09-23
2008-08-19
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Airframe
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Models named: Jetstream 4101. Read the applicability below — it usually turns on serial or part numbers too.

Applicability*9

This AD applies to all BAE Systems (Operations) Limited Model Jetstream 4101 airplanes, certificated in any category, all serial numbers.

Compliance

Unless already done: Within 24 months after the effective date of this AD, do the following actions. (1) Modify the LH and RH wing fuel boost pump wiring in accordance with paragraphs 2.B. and 2.C. of the Accomplishment Instructions of BAE Systems (Operations) Limited Service Bulletin J41-28-014, Revision 1, dated December 21, 2007. (2) Inspect the LH and RH wing fuel high level sensor wiring in accordance with paragraph 2.D. of the Accomplishment Instructions of BAE Systems (Operations) Limited Service Bulletin J41-28-014, Revision 1, dated December 21, 2007. (3) When excess wiring and/or damaged wiring is found during the inspection required by paragraph (f)(2) of this AD, before next flight, accomplish the corrective actions as specified in paragraph 2.D. of the Accomplishment Instructions of BAE Systems (Operations) Limited Service Bulletin J41-28-014, Revision 1, dated December 21, 2007. FAA AD Differences Note: This AD differs from the MCAI and/or service information as follows: No differences. Other FAA AD Provisions (g) The following provisions also apply to this AD: (1) Alternative Methods of Compliance (AMOCs): The Manager, International Branch, ANM-116, Transport Airplane Directorate, FAA, has the authority to approve AMOCs for this AD, if requested using the procedures found in 14 CFR 39.19. Send information to ATTN: Todd Thompson, Aerospace Engineer, International Branch, ANM-116, Transport Airplane Directorate, FAA, 1601 Lind Avenue, SW., Renton, Washington 98057-3356; telephone (425) 227-1175; fax (425) 227-1149. Before using any approved AMOC on any airplane to which the AMOC applies, notify your appropriate principal inspector (PI) in the FAA Flight Standards District Office (FSDO), or lacking a PI, your local FSDO. (2) Airworthy Product: For any requirement in this AD to obtain corrective actions from a manufacturer or other source, use these actions if they are FAA-approved. Corrective actions are considered FAA-approved if they are approved by the State of Design Authority (or their delegated agent). You are required to assure the product is airworthy before it is returned to service. (3) Reporting Requirements: For any reporting requirement in this AD, under the provisions of the Paperwork Reduction Act, the Office of Management and Budget (OMB) has approved the information collection requirements and has assigned OMB Control Number 2120-0056. Related Information (h) Refer to MCAI EASA Airworthiness Directive 2008-0041, dated February 27, 2008; and BAE Systems (Operations) Limited Service Bulletin J41-28-014, Revision 1, dated December 21, 2007; for related information. Material Incorporated by Reference (i) You must use BAE Systems (Operations) Limited Service Bulletin J41-28-014, Revision 1, dated December 21, 2007, to do the actions required by this AD, unless the AD specifies otherwise. (1) The Director of the Federal Register approved the incorporation by reference of this service information under 5 U.S.C. 552(a) and 1 CFR part 51. (2) For service information identified in this AD, contact British Aerospace Regional Aircraft American Support, 13850 Mclearen Road, Herndon, Virginia 20171. (3) You may review copies at the FAA, Transport Airplane Directorate, 1601 Lind Avenue, SW., Renton, Washington; or at the National Archives and Records Administration (NARA). For information on the availability of this material at NARA, call (202) 741-6030, or go to: http://www.archives.gov/federal-register/cfr/ibr-locations.html. Issued in Renton, Washington, on August 5, 2008. Ali Bahrami, Manager, Transport Airplane Directorate, Aircraft Certification Service. [FR Doc. E8-18810 Filed 8-18-08; 8:45 am] BILLING CODE 4910-13-P

Required actions

Unless already done: Within 24 months after the effective date of this AD, do the following actions. (1) Modify the LH and RH wing fuel boost pump wiring in accordance with paragraphs 2.B. and 2.C. of the Accomplishment Instructions of BAE Systems (Operations) Limited Service Bulletin J41-28-014, Revision 1, dated December 21, 2007. (2) Inspect the LH and RH wing fuel high level sensor wiring in accordance with paragraph 2.D. of the Accomplishment Instructions of BAE Systems (Operations) Limited Service Bulletin J41-28-014, Revision 1, dated December 21, 2007. (3) When excess wiring and/or damaged wiring is found during the inspection required by paragraph (f)(2) of this AD, before next flight, accomplish the corrective actions as specified in paragraph 2.D. of the Accomplishment Instructions of BAE Systems (Operations) Limited Service Bulletin J41-28-014, Revision 1, dated December 21, 2007. FAA AD Differences Note: This AD differs from the MCAI and/or service information as follows: No differences. Other FAA AD Provisions (g) The following provisions also apply to this AD: (1) Alternative Methods of Compliance (AMOCs): The Manager, International Branch, ANM-116, Transport Airplane Directorate, FAA, has the authority to approve AMOCs for this AD, if requested using the procedures found in 14 CFR 39.19. Send information to ATTN: Todd Thompson, Aerospace Engineer, International Branch, ANM-116, Transport Airplane Directorate, FAA, 1601 Lind Avenue, SW., Renton, Washington 98057-3356; telephone (425) 227-1175; fax (425) 227-1149. Before using any approved AMOC on any airplane to which the AMOC applies, notify your appropriate principal inspector (PI) in the FAA Flight Standards District Office (FSDO), or lacking a PI, your local FSDO. (2) Airworthy Product: For any requirement in this AD to obtain corrective actions from a manufacturer or other source, use these actions if they are FAA-approved. Corrective actions are considered FAA-approved if they are approved by the State of Design Authority (or their delegated agent). You are required to assure the product is airworthy before it is returned to service. (3) Reporting Requirements: For any reporting requirement in this AD, under the provisions of the Paperwork Reduction Act, the Office of Management and Budget (OMB) has approved the information collection requirements and has assigned OMB Control Number 2120-0056. Related Information (h) Refer to MCAI EASA Airworthiness Directive 2008-0041, dated February 27, 2008; and BAE Systems (Operations) Limited Service Bulletin J41-28-014, Revision 1, dated December 21, 2007; for related information. Material Incorporated by Reference (i) You must use BAE Systems (Operations) Limited Service Bulletin J41-28-014, Revision 1, dated December 21, 2007, to do the actions required by this AD, unless the AD specifies otherwise. (1) The Director of the Federal Register approved the incorporation by reference of this service information under 5 U.S.C. 552(a) and 1 CFR part 51. (2) For service information identified in this AD, contact British Aerospace Regional Aircraft American Support, 13850 Mclearen Road, Herndon, Virginia 20171. (3) You may review copies at the FAA, Transport Airplane Directorate, 1601 Lind Avenue, SW., Renton, Washington; or at the National Archives and Records Administration (NARA). For information on the availability of this material at NARA, call (202) 741-6030, or go to: http://www.archives.gov/federal-register/cfr/ibr-locations.html. Issued in Renton, Washington, on August 5, 2008. Ali Bahrami, Manager, Transport Airplane Directorate, Aircraft Certification Service. [FR Doc. E8-18810 Filed 8-18-08; 8:45 am] BILLING CODE 4910-13-P

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