Airworthiness directives › 2008-13-19
AD 2008-13-19 Airworthiness Directives; ATR Model ATR42-200, -300, -320, -500 Airplanes; and Model ATR72-101, -201, -102, -202, -211, -212, and -212A Airplanes
Models named: ATR42-200, -300, -320, -500, ATR72-101, -201, -102, -202, -211, -212. Read the applicability below — it usually turns on serial or part numbers too.
Applicability*9
This AD applies to ATR Model ATR42-200, -300, -320, and -500 airplanes and Model ATR72-101, -201, -102, -202, -211, -212, and -212A airplanes; certificated in any category; all serial numbers; except for airplanes having ATR Modification 05469 installed in production, or installed in service in accordance with Avions de Transport Regional Service Bulletin ATR42-30-0072 or ATR72-30-1042, both Revision l, both dated June 1, 2005; as applicable.
Compliance
Unless already done, do the following actions. (1) Within 550 flight hours after the effective date of this AD, measure the heating resistance of the three pitot probes, in accordance with the Accomplishment Instructions of Avions de Transport Regional Service Bulletin ATR42-30-0074 or ATR72-30-1044, both Revision 01, both dated September 26, 2007, as applicable. If any resistance exceeds 50 ohms, before next flight, replace the pitot probe in accordance with the Accomplishment Instructions of the applicable service bulletin. Repeat the measurement thereafter at intervals not to exceed 550 flight hours, until the current sensors have been replaced as required by paragraph (f)(2) of this AD. (2) Within 5,000 flight hours after the effective date of this AD, replace the three pitot probe current sensors, in accordance with the Accomplishment Instructions of Avions de Transport Regional Service Bulletin ATR42-30-0072 or ATR72-30-1042, both Revision 1, both dated June 1, 2005, as applicable. Doing this paragraph ends the repetitive inspections required by paragraph (f)(1) of this AD. (3) Actions are also acceptable for compliance with the requirements of paragraph (f)(1) of this AD if done before the effective date of this AD in accordance with the Accomplishment Instructions of Avions de Transport Regional Service Bulletin ATR42-30-0074 or ATR72-30-1044, both dated May 14, 2007, as applicable. 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: Tom Rodriguez, Aerospace Engineer, International Branch, ANM-116, Transport Airplane Directorate, FAA, 1601 Lind Avenue, SW., Renton, Washington 98057-3356; telephone (425) 227-1137; 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 European Aviation Safety Agency (EASA) Airworthiness Directive 2007-0179, dated July 31, 2007, and the service information described in Table 1 of this AD, for related information. Table 1.—Service Information Avions de Transport Regional Service Bulletin Revision Date ATR42-30-0072 1 June 1, 2005. ATR42-30-0074 01 September 26, 2007. ATR72-30-1042 1 June 1, 2005. ATR72-30-1044 01 September 26, 2007. Material Incorporated by Reference (i) You must use the applicable service information specified in Table 2 of this AD to do the actions required by this AD, unless the AD specifies otherwise. Avions de Transport Regional Service Bulletin ATR42-30-0072, Revision, 1 dated June 1, 2005, contains the following effective pages: Page Nos. Revision level shown on page Date shown on page 1, 2 1 June 1, 2005. 3-9 Original October 21, 2004. (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 ATR, 316 Route de Bayonne, 31060 Toulouse, Cedex 03, France. (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 . Table 2.—Material Incorporated by Reference Avions de Transport Regional Service Bulletin Revision Date ATR42-30-0072 1 June 1, 2005. ATR42-30-0074 01 September 26, 2007. ATR72-30-1042 1 June 1, 2005. ATR72-30-1044 01 September 26, 2007. Issued in Renton, Washington, on June 8, 2008. Michael Kaszycki, Acting Manager, Transport Airplane Directorate, Aircraft Certification Service. [FR Doc. E8-14191 Filed 7-1-08; 8:45 am] BILLING CODE 4910-13-P
Required actions
Unless already done, do the following actions. (1) Within 550 flight hours after the effective date of this AD, measure the heating resistance of the three pitot probes, in accordance with the Accomplishment Instructions of Avions de Transport Regional Service Bulletin ATR42-30-0074 or ATR72-30-1044, both Revision 01, both dated September 26, 2007, as applicable. If any resistance exceeds 50 ohms, before next flight, replace the pitot probe in accordance with the Accomplishment Instructions of the applicable service bulletin. Repeat the measurement thereafter at intervals not to exceed 550 flight hours, until the current sensors have been replaced as required by paragraph (f)(2) of this AD. (2) Within 5,000 flight hours after the effective date of this AD, replace the three pitot probe current sensors, in accordance with the Accomplishment Instructions of Avions de Transport Regional Service Bulletin ATR42-30-0072 or ATR72-30-1042, both Revision 1, both dated June 1, 2005, as applicable. Doing this paragraph ends the repetitive inspections required by paragraph (f)(1) of this AD. (3) Actions are also acceptable for compliance with the requirements of paragraph (f)(1) of this AD if done before the effective date of this AD in accordance with the Accomplishment Instructions of Avions de Transport Regional Service Bulletin ATR42-30-0074 or ATR72-30-1044, both dated May 14, 2007, as applicable. 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: Tom Rodriguez, Aerospace Engineer, International Branch, ANM-116, Transport Airplane Directorate, FAA, 1601 Lind Avenue, SW., Renton, Washington 98057-3356; telephone (425) 227-1137; 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 European Aviation Safety Agency (EASA) Airworthiness Directive 2007-0179, dated July 31, 2007, and the service information described in Table 1 of this AD, for related information. Table 1.—Service Information Avions de Transport Regional Service Bulletin Revision Date ATR42-30-0072 1 June 1, 2005. ATR42-30-0074 01 September 26, 2007. ATR72-30-1042 1 June 1, 2005. ATR72-30-1044 01 September 26, 2007. Material Incorporated by Reference (i) You must use the applicable service information specified in Table 2 of this AD to do the actions required by this AD, unless the AD specifies otherwise. Avions de Transport Regional Service Bulletin ATR42-30-0072, Revision, 1 dated June 1, 2005, contains the following effective pages: Page Nos. Revision level shown on page Date shown on page 1, 2 1 June 1, 2005. 3-9 Original October 21, 2004. (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 ATR, 316 Route de Bayonne, 31060 Toulouse, Cedex 03, France. (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 . Table 2.—Material Incorporated by Reference Avions de Transport Regional Service Bulletin Revision Date ATR42-30-0072 1 June 1, 2005. ATR42-30-0074 01 September 26, 2007. ATR72-30-1042 1 June 1, 2005. ATR72-30-1044 01 September 26, 2007. Issued in Renton, Washington, on June 8, 2008. Michael Kaszycki, Acting Manager, Transport Airplane Directorate, Aircraft Certification Service. [FR Doc. E8-14191 Filed 7-1-08; 8:45 am] BILLING CODE 4910-13-P
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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