Airworthiness directives › 2009-17-02
AD 2009-17-02 Airworthiness Directives; Saab AB, Saab Aerosystems Model SAAB 340A (SAAB/SF340A) and SAAB 340B Airplanes
Applicability*9
Saab AB, Saab Aerosystems Model SAAB 340A (SAAB/SF340A) and SAAB 340B airplanes; certificated in any category; all serial numbers.
Compliance
Unless already done, do the following actions: (1) Within 3 months after the effective date of this AD, inspect the illuminated placard of the refuel and defuel panel, part number (P/N) C4FL5031C001, for signs of heat and burn marks, in accordance with Saab Service Bulletin 340-28-027, Revision 01, dated July 7, 2008. (2) If any sign of heat or burn marks are found, before further flight, replace the illuminated placard of the refuel and defuel panel with a new illuminated placard of the refuel and defuel panel, having part number C4FL5031C001, and marked with a manufacturer date before 31/97 ( i.e., week 31 of 1997), or a manufacturing date of 37/07 ( i.e., week 37 of 2007) or higher and marked `Amdt:A.', in accordance with Saab Service Bulletin 340-28-027, Revision 01, dated July 7, 2008. (3) If no signs of heat and burn marks are found, within 12 months after accomplishing the inspection required by (f)(1) of this AD is done, replace the illuminated placard of the fuel and defuel panel with a new illuminated placard of the refuel and defuel panel, having part number C4FL5031C001, and marked with a manufacturer date before 31/97 ( i.e., week 31 of 1997) or a manufacturing date of 37/07 ( i.e., week 37 of 2007) or higher and marked `Amdt:A.', in accordance with Saab Service Bulletin 340-28-027, Revision 01, dated July 7, 2008. (4) As of 15 months after the effective date of this AD, installing an illuminated placard of the refuel and defuel panel is prohibited on any airplane, unless it has a manufacturing date before 31/97, or unless it has a manufacturing date of 37/07 or higher and is marked `Amdt:A'. (5) Actions accomplished before the effective date of this AD in accordance with Saab Service Bulletin 340-28-027, dated April 30, 2008, are considered acceptable for compliance with the corresponding actions specified in paragraphs (f)(1), (f)(2), and (f)(3) of this AD. FAA AD Differences Note 1: 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: Shahram Daneshmandi, Aerospace Engineer, International Branch, ANM-116, Transport Airplane Directorate, FAA, 1601 Lind Avenue, SW., Renton, Washington 98057-3356; telephone (425) 227-1112; fax (425) 227-1149. Before using any approved AMOC on any airplane to which the AMOC applies, notify your principal maintenance inspector (PMI) or principal avionics inspector (PAI), as appropriate, or lacking a principal inspector, your local Flight Standards District Office. The AMOC approval letter must specifically reference this AD. (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 Airworthiness Directive 2008-0127R1, dated August 7, 2008; and Saab Service Bulletin 340-28-027, Revision 01, dated July 7, 2008, for related information. Material Incorporated by Reference (i) You must use Saab Service Bulletin 340-28-027, Revision 01, dated July 7, 2008, 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 Saab Aircraft AB, SAAB Aerosystems, SE-581 88, Linköping, Sweden; telephone +46 13 18 5591; fax +46 13 18 4874; e-mail saab2000.techsupport@saabgroup.com ; Internet http://www.saabgroup.com. (3) You may review copies of the service information at the FAA, Transport Airplane Directorate, 1601 Lind Avenue, SW., Renton, Washington. For information on the availability of this material at the FAA, call 425-227-1221 or 425-227-1152. (4) You may also review copies of the service information that is incorporated by reference 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/code_of_federal_regulations/ibr_locations.html. Issued in Renton, Washington, on August 3, 2009. Ali Bahrami, Manager, Transport Airplane Directorate, Aircraft Certification Service. [FR Doc. E9-19182 Filed 8-17-09; 8:45 am] BILLING CODE 4910-13-P
Required actions
Unless already done, do the following actions: (1) Within 3 months after the effective date of this AD, inspect the illuminated placard of the refuel and defuel panel, part number (P/N) C4FL5031C001, for signs of heat and burn marks, in accordance with Saab Service Bulletin 340-28-027, Revision 01, dated July 7, 2008. (2) If any sign of heat or burn marks are found, before further flight, replace the illuminated placard of the refuel and defuel panel with a new illuminated placard of the refuel and defuel panel, having part number C4FL5031C001, and marked with a manufacturer date before 31/97 ( i.e., week 31 of 1997), or a manufacturing date of 37/07 ( i.e., week 37 of 2007) or higher and marked `Amdt:A.', in accordance with Saab Service Bulletin 340-28-027, Revision 01, dated July 7, 2008. (3) If no signs of heat and burn marks are found, within 12 months after accomplishing the inspection required by (f)(1) of this AD is done, replace the illuminated placard of the fuel and defuel panel with a new illuminated placard of the refuel and defuel panel, having part number C4FL5031C001, and marked with a manufacturer date before 31/97 ( i.e., week 31 of 1997) or a manufacturing date of 37/07 ( i.e., week 37 of 2007) or higher and marked `Amdt:A.', in accordance with Saab Service Bulletin 340-28-027, Revision 01, dated July 7, 2008. (4) As of 15 months after the effective date of this AD, installing an illuminated placard of the refuel and defuel panel is prohibited on any airplane, unless it has a manufacturing date before 31/97, or unless it has a manufacturing date of 37/07 or higher and is marked `Amdt:A'. (5) Actions accomplished before the effective date of this AD in accordance with Saab Service Bulletin 340-28-027, dated April 30, 2008, are considered acceptable for compliance with the corresponding actions specified in paragraphs (f)(1), (f)(2), and (f)(3) of this AD. FAA AD Differences Note 1: 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: Shahram Daneshmandi, Aerospace Engineer, International Branch, ANM-116, Transport Airplane Directorate, FAA, 1601 Lind Avenue, SW., Renton, Washington 98057-3356; telephone (425) 227-1112; fax (425) 227-1149. Before using any approved AMOC on any airplane to which the AMOC applies, notify your principal maintenance inspector (PMI) or principal avionics inspector (PAI), as appropriate, or lacking a principal inspector, your local Flight Standards District Office. The AMOC approval letter must specifically reference this AD. (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 Airworthiness Directive 2008-0127R1, dated August 7, 2008; and Saab Service Bulletin 340-28-027, Revision 01, dated July 7, 2008, for related information. Material Incorporated by Reference (i) You must use Saab Service Bulletin 340-28-027, Revision 01, dated July 7, 2008, 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 Saab Aircraft AB, SAAB Aerosystems, SE-581 88, Linköping, Sweden; telephone +46 13 18 5591; fax +46 13 18 4874; e-mail saab2000.techsupport@saabgroup.com ; Internet http://www.saabgroup.com. (3) You may review copies of the service information at the FAA, Transport Airplane Directorate, 1601 Lind Avenue, SW., Renton, Washington. For information on the availability of this material at the FAA, call 425-227-1221 or 425-227-1152. (4) You may also review copies of the service information that is incorporated by reference 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/code_of_federal_regulations/ibr_locations.html. Issued in Renton, Washington, on August 3, 2009. Ali Bahrami, Manager, Transport Airplane Directorate, Aircraft Certification Service. [FR Doc. E9-19182 Filed 8-17-09; 8:45 am] BILLING CODE 4910-13-P
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