2008-15-06: Original engine mounting brackets

2008-15-06 Cessna Aircraft Company: Amendment 39-15618; Docket No. FAA-2007-29240; Directorate Identifier 2007-CE-076-AD. Effective Date (a) This AD becomes effective on September 2, 2008. Affected ADs (b) None. Applicability (c) This AD applies to the following airplane models and serial numbers that are certificated in any category: Model Serial Numbers Year Manufactured (1) 175 55001 through 55703. 1958 (2) 175 55704 through 56238... 1959 (3) 175 28700A, 626, and 640.... 1958 and 1959 (4) 175A 691, and 56239 through 56777. 1960 Unsafe Condition (d) A report that the engine became unattached from the firewall during landing on one of the affected airplanes prompts this AD. We are issuing this AD to detect and correct cracks in the engine mounting brackets, which could result in failure of the engine mounting bracket. This failure could lead to the engine detaching from the firewall. Compliance (e) To address thisproblem, you must do the following, unless already done: Actions Compliance Procedures (1) Check the airplane logbook to determine if all four of the original engine mounting brackets have been replaced. Within the next 30 days after September 2, 2008 (the effective date of this AD). The owner/operator holding at least a private pilot certificate as authorized by section 43.7 may do this action. (2) If you can positively determine that all four of the original engine mounting brackets have been replaced, no further action is required. Not applicable. Make an entry into the aircraft logbook showing compliance with this portion of the AD in accordance with 14 CFR 43.9. The owner/operator holding at least a private pilot certificate as authorized by section 43.7 may do this action. (3) If you cannot positively determine that all four of the original engine mounting brackets have been replaced, inspect each of the upper and lower engine mounting brackets on both the leftand right sides for cracks as specified in the service bulletin. Initially inspect within the next 12 months after September 2, 2008 (the effective date of this AD). If no cracks are found, repetitively inspect thereafter at intervals not to exceed 500 hours time-in-service (TIS) until all four of the original engine mounting brackets are replaced. Follow Cessna Single Engine Service Bulletin SEB07-2, Revision 2, dated June 18, 2007. (4) If cracks are found in any of the engine mounting brackets during any inspection required in paragraph (e)(3) of this AD, replace the cracked engine mounting bracket(s). Before further flight after the inspection in which cracks are found. Replacing the cracked engine mounting bracket terminates the repetitive inspection required in paragraph (e)(3) of this AD only for the replaced engine mounting bracket. Follow Cessna Single Engine Service Bulletin SEB07-2, Revision 2, dated June 18, 2007. (5) To terminate the repetitive inspections required inparagraph (e)(3) of this AD, you may replace all four original engine mounting brackets. At any time before or after the initial inspection required in paragraph (e)(3) of this AD. Follow Cessna Single Engine Service Bulletin SEB07-2, Revision 2, dated June 18, 2007. (6) Dispose of every replaced bracket following 14 CFR 43.10, paragraph (c)(6), which states the following: Mutilation. The part may be mutilated to deter its installation in a type certificated product. The mutilation must render the part beyond repair and incapable of being reworked to appear to be airworthy. Before further flight after the engine mounting bracket is removed for replacement. Not applicable. Alternative Methods of Compliance (AMOCs) (f) The Manager, Wichita Aircraft Certification Office (ACO), 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: Gary Park, Aerospace Engineer, FAA, Wichita ACO, 1801 AirportRoad, Room 100, Wichita, Kansas 67209; telephone: 316-946-4123; fax: 316-946-4107; e-mail address: [email protected]. 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. Material Incorporated by Reference (g) You must use Cessna Single Engine Service Bulletin SEB07-2, Revision 2, dated June 18, 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 Cessna Aircraft Company, Product Support, P.O. Box 7706, Wichita, Kansas 67277. (3) You may review copies at the FAA, Central Region, Office of the Regional Counsel, 901 Locust, Kansas City, Missouri 64106; or at the National Archives andRecords 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.