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AD/CESSNA 180/95 - Intercooler and Associated Hoses
Cessna 180, 182 and Wren 460 Series AeroCessna 180, 182 and Wren 460 Series Aeroplanes
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Cessna 180, 182 and Wren 460 Series Aeroplanes
| AD/CESSNA 180/95 | Intercooler and Associated Hoses | 4/2009 DM |
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| Applicability: | Cessna Models 182Q and 182R aeroplanes equipped with:Societé de Motorisations Aéronautiques (SMA) aircraft diesel engine (ADE) Model SR305-230-1 installed under Supplemental Type Certificate (STC) SA03302AT; orSMA ADE Model SR305-230 converted to Model SR305-230-1 (by incorporation of SMA Service Bulletin SB-01-76-002) installed under STC SA03302AT. |
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| Requirement: | 1. Remove intercooler part number (P/N) SF01170004-0 and install reworked intercooler P/N SF01170004-1 and remove intercooler inlet and outlet hoses and install new intercooler inlet hose P/N SF01170083-0 and intercooler outlet hose P/N SF01170048-0.2. Inspect intercooler inlet and outlet hoses and clamps for displacement and re-torque clamps. If you find any displacement do the displacement recovery.3. Inspect the installation of the intercooler outlet hose and intercooler inlet hose assembly for any displacement or damage of clamps or hoses.4. If, any displacement or damage of clamps or hoses is found during the inspection detailed in Requirement 3 of this AD, replace any damaged clamps and hoses.5. Do not install any intercooler P/N SF01170004-0.SMA SAFRAN Group Service Bulletin SB-C182-75-004, Revision No. Basic Issue, dated 8 July 2008 provides the instructions for compliance with Requirements 1 through 4 of this AD.Later revisions of the above SB, approved by the United States Federal Aviation Administration (FAA) as an Alternate Method of Compliance (AMOC) to FAA AD 2009-04-05 are considered acceptable for compliance with the equivalent Requirements of this Directive.Note: FAA AD 2009-04-05 Amdt 39-15811 dated 6 February 2009 refers. |
| Compliance: | For Requirement 1 - Before further flight after the effective date of this AD.For Requirement 2 - Within the next 25 hours time-in service (TIS) following installation detailed in Requirement 1 of this AD.For Requirement 3 - Initially inspect within the next 100 hours TIS or within 12 months after the action detailed in Requirement 1 of this AD is carried out, whichever occurs first.Thereafter repeat the inspection at intervals not to exceed 100 hours TIS or 12 months, whichever occurs first.For Requirement 4 - Before further flight, after the inspection detailed in Requirement 3 of this AD is carried out and any displacement or damage of clamps or hoses is found.For Requirement 5 - From the effective date of this AD. |
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