Airworthiness directives › 2014-01-01
AD 2014-01-01 Airworthiness Directives; Turbomeca S.A. Turboshaft Engines
Applicability*9
This AD applies to all Turbomeca S.A. Arrius 2F turboshaft engines.
Compliance
After the effective date of this AD, do not install onto any engine a nozzle ejector assembly subject to this AD, or install any engine onto any helicopter if the engine has an ejector assembly containing a lubricating device with an S/N listed in Figure 1 to paragraph (e) of this AD, unless the engine has been inspected per the requirements of paragraph (e) of this AD.
Required actions
The Manager, Engine Certification Office, FAA, may approve AMOCs to this AD. Use the procedures found in 14 CFR 39.19 to make your request.
Unsafe condition
Comply with this AD within the compliance times specified, unless already done. (1) For engines equipped with a lubricating device having a serial number (S/N) listed in Figure 1 to paragraph (e) of this AD, within 30 days after the effective date of this AD, inspect the nozzle of the ejector assembly and the tightening torque. Use paragraph 6.B.(2)(b) 2 through 6.B.(2)(c) 4.2, excluding paragraph 6.B.(2)(b) 4, of Turbomeca Mandatory Service Bulletin (MSB) No. 319 79 4835, Version A, dated May 22, 2013, to do your inspection. (2) For any part that fails the inspection required by paragraph (e)(1) of this AD, before further flight, remove and replace the failed part with a part eligible for installation. Figure 1 to Paragraph ( e )—S/N's of Affected Lubricating Devices S/N's 105M 108M 109M 112B 120 122B 129M 134B 138B 141M 142B 147M 149B 210M 231 247 254 266M 270 292M 333M 443M 445M 467M 479M 526M 563M
Affected ADs
None.
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