Airworthiness directives › 2015-14-02
AD 2015-14-02 Airworthiness Directives; GE Aviation Czech s.r.o. Turboprop Engines
Applicability*9
This AD applies to GE Aviation Czech s.r.o. M601E-11, M601E-11A, and M601F turboprop engines with the following serial numbers (S/Ns): (1) Model M601E-11: S/Ns 833244, 841289, 852239, 861007, 881217, 884021, 892046, 892219, 894018, 903028, 913038, and 912023. (2) Model M601E-11A: S/Ns 902004 and 883046. (3) Model M601F: S/Ns 912001 and 924002.
Compliance
If you performed the actions required by paragraphs (e)(1) and (e)(2) of this AD before the effective date of this AD using GE Aviation Czech s.r.o. ASBs No. M601E-11/28, M601E-11A/15, or M601F/26, all Revision 1, all dated December 23, 2014, as applicable, or Initial Issues, all dated June 27, 2014, as applicable, you have met the requirements of this AD.
Required actions
The Manager, Engine Certification Office, FAA, may approve AMOCs for this AD. Use the procedures found in 14 CFR 39.19 to make your request. You may email your request to: ANE-AD-AMOC@faa.gov.
Unsafe condition
Comply with this AD within the compliance times specified, unless already done. (1) Within 300 flight hours, or six months after the effective date of this AD, whichever occurs first, inspect the reduction gearbox and supporting cone. Use GE Aviation Czech s.r.o. Alert Service Bulletins (ASBs) No. M601E-11/28, M601E-11A/15, and M601F/26, all Revision 2, all dated January 23, 2015, including Appendix 2, paragraph 4., Inspection, (the issue date is not specified in the appendix), as applicable, to do the inspection. (2) If any crack is detected on the quill shaft, PT shaft, or the supporting cone, or if the quill shaft or PT shaft involute spline wear exceeds 0.12 mm, then before further flight, replace each cracked or worn part with a part eligible for installation.
Affected ADs
None.
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