AD/CF6/48 Amdt 1 - Nozzle Guide Vanes
2. NGVs Not Previously Inspected by Flex2. NGVs Not Previously Inspected by Flex Borescope:
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2. NGVs Not Previously Inspected by Flex Borescope:
Remove from service, or re-inspect using the Accomplishment Instructions of GE SB No. CF6-80E1 S/B 72-0217, Revision 2, dated 5 January 5 2004.
Note 3: FAA AD 2004-09-34 Amdt 39-13625 refers.
Compliance: For Requirement 1: Unless previously accomplished in accordance with the Conditions and Reinspection intervals listed in the "Inspection Table for Cracking in the Airfoil Outer Fillet," Figure 5, of GE Service Bulletin (SB) No. CF6-80E1 S/B 72-0217, Revision 2, or within 200 cycles-in-service-since-last inspection (CSLI), whichever is earlier.
For Requirement 2: For NGVs with more than 800 cycles-since-overhaul (CSO) on the effective date of this AD, within 50 cycles-in-service (CIS) after the effective date of this AD; thereafter in accordance with the Conditions and Reinspection intervals listed in the "Inspection Table for Cracking in the Airfoil Outer Fillet," Figure 5, of GE SB No. CF6-80E1 S/B 72-0217, Revision 2.