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Airworthiness directives › 2019-06-06

AD 2019-06-06 Airworthiness Directives; International Aero Engines AG Turbofan Engines

Superseded. This directive was replaced by AD 2021-05-18. Work to the current one.
2019-04-12
2019-03-28
39-19604
FAA-2019-0151
Engine
2021-05-18

Applicability*9

This AD applies to International Aero Engines AG (IAE) V2500-A1, V2522-A5, V2524-A5, V2525-D5, V2527-A5, V2527E-A5, V2527M-A5, V2528-D5, V2530-A5, V2533-A5 turbofan engines.

Compliance

Comply with this AD within the compliance times specified, unless already done.

Required actions

(1) For diffuser cases with a rear outer flange that is equal to or greater than 20,000 cycles since new (CSN) on the effective date of this AD, perform an initial borescope inspection (BSI) of zones 1, 2, and 3 of the diffuser case M-flange before accumulating the BSI Within (Cycles) listed in Table 1 to paragraph (g)(1) of this AD. Use the Accomplishment Instructions, paragraphs 2.A. through 2.G. for the appropriate engine model, of IAE Alert Non-Modification Service Bulletin (NMSB) V2500-ENG-72-A0706, dated February 14, 2019, to perform the inspection. ER28MR19.000 (2) For diffuser cases with a rear outer flange that have fewer than 20,000 CSN on the effective date of this AD, perform an initial BSI of zones 1, 2, and 3 of the diffuser case M-flange within 21,300 CSN, in accordance with the Accomplishment Instructions, paragraphs 2.A. through 2.G. for the appropriate engine model, of IAE Alert NMSB V2500-ENG-72-A0706, dated February 14, 2019. (3) If no cracks are found, perform a repetitive BSI not to exceed every 2,100 cycles since the previous BSI. (4) If cracks are found, remove the diffuser case and replace with a part eligible for installation or repeat the BSI within the intervals in either Table 2: Fly on Limits or Table 4: Fly on Limits, as appropriate for the affected the engine model, of IAE Alert NMSB V2500-ENG-72-A0706, dated February 14, 2019.

Unsafe condition

This AD was prompted by a crack found at the diffuser case M-flange during overhaul inspection. We are issuing this AD to prevent failure of the diffuser case. The unsafe condition, if not addressed, could result in uncontained diffuser case rupture, damage to the engine, and damage to the airplane.

Affected ADs

None.

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