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Airworthiness directives › 2012-06-18

AD 2012-06-18 Airworthiness Directives; Pratt & Whitney Division Turbofan Engines

2012-04-27
2012-03-23
39-16999
FAA-2011-1194
Engine
—

Applicability*9

This AD applies to all Pratt & Whitney PW4050, PW4052, PW4056, PW4060, PW4060A, PW4060C, PW4062, PW4062A, PW4152, PW4156, PW4156A, PW4158, PW4160, PW4460, PW4462, and PW4650 turbofan engines, including models with any dash number suffix, that have not incorporated Pratt & Whitney Alert Service Bulletin (ASB) No. PW4ENG-A72-436; Service Bulletin (SB) No. PW4ENG-79-76; and SB No. PW4ENG-72-472.

Compliance

(1) Within 1,000 cycles-in-service (CIS) after the effective date of this AD, inspect and clean the No. 4 bearing compartment. (2) Thereafter, within every additional 1,000 CIS, re-inspect and clean the No. 4 bearing compartment.

Required actions

At the next engine shop visit, but not to exceed 5 years after the effective date of this AD, do the following: (1) Replace the No. 4 bearing packing transfer tube assembly; (2) Replace the No. 4 bearing internal scavenge tube assembly; (3) Remove the No. 4 bearing shield, and the No. 4 bearing shield option; and (4) Install the new No. 4 bearing shield options. (5) Modify the turbine exhaust case to relocate the No. 4 bearing pressure and scavenge tube ports to below the engine centerline; (6) Replace the internal No. 4 bearing pressure and scavenge tubes; (7) Modify or replace the turbine case cooling brackets to support the new No. 4 bearing pressure and scavenge tubes; (8) Replace the turbine case manifolds as necessary; and (9) Install the new brackets and clamps to support the new routing configuration.

Unsafe condition

(1) If you have incorporated Pratt & Whitney ASB No. PW4ENG-A72-436; SB No. PW4ENG-79-76; and SB No. PW4ENG-72-472, then no further action is required. (2) Comply with this AD within the compliance times specified, unless already done.

Affected ADs

None.

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