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Airworthiness directives › 2015-14-05

AD 2015-14-05 Airworthiness Directives; Pratt & Whitney Turbofan Engines

2015-08-25
2015-07-21
39-18203
FAA-2014-1127
Engine
—

Applicability*9

This AD applies to all Pratt & Whitney (PW) JT8D-217C and JT8D-219 turbofan engines with low-pressure turbine (LPT) shaft part numbers 783319, 783319-001, 783319-003, 783319-004, 783320, 783320-001, 783320-003, 783320-004, 820514-001, 820514-003, 820514-004, or 820514-005, installed.

Compliance

For the purpose of this AD, piece-part exposure is when the LPT shaft is completely disassembled from the engine.

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) If the LPT shaft has 15,000 or fewer cycles-since-new (CSN) on the effective date of this AD, remove it from service before it accumulates 20,000 CSN. (2) If the LPT shaft has more than 15,000 CSN on the effective date of this AD, remove it from service before it accumulates 5,000 additional cycles in service, or at the next piece-part exposure after accumulating 20,000 CSN, whichever occurs first. (3) After the effective date of this AD, do not install any LPT shaft listed in paragraph (c) of this AD that is at piece-part exposure and exceeds the new life limit of 20,000 CSN, into any engine.

Affected ADs

None.

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