AD 2012-14-09

final rule
Data completeness: 80%

Airworthiness Directives; Pratt & Whitney (P&W) Division Turbofan Engines

AD Number
2012-14-09
Status
final_rule
Effective Date
Product Category
engine
Docket
Docket No. FAA-2012-0060
FR Citation
77 FR 60288

Applicability

TypeManufacturerModelDetails
aircraft Pratt & Whitney (P&W) Division Turbofan Airworthiness Directives; Pratt & Whitney (P&W) Division Turbofan Engines

Unsafe Condition

Reports of 3rd and 4th stage vane fractures in the low-pressure turbine (LPT) of certain PW4000-94'' and PW4000-100'' turbofan engines.

AI-generated summary from the source AD text. Verify against the official source before acting.

Required Actions

Dimensional inspections of LPT 3rd stage vanes and the rear turbine case. Inspection of LPT 4th stage vanes at the next LPT overhaul, with removal of vanes with non-conforming airfoil fillet radii and vanes with more than one strip and recoat repair. Disassembly and reassembly of the 2nd stage high-pressure turbine (HPT) rotor and 3rd stage LPT rotor at the next HPT and LPT overhauls.

AI-generated summary from the source AD text. Verify against the official source before acting.

Compliance Time

Within the specified compliance times for each action.

AI-generated summary from the source AD text. Verify against the official source before acting.

Affected Aircraft

Pratt & Whitney PW4000-94'' and PW4000-100'' turbofan engines.

AI-generated summary from the source AD text. Verify against the official source before acting.

Source: Official FAA Source ↗

Retrieved: Apr 4, 2026

Rights: U.S. Government Public Domain

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