AD 2017-12-03

final rule
Data completeness: 80%

Airworthiness Directives; Pratt & Whitney Division Turbofan Engines

AD Number
2017-12-03
Status
final_rule
Effective Date
Product Category
engine
Docket
Docket No. FAA-2016-9405
FR Citation
82 FR 27411

Applicability

TypeManufacturerModelDetails
engine Pratt & Whitney Division Airworthiness Directives; Pratt & Whitney Division Turbofan Engines

Unsafe Condition

An unrecoverable engine in-flight shutdown (IFSD) after an ice crystal icing event, followed by an attempt to rapidly restart the engine with the Electronic Engine Control (EEC) Active Clearance Control (ACC) turned on, caused contraction of the high-pressure turbine (HPT) case, reduced clearances in the HPT, subsequent HPT damage, and rotor seizure.

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Required Actions

Install a software standard eligible for installation and preclude the use of EEC software standards earlier than SCN 5B/I. All engines with EEC model numbers EEC104-40 and EEC104-60 must upgrade software earlier than software standard SCN 5B/I by 2024.

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Compliance Time

Within the next engine shop visit for engines currently operating in the Asia Pacific region; for all other engines, compliance is required by 2024.

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Affected Aircraft

Pratt & Whitney Division PW2037, PW2037M, and PW2040 turbofan engines with EEC model numbers EEC104-40 and EEC104-60.

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Source: Official FAA Source ↗

Retrieved: Apr 4, 2026

Rights: U.S. Government Public Domain

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