AD 2015-20-03

final rule
Data completeness: 70%

Airworthiness Directives; Pratt & Whitney Canada Corp. Turboprop Engines

AD Number
2015-20-03
Status
final_rule
Effective Date
Product Category
engine
Docket
Docket No. FAA-2013-1059
FR Citation
80 FR 61719

Applicability

TypeManufacturerModelDetails
engine Pratt & Whitney Canada Corp Airworthiness Directives; Pratt & Whitney Canada Corp. Turboprop Engines

Unsafe Condition

fuel seepage past the metal-to-metal sealing surfaces of the fuel nozzle and fuel manifold flow adapter

Required Actions

remove the O-ring seal from the fuel manifold fitting, remove fuel manifold flow adapter, part numbers (P/Ns) 3059754-01, 3059757-01, and 3059760-01, install a fuel nozzle gasket and fuel manifold flow adapter that are eligible for installation, in accordance with paragraphs 3.A, 3.B, and 3.C of P&WC SB No. PW100-72-21861, dated November 21, 2014

Compliance Time

Within 1,500 flight hours after the effective date of this AD, or at the next engine shop visit, whichever occurs first

Affected Aircraft

Pratt & Whitney Canada Corp. (P&WC) PW120, PW121, and PW121A turboprop engines with post SB 21610 configuration; PW124B, PW127, PW127E, and PW127F turboprop engines with post SB 21607 configuration; PW127E and PW127F turboprop engines with serial numbers (S/Ns) PCE-EB0366 and earlier; PW127G turboprop engines with S/Ns PCE-AX0275 and earlier; and PW127M turboprop engines with S/Ns PCE-ED0810 and earlier

Source: Official FAA Source ↗

Retrieved: Apr 6, 2026

Rights: U.S. Government Public Domain

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