AD 97-17-05

final rule
Data completeness: 70%

Airworthiness Directives; Pratt & Whitney Canada PW100 Series Turboprop Engines

AD Number
97-17-05
Status
final_rule
Effective Date
Product Category
engine
Docket
97-ANE-32-AD
FR Citation
Federal Register: August 25, 1997 (Volume 62, Number 164)

Applicability

TypeManufacturerModelDetails
engine Pratt & Whitney Canada Corp. PW118 Airworthiness Directives; Pratt & Whitney Canada PW100 Series Turboprop Engines
engine Pratt & Whitney Canada Corp. PW118A Airworthiness Directives; Pratt & Whitney Canada PW100 Series Turboprop Engines
engine Pratt & Whitney Canada Corp. PW118B Airworthiness Directives; Pratt & Whitney Canada PW100 Series Turboprop Engines
engine Pratt & Whitney Canada Corp. PW119B Airworthiness Directives; Pratt & Whitney Canada PW100 Series Turboprop Engines
engine Pratt & Whitney Canada Corp. PW119C Airworthiness Directives; Pratt & Whitney Canada PW100 Series Turboprop Engines
engine Pratt & Whitney Canada Corp. PW120 Airworthiness Directives; Pratt & Whitney Canada PW100 Series Turboprop Engines
engine Pratt & Whitney Canada Corp. PW120A Airworthiness Directives; Pratt & Whitney Canada PW100 Series Turboprop Engines
engine Pratt & Whitney Canada Corp. PW121 Airworthiness Directives; Pratt & Whitney Canada PW100 Series Turboprop Engines
engine Pratt & Whitney Canada Corp. PW121A Airworthiness Directives; Pratt & Whitney Canada PW100 Series Turboprop Engines
engine Pratt & Whitney Canada Corp. PW123 Airworthiness Directives; Pratt & Whitney Canada PW100 Series Turboprop Engines

Unsafe Condition

The gas generator case rear drain port may permit fluid to exit through the port and accumulate in the nacelle, resulting in a possible hazardous situation such as a nacelle fire caused by fluid leaking from the gas generator case drain ports.

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

Required Actions

Visually inspect the two gas generator case drain ports to ensure they are connected to drain lines or capped in accordance with PWC Service Information Letter No. PW100-003. Compliance must be accomplished within 10 hours time in service after the effective date of this AD.

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

Compliance Time

within 10 hours time in service after the effective date of this AD

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

Affected Aircraft

Pratt & Whitney Canada PW118, PW118A, PW118B, PW119B, PW119C, PW120, PW120A, PW121, PW121A, PW123, PW123B, PW123C, PW123D, PW123E, PW124B, PW125B, PW126A, PW127, PW127E, and PW127F series turboprop engines installed on but not limited to specific aircraft models.

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

Source: Official FAA Source ↗

Retrieved: Apr 8, 2026

Rights: U.S. Government Public Domain

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