AD 98-14-02

final rule
Data completeness: 70%

Airworthiness Directives; Pratt & Whitney Canada PW100 Series Turboprop Engines

AD Number
98-14-02
Status
final_rule
Effective Date
Product Category
engine
Docket
97-ANE-33-AD
FR Citation
Federal Register: October 08, 1998 (Volume 63, Number 195)

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

Fuel manifold transfer tubes, transfer tube lock plates, and fuel manifold drain tubes may develop fuel leaks, which can result in inflight engine shutdowns or fire warnings.

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

Required Actions

Remove existing fuel manifold transfer tubes, transfer tube lock plates, and fuel manifold drain tubes per PWC SB 21077, Rev 8. Replace with improved components per applicable SBs (21077, 21516, 21549, 21373, 21364). Perform leak check before further flight.

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

Compliance Time

Whichever occurs first following the AD effective date: next engine removal, next fuel nozzle change, or prior to November 30, 1998.

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, PW127F series engines installed on Dornier 328, Fokker 50, British Aerospace ATP, Aerospatiale ATR42, ATR42-500, ATR72, Embraer EMB-120, Canadair CL215T, CL415, and DeHavilland Dash-8-100/-200/-300/-315.

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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