AD 92-17-14

final rule
Data completeness: 70%

PRATT & WHITNEY CANADA Models PW123, PW124B, PW125B, and PW126A Engines

AD Number
92-17-14
Status
final_rule
Effective Date
Product Category
engine
Docket
91-ANE-24
FR Citation
This information is not available.

Applicability

TypeManufacturerModelDetails
engine Pratt & Whitney Canada Corp. PW123 PRATT & WHITNEY CANADA Models PW123, PW124B, PW125B, and PW126A Engines
engine Pratt & Whitney Canada Corp. PW124B PRATT & WHITNEY CANADA Models PW123, PW124B, PW125B, and PW126A Engines
engine Pratt & Whitney Canada Corp. PW125B PRATT & WHITNEY CANADA Models PW123, PW124B, PW125B, and PW126A Engines
engine Pratt & Whitney Canada Corp. PW126A PRATT & WHITNEY CANADA Models PW123, PW124B, PW125B, and PW126A Engines

Unsafe Condition

Large engine torque variations and a subsequent aircraft asymmetric thrust condition.

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Required Actions

Install a new or reworked fuel pump in accordance with PWC Service Bulletin 20946R2, Revision 2. A shop visit is defined as engine induction into a maintenance facility for maintenance. Alternative methods may be approved by the FAA Manager, Engine Certification Office.

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Compliance Time

At the next shop visit or within 12 months from the effective date of this AD, whichever occurs first.

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Affected Aircraft

Pratt & Whitney Canada PW123, PW124B, PW125B, and PW126A engines installed on DeHavilland DHC-8 Series 300, Canadair CL-215T, Aerospatiale ATR-42, ATR-72, Fokker 50, and British Aerospace ATP aircraft.

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Source: Official FAA Source ↗

Retrieved: Apr 8, 2026

Rights: U.S. Government Public Domain

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