AD 2001-25-11

Recurring final rule
Data completeness: 70%

Airworthiness Directives; Pratt and Whitney PW4000 Series Turbofan Engines

AD Number
2001-25-11
Status
final_rule
Effective Date
Product Category
engine
Docket
Docket No. 2000-NE-47-AD
FR Citation
67 FR 1

Applicability

TypeManufacturerModelDetails
aircraft Pratt and Whitney PW4000 Series Turbofan Airworthiness Directives; Pratt and Whitney PW4000 Series Turbofan Engines

Unsafe Condition

Reports of surges during takeoff on airplanes equipped with PW4000 series turbofan engines, potentially leading to reduced engine stability and power loss due to high pressure compressor (HPC) surge.

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

Required Actions

Limit the number of PW4000 engines with potentially reduced stability to no more than one on each airplane. Introduce a new cool engine fuel spike test for engines exceeding cyclic limits or undergoing shop work. Limit the number of engines with HPC cutback stator (CBS) configuration to one on each airplane. Place a cyclic limit on CBS engines in service. Establish a minimum rebuild standard for engines returned to service.

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

Compliance Time

Before further flight for affected engines exceeding cyclic limits or undergoing shop work.

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

Affected Aircraft

Pratt and Whitney PW4000 series turbofan engines, as specified by the affected configurations and cyclic limits outlined in the AD.

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

Source: Official FAA Source ↗

Retrieved: Apr 6, 2026

Rights: U.S. Government Public Domain

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