AD 2002-18-03

final rule
Data completeness: 70%

Airworthiness Directives; Rolls-Royce plc Models Spey 506-14A, 555-15, 555-15H, 555-15N, and 555-15P Turbojet Engines

AD Number
2002-18-03
Status
final_rule
Effective Date
Product Category
engine
Docket
Docket No. 2001-NE-14-AD
FR Citation
67 FR 57514

Applicability

TypeManufacturerModelDetails
engine Rolls-Royce plc Models Spey 506-14A Airworthiness Directives; Rolls-Royce plc Models Spey 506-14A, 555-15, 555-15H, 555-15N, and 555-15P Turbojet Engines

Unsafe Condition

Failure of stage 2 low pressure turbine (LPT) blades, which could result in an engine shutdown.

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Required Actions

Replace certain stage 2 LPT blades with new redesigned stage 2 LPT blades.

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Compliance Time

Before further flight.

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Affected Aircraft

Rolls-Royce plc Spey 506-14A, 555-15, 555-15H, 555-15N, and 555-15P turbojet engines.

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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