AD 2006-25-13

final rule
Data completeness: 80%

Airworthiness Directives; Rolls-Royce Corporation AE 2100D3 Turboprop Engines

AD Number
2006-25-13
Status
final_rule
Effective Date
Product Category
engine
Docket
Docket No. FAA-2006-26414
FR Citation
71 FR 75108

Applicability

TypeManufacturerModelDetails
engine Rolls-Royce Corporation AE 2100D3 Airworthiness Directives; Rolls-Royce Corporation AE 2100D3 Turboprop Engines

Unsafe Condition

Uncontained failure of the compressor cone shaft assembly, leading to engine shutdown and damage to the airplane.

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

Required Actions

Remove compressor cone shaft assemblies, part numbers 23050728, 23070729, and 23076017, from service at the new reduced cyclic life limit of 5,000 engine cycles.

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

Compliance Time

Within 5,000 engine cycles after the effective date.

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

Affected Aircraft

Rolls-Royce Corporation AE 2100D3 turboprop engines with compressor cone shaft assemblies, part numbers 23050728, 23070729, or 23076017, installed.

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

Source: Official FAA Source ↗

Retrieved: Apr 4, 2026

Rights: U.S. Government Public Domain

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