AD 2009-21-04

final rule
Data completeness: 70%

Airworthiness Directives; Rolls-Royce Deutschland Ltd & Co KG Model BR700-715A1-30, BR700-715B1-30, and BR700-715C1-30 Turbofan Engines

AD Number
2009-21-04
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Docket No. FAA-2009-0045
FR Citation
74 FR 55759

Applicability

TypeManufacturerModelDetails
aircraft Aviat Various Airworthiness Directives; Rolls-Royce Deutschland Ltd & Co KG Model BR700-715A1-30, BR700-715B1-30, and BR700-715C1-30 Turbofan Engines

Unsafe Condition

Failure of front HP compressor rotors, which could result in an uncontained engine failure and damage to the airplane.

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

Required Actions

Remove the specified HP Compressor drum assemblies from operation before reaching the life limit specified in Table 1 of this AD.

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

Compliance Time

Before reaching the life limit specified in Table 1 of this AD.

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

Affected Aircraft

Rolls-Royce Deutschland Ltd & Co KG model BR700-715A1-30, BR700-715B1-30, and BR700-715C1-30 turbofan engines, installed on, but not limited to, McDonnell Douglas 717-200 airplanes.

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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