AD 2001-01-01

final rule
Data completeness: 70%

Airworthiness Directives; BMW Rolls-Royce GmbH Models BR700-710A1-10 and BR700-710A2-20 Turbofan Engines.

AD Number
2001-01-01
Status
final_rule
Effective Date
Product Category
engine
Docket
Docket No. 2000-NE-44-AD
FR Citation
66 FR 3448

Applicability

TypeManufacturerModelDetails
engine Rolls-Royce GmbH Models BR700-710A1-10 and BR700-710A2-20 Airworthiness Directives; BMW Rolls-Royce GmbH Models BR700-710A1-10 and BR700-710A2-20 Turbofan Engines.

Unsafe Condition

Defective oil filter differential pressure switch causing severe engine oil loss, resulting in in-flight shutdowns.

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

Required Actions

Inspect and mark or replace oil filter differential pressure switches P/N 21SN04-419 or P/N 21SN04-431 in accordance with Rolls-Royce Service Bulletin No. SB-BR700-79-900215, Revision 2.

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

Compliance Time

Within 50 flight hours after the effective date of this AD.

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

Affected Aircraft

BMW Rolls-Royce GmbH Models BR700-710A1-10 and BR700-710A2-20 turbofan engines with oil filter differential pressure switch part number (P/N) 21SN04-419 or P/N 21SN04-431 installed.

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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