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Airworthiness Directive 03-9982

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AD 03-9982 · 2003-04-23 · turbine engine

Airworthiness Directives; Rolls-Royce Deutschland Ltd & Co KG Models BR700-710A1-10 and BR700-710A2-20 Turbofan Engines; Correction

What this AD requires

This document makes corrections to Airworthiness Directive (AD) 2003-07-11, applicable to Rolls-Royce Deutschland Ltd & Co KG (formerly Rolls-Royce Deutschland GmbH, formerly BMW Rolls-Royce GmbH), models BR700-710A1-10 and BR700-710A2-20 turbofan engines. AD 2003-07- 11 was published in the Federal Register on April 11, 2003 (68 FR 17727). In the compliance section, paragraph (g) incorrectly references cycles and should reference hours, and the paragraph lettering sequence after paragraph (g) is incorrect. This document corrects cycles to hours and corrects the paragraph lettering sequence. In all other respects, the original document remains the same.

Which aircraft AD 03-9982 applies to

MakesRolls-Royce Deutschland Ltd & Co Kg

Whether AD 03-9982 actually applies to your aircraft (by serial and installed parts) and whether it’s already complied with comes from that aircraft’s records.

How AD compliance is recorded

A valid compliance record (14 CFR 43.9) states:

Method of compliance — The specific action taken (inspected, replaced, modified) and to what revision.
Date — When the work was done.
Aircraft time — Total time in service / tach at compliance — how recurring next-due is computed.
Signature & certificate — The A&P/IA who returned it to service, with certificate number.
Is AD 03-9982 complied with on your aircraft?

Tailplate reads a tail number’s logbooks and matches every applicable AD — including this one — to its compliance evidence, with recurring next-due dates computed.

Look up a tail number →Read the full directive (Federal Register)

Applicability is derived from the FAA directive corpus and is advisory, not a legal airworthiness determination. Compliance is established only from an aircraft’s actual records.