Airworthiness Directive 03-11537
one-timeAirworthiness 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 a correction 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). Subsequently, a correction document was published in the Federal Register on April 23, 2003 (68 FR 19944) that made corrections to the compliance section starting at paragraph (g). This document corrects paragraph (f) of the compliance section that incorrectly references cycles instead of hours. This document changes cycles to hours in paragraph (f). In all other respects, the original document, with the corrections published on April 23, 2003, remains the same.
Which aircraft AD 03-11537 applies to
Whether AD 03-11537 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:
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.