Is AD 05-15895 a recurring Airworthiness Directive?

No — AD 05-15895 is a one-time directive. Verify it was complied with in the aircraft's records.

Airworthiness Directive 05-15895

Q: Which aircraft does AD 05-15895 apply to?

AD 05-15895 applies to Rolls-Royce Deutschland Ltd & Co Kg — models BR700-715A1-30, BR700-715B1-30, BR700-715C1-30, BR700. Serial/part conditions may narrow it to specific aircraft.

one-time

AD 05-15895 · 2005-08-11 · turbine engine

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

What this AD requires

The FAA is adopting a new airworthiness directive (AD) for Rolls-Royce Deutschland Ltd & Co KG (RRD) (formerly Rolls-Royce Deutschland GmbH, formerly BMW Rolls-Royce GmbH) model BR700-715A1-30, BR700-715B1-30, and BR700-715C1-30 turbofan engines. This AD requires a onetime inspection of the Independent Overspeed Protection (IOP) unit, part number (P/N) 112E9321G2, for 19 specific serial numbers (SNs), and removal from service of those units. This AD results from a report that incorrect capacitors were installed in 19 IOP units. The incorrect capacitor in the IOP unit can lead to an inadvertent IOP command resulting in an in-flight engine shutdown. We are issuing this AD to prevent inadvertent dual-engine in-flight shutdown.

Which aircraft AD 05-15895 applies to

MakesRolls-Royce Deutschland Ltd & Co Kg

ModelsBR700-715A1-30, BR700-715B1-30, BR700-715C1-30, BR700

Manufacturer formerly Rolls-Royce Deutschland GmbH, formerly BMW Rolls-Royce GmbH. These turbofan engines are installed on, but not limited to, McDonnell Douglas Model 717-200 airplanes; concerns incorrect capacitors in Independent Overspeed Protection (IOP) units.

Whether AD 05-15895 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 05-15895 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.