Is AD 2005-10-13 a recurring Airworthiness Directive?

No — AD 2005-10-13 is a one-time directive. Verify it was complied with in the aircraft's records.

Airworthiness Directive 2005-10-13

Q: Which aircraft does AD 2005-10-13 apply to?

AD 2005-10-13 applies to Rolls-Royce Corporation — models 250-B17B, 250-B17C, 250-B17D, 250-B17E, 250-C20, 250-C20B, 250-C20F, 250-C20J. Serial/part conditions may narrow it to specific aircraft.

one-time

Official AD 2005-10-13 · FR doc 05-9660 · 2005-05-18 · turboshaft engine

Airworthiness Directives; Rolls-Royce Corporation (Formerly Allison Engine Company) 250-B17B, -B17C, -B17D, -B17E, -C20, -C20B, -C20F, -C20J, -C20S, and -C20W Turboprop and Turboshaft Engines

What this AD requires

The FAA is adopting a new airworthiness directive (AD) for Rolls- Royce Corporation (RRC) (formerly Allison Engine Company) 250-B17B, - B17C, -B17D, -B17E, -C20, -C20B, -C20F, -C20J, -C20S, and -C20W turboprop and turboshaft engines that do not have turbine energy absorbing ring, RRC part number (P/N) 23035175, or an equivalent FAA- approved serviceable turbine energy absorbing ring, installed. This AD requires installation of a turbine energy absorbing ring in the plane of the 1st stage turbine wheel. This AD results from an unacceptable rate of uncontained 1st stage turbine wheel failures. We are issuing this AD to minimize the risk of uncontained 1st stage turbine wheel fragments from causing damage to the aircraft or damage to the second engine on twin-engine installations, which could lead to loss of control and loss of the aircraft.

Which aircraft AD 2005-10-13 applies to

MakesRolls-Royce Corporation

Models250-B17B, 250-B17C, 250-B17D, 250-B17E, 250-C20, 250-C20B, 250-C20F, 250-C20J, 250-C20S, 250-C20W, 250

Part-conditional — 23035175.

Manufacturer formerly Allison Engine Company. Applies only to engines that do NOT have turbine energy absorbing ring, RRC P/N 23035175, or an FAA-approved equivalent serviceable ring, installed. Covers both turboprop and turboshaft applications; installed on, but not limited to, Agusta A109/A109A/A109A II, B-N Group BN-2T (turboprop), Bell 206A/206B/206L, Bell 47G-2A/2A-1/3B/3B-1/3B-2/3B-2A/4/4A/5/5A (various STCs), Eurocopter Deutschland BO-105C/S, Eurocopter France AS355E/F/F1/F2, FH-1100, Hiller UH-12D, MDHI 369D/E/HM/HS/HE, Rogerson Hiller UH-12E/UH-12E-L, and SIAI Marchetti SF600 aircraft.

Whether AD 2005-10-13 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 2005-10-13 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.