Airworthiness Directive 2016-15351

one-time
AD 2016-15351 · 2016-07-01 · turbine engine

Airworthiness Directives; Rolls-Royce Deutschland Ltd & Co KG Turbofan Engines

What this AD requires

We are adopting a new airworthiness directive (AD) for certain Rolls-Royce Deutschland Ltd & Co KG (RRD) BR700-710A1-10, -710A2-20, and -710C4-11 turbofan engines. This AD requires removing the pawl carrier pivot pins, part number (P/N) BRR17117, from service and replacing them with parts eligible for installation. This AD was prompted by a seized low-pressure turbine (LPT) fuel shut-off pawl carrier caused by corrosion of the pawl carrier pivot pin. We are issuing this AD to prevent failure of the fuel shut-off mechanism, which could result in uncontained part release, damage to the engine, and damage to the airplane.

Which aircraft AD 2016-15351 applies to

MakesRolls-Royce Deutschland (Rrd)
ModelsBR700-710A1-10, BR700-710A2-20, BR700-710C4-11, BR700
Serial-conditional — narrows to serials ?–11505, ?–12492, ?–15277, ?–15329.
Part-conditionalM51-104, M51-111, M51-108, M51-112.

Applies at/below a per-model serial number threshold with a specific LPT module P/N installed: BR700-710A1-10 S/N 11505 and below w/ LPT P/N M51-104 or M51-111; BR700-710A2-20 S/N 12492 and below w/ LPT P/N M51-108 or M51-111; BR700-710C4-11 (config 710C4-11 on data plate) S/N 15277 and below w/ LPT P/N M51-112; BR700-710C4-11 (config 710C4-11/10 on data plate) S/N 15329 and below w/ LPT P/N M51-112.

Whether AD 2016-15351 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 complianceThe specific action taken (inspected, replaced, modified) and to what revision.
DateWhen the work was done.
Aircraft timeTotal time in service / tach at compliance — how recurring next-due is computed.
Signature & certificateThe A&P/IA who returned it to service, with certificate number.
Is AD 2016-15351 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.