Airworthiness Directive E9-6226

one-time
AD E9-6226 · 2009-03-23 · turbine engine

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

What this AD requires

We are adopting a new airworthiness directive (AD) for the products listed above. This AD results from mandatory continuing airworthiness information (MCAI) issued by an aviation authority of another country to identify and correct an unsafe condition on an aviation product. The MCAI describes the unsafe condition as:

Which aircraft AD E9-6226 applies to

MakesRolls-Royce Deutschland Ltd & Co Kg
ModelsBR700-715A1-30, BR700-715B1-30, BR700-715C1-30, BR700-715
Part-conditionalBRH20130, BRH20131, BRH19423, BRH19427.

Decreases the maximum approved life limits in the BR715 Time Limits Manual for the HP Turbine Stage 1 Rotor Disc (P/N BRH20130 and P/N BRH20131) and HP Turbine Stage 2 Rotor Disc (P/N BRH19423 and P/N BRH19427).

Whether AD E9-6226 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 E9-6226 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.