Airworthiness Directive 2018-04-13

one-time
Official AD 2018-04-13 · FR doc 2018-04614 · 2018-03-08 · turbine engine

Airworthiness Directives; Honeywell International Inc. Turbofan Engines

What this AD requires

We are adopting a new airworthiness directive (AD) for certain Honeywell International Inc. AS907 series turbofan engines. This AD was prompted by seven loss-of-thrust-control events attributed to water intrusion of the engine electronic control unit (ECU). This AD requires applying sealant to identified areas of the ECU and requires inserting a copy of certain airplane operating procedures into the applicable flight manuals. We are issuing this AD to address the unsafe condition on these products.

Which aircraft AD 2018-04-13 applies to

MakesHoneywell International Inc.
ModelsAS907-1-1A, AS907-2-1A, AS907-2-1G, AS907-3-1E, AS907
Part-conditional2119576-1001, 2119576-1011, 2119576-1102, 2119576-3002, 2119576-3102, 2119576-4102, 2119576-4103.

Applies per model to engines with specific engine electronic control unit (ECU) part numbers installed: AS907-1-1A with P/N 2119576-1001 through -1011; AS907-2-1A with P/N 2119576-1102; AS907-2-1G with P/Ns 2119576-3002 and -3102; AS907-3-1E with P/Ns 2119576-4102 and -4103; with applicable engine serial numbers in Table 3 of Honeywell SB AS907-76-9021, Revision 1, dated April 20, 2017, that are not sealed in the areas identified in Figures 1 through 13 of that SB.

Whether AD 2018-04-13 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 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 2018-04-13 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.