Airworthiness Directive E6-17007

one-time
AD E6-17007 · 2006-10-16 · turbine engine

Airworthiness Directives; General Electric Company CF34-10E Series Turbofan Engines; Correction

What this AD requires

This document makes a correction to Airworthiness Directive (AD) 2006-20-06. That AD applies to General Electric Company (GE) CF34- 10E series turbofan engines. We published AD 2006-20-06 in the Federal Register on September 29, 2006 (71 FR 57403). The issue date of the AD was inadvertently omitted. This document adds the AD issue date. In all other respects, the original document remains the same.

Which aircraft AD E6-17007 applies to

MakesGeneral Electric Company Cf34-10E

Whether AD E6-17007 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 E6-17007 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.