Airworthiness Directive 2010-23-20
one-timeAirworthiness Directives; General Electric Company (GE) CT7-9C and -9C3 Turboprop Engines
What this AD requires
We are adopting a new airworthiness directive (AD) for the products listed above. This AD requires inspecting certain serial number (S/N) gas generator turbine (GGT) shafts for nonconforming land balance-cuts, and if found, removing the shaft from service. This AD was prompted by reports of a manufacturing quality problem. We are issuing this AD to detect nonconforming GGT shaft land balance-cuts, which could result in the shaft failing before its published life limit, and which could result in an uncontained engine failure and damage to the airplane.
Which aircraft AD 2010-23-20 applies to
Applies only to engines with a gas generator turbine (GGT) shaft, P/N 6068T44P02, bearing one of the affected serial numbers listed in Table 1 of this AD (GATHHCPC, GATHHJR7, GATHHJR9, GATHHKG6, GATHHM9R, GATHHWM3, GATHJ4ED, GATHJ9FL, GATHJ19J, GATHJE8P, GATHJWWR, GATHK0KM, GATHK2N1, GATHK3M3, GATHK90K, GATHK96D, GATHKF9R, GATHKH36, GATHKMP7, GATHKRKN, NCE715DA) installed.
Whether AD 2010-23-20 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:
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.