Is AD 2006-16-01 a recurring Airworthiness Directive?

No — AD 2006-16-01 is a one-time directive. Verify it was complied with in the aircraft's records.

Which aircraft does AD 2006-16-01 apply to?

AD 2006-16-01 applies to Hamilton Sundstrand — models 14RF-19, 14RF. Serial/part conditions may narrow it to specific aircraft.

Airworthiness Directive 2006-16-01

one-time

Official AD 2006-16-01 · FR doc E6-12109 · 2006-07-31 · propeller

Airworthiness Directives; Hamilton Sundstrand Model 14RF-19 Propellers

What this AD requires

The FAA is superseding an existing airworthiness directive (AD) for Hamilton Sundstrand model 14RF-19 propellers. That AD currently requires replacing certain actuator yokes with improved actuator yokes. This AD requires the same actions. This AD results from the discovery of a part number (P/N) error in the applicability paragraph of AD 2006-12-19. We are issuing this AD to prevent actuator yoke arms breaking during flight, which could cause high propeller vibration and contribute to reduced controllability of the airplane.

Which aircraft AD 2006-16-01 applies to

MakesHamilton Sundstrand

Models14RF-19, 14RF

Part-conditional — 810436-2, 790199-6.

Applies to propellers with actuator yoke arm part number 810436-2, which might be installed in actuator assemblies part number 790199-6 (correction of a part-number error in AD 2006-12-19). Installed on, but not limited to, SAAB 340 airplanes.

Whether AD 2006-16-01 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 compliance — The specific action taken (inspected, replaced, modified) and to what revision.

Date — When the work was done.

Aircraft time — Total time in service / tach at compliance — how recurring next-due is computed.

Signature & certificate — The A&P/IA who returned it to service, with certificate number.

Is AD 2006-16-01 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.