Is AD 2019-23-06 a recurring Airworthiness Directive?

Yes — AD 2019-23-06 requires a repetitive inspection. Next-due depends on the aircraft's time in service.

Which aircraft does AD 2019-23-06 apply to?

AD 2019-23-06 applies to Boeing — models 757-200, 757-200CB, 757-300, 757. Serial/part conditions may narrow it to specific aircraft.

Airworthiness Directive 2019-23-06

recurring

Official AD 2019-23-06 · FR doc 2019-26400 · 2019-12-09 · airframe

Airworthiness Directives; The Boeing Company Airplanes

What this AD requires

The FAA is adopting a new airworthiness directive (AD) for certain The Boeing Company Model 757-200, -200CB, and -300 series airplanes. This AD was prompted by reports of cracks initiating in the fuselage frame web at body station (STA) 1640. This AD requires, depending on configuration, a general visual inspection for any previous repair, such as any reinforcing repair or local frame replacement repair, repetitive open hole high frequency eddy current (HFEC) inspections for any crack of the fuselage frame web fastener holes, on the left and right side of the airplane, and applicable on- condition actions. The FAA is issuing this AD to address the unsafe condition on these products.

Repetitive inspection. Re-inspect. The next-due date/hours depend on this aircraft’s time in service — a records report computes it from the logbooks.

Which aircraft AD 2019-23-06 applies to

MakesBoeing

Models757-200, 757-200CB, 757-300, 757

Applicability as identified in Boeing Alert Requirements Bulletin 757-53A0112 RB, dated November 16, 2018.

Whether AD 2019-23-06 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 2019-23-06 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.