Is AD 2010-15655 a recurring Airworthiness Directive?

No — AD 2010-15655 is a one-time directive. Verify it was complied with in the aircraft's records.

Which aircraft does AD 2010-15655 apply to?

AD 2010-15655 applies to Boeing — models 737-200, 737-300, 737-400, 737-500, 737-600, 737-700, 737-800, 737-900. Serial/part conditions may narrow it to specific aircraft.

Airworthiness Directive 2010-15655

one-time

AD 2010-15655 · 2010-07-01 · airframe

Airworthiness Directives; The Boeing Company Model 737-200, -300, -400, -500, -600, -700, -800, and -900 Series Airplanes; Model 747-400 Series Airplanes; Model 757-200 and 757-300 Series Airplanes; Model 767-200, 767-300, and 767-400ER Series Airplanes; and Model 777-200 Series Airplanes

What this AD requires

This document publishes in the Federal Register an amendment adopting airworthiness directive (AD) 2008-01-01 that was sent previously to all known U.S. owners and operators of certain Model 737- 200, -300, -400, -500, -600, -700, -800, and -900 series airplanes; Model 747-400 series airplanes; Model 757-200 and 757-300 series airplanes; Model 767-200, 767-300, and 767-400ER series airplanes; and Model 777-200 series airplanes by individual notices. This AD requires replacing a certain flight deck door feature and revising the modification record placard. This AD is prompted by a report indicating that the feature of the flight deck door is defective. We are issuing this AD to prevent failure of this feature, which could jeopardize flight safety.

Which aircraft AD 2010-15655 applies to

MakesBoeing

Models737-200, 737-300, 737-400, 737-500, 737-600, 737-700, 737-800, 737-900, 747-400, 757-200, 757-300, 767-200, 767-300, 767-400ER, 777-200, 737, 747, 757, 767, 777

Applies only to airplanes modified per specific Jamco supplemental type certificates/service bulletins: 737-200/-300/-400/-500/-600/-700/-800/-900 per STC ST01143SE, SB 52-2295 Rev 1 (Oct 10, 2007); 747-400 per STC ST01194SE, SB 52-2303 Rev 1 (Oct 10, 2007); 757-200/-300 per STC ST01150SE, SB 52-2304 Rev 2 (Nov 1, 2007); 767-200/-300/-400ER per STC ST01121SE, SB 52-2302 Rev 1 (Oct 10, 2007); 777-200 per STC ST01201SE, SB 52-2305 Rev 1 (Oct 10, 2007).

Whether AD 2010-15655 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 2010-15655 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.