Is AD 2011-07-05 a recurring Airworthiness Directive?

No — AD 2011-07-05 is a one-time directive. Verify it was complied with in the aircraft's records.

Which aircraft does AD 2011-07-05 apply to?

AD 2011-07-05 applies to Sicma Aero Seat — models 9140, 9166, 9173, 9174, 9184, 9188, 9196, 91B7. Serial/part conditions may narrow it to specific aircraft.

Airworthiness Directive 2011-07-05

one-time

Official AD 2011-07-05 · FR doc 2011-6628 · 2011-04-01 · appliance

Airworthiness Directives; Sicma Aero Seat 9140, 9166, 9173, 9174, 9184, 9188, 9196, 91B7, 91B8, 91C0, 91C2, 91C4, 91C5, and 9301 Series Passenger Seat Assemblies; and Sicma Aero Seat 9501311-05, 9501301-06, 9501311-15, 9501301-16, 9501441-30, 9501441-33, 9501311-55, 9501301-56, 9501441-83, 9501441-95, 9501311-97, and 9501301-98 Passenger Seat Assemblies; Installed on Various Transport Category Airplanes

What this AD requires

We are adopting a new airworthiness directive (AD) for the products listed above. This AD results from mandatory continuing airworthiness information (MCAI) originated by an aviation authority of another country to identify and correct an unsafe condition on an aviation product. The MCAI describes the unsafe condition as:

Which aircraft AD 2011-07-05 applies to

MakesSicma Aero Seat

Models9140, 9166, 9173, 9174, 9184, 9188, 9196, 91B7, 91B8, 91C0, 91C2, 91C4, 91C5, 9301, 9501311-05, 9501301-06, 9501311-15, 9501301-16, 9501441-30, 9501441-33, 9501311-55, 9501301-56, 9501441-83, 9501441-95, 9501311-97, 9501301-98

Part-conditional — 90-000200-104-1, 90-000200-104-2.

Applies to listed Sicma Aero Seat passenger seat assemblies identified in Annex 1, Issue 2, of Sicma Aero Seat Service Bulletin 90-25-012, Issue 5, dated March 19, 2004, that have backrest link part numbers 90-000200-104-1 and 90-000200-104-2 installed, as installed on (but not limited to) Airbus A330-200/-300, A340-200/-300/-500/-600, and Boeing 777-200/-300/-300ER/-200LR series airplanes (Table 1), regardless of subsequent airplane modification, alteration, or repair.

Whether AD 2011-07-05 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 2011-07-05 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.