Airworthiness Directive 2013-25-01

one-time
Official AD 2013-25-01 · FR doc 2013-29122 · 2013-12-09 · airframe

Airworthiness Directives; DASSAULT AVIATION Airplanes

What this AD requires

We are adopting a new airworthiness directive (AD) for all DASSAULT AVIATION Model Falcon 10 airplanes. This AD requires a one- time inspection for cracking of the right-hand (RH) and left-hand (LH) inboard flaps, and replacement if necessary. This AD was prompted by reports of cracking found on the inboard end plate (rib) of the RH inboard flap. We are issuing this AD to detect and correct such cracking, which could lead to complete fracture of the rib and loss of integrity of the flap structure, resulting in loss of control of the airplane.

Which aircraft AD 2013-25-01 applies to

MakesDassault Aviation
ModelsFalcon 10

Applies to all serial numbers of the listed models.

Whether AD 2013-25-01 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 complianceThe specific action taken (inspected, replaced, modified) and to what revision.
DateWhen the work was done.
Aircraft timeTotal time in service / tach at compliance — how recurring next-due is computed.
Signature & certificateThe A&P/IA who returned it to service, with certificate number.
Is AD 2013-25-01 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.