Is AD 2001-25-03 a recurring Airworthiness Directive?

No — AD 2001-25-03 is a one-time directive. Verify it was complied with in the aircraft's records.

Which aircraft does AD 2001-25-03 apply to?

AD 2001-25-03 applies to Cirrus Design — models SR20, SR22. Serial/part conditions may narrow it to specific aircraft.

Airworthiness Directive 2001-25-03

one-time

Official AD 2001-25-03 · FR doc 01-30423 · 2001-12-11 · airframe

Airworthiness Directives; Cirrus Design Corporation Models SR20 and SR22 Airplanes

What this AD requires

This amendment adopts a new airworthiness directive (AD) that applies to certain Cirrus Design Corporation (CDC) Models SR20 and SR22 airplanes. This AD requires you to inspect one time for understrength rivets on the elevator torque tube and rudder hinge and replace any understrength rivets. This AD is the result of CDC notifying FAA that understrength rivets were mixed in production supplies. The actions specified by this AD are intended to detect and replace understrength rivets in the elevator and rudder, which could result in failure of the control surfaces. Such failure could lead to a loss of control of the airplane in flight.

Which aircraft AD 2001-25-03 applies to

MakesCirrus Design

ModelsSR20, SR22

Serial-conditional — narrows to serials 1134–1159, 0003–0119.

Part-conditional — MS20470AD4.

Applies to SR20 airplanes serial Nos. 1134 through 1159 and SR22 airplanes serial Nos. 0003 through 0119; inspect elevator torque tube and rudder hinge for understrength rivets and replace per Cirrus Design SB 20-55-06 (SR20) / SB 22-55-03 (SR22).

Whether AD 2001-25-03 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 2001-25-03 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.