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Airworthiness Directive

AD 2001-25-03 66 FR 63913 Active

Federal Aviation Administration · 14 CFR part 39

Requires you to inspect one time for understrength rivets on the elevator torque tube and rudder hinge and replace any understrength rivets.

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FR document
01-30423
Amendment
39-12556
Published
2001-12-11
Effective
2001-12-17
Models covered
2

Last live check: 2026-08-19

Printed from https://aircraftdirectives.com/ad/2001-25-03 · AircraftDirectives restates official FAA and manufacturer records; the official sources named on this sheet control. Not an airworthiness determination.

This page is a reference Record, not an airworthiness or compliance determination. Official FAA and manufacturer sources control over our restatement, subject to governing law. Check applicability, current requirements and incorporated documents before acting. The owner or operator remains responsible for airworthiness and required records under 14 CFR 91.403 and 91.417, as applicable. Terms of Use: /terms.

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AD

2001-25-03

FR doc 01-30423 · 66 FR 63913

AD 2001-25-03Published 2001-12-11Effective 2001-12-17

FAA rule - 14 CFR 39

FAA rule. Compliance with an applicable AD is required under 14 CFR 39.7. Check its effective date, applicability, compliance times and current status.

Requires you to inspect one time for understrength rivets on the elevator torque tube and rudder hinge and replace any understrength rivets.

Full official abstract

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.

More directives for Cirrus SR20

  1. AD 2024-24-11 Airworthiness Directives; Cirrus Design Corporation Airplanes Effective 2024-12-23
  2. AD 2008-14-13 Airworthiness Directives; Cirrus Design Corporation Model SR20 and SR22 ... Effective 2008-08-14
  3. AD 2008-11-18 Airworthiness Directives; Cirrus Design Corporation Model SR20 Airplanes Effective 2008-07-07
  4. AD 2008-03-16 Airworthiness Directives; Cirrus Design Corporation Models SR20 and SR22... Effective 2008-03-11
  5. AD 2007-14-03 Airworthiness Directives; Cirrus Design Corporation Models SR20 and SR22... Effective 2007-08-16

All Cirrus SR20 directives

View on Federal Register (opens in a new tab) View this AD in FAA DRS (opens in a new tab) Print AD packet (opens the full Federal Register document in a new tab)

Applies to 2 models in our index