Airworthiness Directive

AD 2002-21-02 67 FR 63815

Federal Aviation Administration · 14 CFR part 39

FR document
02-26052
Amendment
39-12908
Published
2002-10-16
Models covered
2
Last live check
2026-08-17
AD

2002-21-02

FR doc 02-26052 · 67 FR 63815

AD 2002-21-02Published 2002-10-16Effective 2002-11-08

Requires you to replace the self-locking retaining nut on the roll and yaw trim cartridges with a new self- locking retaining nut with a higher axial load capability.

Full official abstract

This amendment adopts a new airworthiness directive (AD) that applies to certain Cirrus Design Corporation (Cirrus) Model SR20 and SR22 airplanes. This AD requires you to replace the self-locking retaining nut on the roll and yaw trim cartridges with a new self- locking retaining nut with a higher axial load capability. This AD is the result of a report that, during a production flight test, the self- locking retaining nut on the yaw trim cartridge came off. The actions specified by this AD are intended to prevent loss of the self-locking retaining nut on the roll and yaw trim cartridges during flight, which could result in jamming of the corresponding flight control system. Such jamming could lead to loss of control of the airplane.

Applies to 2 models in our index