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AD FAA-2007-28478

Airworthiness Directives; Taylorcraft A, B, and F Series Airplanes

Summary

The FAA is adopting a new airworthiness directive (AD) for all Taylorcraft A, B, and F series airplanes. This AD requires you to initially inspect the left and right wing front and aft lift struts for corrosion and cracks, replace any cracked strut or strut with corrosion that exceeds certain limits with either sealed or non-sealed struts, and repetitively inspect any non-sealed struts. This AD results from inspections where several different struts were found with moderate to severe corrosion and required strut replacement. We are issuing this AD to detect and correct corrosion or cracks in the right and left wing front and aft lift struts. This condition, if not corrected, could result in failure of the lift strut and lead to in-flight separation of the wing with consequent loss of control.

Directive Details

AD Number

FAA-2007-28478

Document Number

E7-15581

Type

Rule

Publication Date

August 13, 2007

Effective Date

August 20, 2007

Affected Manufacturer

Taylorcraft A, B, and F Series

Criticality

important

Emergency

No

Docket ID

Docket No. FAA-2007-28478

Topics

Air transportationAircraftAviation safetyIncorporation by referenceSafety

Official Documents

View all ADs for Taylorcraft A, B, and F Series →

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AD FAA-2007-28478 — Airworthiness Directives; Taylorcraft A, B, and F Series Airplanes