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Correction notice

AD 96-24-17 R1 62 FR 63828 Correction

Federal Aviation Administration · 14 CFR part 39

FR document
97-31680
Published
1997-12-03
Effective
1997-01-27
Models covered
1
Last live check
2026-10-03

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Correction

96-24-17 R1

FR doc 97-31680 · 62 FR 63828

AD 96-24-17 R1Published 1997-12-03Effective 1997-01-27

Requires installing new inspection holes, modifying the wing tip fairings, and inspecting the wing spars for intergranular corrosion.

Full official abstract

This document clarifies information in airworthiness directive (AD) 96-24-17, which applies to Don Luscombe Aviation History Foundation (Luscombe) Models 8, 8A, 8B, 8C, 8D, 8E, 8F, T-8F airplanes. AD 96-24-17 currently requires installing new inspection holes, modifying the wing tip fairings, and inspecting the wing spars for intergranular corrosion. The actions specified in AD 96-24-17 are intended to prevent wing spar failure from intergranular corrosion, which could result in structural failure of the wings and loss of control of the airplane. The AD was published with an Appendix providing an alternative method of compliance. Since issuance of AD 96- 24-17, the FAA has re-examined the Appendix and has determined that clarification of certain inspections procedures is needed. This action clarifies the procedures specified in the Appendix of AD 96-24-17.

More directives for Luscombe 8 Silvaire

  1. AD 96-24-17 Airworthiness Directives; The Don Luscombe Aviation History Foundation M... 1996-12-19

All Luscombe 8 Silvaire directives

This is a correction notice. The AD it corrects is not in our index yet, so we are showing the correction alone rather than implying we hold the directive itself.

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Applies to 1 model in our index