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Airworthiness Directive

AD 95-04-03 60 FR 9621 Active

Federal Aviation Administration · 14 CFR part 39

FR document
95-4133
Amendment
39-9155
Published
1995-02-21
Effective
1995-04-07
Models covered
1
Last live check
2026-10-01

Printed from https://aircraftdirectives.com/ad/95-04-03 · AircraftDirectives restates official FAA and manufacturer records; the official sources named on this sheet control. Not an airworthiness determination.

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AD

95-04-03

FR doc 95-4133 · 60 FR 9621

AD 95-04-03Published 1995-02-21Effective 1995-04-07

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 inspecting (one-time) the wing front spar carry-through frame structure for cracks on certain Beech 33, 35, and 36 series airplanes, and repairing or reinforcing any cracked wing front spar carry-through frame structure.

Full official abstract

This amendment supersedes Airworthiness Directive (AD) 92-08- 07, which currently requires inspecting (one-time) the wing front spar carry-through frame structure for cracks on certain Beech 33, 35, and 36 series airplanes, and repairing or reinforcing any cracked wing front spar carry-through frame structure. This action would make this one-time inspection repetitive. This action was prompted by numerous (43) reports received by the Federal Aviation Administration (FAA) of cracks found on the wing front spar carry-through frame structure of the affected airplanes. These cracks were found during the inspection required by AD 92-08-07. The actions specified by the proposed AD are intended to prevent spar carry-through frame structure failure caused by cracking, which, if not detected and corrected, could result in severe structural damage to the wing.

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Applies to 1 model in our index