Airworthiness Directive

AD 95-03-14 60 FR 10308 Active

Federal Aviation Administration · 14 CFR part 39

FR document
95-4124
Amendment
39-9150
Published
1995-02-24
Effective
1995-03-13
Models covered
2
Last live check
2026-10-01
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AD

95-03-14

FR doc 95-4124 · 60 FR 10308

AD 95-03-14Published 1995-02-24Effective 1995-03-13

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 initial and repetitive inspections of the engine mount brackets for cracks, and if found cracked, replacement with improved design engine mount brackets.

Full official abstract

This amendment supersedes an existing airworthiness directive (AD), applicable to certain Teledyne Continental Motors (TCM) IO-346, IO-520, and IO-550 series reciprocating engines, that currently requires initial and repetitive inspections of the engine mount brackets for cracks, and if found cracked, replacement with improved design engine mount brackets. All engine mount brackets require replacement with improved design engine mount brackets at the next engine removal after the effective date of that airworthiness directive (AD). This amendment clarifies the identification procedures to determine which engine mount brackets must be inspected. This amendment is prompted by reports that the engine mount bracket part numbers, which are ink stamped, can be easily obliterated. The actions specified by this AD are intended to prevent engine separation from the aircraft due to cracks in the engine mount brackets.

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All Continental IO-520 directives

Applies to 2 models in our index