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STC SA00780SE (PAGE 1)

Historical · Amended · Aircraft · Single-Engine · Rev 08/26/2015 · FAA STC database

Installation of the True Lock Safety Retention Axle Lock Nut System in accordance with AML No. SA00780SE, dated February 1, 2001, or later FAA approved revision. View PDF on drs.faa.gov ↗

The STC PDF is authoritative: installation instructions, ICA requirements and limitations.

Applicable aircraft (246)

+ 196 more aircraft

Certification basis — 14 CFR

Specific sections