Continental SB CG 300-1002 P1 - SB CG 300-1002 P1, Initia...

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SB CG 300-1002 P1

Continental Aerospace Technologies

Issued 2025-11-07

Manufacturer - not an FAA rule

NOT AN FAA REQUIREMENT — This is a manufacturer document. It is not an FAA Airworthiness Directive and compliance is not required by 14 CFR 39 unless an AD cites it.

SB CG 300-1002 P1, Initial Issue, Rear Engine Mount Tightening Torque Inspection, 251107

Source: Continental Aerospace Technologies, retrieved 2026-09-01

View on Continental Aerospace Technologies' site

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