Engine model

Continental C-90

Continental Aerospace Technologies

Airworthiness Directives
1
Service Bulletins
1
Last live check
2026-08-171 of 1 re-verified
What this page is: a restatement of what the official Federal Register and manufacturer records show as of the date listed below each item. It is not a determination that any specific aircraft or engine is, or is not, in compliance. Under 14 CFR §91.403 and §91.417, the aircraft owner/operator is responsible for maintaining airworthiness and required records. Always verify against the official FAA and manufacturer sources linked below before making a maintenance or airworthiness decision.

Airworthiness Directives

1 record
AD

94-05-05 R1

FR doc 96-1409 · 61 FR 2708

AD 94-05-05 R1Published 1996-01-29Effective 1996-02-13

Teledyne Continental Motors Models C75, C85, C90, C125, C145, O-200, O-300, and GO-300 Series and Rolls-Royce, plc C90, O-200 and O-300 Series Reciprocating Engines

Requires inspection of the cylinder rocker shaft bosses for cracks, and inspection of the cylinder rocker shaft for looseness and replacement, if necessary, with a serviceable part.

Full official abstract

Airworthiness Directives; Teledyne Continental Motors Models C75, C85, C90, C125, C145, O-200, O-300, and GO-300 Series and Rolls-Royce, plc C90, O-200 and O-300 Series Reciprocating Engines

This amendment revises an existing airworthiness directive (AD), applicable to Teledyne Continental Motors (TCM) Models C75, C85, C90, C125, C145, O-200, O-300, and GO-300 series reciprocating engines, that currently requires inspection of the cylinder rocker shaft bosses for cracks, and inspection of the cylinder rocker shaft for looseness and replacement, if necessary, with a serviceable part. This amendment clarifies that the inspection must be accomplished at the next cylinder removal from the engine or engine overhaul, whichever occurs first, and adds certain Rolls-Royce, plc engines to the AD's applicability. This amendment is prompted by the need to clarify when the inspection must be performed. The actions specified by this AD are intended to prevent engine power loss and engine failure.

Source: Federal Register document 96-1409, retrieved 2026-08-15 · re-verified against the live Federal Register API 2026-08-17

Service Bulletins

1 record

This page indexes 1 AD and 1 SB from primary sources. The FAA may have issued additional directives for this engine that are not yet included.

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