CESSNA 172Q CUTLASS — Airworthiness Directives
1 airworthiness directives reference for the CESSNA 172Q CUTLASS.
This document is an Airworthiness Directive (AD) issued by the FAA concerning Lycoming Engines, specifically models 320, 360, and 540 series, which are equipped with certain Engine Components, Inc. (ECi) cylinder assemblies. The directive aims to address safety concerns related to potential cylinder head separations that could lead to engine failure and loss of control of the aircraft. The AD outlines compliance requirements for visual inspections and compression tests of the affected cylinder assemblies, as well as replacement protocols for those found to be defective. It is crucial for operators of affected engines to adhere to the specified compliance times to ensure safety and airworthiness.
- The AD is effective from February 4, 2010.
- It applies to specific Lycoming Engines models with ECi cylinder assemblies.
- Operators must perform visual inspections and compression tests within specified timeframes.
- Cracked cylinder assemblies must be replaced before further flight.
- Group 'B' ECi cylinder assemblies cannot be installed after the AD's effective date.
How many Airworthiness Directives documents does Sprinkle have for the CESSNA 172Q CUTLASS?
Sprinkle has 1 Airworthiness Directives document on file for the CESSNA 172Q CUTLASS.
What year is the CESSNA 172Q CUTLASS Airworthiness Directives?
The CESSNA 172Q CUTLASS Airworthiness Directives on file is dated 2009.
How many pages is the CESSNA 172Q CUTLASS Airworthiness Directives?
The CESSNA 172Q CUTLASS Airworthiness Directives runs 14 pages.
Where does Sprinkle's CESSNA 172Q CUTLASS Airworthiness Directives come from?
This CESSNA 172Q CUTLASS Airworthiness Directives was originally published by safarihelicopter.com and is hosted on Sprinkle with full text and specs.