CESSNA 180 — Airworthiness Directives
6 airworthiness directives references for the CESSNA 180.
This document is an Airworthiness Directive (AD) issued by the FAA for various Textron Aviation Inc. aircraft models, including the Cessna 185. The directive addresses safety concerns related to cracks in the tailcone and horizontal stabilizer attachment structure. It mandates inspections and potential repairs to ensure the structural integrity of these components, which are critical for safe flight. The AD is effective from December 7, 2020, and applies to all affected aircraft regardless of their service history. The document outlines compliance requirements, inspection intervals, and the necessary actions to rectify identified issues, ensuring continued airworthiness of the aircraft.
- The AD is effective from December 7, 2020.
- Inspections must be conducted within 100 hours TIS or 12 months after the effective date.
- Subsequent inspections are required every 500 hours TIS or 5 years.
- Cracks in the tailcone and stabilizer attachment can lead to loss of control if not addressed.
- Operators may receive credit for previous inspections performed under specific service letters.
- AD 2020-21-22 - McFarlane Aviation202010 pages· 152 KB· via media.mcfarlaneaviation.com
- Airworthiness Directive Schedule - Cessna 180 Series - CAA202014 pages· 239 KB· via www.aviation.govt.nz
- Airworthiness Directive - AD/CESSNA 180/15 Amdt 4 - Rear Spar20045 pages· 87 KB· via services.casa.gov.au
- AD/CESSNA 180/79 - Wing Lower Spar Cap Angle Stiffener - CASA19981 pages· 11 KB· via services.casa.gov.au
- Airworthiness Directive | Sensenich Propellers19963 pages· 118 KB· via www.sensenich.com
- AD/CESSNA 180/70 Amdt 1 - Fuel Filler Caps and Adaptors - CASA19881 pages· 12 KB· via services.casa.gov.au


