60-07-08: Master Rod Assemblies
FAA order 60-07-08 is an airworthiness directive. The FAA's subject line: Master Rod Assemblies. System: engine.
What it applies to as the FAA lists it
- Kind of product
- Engine
- Makes
- Wright Aeronautical Division, Curtiss-Wright Corporation
- Models
- Military Cyclone R-1820 Series
Dates and paperwork
- Docket
- Unknown
- Status
- Current
- The FAA's document
- Read the order on the FAA's site
The order itself the regulatory text, as published
Show the full text (480 characters)
60-07-08 WRIGHT: Amdt. 121 Part 507 Federal Register March 29, 1960. Applies to All R-1820-103 Engines Installed In Helicopters.
Compliance required at first engine overhaul after June 1, 1960, but not later than December 31, 1960.
To alleviate failures of the master rod assemblies, strengthened master and articulating rods with associated parts must be installed in accordance with the instructions contained in Wright Aeronautical Division Service Bulletin No. C9-353.
Source: FAA Dynamic Regulatory System, airworthiness directives. The FAA's document is the authority; the register counts are this site's, from the FAA register of November 6, 2026. Connections as data: /graph/directive/60-07-08.json · aircraft systems.