47-06-08: Starter Solenoid and Buss Lead Wires
FAA order 47-06-08 is an airworthiness directive. The FAA's subject line: Starter Solenoid and Buss Lead Wires. System: engine.
What it applies to as the FAA lists it
- Kind of product
- Aircraft
- Makes
- Textron Aviation Inc.
- Models
- Army AT-11, C18S
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 (673 characters)
47-06-08 BEECH: (Was Service Note 1 of AD-757-2 and Service Note 1 of AD-2-582- 2.) Applies to AT-11 and C18S Aircraft.
Compliance required immediately and after each 100 hours of operation thereafter.
Remove the battery covers from the right and left-hand wing stubs. Inspect the starter solenoid and main buss lead wires. In the right wing these wires are numbered 4 and 5. In the left wing they are numbered 2 and 3. If these wires show signs of chafing on the cold air duct junction box or any other part of the structure they should be supported by an insulated clip to give ample clearance.
(Beech Service Bulletin No. C18-5 covers this same subject.)
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/47-06-08.json · aircraft systems.