256 Installation Manual __link__: Ki
The BendixKing KI 256 Flight Command Indicator (FCI) installation manual is a technical document that outlines the integration and setup of this self-contained vertical gyro into BendixKing flight control systems like the KFC-150, KFC-200, KFC-225, and KFC-250 Bendix/King Key Technical Aspects System Integration:
Post-connection test: With engine running and gyro powered, vacuum gauge at KI 256 case must read steady 5.0 ±0.2 inHg after 5 minutes. ki 256 installation manual
Panel Compatibility: Available in versions designed for 0-degree or 8-degree instrument panel tilts to ensure proper viewing angles. The BendixKing KI 256 Flight Command Indicator (FCI)
Attitude Outputs: Pins provide buffered pitch and roll attitude signals to the flight computer. Do not install in aircraft with unregulated 28V
6. Limitations & Compatibility
- Do not install in aircraft with unregulated 28V bus exceeding 32V DC.
- Not approved as primary attitude source for IFR without operative KCS 55/55A system and standby attitude indicator.
- Operating temperature: –20°C to +70°C.
- Offer solutions to common problems that might arise during installation.