P/N: 7004187-903
Category: Flight Computers
This product requires a custom quote. Please contact our sales team for pricing information or submit an RFQ (Request for Quote).
| Condition | Stock |
|---|---|
| As Removed | 2 Available |
The 7004187-903 is an analog stability augmentation computer for aircraft flight-control systems. This component processes sensor inputs to provide rate damping that stabilizes pitch, roll, and yaw motion during flight. Integrated within yaw damper or SAS channels, it conditions signals and commands servos to improve aircraft handling characteristics.
Installation and testing follow aircraft maintenance manual procedures and approved avionics standards per 14 CFR §25.672 and §27.672. Used in general aviation and transport aircraft requiring enhanced flight stability.
Please note: Product descriptions are provided for informational purposes. Always refer to your aircraft's Illustrated Parts Catalog (IPC) to verify part compatibility and specifications.
The 7004187-903 is an analog stability augmentation computer for aircraft flight-control systems. This component processes sensor inputs to provide rate damping that stabilizes pitch, roll, and yaw motion during flight.
Avionics compatibility depends on your aircraft model and existing installation. The ANALOG STAB AUG COMPUTER is available in: As Removed. We recommend checking your aircraft's wiring diagrams and STC documentation, or contact our avionics team for compatibility assistance.
Availability of an FAA 8130-3 tag depends on the part condition. Overhauled and repaired units typically include 8130-3 documentation. As-removed units may include a removal tag with trace history. Contact us for specific documentation on the condition you need.
We can arrange bench testing through our network of FAA-certified repair stations. Call (904) 998-9101 for testing availability and turnaround times, or submit an RFQ with your specific requirements.