P/N: 586-12
Category: Structural Components
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 | 1 Available |
The 586-12 is a panel-mounted angle of attack indicator that displays the wing's angle relative to incoming airflow. This instrument helps pilots manage stall margin and approach stability by showing real-time AOA data during flight operations. The indicator integrates with vane or pressure-based AOA sensors mounted on the aircraft fuselage.
Installation requires calibration per the avionics installation manual and FAA-approved data specific to your aircraft and sensor system. Essential for approach guidance and situational awareness on the flight deck.
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 586-12 is a panel-mounted angle of attack indicator that displays the wing's angle relative to incoming airflow. This instrument helps pilots manage stall margin and approach stability by showing real-time AOA data during flight operations.
The angle of attatck indicator may be available as an OEM (Original Equipment Manufacturer) or PMA (Parts Manufacturer Approval) part depending on condition and source. Both carry FAA certification for airworthiness. Currently available in: As Removed. Contact us for sourcing details.
Installation hardware requirements vary by application. Check your aircraft's Structural Repair Manual (SRM) or Illustrated Parts Catalog (IPC) for the complete installation kit requirements for the angle of attatck indicator. We stock related hardware and can help identify companion parts.
Yes, we ship airframe components worldwide. International orders typically arrive within 3-14 business days depending on destination. Export documentation and customs forms are included. Contact us for international shipping quotes on the 586-12.