P/N: 1462020-28
Category: Controls & Cables
This product requires a custom quote. Please contact our sales team for pricing information or submit an RFQ (Request for Quote).
| Condition | Stock |
|---|---|
| New Surplus | 1 Available |
The 1462020-28 is a flap control quadrant assembly for Cessna O-2A aircraft. This mechanical component mounts in the cockpit and translates pilot lever input into proportional motion for the flap control linkage. The quadrant interfaces between the control column area and the flap actuation system, allowing pilots to command flap extension and retraction.
Installation requires proper rigging per the aircraft maintenance manual to ensure correct flap positioning and travel limits. NSN 1560-00-903-1308.
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 1462020-28 is a flap control quadrant assembly for Cessna O-2A aircraft. This mechanical component mounts in the cockpit and translates pilot lever input into proportional motion for the flap control linkage.
The QUADRANT ASSEMBLY 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: New Surplus. 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 QUADRANT ASSEMBLY. 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 1462020-28.