SUB ASSEMBLY CONTROL COLUMN (P/N 25-8cf53-217a) - As Removed
P/N: 25-8cf53-217a
Category: Flight Control Surfaces
This product requires a custom quote. Please contact our sales team for pricing information or submit an RFQ (Request for Quote).
Available Inventory
| Condition | Stock |
|---|---|
| As Removed | 1 Available |
Product Description
The 25-8cf53-217a is a sub-assembly control column that transmits pilot pitch and roll inputs to the elevator and aileron surfaces via mechanical linkages. This cockpit-mounted component serves as the primary interface between pilot control inputs and the aircraft's flight control systems. The assembly typically incorporates steel and aluminum construction for strength and weight efficiency.
Installation requires rigging per the Aircraft Maintenance Manual to ensure full travel range and free movement without binding. Proper operation is critical for safe aircraft control.
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.
Frequently Asked Questions
What is the SUB ASSEMBLY CONTROL COLUMN (P/N 25-8cf53-217a)?
The 25-8cf53-217a is a sub-assembly control column that transmits pilot pitch and roll inputs to the elevator and aileron surfaces via mechanical linkages. This cockpit-mounted component serves as the primary interface between pilot control inputs and the aircraft's flight control systems.
Is the 25-8cf53-217a a PMA or OEM part?
The SUB ASSEMBLY CONTROL COLUMN 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.
Does the 25-8cf53-217a include installation hardware?
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 SUB ASSEMBLY CONTROL COLUMN. We stock related hardware and can help identify companion parts.
Can the 25-8cf53-217a be shipped internationally?
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 25-8cf53-217a.
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- TIP, RUDDER BUTT – P/N 26-11
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