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TAB - P/N 5024000-61

TAB (P/N 5024000-61) - As Removed

P/N: 5024000-61

Category: Flight Control Surfaces

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Available Inventory

Condition Stock
As Removed 1 Available

Product Description

The 5024000-61 is an aileron trim tab assembly for Cessna 310/310F aircraft. This component mounts on the aileron trailing edge to balance roll forces and reduce pilot control input requirements. By adjusting the aileron's neutral position, the trim tab maintains coordinated flight without constant stick pressure.

Installation uses existing hinges and linkages per the aircraft maintenance manual. Verify compatibility with your aircraft's Illustrated Parts Catalog before installation.

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 TAB (P/N 5024000-61)?

The 5024000-61 is an aileron trim tab assembly for Cessna 310/310F aircraft. This component mounts on the aileron trailing edge to balance roll forces and reduce pilot control input requirements.

Is the 5024000-61 a PMA or OEM part?

The TAB 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 5024000-61 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 TAB. We stock related hardware and can help identify companion parts.

Can the 5024000-61 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 5024000-61.

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