FIN ASSY (P/N 63500-008) - As Removed
P/N: 63500-008
Category: Structural Components
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 | 2 Available |
Product Description
The 63500-008 fin assembly is the fixed vertical tail surface of an aircraft empennage. This aluminum structural component provides directional stability during flight by resisting yaw movement. Installed as part of the vertical tail structure per the aircraft Maintenance Manual or Structural Repair Manual, the fin assembly mounts to the fuselage using standard aerospace fasteners.
Verify compatibility with your aircraft's Illustrated Parts Catalog before installation. Maintenance may reference FAA AC 43.13-1B when manufacturer data is unavailable.
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 FIN ASSY (P/N 63500-008)?
The 63500-008 fin assembly is the fixed vertical tail surface of an aircraft empennage. This aluminum structural component provides directional stability during flight by resisting yaw movement.
Is the 63500-008 a PMA or OEM part?
The FIN ASSY 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 63500-008 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 FIN ASSY. We stock related hardware and can help identify companion parts.
Can the 63500-008 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 63500-008.
Related Structural Components
- FITTING: – P/N 67040-013
- SUPPORT – P/N 0513252-1
- Stabilizer, Right, Comnlete – P/N 34004
- FITTING – P/N 20392-000
- ANGLE – P/N 0713070-36
- RIB – P/N 17104-8
- SKIN-ELEV HORN – P/N 45-660012-1
- CHANNEL ASSEMBLY – P/N 25-8sf683-3a
- SUPPORT – P/N 120-64862-001
- SUPPORT – P/N 0441211-1
- RH WING TIP – P/N 18317-002
- angle of attatck indicator – P/N 586-12