PLATE (P/N c54005) - New
P/N: c54005
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 |
|---|---|
| New | 4 Available |
Product Description
The c54005 is a structural reinforcement plate designed for aircraft fuselage and wing panel repairs. This aluminum or steel plate distributes concentrated loads across skin and frame members, preventing crack propagation in high-stress areas. Installed as a doubler or splice member where localized reinforcement is required, the plate fastens using rivets or bolts per approved structural repair manual data.
Installation follows FAA AC 43.13-1B acceptable methods, with fastener patterns and spacing determined by aircraft-specific documentation and load requirements.
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 PLATE (P/N c54005)?
The c54005 is a structural reinforcement plate designed for aircraft fuselage and wing panel repairs. This aluminum or steel plate distributes concentrated loads across skin and frame members, preventing crack propagation in high-stress areas.
Is the c54005 a PMA or OEM part?
The PLATE 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. Contact us for sourcing details.
Does the c54005 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 PLATE. We stock related hardware and can help identify companion parts.
Can the c54005 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 c54005.
Related Structural Components
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- FITTING – P/N 001A711E2252-201
- LORD MOUNTS – P/N lm431-98
- BRACKET – P/N 2413051-1
- BRACKET – P/N 416611
- COVER, TAILCONE, TRANSPARENT – P/N a558-1
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