P/N: 5554100-49
Category: Structural Components
This product requires a custom quote. Please contact our sales team for pricing information or submit an RFQ (Request for Quote).
| Condition | Stock |
|---|---|
| As Removed | 1 Available |
The 5554100-49 is an aluminum alloy structural doubler designed to reinforce aircraft sheet metal around cutouts, fastener rows, and repairs. This component distributes loads across weakened areas and arrests fatigue cracking in fuselage and wing skin panels. Installed during maintenance using approved fasteners or adhesive bonding per aircraft maintenance manual specifications, the doubler restores structural integrity to damaged or modified sections.
Installation follows FAA AC 43.13-1B methods when manufacturer instructions are 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.
The 5554100-49 is an aluminum alloy structural doubler designed to reinforce aircraft sheet metal around cutouts, fastener rows, and repairs. This component distributes loads across weakened areas and arrests fatigue cracking in fuselage and wing skin panels.
The DOUBLER 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.
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 DOUBLER. 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 5554100-49.