P/N: 35-e2103-0202
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 |
|---|---|
| New Surplus | 1 Available |
The 35-e2103-0202 is a structural reinforcement plate designed to stiffen aircraft skins and distribute fastener loads in high-stress areas. Made from aluminum or steel, this reinforcement arrests crack growth and shares bearing loads during airframe repairs. Install with approved AN or NAS fasteners per the aircraft maintenance manual and FAA AC 43.13-1B guidance.
Verify compatibility with the 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.
The 35-e2103-0202 is a structural reinforcement plate designed to stiffen aircraft skins and distribute fastener loads in high-stress areas. Made from aluminum or steel, this reinforcement arrests crack growth and shares bearing loads during airframe repairs.
The REINFORCEMENT 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 Surplus. 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 REINFORCEMENT. 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 35-e2103-0202.