P/N: 5111301-107
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 5111301-107 is a longitudinal stringer that reinforces aircraft fuselage and wing skin panels. This open-section profile stiffener transfers structural loads to frames while resisting buckling under compression. Stringers are bonded or riveted to skin surfaces in metallic and composite airframe assemblies to maintain panel integrity during flight loads.
Installation follows manufacturer specifications and FAA-accepted methods per AC 43.13-1B. Verify part compatibility in the aircraft's Illustrated Parts Catalog before assembly.
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 5111301-107 is a longitudinal stringer that reinforces aircraft fuselage and wing skin panels. This open-section profile stiffener transfers structural loads to frames while resisting buckling under compression.
The STRINGER 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 STRINGER. 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 5111301-107.