P/N: 65b07657-125
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 65b07657-125 is an aircraft stringer that reinforces fuselage and wing skin in semi-monocoque structures. This aerospace aluminum component prevents skin buckling under flight loads and bending stresses. Stringers are riveted to skin panels between frame stations, creating a stiffened structure that carries both axial and bending loads efficiently.
Installation follows FAA AC 43.13-1B guidance with attention to edge distance, rivet spacing, and fit verification per the aircraft's Illustrated Parts Catalog. Proper attachment maintains structural integrity during pressurization and maneuvering.
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 65b07657-125 is an aircraft stringer that reinforces fuselage and wing skin in semi-monocoque structures. This aerospace aluminum component prevents skin buckling under flight loads and bending stresses.
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 65b07657-125.