P/N: 105-30402.39
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 105-30402.39 is a left-hand aircraft stringer, a formed metal longitudinal stiffener installed in fuselage bays. This structural member reinforces the skin and transfers loads between frames and ribs, preventing buckling under flight stresses. Typically fabricated from aluminum alloy, the stringer runs the length of the fuselage section on the left side.
Installation follows OEM structural repair manual specifications and 14 CFR Part 43 acceptable methods. Used in general aviation and commercial aircraft fuselage construction and repair.
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 105-30402. 39 is a left-hand aircraft stringer, a formed metal longitudinal stiffener installed in fuselage bays.
The STRINGER LH 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 LH. 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 105-30402.39.