P/N: 1712136-1
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 1712136-1 is a fuselage stringer that reinforces aircraft skin by carrying axial loads into frames and formers. This longitudinal stiffening member prevents buckling under pressurization and flight loads in fuselage skin bays. Installation requires approved fasteners and procedures per the aircraft Structural Repair Manual.
Confirm configuration and fit before replacement to ensure proper load transfer and structural integrity.
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 1712136-1 is a fuselage stringer that reinforces aircraft skin by carrying axial loads into frames and formers. This longitudinal stiffening member prevents buckling under pressurization and flight loads in fuselage skin bays.
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: 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 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 1712136-1.