P/N: t700a5540027002
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 | 2 Available |
The t700a5540027002 is an upper fitting for aircraft structural attachment points. This aerospace-grade metal component transfers loads between adjoining airframe members in wing attachment structures. It accepts standard AN/MS/NAS fasteners for secure assembly.
Installation follows OEM Structural Repair Manual specifications with published torque values and inspection criteria. Commonly found in general aviation and regional aircraft wing systems where load-bearing connections require precision engineering and reliable 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 t700a5540027002 is an upper fitting for aircraft structural attachment points. This aerospace-grade metal component transfers loads between adjoining airframe members in wing attachment structures.
The UPPER FITTING 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 UPPER FITTING. 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 t700a5540027002.