P/N: 25-8sf41-1a
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 25-8sf41-1a is a bracket assembly that mounts aircraft components and system hardware to fuselage or wing structure. This assembly provides rigid attachment points for clamps, supports, and fastener interfaces using AN/MS/NAS hardware. Commonly used to secure cushion clamps (MS21919) that protect and route hoses or wire harnesses along structural members.
Installation follows the aircraft maintenance manual or FAA AC 43.13 guidance when manufacturer data is unavailable. Fastener torque and alignment requirements depend on the specific aircraft type and structural location.
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 25-8sf41-1a is a bracket assembly that mounts aircraft components and system hardware to fuselage or wing structure. This assembly provides rigid attachment points for clamps, supports, and fastener interfaces using AN/MS/NAS hardware.
The BRACKET ASSY 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 BRACKET ASSY. 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 25-8sf41-1a.