P/N: 137187E448
Category: Controls & Cables
This product requires a custom quote. Please contact our sales team for pricing information or submit an RFQ (Request for Quote).
| Condition | Stock |
|---|---|
| New | 2 Available |
The 137187E448 is a stainless-steel aircraft control cable with swaged terminals for cockpit-to-component mechanical linkages. Constructed from stranded wire rope per MIL-DTL-83420 and MIL-DTL-781 specifications, it transmits control inputs with minimal stretch and high reliability. Used in flight-control systems to transfer force from pilot controls to flight surfaces and engine components.
Installation requires proper tensioning and routing per aircraft maintenance manual specifications to maintain control authority and prevent cable slack or binding during operation.
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 137187E448 is a stainless-steel aircraft control cable with swaged terminals for cockpit-to-component mechanical linkages. Constructed from stranded wire rope per MIL-DTL-83420 and MIL-DTL-781 specifications, it transmits control inputs with minimal stretch and high reliability.
The CABLE 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. 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 CABLE. 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 137187E448.