P/N: 50-430016-17
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 |
|---|---|
| As Removed | 1 Available |
The 50-430016-17 is a main door latch rod that connects the entry/airstair door handle to the latch pin mechanism. This steel linkage component transmits handle motion through the door frame assembly, enabling controlled locking and unlocking of the main door. Installed within the door latch mechanism per ATA Chapter 52 specifications, the rod coordinates with handle rotation to engage or disengage latch hardware.
Verify compatibility with your aircraft's Illustrated Parts Catalog before installation.
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 50-430016-17 is a main door latch rod that connects the entry/airstair door handle to the latch pin mechanism. This steel linkage component transmits handle motion through the door frame assembly, enabling controlled locking and unlocking of the main door.
The ROD-LATCH MAIN DOOR 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 ROD-LATCH MAIN DOOR. 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 50-430016-17.