P/N: 212-61123-1
Category: Manifolds
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 |
| New | 1 Available |
The 212-61123-1 is a pitot system manifold that distributes ram-air pressure from the pitot probe to flight instruments and air data computers. This aluminum manifold serves as the central junction in the pitot-static system, routing high-pressure air to airspeed indicators, altimeters, and related avionics. Installed between the pitot probe and downstream instruments, it maintains pressure integrity across multiple connection points.
After installation or maintenance, perform leak checks and pitot-static system tests per 14 CFR Part 91.411 to ensure accurate instrument readings.
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 212-61123-1 is a pitot system manifold that distributes ram-air pressure from the pitot probe to flight instruments and air data computers. This aluminum manifold serves as the central junction in the pitot-static system, routing high-pressure air to airspeed indicators, altimeters, and related avionics.
Depending on condition, the 212-61123-1 may include an FAA 8130-3 Airworthiness Approval Tag, a yellow serviceable tag, or manufacturer documentation. Currently available in: New Surplus, New. Contact us for specific documentation details on the condition you need.
Yes, the MANIFOLD, PITOT SYS can be used in engine overhauls and maintenance events. Always verify part compatibility against your engine's Type Certificate Data Sheet (TCDS) and Illustrated Parts Catalog (IPC) before installation.
In-stock items ship same business day when ordered before 3 PM EST. We also offer 24/7 AOG (Aircraft on Ground) support at (904) 998-9101 for urgent engine part needs.