PLENUM (P/N 2615111-36) - As Removed

The 2615111-36 is an aircraft plenum that forms a pressure chamber within the engine cowling. This component manages cooling airflow around engine cylinders on air-cooled piston engines, equalizing upper plenum pressure to ensure efficient heat removal through cylinder fins. The aluminum plenum directs incoming air flow while maintaining proper pressure distribution during engine operation.

Install and service per manufacturer specifications and FAA AC 43.13 guidance. Verify fitment using your aircraft's Illustrated Parts Catalog and torque all fasteners per the maintenance manual.

What is the PLENUM (P/N 2615111-36)?

The 2615111-36 is an aircraft plenum that forms a pressure chamber within the engine cowling. This component manages cooling airflow around engine cylinders on air-cooled piston engines, equalizing upper plenum pressure to ensure efficient heat removal through cylinder fins.

Is the 2615111-36 a PMA or OEM part?

The PLENUM 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.

Does the 2615111-36 include installation hardware?

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 PLENUM. We stock related hardware and can help identify companion parts.

Can the 2615111-36 be shipped internationally?

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 2615111-36.