COWL (P/N 202-0020-33) - As Removed

The 202-0020-33 is an aircraft cowl panel that encloses the engine compartment and manages cooling airflow around the powerplant. Constructed from metal or composite materials, this nacelle component streamlines airflow while reducing drag and maintaining optimal engine temperatures during flight. Installation follows 14 CFR Part 43 maintenance standards and the aircraft's maintenance manual.

Verify compatibility with your aircraft's Illustrated Parts Catalog before installation to ensure proper fit and fastener alignment.

What is the COWL (P/N 202-0020-33)?

The 202-0020-33 is an aircraft cowl panel that encloses the engine compartment and manages cooling airflow around the powerplant. Constructed from metal or composite materials, this nacelle component streamlines airflow while reducing drag and maintaining optimal engine temperatures during flight.

Is the 202-0020-33 a PMA or OEM part?

The COWL 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 202-0020-33 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 COWL. We stock related hardware and can help identify companion parts.

Can the 202-0020-33 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 202-0020-33.