P/N: 21950-007
Category: Doors & Access Panels
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 21950-007 is a sheet-metal cowl bottom assembly for Piper Aircraft engine compartments. This aluminum component forms the lower cowling structure, directing cooling airflow around the engine and shielding internal components from debris and weather exposure. It provides access to engine bay service points during routine maintenance and inspection.
Installation requires proper alignment with mating cowl sections and fastening per the aircraft maintenance manual. 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 21950-007 is a sheet-metal cowl bottom assembly for Piper Aircraft engine compartments. This aluminum component forms the lower cowling structure, directing cooling airflow around the engine and shielding internal components from debris and weather exposure.
The COWL BOTTOM ASSY 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 COWL BOTTOM ASSY. 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 21950-007.