P/N: 44b232-1
Category: Structural Components
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 | 7 Available |
The 44b232-1 is an aluminum patch plate designed to restore structural integrity in aircraft skin repairs. This external doubler covers trimmed damage areas and redistributes loads across the repair zone. Installed using AN/MS/NAS fasteners per FAA AC 43.13-1B standards, the plate reinforces metal-skin panels on general and commercial aircraft.
Fastener spacing and edge distances must comply with structural repair manual specifications. Compatible with most aluminum airframe repairs where local strength restoration is required.
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 44b232-1 is an aluminum patch plate designed to restore structural integrity in aircraft skin repairs. This external doubler covers trimmed damage areas and redistributes loads across the repair zone.
The PATCH PLATE 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: New Surplus. 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 PATCH PLATE. 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 44b232-1.