Piper Aircraft Composite Stiffener 101809-002 OEM Replacement
This genuine Piper Aircraft OEM stiffener is intended for use in Piper aircraft airframe composite assemblies. Part number 101809-002 is a pre-impregnated fiber composite component intended to reinforce structural panels or skins within the airframe.
The stiffener is manufactured in the United States, carries FAA approval code PC, and is 8130-3 eligible. It measures 8.27 x 5.51 x 0.59 inches and weighs 0.16 lb. Classified under HTS 8807300010, ECCN 9A991.d, and Schedule B 8807300010. Non-hazardous, supplied as a single unit.
Installation must be performed in accordance with the applicable Piper Aircraft structural repair manual and current airworthiness directives.
| Manufacturer Part Number | 101809-002 |
| Manufacturer | Piper Aircraft |
| Country of Origin | United States |
| Dimensions (L x W x H) | 8.27 x 5.51 x 0.59 in |
| Weight | 0.16 lb |
| ECCN | 9A991.d |
| Schedule B | 8807300010 |
| FAA Approval Code | PC |
| 8130-3 Eligible | Yes |
Refer to the aircraft Illustrated Parts Catalog (IPC) to verify applicability before ordering.
Original: $3.17
-65%$3.17
$1.11Piper Aircraft Composite Stiffener 101809-002 OEM Replacement
This genuine Piper Aircraft OEM stiffener is intended for use in Piper aircraft airframe composite assemblies. Part number 101809-002 is a pre-impregnated fiber composite component intended to reinforce structural panels or skins within the airframe.
The stiffener is manufactured in the United States, carries FAA approval code PC, and is 8130-3 eligible. It measures 8.27 x 5.51 x 0.59 inches and weighs 0.16 lb. Classified under HTS 8807300010, ECCN 9A991.d, and Schedule B 8807300010. Non-hazardous, supplied as a single unit.
Installation must be performed in accordance with the applicable Piper Aircraft structural repair manual and current airworthiness directives.
| Manufacturer Part Number | 101809-002 |
| Manufacturer | Piper Aircraft |
| Country of Origin | United States |
| Dimensions (L x W x H) | 8.27 x 5.51 x 0.59 in |
| Weight | 0.16 lb |
| ECCN | 9A991.d |
| Schedule B | 8807300010 |
| FAA Approval Code | PC |
| 8130-3 Eligible | Yes |
Refer to the aircraft Illustrated Parts Catalog (IPC) to verify applicability before ordering.
Product Information
Product Information
Shipping & Returns
Shipping & Returns
Description
This genuine Piper Aircraft OEM stiffener is intended for use in Piper aircraft airframe composite assemblies. Part number 101809-002 is a pre-impregnated fiber composite component intended to reinforce structural panels or skins within the airframe.
The stiffener is manufactured in the United States, carries FAA approval code PC, and is 8130-3 eligible. It measures 8.27 x 5.51 x 0.59 inches and weighs 0.16 lb. Classified under HTS 8807300010, ECCN 9A991.d, and Schedule B 8807300010. Non-hazardous, supplied as a single unit.
Installation must be performed in accordance with the applicable Piper Aircraft structural repair manual and current airworthiness directives.
| Manufacturer Part Number | 101809-002 |
| Manufacturer | Piper Aircraft |
| Country of Origin | United States |
| Dimensions (L x W x H) | 8.27 x 5.51 x 0.59 in |
| Weight | 0.16 lb |
| ECCN | 9A991.d |
| Schedule B | 8807300010 |
| FAA Approval Code | PC |
| 8130-3 Eligible | Yes |
Refer to the aircraft Illustrated Parts Catalog (IPC) to verify applicability before ordering.
