Piper - 487-483 - Spring - Inner Arm Nose Gear

Piper Aircraft

Piper - 487-483 - Spring - Inner Arm Nose Gear

P/N: 487-483

Product Code: AFP1009F

Certificate Type: FAA 8130-3

68,17 $
The Piper 487-483 Spring – Inner Arm Nose Gear is an aircraft landing gear spring designed for use within the nose landing gear assembly of applicable Piper aircraft.
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P/N 487-483
Product Code AFP1009F
Product Category Airframe Parts
Certificate Type FAA 8130-3
Country of Manufacture United States
Delivery Please add to cart for availability. If no stock delivery term is usually 3-4 weeks.
Importer for Serbia Grappolo Aviation Supply Co. Ltd
Manufacturer Piper Aircraft
Alternate P/N 67168-000

The 487-483 is identified as a Piper landing gear spring and is specifically associated with the inner arm of the nose gear. The part number is also associated with Piper P/N 67168-000, which is listed as an original or alternate part number for this component.

This component is suitable for aircraft operators, maintenance organizations, repair stations, aircraft owners, and aviation parts distributors sourcing replacement landing gear components for applicable Piper aircraft.

Product Information:

Manufacturer: Piper Aircraft
Part Number: 487-483
Original/Alternate Part Number: 67168-000
Component: Spring
Description: Inner Arm Nose Gear Spring
System: Nose Landing Gear
Application: Applicable Piper aircraft
Quantity: 1 each
Weight: 0.113 kg (0.25 lb)
Application & Compatibility:
The 487-483 spring should be matched to the applicable aircraft model and landing gear configuration before purchase. Verify the part number against the current Piper Illustrated Parts Catalog (IPC), aircraft maintenance manual, and other applicable manufacturer documentation to ensure the component is approved for the intended installation.

Maintenance & Installation:
Installation should be performed by appropriately qualified aircraft maintenance personnel in accordance with the applicable Piper maintenance documentation. Proper inspection of the landing gear assembly and associated hardware should be completed during installation, with all applicable procedures and requirements followed.

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