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CherryMAX CR3523-4-02 Universal Head Monel Rivet

CherryMAX CR3523-4-02 Universal Head Monel Rivet

Cherry Aerospace

SKU:CR3523-4-02_EACH

Regular price $5.99 USD
Regular price $11.27 USD Sale price $5.99 USD
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CherryMAX CR3523-4-02 Universal Head Monel Rivet

The Cherry Aerospace CR3523-4-02 CherryMAX® rivet is a locked-spindle blind rivet with a universal head. The CR3523 series uses a Monel rivet sleeve with a CRES stem and is part of Cherry Aerospace's nominal-diameter CherryMAX family.

Part number CR3523-4-02 is a 1/8" nominal diameter size with a 1/16"–1/8" (0.062"–0.125") grip range. This product is configured with Each and Bag of 100 purchase options.

Product Details

  • Manufacturer: Cherry Aerospace
  • Product Family: CherryMAX®
  • Part Number: CR3523-4-02
  • Series: CR3523
  • Rivet Type: Locked-Spindle Blind Rivet
  • Head Style: Universal
  • Diameter Type: Nominal CherryMAX®
  • Nominal Diameter: 1/8" (-4)
  • Recommended Hole Diameter: 0.129"–0.132"
  • Grip Range: 1/16"–1/8" (0.062"–0.125")
  • Sleeve Material: Monel
  • Stem Material: CRES
  • Series Standard: NAS9307M
  • Package Quantity: Each / Bag of 100 variants

Understanding the CherryMAX Part Number

CherryMAX part numbers identify the rivet series and material combination, head style, diameter, and grip length. Use the CherryMAX identification guide below to help interpret the part number.

CherryMAX part number identification guide for aircraft blind rivets

For CR3523-4-02, the -4 diameter code identifies the 1/8" nominal size, while -02 identifies the grip range. The CR3523 series is a nominal-diameter CherryMAX series.

CherryMAX Rivet

The CR3523 series is specified by Cherry Aerospace as a nominal CherryMAX rivet with a universal head, Monel sleeve, and CRES stem. For the -4 diameter size, Cherry specifies a recommended hole diameter of 0.129"–0.132".

Verify Rivet Size & Application

Before ordering or installing the CherryMAX CR3523-4-02, verify the required rivet series, diameter, grip range, head style, hole preparation, material combination, and installation requirements against the applicable aircraft structural repair manual, maintenance documentation, engineering data, or other approved technical data.

Confirm that the 1/16"–1/8" (0.062"–0.125") grip range and nominal CR3523 configuration are appropriate for your specific installation.

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