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CR3213-5-04 - Cherry Aerospace Textron Blind Rivet
CR3213-5-04 - Cherry Aerospace Textron Blind Rivet
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CR3243-4-3 - Cherry Aerospace Rivet Blind
CR3243-4-3 - Cherry Aerospace Rivet Blind
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6.82

CR3242-4-3 - Cherry Aerospace Oversized Blind Cherrymax Rivet

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CR3242-4-3 – CherryMAX® Blind Flush Rivet (Oversize)

Part Number: CR3242-4-3 (also referenced as CR3242-4-03)

Manufacturer: Cherry Aerospace (A PCC Company)

Military Specification: NAS1097 / MIL-R-7885

Overview Section

The CR3242-4-3 is a high-strength oversize structural blind rivet featuring a 100° flush (countersunk) head. It is part of the world-renowned CherryMAX® family, recognized as the industry standard for high-reliability blind fastening in aerospace maintenance and manufacturing.

The "42" designation signifies the oversize diameter (1/64" larger than nominal), engineered specifically for MRO (Maintenance, Repair, and Overhaul) applications. It is the designated solution for restoring structural integrity when a standard 1/8" rivet hole has been enlarged, damaged, or cleaned of corrosion during the removal of an old fastener. By using the CR3242-4-3, technicians can achieve a precision interference fit in a reworked hole, maintaining the aerodynamic profile and structural load-bearing capacity of the airframe.

Enhanced Technical Data

Technical MetricSpecification Data
Nominal Diameter1/8 in
Actual Shank Diameter0.140 in – 0.143 in (Oversize)
Grip Range (-3)0.126 in – 0.187 in
Head Style100° Flush Head (Reduced Profile per NAS1097)
Ultimate Shear Strength530 lbs (minimum)
Ultimate Tensile Strength245 lbs (minimum)
Sleeve Material5056 Aluminum Alloy (AMS 4118)
Stem Material8740 Alloy Steel (AMS 6322)
Locking Collar MaterialA-286 Corrosion Resistant Steel
Required Hole Size#27 Drill Bit (0.144" – 0.147")

Advanced Engineering & Structural Application

The CR3242-4-3 is designed for Structural Load Path Restoration. In aerospace structures, a loose or "smoking" rivet compromises the aircraft's fatigue life. The oversize shank of the -42 series fills the void created by hole wear, preventing "shuttling" (micro-movements) of the fastener.

Engineering Insight: The Bulbed Blind Head

During installation, the sleeve "bulbs" against the blind side of the structure. This creates a large, uniform bearing surface that distributes the clamping force over a wider area. This is particularly advantageous when fastening thin skins to heavier internal frames, as it prevents the rivet from pulling through the skin under high tensile loads.

Mechanical Safe-Locking Spindle

The hallmark of the CherryMAX system is the Integral Driving Anvil and Locking Collar.3 As the tool reaches the final pull stage, it drives the collar into the stem's locking groove. This ensures the stem is permanently retained, contributing its high-shear steel strength to the overall joint, unlike "pop" rivets where the mandrel is lost or non-structural.

Aircraft Compatibility

The CR3242-4-3 is ubiquitous in the Structural Repair Manuals (SRM) of virtually all metallic aircraft:

  • Textron Aviation: Essential for Cessna Citation and King Air skin-to-rib repairs.

  • Bombardier: Extensively used in the CRJ and Challenger series secondary structures.

  • Gulfstream: Found in cabin pressurized bulkheads and floor structures.

  • General Aviation: The "gold standard" for repairing loose 1/8" rivets on Piper, Beechcraft, and Mooney airframes.

The Cherry Aerospace CR3242-4-3 provides a critical engineering solution for airframe technicians. When a standard 1/8" rivet hole becomes oversized due to vibration or repair work, the CR3242-4-3 restores the original structural integrity of the joint. With a grip range specifically suited for material thicknesses between 1/8" and 3/16", this fastener combines the aerodynamic superiority of a NAS1097 flush head with the shear-load capacity of an 8740 alloy steel stem. The CherryMAX "Safe-Lock" system ensures that the stem stays put, providing peace of mind for pressurized cabins and high-stress airframe components.6

Installation & Maintenance Addendum

  1. Hole Size Warning: Do not attempt to install this rivet in a standard #30 hole. It must be prepared with a #27 drill bit.

  2. Tool Compatibility: Compatible with standard power and manual pulling tools, including the Cherry G704B, G747, and the G29 hand riveter. Ensure the pulling head is a dedicated CherryMAX type (e.g., H701-456).

  3. Visual Confirmation: A correctly installed CR3242-4-3 will show the gold locking collar seated flush within the rivet head. If the stem breaks off below the head surface and the collar is missing, the rivet has not locked and must be replaced.


FAA PMA Alternate Part Number: Textron Aerospace Fasteners P/N - CR3242-4-3 [Click Here]


Product Overview

An item consisting of two or more of the following components: stem, rivet body, sleeve, expander, bolt, and collar. It is a headed fastening device with the shank designed to be expanded by means of a separate or integral stem or mandrel, or bolt and expander. It is designed to be installed or expanded from one side only. Excludes nut, blind assembly.


Specification:

Fastener Length
:0.267" Inches Minimum and 0.287" Inches Maximum
Head Style
:Flush (flat) countersunk (included angle - less than 135 deg W or W/O chamfer)
Shank Diameter
:0.140" Inches Minimum and 0.143" Inches Maximum
Shank Style
:Self-plugging mechanically locked stem
Head Major Diameter
:0.211" Inches Minimum
Expansion Device
:Serrated stem-type W
Grip Length
:0.126" Inches Minimum and 0.187" Inches Maximum
Countersink Angle
:100.0 Degrees Nominal
Special Features




:



Ns" letters after the material code "b" indicate no preference to lock type
(may be visible or internal). rivets with no letter code (indicating visible lock
type) and rivets with the letter "h" after the material code (indicating internal
lock type) are both acceptable for this item of supply.
Material
:Aluminum alloy 5056 body
Material
:Steel comp 8740 stem
Material Document and Classification
:Ams 6322 assn std single material response stem
Material Document and Classification
:QQ-A-430 fed spec single material response body
Surface Treatment
:Cadmium stem
Surface Treatment
:Chromate body
Surface Treatment Document and Classification
:MIL-C-5541 mil spec single treatment response body
Surface Treatment Document and Classification
:QQ-P-416, ty 2, cl 3 fed spec single treatment response stem








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Dimensions
Dimensions (W x H x D) 0.211'' x 0.287'' x 0.143'' Inches
Length 0.287'' Inches
Weight 0.001 lbs
Specifications
8130-3 Eligible Yes
ATA Chapter 51 ATA Standard Practices
Available Conditions NE
Cage Code FB009
Country of origin United States
ECCN / USML 9A991.d
FAA Approval Code TSO
Grip 0.126'' Inches Minimum and 0.187'' Inches Maximum
Hazmat Code Not Applicable
Hazmat(Y/N) N
Material Aluminum alloy 5056 body And Steel comp 8740 Stem
NSN 5320-01-034-1885
Schedule B 7616.10.3000
Total Shelf Life (days) Not Applicable
Type Rivet
Units of Measure (UoM) Each
Brand Cherry Aerospace
Condition status Depreciated
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