MS35214-42 - Pan Head Machine Screw 1/2 8-32

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MS35214-42 - Pan Head Machine Screw 1/2 8-32

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MS35214-42 – Pan Head Machine Screw 1/2 8-32

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Overview

The MS35214-42 is a military-standard pan head machine screw engineered for specific non-structural applications within aircraft, particularly in instrument mounting and cockpit assemblies. Conforming to the rigorous MS35214 standard, this fastener is differentiated by its material composition—a high-quality copper alloy (brass)—which provides excellent natural corrosion resistance and non-magnetic properties. The pan head design offers a low-profile, clean finish with a broad bearing surface, making it an ideal and certified choice for securing instruments and panels where a non-steel fastener is required.

Key Features

  • Copper Alloy (Brass) Construction: Fabricated from a high-quality brass alloy. This material is inherently resistant to corrosion and is non-magnetic, which is critical for fasteners used in close proximity to sensitive magnetic compasses and other flight instruments.
  • Pan Head Design: Features a versatile pan head with a flat bearing surface that provides good clamping force without a high profile. This ensures a secure fit for panels and components without creating an obstruction.
  • Black Oxide Finish: Coated with a durable, black chemical oxide finish. This non-reflective coating is ideal for use within the cockpit and on instrument panels to minimize glare and reflections, enhancing pilot readability.
  • MS Certified Quality: As a certified Military Standard part, the MS35214-42 guarantees full traceability, dimensional accuracy, and material composition, ensuring it meets the highest quality standards for aviation use.
  • Non-Structural Application: Specifically designed for light-duty applications where the high tensile strength of steel is not required, but material properties like corrosion resistance and non-interference are paramount.

Technical Specifications

  • Standard: MS35214 (Screw, Machine, Pan Head, Cross-Recessed, Brass)
  • Full Part Number: MS35214-42
  • Material: Copper Alloy (Brass)
  • Finish: Black Oxide
  • Head Style: Pan Head
  • Drive Type: Phillips / Cross-Recess Type I
  • Thread Specification: 8-32 UNC-2A
    • Nominal Diameter: #8 (0.164 inches)
    • Threads Per Inch: 32 (Coarse Thread)
  • Length: 1/2 inch (0.500 inches), measured from under the head.
  • Minimum Tensile Strength: 57,000 PSI

Aircraft Compatibility

The MS35214-42 is a standard component used across a vast range of general aviation, commercial, and military aircraft. Its use is specified by manufacturers wherever a non-magnetic, corrosion-resistant machine screw of this size is needed.

  • Common Applications:
    • Instrument Panel Installation: Securing flight instruments, gauges, and avionics faceplates.
    • Interior Components: Fastening trim pieces, placards, and cabin furnishings.
    • Electrical Grounding: Used in specific applications where a brass screw is required for electrical conductivity or to prevent galvanic corrosion with other materials.
    • Light-Duty Panel Fastening: Attaching inspection covers and panels where structural loads are not a factor.

Applications

The MS35214-42 is the specified fastener for applications where its unique material properties are essential:

  • Non-Magnetic Zones: Crucial for installations near magnetic compasses or other instruments sensitive to magnetic interference.
  • Corrosion-Prone Areas: Provides a durable fastening solution in areas where moisture may be present.
  • Instrument Assembly: The black, non-reflective head is standard for visible fasteners on instrument panels to reduce glare for the pilot.

Why Choose MS35214-42?

Using the correct, certified hardware is a cornerstone of aviation safety and airworthiness. The MS35214-42 screw provides the specific non-magnetic and corrosion-resistant properties required for many cockpit and instrument installations. Substituting with a standard steel screw could induce compass errors or lead to premature corrosion. By choosing a genuine MS35214-42, you are ensuring the use of a fastener with a certified material pedigree, correct dimensions, and a finish designed for the specific challenges of the flight deck environment.

Order Your MS35214-42 Screws Now

Ensure your instrument and panel installations are professional and airworthy with certified hardware. Visit Airparts.aero to order your MS35214-42 brass machine screws today.

The Military Standard MS35214 specification is dedicated to a series of pan head, cross-recessed machine screws made from copper alloy (brass). This standard fills a critical niche where the properties of steel are undesirable. Brass offers excellent resistance to corrosion, especially in moist environments, and is inherently non-magnetic, making it the ideal choice for fasteners near sensitive avionics. The black oxide finish is not for corrosion protection (as the brass itself is resistant) but is primarily a surface treatment to reduce reflectivity, a key human factors consideration in cockpit design. The coarse UNC thread pattern ensures quick and easy assembly without the risk of cross-threading, which is ideal for maintenance and installation tasks.

Note: Always verify the correct screw part number (including material, thread size, and length) from the applicable aircraft maintenance manual or Illustrated Parts Catalog (IPC). The use of a brass screw is often a specific engineering choice that should not be substituted.

Item Specification

Thread Class

 

:

2A

Thread Direction


:Right-hand

Thread Length


:0.438" inches minimum and 0.500" inches maximum

Fastener Length

:

0.500" inches nominal

Head Style

:

PAN

Head Diameter


:0.306" inches minimum and 0.322" inches maximum

Head Height

:

0.105" inches minimum and 0.115" inches maximum

Internal Drive Style

:

Cross recess type 1

Nominal Thread Diameter

:

0.164" inches

Thread Quantity per Inch

:

32

Minimum Tensile Strength

:

57000 pounds per square inch

Screw Material

:

Copper alloy

Screw Material Document
and Classification

:

QQ-B-626 fed spec single material response or
QQ-W-321 fed spec single material response

Thread Series Designator

:

UNC

 

Fits in

  • • Bombardier Challenger 601
  • • Bombardier Challenger 604
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  • • Textron Aviation Beechcraft King Air 90 - all variants
  • • Textron Aviation Beechcraft Premier
  • • Textron Aviation Cessna 525 Citation Citationjet
  • • Textron Aviation Cessna 560 Citation V-Ultra-Encore-Excel-XLS
  • • Textron Aviation Cessna 750 Citation X
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Additional info
Colors Black
Dimensions
Dimensions (W x H x D) 0.57" x 0.29" x 0.29" inches
Length 0.57" inch
Weight 0.01 lb
Specifications
8130-3 Eligible No
ATA Chapter 51 ATA Standard Practices and Structures
Available Conditions NE / NS
Cage Code 96906
Country of origin United States of America
ECCN / USML 9A991.d
FAA Approval Code STD
Grip 0.438 inches minimum and 0.500 inches maximum
Hazmat Code Not Applicable
Hazmat(Y/N) N
Material Copper alloy
NSN 5305-00-637-1123
Schedule B 7415.33.8550
Thread 2A
Total Shelf Life (days) Not Applicable
Type Screw
Units of Measure (UoM) Each
Brand Standard
Color Black
Condition status Depreciated