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 | : | 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
- • Bombardier Challenger 605
- • Textron Aviation Beechcraft King Air 200 - all variants
- • Textron Aviation Beechcraft King Air 300 - all variants
- • 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
- • Textron Aviation Hawker 400-400XP
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 |