Pan Head Machine Screw - MS35207-265
Standard Part
Description: Pan Head Machine Screw
Part Number: MS35207-265
Alternate Part Numbers: AN520-10R11, AN520-10R12, 19088ADX, A1BMW6024G, 2537, 31145, A207D24, 5338-306, 402343, 859001-00, BM12297-05, 19088, 6543, 436752, 7-099-000154, 5305PL0631723, 71137-265, G0005404, DSR1523-8, MS24584-57, 1055-845
Product Overview
An externally threaded fastener whose threaded portion is of one nominal diameter, no 0 (0.060 in./1.5 mm) or larger, designed to be held or driven with either a wrench or an inserted driver or both (excluding internal socket or internal multiple spline types), in sizes below no. 10 (0.190 in./5 mm). No. 10 and larger sizes must have a head designed for any type inserted driver (excluding internal socket or internal multiple spline types), but may also be designed for external wrenching. A locking feature may be incorporated in the design of the head or threads. Excludes bolt, clevis; bolt, externally relieved body; screw, externally relieved body; and screw, assembled washer. See also, screw, instrument; bolt, machine; bolt, internal wrenching; and screw, cap socket head.
Item Specification
| Thread Class | 2A | |
| Thread Direction | Right-hand | |
| Thread Length | 0.657 inches minimum and 0.750 inches maximum | |
| Fastener Length | 0.719 inches minimum and 0.750 inches maximum | |
| Head Style | PAN | |
| Head Diameter | 0.357 inches minimum and 0.373 inches maximum | |
| Head Height | 0.122 inches minimum and 0.133 inches maximum | |
| Internal Drive Style | Cross recess type 1 | |
| End Item Identification | Acf; A4N; abm; auf; aga; atf; 95A; byn; aun; ahn; RG-33 mrap; multiple launch rocket system (mlrs); A4 bradley fighting vehicle; A3 bradley fighting vehicle | |
| Nominal Thread Diameter | 0.190 inches | |
| Thread Quantity per Inch | 32 | |
| Minimum Tensile Strength | 55000 pounds per square inch | |
| Screw Material | Steel comp 1010 or steel comp 1011 or steel comp 1013 | |
| Screw Material Document and Classification | 66 fed std all material responses | |
| Screw Surface Treatment | Cadmium and chromate | |
| Screw Surface Treatment Document and Classification | QQ-P-416, ty 2, cl 3 fed spec single treatment response | |
| Thread Series Designator | UNF |
Fits in
- Bombardier Challenger 300
- Bombardier Challenger 601
- Bombardier Challenger 604
- Bombardier Challenger 605
- Bombardier Global Express
- Bombardier Learjet 40
- Bombardier Learjet 45
- Bombardier Learjet 55
- Bombardier Learjet 60 - all variants
- Embraer Legacy 600-650
- Gulfstream G-IV/GIV-SP/G-400/G-450/G-300
- Gulfstream G-V/G-V-SP/G-550/G-500
- Piaggio Avanti II
- Piaggio Avanti P180
- Pilatus PC-12
- Piper Aircraft PA-42 Cheyenne
- 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 Bell 206 Jetranger/Longranger
- Textron Aviation Cessna 500 Citation I-ISP
- Textron Aviation Cessna 510 Citation Mustang
- Textron Aviation Cessna 525 Citation Citationjet
- Textron Aviation Cessna 550 Citation I-II-Bravo
- Textron Aviation Cessna 560 Citation V-Ultra-Encore-Excel-XLS
- Textron Aviation Cessna 650 Citation III-IV-VI-VII
- Textron Aviation Cessna 680 Citation Sovereign
- Textron Aviation Cessna 750 Citation X
- Textron Aviation Hawker 400-400XP
- Textron Aviation Hawker 700
- Textron Aviation Hawker 800
- Textron Aviation Hawker 800XP-850XP
- Textron Aviation Hawker 900XP