Request a Quote for Part Number 4038404A with NSN 5340003775658 by United Technologies Corporation Today!
Bracket Angle
RFQ Axis is more than just a one-stop shop for NSN components; we are a premium sourcing partner that uses our market expertise and resources to find custom solutions catered to our customers’ needs. On this page, you can request a quote for your comparison for part number 4038404A, a Bracket Angle item by United Technologies Corporation. Listed alongside the NSN 5340003775658, part number 4038404A is a fully traceable component that has met rigorous military and industrial standards. Simply fill in details below about your requirements, and a dedicated member of our team will be able to formulate a solution that matches your stated needs in 15 minutes or less after receiving a submission.
Part number 4038404A is manufactured by United Technologies Corporation, a trusted entity on our Approved Vendor List (AVL) that is associated with the CAGE Code . As part of our vast supply network, this manufacturer is just one of the many accredited entities we work with across the globe that allow us to offer competitive pricing and expedited shipping times. Additionally, if you would like to explore other products with the NSN 5340003775658 or similar parts, we invite you to check out our page of listings or look at the list of related items below.
Procurement notes for 4038404A.
Bracket Angle ASAP can support availability checks, alternate review, lead-time confirmation, and documentation requirements tied to the part number, NSN, CAGE code, or active bill of materials.
Catalog classifications
NSN Information for Part Number 4038404A with NSN 5340-00-377-5658, 5340003775658
Characteristics Data of NSN 5340-00-377-5658, 5340003775658
| MRC | Criteria | Characteristic |
|---|---|---|
| ADLK | FIRST LEG LENGTH | 0.405 INCHES MINIMUM AND 0.435 INCHES MAXIMUM |
| ADLL | SECOND LEG LENGTH | 0.630 INCHES MINIMUM AND 0.650 INCHES MAXIMUM |
| AGAV | III END ITEM IDENTIFICATION | W/S: ENGINE, AIRCRAFT, F100-PW-200 (F-16A/B/C/D); AIRCRAFT, EAGLE F-15; SUPPORT EQUIPMENT, C-5 AIRCRAFT; AIRCRAFT, F-16; ENGINE, AIRCRAFT, F100-PW-100 (F-15A/B/C/D); ADVANCE AIR TRAFFIC CONTR. & LAND. SYS (ATCALS) 404L; AIRCRAFT, F-111; ENG |
| AHLF | SECOND LEG WIDTH | 0.190 INCHES MINIMUM AND 0.210 INCHES MAXIMUM |
| AHLK | FIRST LEG HOLE DIAMETER | 0.160 INCHES MINIMUM AND 0.170 INCHES MAXIMUM |
| AHPW | FIRST LEG THICKNESS | 0.023 INCHES MINIMUM AND 0.027 INCHES MAXIMUM |
| AHPX | SECOND LEG THICKNESS | 0.023 INCHES MINIMUM AND 0.027 INCHES MAXIMUM |
| AHQN | FIRST LEG WIDTH | 0.330 INCHES MINIMUM AND 0.350 INCHES MAXIMUM |
| AHRA | FIRST LEG DISTANCE FROM EDGE TO HOLE CENTER ALONG WIDTH | 0.165 INCHES MINIMUM AND 0.175 INCHES MAXIMUM |
| AHRB | FIRST LEG DISTANCE FROM EDGE TO HOLE CENTER ALONG LENGTH | 0.165 INCHES MINIMUM AND 0.175 INCHES MAXIMUM |
| AJFP | FIRST LEG END RADIUS | 0.165 INCHES MINIMUM AND 0.175 INCHES MAXIMUM |
| AJFQ | SECOND LEG END RADIUS | 0.095 INCHES MINIMUM AND 0.105 INCHES MAXIMUM |
| AJZU | FIRST LEG STYLE | END RADIUS |
| AKAU | FIRST LEG HOLE ARRANGEMENT STYLE | ONE HOLE |
| AKBU | SECOND LEG STYLE | END RADIUS |
| AKCU | SECOND LEG HOLE ARRANGEMENT STYLE | NO HOLE |
| CSSP | SECOND LEG RELATIONSHIP TO FIRST LEG | NOT IDENTICAL |
| CSSQ | FIRST LEG ANGLE | 90.0 DEGREES NOMINAL |
| MATT | MATERIAL | STEEL |
| MDCL | MATERIAL DOCUMENT AND CLASSIFICATION | AMS 5540 ASSN STD SINGLE MATERIAL RESPONSE |
| STYL | STYLE DESIGNATOR | ANGLE |