You are currently exploring our in-stock options for part number 1270M42G01 with the NSN 5340012150149. This product is listed with the description “Bracket Angle” and is manufactured by Aerospace Industries Inc. If you are looking to purchase this part, we encourage you to complete and submit the RFQ form below with as much information as you can provide, such as your desired quantity, budget, shipping time frame, and more. Within 15 minutes of receiving and reviewing your submission, one of our experts will reach out with a quote that is tailored to your needs.
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We supply all relevant information alongside the listings on our website, that way you know you are always getting the exact item you require. For example, part number 1270M42G01 is listed alongside the NSN 5340-01-215-0149 and belongs to the FSC 5340 Hardware Commercial. Additionally, it is also under the CAGE Code 0AMR1, which is assigned to Aerospace Industries Inc. At Aerospace Procurement, you can trust that each product in our inventory is up to industry standards, as we are committed to various quality assurance practices. For example, we uphold a strict NO CHINA SOURCING pledge to ensure that each part is shipped out alongside its manufacturer trace documentation and qualifying certifications. These practices and more allow us to operate with AS9120B, ISO 9001:2015, and FAA AC 00-56B accreditation. Get in contact with us today to see how we can make the procurement process for part number 1270M42G01 seamless.
| NSN | FSC | NIIN | CLS | Hazmat | DEMIL | Cancelled NSN |
|---|---|---|---|---|---|---|
| 5340-01-215-0149 Item PartTypeName: BRACKET,ANGLE | 5340 | 012150149 | 0 | P | ||
| CIIC | HCC | ESD | PMIC | Criticality | ENAC | |
| U | A | 0 | ||||
| Part Number | ISC | RNVC | RNCC | HCC | MSDS | SADC |
| 1270M42G01 | 5 | 2 | 5 |
| MRC | Criteria | Characteristic |
|---|---|---|
| ACHY | MOUNTING HOLE TYPE | PLAIN |
| AGAV | END ITEM IDENTIFICATION | W/S: MISSILE,AIR LAUNCH CRUISE (ALCM) AGM-86B; ENGINE,AIRCRAFT,TF-33-P-7 (C-141A/B); U-2 ENGINE (F-118-GE-101); ENGINE,F118-GE-100 (B-2 BOMBER); ENGINE,AIRCRAFT,F110-GE-100/129 (F-16 C/D); ENGINE,AIRCRAFT,F-108 (CFM-56,KC-135A); EN |
| AHLK | FIRST LEG HOLE DIAMETER | 0.337 INCHES MINIMUM AND 0.351 INCHES MAXIMUM |
| AHLN | SECOND LEG HOLE DIAMETER | 0.274 INCHES MINIMUM AND 0.288 INCHES MAXIMUM |
| AHLS | SECOND LEG DISTANCE BETWEEN HOLE CENTERS ALONG LENGTH | 1.150 NOMINAL INCHES |
| AHPW | FIRST LEG THICKNESS | 0.060 INCHES MINIMUM AND 0.066 INCHES MAXIMUM |
| AHPX | SECOND LEG THICKNESS | 0.060 INCHES MINIMUM AND 0.066 INCHES MAXIMUM |
| AHQU | FIRST LEG DISTANCE BETWEEN HOLE CENTERS ALONG WIDTH | 1.088 INCHES NOMINAL |
| AJZU | FIRST LEG STYLE | CORNER RADIUS |
| AKAU | FIRST LEG HOLE ARRANGEMENT STYLE | TWO HOLES |
| AKCU | SECOND LEG HOLE ARRANGEMENT STYLE | TWO HOLES |
| CBBL | FEATURES PROVIDED | NUT |
| CSSP | SECOND LEG RELATIONSHIP TO FIRST LEG | NOT IDENTICAL |
| CSSQ | FIRST LEG ANGLE | 90.0 DEGREES NOMINAL |
| FEAT | SPECIAL FEATURES | FURNISHED WITH 2 NUTPLATES (ITEM 2); EACH NUTPLATE HAS FLOATING NUT AND 2 RIVET HOLES,0.098 IN. MIN,0.102 IN. MAX DIA,AND 4 RIVETS (ITEM 3),2 FOR EACH NUTPLATE |
| MATT | MATERIAL | NICKEL ALLOY 625 |
| MDCL | MATERIAL DOCUMENT AND CLASSIFICATION | AMS 5599 ASSN STD SINGLE MATERIAL RESPONSE |
| STYL | STYLE DESIGNATOR | ANGLE |
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