We appreciate your interest in Laminated Materials Corporation part number 7688727, which is currently ready for procurement here on Prompt Aerospace. For your reference, part number 7688727 is listed with the NSN 1240-00-768-8727 and description “Cell Optical Elemen.” If this is the item you are seeking and you would like to request a quote for your comparisons, simply complete the form below with information like your desired quantity, budget, and anticipated fulfillment timeframe. We regularly respond to requests within 15 minutes of receiving them, using the details we are offered to curate the most ideal purchasing options.
Note : We Will Not Share Your Information To Any Third Parties.
If you want to explore other items produced by Laminated Materials Corporation under the CAGE Code 20200 or that similarly fall under the FSC 1240 Optical Sighting And Ranging Equipment, keep in mind that since we list everything with relevant information, you can easily locate related part numbers using our search engine or catalogs. We also excel at tracking down parts with long lead times or that are generally hard to find, meaning that we can serve you even if you do not see exactly what you need on our website. With all of this being said, we are ready to help you source any of the NSN 1240-00-768-8727 parts and Cell Optical Elemen items your operations require, so request a quote today.
| MRC | Criteria | Characteristic |
|---|---|---|
| ZZZV | Fsc Application Data | PERISCOPE,TANK |
| AGAV | End Item Identification | 2350-00-678-5773;2350-01-058 9487 |
| FEAT | Special Features | 2.090 IN. FLANGE DIA;1.781 IN. FIRST SHOULDER DIA;1.761 IN.-48NS-2A THREAD;1.726 IN. SHOULDER END DIA; 0.125 IN. FLANGE THK;0.140 IN. FIRST SHOULDER LG;0.187 IN. THREAD LG;0.063 IN. WIDE UNDERCUT BETWEEN THREAD AND FIRST SHOULDER;1.572 IN.-48NS-2B BORE THREAD;0.390 IN. BORE THREAD LG; COUNTERBORE 1.581 IN. BY 0.060 IN. DEEP ON SHOULDER END;ONE SLOT 0.063 IN. W. BY 0.050 IN. DEEP ON FACE OF SHOULDER END;0.030 TO 0.034 IN. BORE ECCENTRICITY FROM GEOMETRIC AXIS;250 MICROINCH FINISH OVERALL EXCEPT 125 MICROINCH FINISH ON FIRST SHOULDER AND INSIDE FACE OF FLANGE;ALL EDGES CHAMFERED 0.010 IN. MAX. BY 45 DEG |
| BMTZ | Eccentric Construction | NOT PROVIDED |
| BPDC | Chamfer Location | BOTH ENDS |
| MRC | Decoded Requirement | Clear Text Reply |
| ABHP | Overall Length | 0.575 INCHES NOMINAL |
| MATT | Material | ALUMINUM ALLOY 2011 OR ALUMINUM ALLOY 6061 |
If You’re Ever Looking for NSN parts Or Have an Aircraft On Ground Situation, Don’t forget That We offer Competitive Pricing and Guaranteed On-Time Delivery.
Request for Quote
