ASAP Aviation Procurement is pleased to announce that part number A12752 of NSN 1240-00-768-8703 is now available and in stock. We can get you one of the fastest and most competitive quotes on this part. Part number A12752 is a Cell Optical Elemen manufactured by Autodyne Manufacturing Co Inc under CAGE Code 05584. Simply fill out the Request for Quote (RFQ) form provided here to get started on your quote. In order to make sure that we get you your quote in a timely manner, please take the time to make sure that all fields are completely filled out, particularly the asterisk-marked (*) fields like Parts Needed By and Quantity (ea).
We will be using your response to these fields to calculate your quote. Within 15 minutes of receiving your RFQ, a member of our sales team will contact you with your quote. ASAP Aviation Procurement, owned and operated by ASAP Semiconductor, is a leading distributor of new and obsolete NSN parts for the aerospace, civil aviation, and defense industries. With our inventory of more than 2 billion parts sourced from over 5000 manufacturers from around the world, we do our level best to become your go-to one-stop shop. And to help us offer you the best streamlined parts procurement experience, we have advanced shipping facilities across USA. A12752 Autodyne Manufacturing Co Inc is in stock.
Are you interested in learning more about part number A12752? If so, feel free to contact us by phone at +1-714-705-4780, or by email at sales@asap-aviationprocurement.com.
| MRC | Criteria | Characteristic |
|---|---|---|
| SR-5 | THE MANUFACTURERS DATA | |
| SR-5 | DESIGN CONTROL REFERENCE | 7688703 |
| ABHP | OVERALL LENGTH | 0.210 INCHES NOMINAL |
| APJC | THREAD LOCATION | INTERNAL |
| SR-5 | MANUFACTURERS CODE | 19200 |
| ZZZV | III FSC APPLICATION DATA | PERISCOPE,TANK |
| MATL | MATERIAL | ALUMINUM ALLOY, QQ-A-225/3, ALLOY 2011, T3 OR ALUMINUM ALLOY, QQ-A-200/8, 6061, T6 |
| AGAV | III END ITEM IDENTIFICATION | 2350-00-678-5773;2350-01-058- 9487 |
| FEAT | SPECIAL FEATURES | FLANGE DIA,1.946 IN.;SHOULDER DIA,0.060 IN.;FLANGE THICKNESS,0.150 IN.;SHOULDER LG,1.784 IN.;STRAIGHT BORE DIA,0.030 TO 0.034 IN.;BORE ECCENTRICITY FROM GEOMETRIC AXIS,ONE SLOT 0.063 IN. WIDE ON FLANGE PERIPHERY;125 MICROINCH FINISH ON SURFACES OF BORE,SHOULDER AND FLANGE END FACE;250 MICROINCH FINISH ON SURFACES OF SHOULDER END FACE AND FLANGE PERIPHERY |
| SURF | SURFACE TREATMENT | ANODIZED BLACK |
| BMTZ | ECCENTRIC CONSTRUCTION | NOT PROVIDED |
| BPDC | CHAMFER LOCATION | BOTH ENDS |
| BPDD | CHAMFER SIZE | 0.010 IN. BY 45 DEG |
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AS9120B and ISO 9001:2015 |
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Aviation Suppliers Association Member |
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FAA AC 0056B Accredited |
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AS 6081:2012 Certification |
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ESD S20.20-2014 Certification |
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