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| 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 |
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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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