Thank you for taking an interest in our selection of 5320-00-117-6959 parts here on Boost AOG. You are currently on the RFQ form for part number MS20426AD4-18, a National Aerospace Standards Com product listed with the Rivet Solid If part number MS20426AD4-18 catches your eye, be sure to use our online RFQ service to request quotes, with customized responses provided within 15 minutes of us receiving and reviewing a completed submission.
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| NSN | FSC | NIIN | CLS | Hazmat | DEMIL | Cancelled NSN |
|---|---|---|---|---|---|---|
| 5320-00-117-6959 Item PartTypeName: RIVET,SOLID | 5320 | 001176959 | 0 | N | ||
| CIIC | HCC | ESD | PMIC | Criticality | ENAC | |
| U | U | |||||
| Part Number | ISC | RNVC | RNCC | HCC | MSDS | SADC |
| MS20426AD4-18 | 2 | 2 | 3 |
| MRC | Criteria | Characteristic |
|---|---|---|
| AASB | FASTENER LENGTH | 1.115 INCHES MINIMUM AND 1.135 INCHES MAXIMUM |
| AASK | HEAD STYLE | FLUSH (FLAT) COUNTERSUNK (INCLUDED ANGLE-LESS THAN 135 DEG W OR W/O CHAMFER) |
| AAZE | SHANK DIAMETER | 0.124 INCHES MINIMUM AND 0.128 INCHES MAXIMUM |
| AAZF | SHANK STYLE | STRAIGHT W/RADIUS CHAMFERED TIP |
| AAZG | HEAD MAJOR DIAMETER | 0.221 INCHES MINIMUM AND 0.229 INCHES MAXIMUM |
| AGAV | END ITEM IDENTIFICATION | W/S: F/A-18E/F HORNET AIRCRAFT; FMS-AIRCRAFT,HAWKEYE E-2C; LOS ANGELES CLASS SSN (688); AIRCRAFT,C-2A (REPROCURED); MISSILE,ADVANCED MEDIUM RANGE AIR-T0-AIR (AMRAAM)/AIM120A; AIRCRAFT,AIRLIFTER C-17A; MISSILE,MINUTEMAN LGM-30; JOINT ST |
| ANEE | GRIP LENGTH | 0.927 INCHES MINIMUM AND 0.947 INCHES MAXIMUM |
| CQSX | SHEAR STRENGTH | 26000 SINGLE POUNDS PER SQUARE INCH |
| CRSQ | COUNTERSINK ANGLE | 99.5 DEGREES MINIMUM AND 100.5 DEGREES MAXIMUM |
| MATT | MATERIAL | ALUMINUM ALLOY 2117 OVERALL |
| MDCL | MATERIAL DOCUMENT AND CLASSIFICATION | QQ-A-430 FED SPEC SINGLE MATERIAL RESPONSE OVERALL |
| SFTT | SURFACE TREATMENT | ANODIZE OVERALL OR OXIDE FILM OVERALL |
| STDC | SURFACE TREATMENT DOCUMENT AND CLASSIFICATION | MIL-A-8625 MIL SPEC 1ST TREATMENT RESPONSE OVERALL OR MIL-C-5541 MIL SPEC 2ND TREATMENT RESPONSE OVERALL |
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