| Item Name | Nut Self Locking Pl |
| INC Code | 05280 |
| Federal Supply Group (FSG) | Hardware and Abrasives |
| Federal Supply Class (FSC) | 5310 Nuts and Washers |
| National Item Identification Number (NIIN) | 00-678-9962 (006789962) |
| NCB Code | USA (00) |
| Manufacturer | Atlas Corp, Marty Gilman Incorporated, Monadnock Company The, The Boeing Company, Rockwell International Corp |
| Associated Parts Numbers of NSN 5310-00-678-9962 | ||||||
|---|---|---|---|---|---|---|
| Part Number | Manufacturer | Item Name | Cage Code | Type | Status | RFQ |
| WSI4-10 | atlas corp | nut self locking pl | 04169 | A | F | RFQ |
| WS1 4 10 | atlas corp | nut self locking pl | 04169 | A | F | RFQ |
| BACN10TL3-10 | marty gilman incorporated | nut self locking pl | 91730 | A | A | RFQ |
| BACN10TL3-10 | monadnock company the | nut self locking pl | 60119 | A | A | RFQ |
| HE114-0077-0003 | the boeing company | nut self locking pl | 81205 | A | A | RFQ |
| HE114-0077-0003 | rockwell international corp | nut self locking pl | 89372 | A | F | RFQ |
| BACN10TL3-10 | the boeing company | nut self locking pl | 81205 | A | A | RFQ |
| MRC | Criteria | Characteristic |
|---|---|---|
| AAJD | THREAD CLASS | 2B |
| AAJF | THREAD DIRECTION | RIGHT-HAND |
| AAUM | LOCKING FEATURE | PREVAILING TORQUE WITH METALLIC INSERT |
| ACTA | NUT STYLE | PLATE |
| ADFU | MOUNTING HOLE ARRANGEMENT STYLE | 2 HOLES |
| ADFW | DISTANCE FROM APERTURE CENTER TO MOUNTING HOLE CENTER | 0.334 INCHES MINIMUM AND 0.354 INCHES MAXIMUM |
| AGAV | END ITEM IDENTIFICATION | W/S: HELICOPTER,CHINOOK,CH-47; TRAINER,B-1B AIRCRAFT; AIRCRAFT,(AC-130H,MC-130H,EC-130E,HC-130); AIRCRAFT,AIRLIFTER C-17A; AIRCRAFT MH-47E SPECIAL OPERATIONS AIRCRAFT; AIRCRAFT,AWACS,E-3A; AIRCRAFT,STRATOFORTRESS B-52; JOINT STAR |
| CMLP | THREAD QUANTITY PER INCH | 32 |
| CQJX | NOMINAL THREAD SIZE | 0.190 INCHES |
| MATT | MATERIAL | STEEL CORROSION RESISTING OVERALL EXCEPT INSERT |
| MDCL | MATERIAL DOCUMENT AND CLASSIFICATION | MIL-A-25493 MIL SPEC 2ND MATERIAL RESPONSE OR MIL-A-12545 TEMPER T6 MIL SPEC 2ND MATERIAL RESPONSE LOCKING INSERT |
| ABTB | MOUNTING HOLE DIAMETER | 0.097 INCHES MINIMUM AND 0.100 INCHES MAXIMUM |
| ACVN | NUT LENGTH | 0.975 INCHES MINIMUM AND 0.995 INCHES MAXIMUM |
| ADEA | NUT HEIGHT | 0.980 INCHES MINIMUM AND 1.020 INCHES MAXIMUM |
| ADEB | PLATE THICKNESS | 0.050 INCHES MINIMUM AND 0.070 INCHES MAXIMUM |
| ADEC | PLATE WIDTH | 0.386 INCHES MINIMUM AND 0.406 INCHES MAXIMUM |
| ADFP | NUT MOUNTING PROVISION | STRAIGHT HOLES |
| ADFY | CENTER TO CENTER DISTANCE BETWEEN MOUNTING HOLES ALONG LENGTH | 0.678 INCHES MINIMUM AND 0.698 INCHES MAXIMUM |
| BZRR | THREAD SERIES | UNF |
| MATT | MATERIAL | ALUMINUM ALLOY 6066 OR ALUMINUM ALLOY 6061 LOCKING INSERT |
| SFTT | SURFACE TREATMENT | CHROMATE OVERALL |
| STDC | SURFACE TREATMENT DOCUMENT AND CLASSIFICATION | MIL-C-5541 MIL SPEC SINGLE TREATMENT RESPONSE OVERALL |
| Relevant Components for NSN - 5310-00-678-9962, 5310006789962 | ||||
| 5310-01-011-9703 (5310010119703) | 5310-01-631-4489 (5310016314489) | 5310-00-020-9053 (5310000209053) | 5310-01-041-3831 (5310010413831) | |
| 5310-01-180-5326 (5310011805326) | 5310-01-187-5440 (5310011875440) | 5310-00-092-6831 (5310000926831) | 5310-01-210-4885 (5310012104885) | |
| 5310-00-474-5240 (5310004745240) | 5310-00-474-3114 (5310004743114) | 5310-00-159-9146 (5310001599146) | 5310-01-528-9271 (5310015289271) | |
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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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