We appreciate your interest in our selection of parts that fall under the NSN 5310-01-035-9475. Below, top-requested part numbers like 760423, and others are presented alongside their manufacturer for your perusal. In order to receive pricing options on any featured NSN 5310-01-035-9475, simply click on the “RFQ” button next to it and complete the quote request form you are directed to. Be sure to include as many details as you can about your requirements and restrictions alike so our team can best formulate ideal fulfillment options for your consideration.
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| Item Name | Nut Self Locking Plate |
| Federal Supply Group (FSG) | Hardware and Abrasives |
| Federal Supply Class (FSC) | 5310 Nuts and Washers |
| National Item Identification Number (NIIN) | 01-035-9475 (010359475) |
| NCB Code | USA (01) |
| Manufacturer | Turbo Power And Marine System Inc, United Technologies Corporation, Paradigm Manchester Inc, Dynamic Gunver Technologies Llc |
| MRC | Criteria | Characteristic |
|---|---|---|
| AAJD | THREAD CLASS | 3B |
| AAJF | THREAD DIRECTION | RIGHT-HAND |
| AAUM | LOCKING FEATURE | PREVAILING TORQUE ALL METAL DESIGN |
| ABAJ | LUBRICATION | DRY FILM LUBRICANT |
| ABTB | MOUNTING HOLE DIAMETER | 0.339 INCHES MINIMUM AND 0.349 INCHES MAXIMUM |
| ACTA | NUT STYLE | PLATE |
| ACVN | NUT LENGTH | 1.909 INCHES MINIMUM AND 1.969 INCHES MAXIMUM |
| ADBR | DISTANCE FROM BASE TO CENTER OF APERTURE | 1.030 INCHES MINIMUM AND 1.050 INCHES MAXIMUM |
| ADEB | PLATE THICKNESS | 0.056 INCHES MINIMUM AND 0.068 INCHES MAXIMUM |
| ADEC | PLATE WIDTH | 0.610 INCHES MINIMUM AND 0.640 INCHES MAXIMUM |
| ADFP | NUT MOUNTING PROVISION | STRAIGHT HOLES |
| ADFU | MOUNTING HOLE ARRANGEMENT STYLE | 2 HOLES |
| ADFV | DISTANCE FROM MOUNTING HOLE CENTER TO BASE | 0.302 INCHES MINIMUM AND 0.322 INCHES MAXIMUM |
| ADFY | CENTER TO CENTER DISTANCE BETWEEN MOUNTING HOLES ALONG LENGTH | 1.067 INCHES MINIMUM AND 1.087 INCHES MAXIMUM |
| AGAV | END ITEM IDENTIFICATION | W/S: ENGINE,AIRCRAFT TF33-PW-102 (C-135E,EC-135H/K/P); ENGINE,AIRCRAFT T33-P-3/5/9 (C/EC-135,B-52H); ENGINE,AIRCRAFT,TF33-100 (E3A/B/C); ENGINE,AIRCRAFT,TF-33-P-7 (C-141A/B); AIRCRAFT,F-111; AIRCRAFT,STRATOLIFTER C-135; AIRCRAFT |
| BZRR | THREAD SERIES | UNJF |
| CMLP | THREAD QUANTITY PER INCH | 32 |
| CQFM | HARDNESS RATING | 36.0 ROCKWELL C MINIMUM AND 44.0 ROCKWELL C MAXIMUM |
| CQJX | NOMINAL THREAD SIZE | 0.190 INCHES |
| CRTL | CRITICALITY CODE JUSTIFICATION | FEAT |
| FEAT | SPECIAL FEATURES | DUE TO CRITICAL FEATURES,TOLERANCES,FIT RESTRICTIONS,MATERIL PROPERTIES MANUFACTURING PROCESS. FAILURE COULD RESULT IN LOSS OR SUBSTANTIAL DAMAGE TO WEAPON SYSTEM,DEATH OR SERIOUS INJURY |
| MATT | MATERIAL | STEEL BASE |
| MATT | MATERIAL | STEEL NUT |
| MDCL | MATERIAL DOCUMENT AND CLASSIFICATION | AISI1045 ASSN STD 1ST MATERIAL RESPONSE OR AISI1050 ASSN STD 2ND MATERIAL RESPONSE OR AISI4130 ASSN STD 3RD MATERIAL RESPONSE NUT |
| MDCL | MATERIAL DOCUMENT AND CLASSIFICATION | AMS5504 ASSN STD SINGLE MATERIAL RESPONSE BASE |
| SFTT | SURFACE TREATMENT | CADMIUM NUT |
| STDC | SURFACE TREATMENT DOCUMENT AND CLASSIFICATION | AMS2400 ASSN STD SINGLE TREATMENT RESPONSE NUT |
| Relevant Components for NSN - 5310-01-035-9475, 5310010359475 | ||||
| 5305-00-717-3100 (5305007173100) | 5315-01-347-4167 (5315013474167) | 5310-01-692-4808 (5310016924808) | 5310-00-852-2485 (5310008522485) | |
| 5315-01-213-4939 (5315012134939) | 5365-01-452-4206 (5365014524206) | 5340-01-625-1251 (5340016251251) | 5330-01-223-1696 (5330012231696) | |
| 5365-01-504-9604 (5365015049604) | 5340-01-479-0441 (5340014790441) | 5306-01-568-1815 (5306015681815) | 5340-00-720-7040 (5340007207040) | |
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