NSN 5310-01-509-8621 · NIIN 015098621 · FSC 5310
NO DASHES 5310015098621
In Stock
NUT,SELF-LOCKING,PLATE
Nuts and Washers
Application: F100 ENGINES
Technical characteristics
17 rows
Straight from the federal item record. Entries the record leaves empty are shown empty — nothing is filled in on its behalf.
| MRC | Requirement | Value |
|---|---|---|
| AAJD | THREAD CLASS | 3B |
| AAJF | THREAD DIRECTION | RIGHT-HAND |
| AAUM | LOCKING FEATURE | PREVAILING TORQUE ALL METAL DESIGN |
| AAWY | COUNTERBORE DIAMETER | FIRST END INCHES MINIMUM 0.194 |
| ACTA | NUT STYLE | |
| ACVN | NUT LENGTH | INCHES MAXIMUM 0.903 |
| ADEA | NUT HEIGHT | INCHES MAXIMUM 0.202 |
| ADEB | PLATE THICKNESS | INCHES MAXIMUM 0.036 |
| ADEC | PLATE WIDTH | INCHES MAXIMUM 0.328 |
| ADFK | NUT COUNTERBORE DEPTH | FIRST END INCHES MINIMUM 0.062 |
| AGAV | END ITEM IDENTIFICATION | F100 ENGINES |
| BZRR | THREAD SERIES | UNIFIED NATIONAL JOINT FINE (UNJF) |
| CMLP | THREAD QUANTITY PER INCH | 32 |
| CQJX | NOMINAL THREAD SIZE | INCHES 0.190 |
| CRTL | CRITICALITY CODE JUSTIFICATION | FEAT |
| FEAT | SPECIAL FEATURES | THE ITEM IS AN AVIATION CRITICAL SAFETY ITEM/FLIGHT SAFETY CRITICAL AIRCRAFT PART (ACSI/FSCAP). THIS SELF-LOCKING NUT PLATE FOR THE 220 & SS0 ENGINE IS MADE OF (AMS 5525, 5736 OR 5739, SST ALLOY, 0.940 INCH LONG BY 0.215" TALL W/TWO RIVET HOLES & CENTRAL THREADED HOLE. FAILURE OF THIS NUT COULD CAUSE LIBERATION OF THE AFT END NOZZLE SEGMENT BUT WOULD NOT CAUSE AN ENGINE SHUT DOWN OR CATASTROPHIC FAILURE. IT WOULD ALSO CAUSE MAINTENANCE TO REMOVE AND REPLACE BROKEN NUT AND/OR NOZZLE SEGMENT |
| MATT | MATERIAL | OVERALL IRON ALLOY 660 |