| AAJD | Thread Class | 3A |
| AAJF | Thread Direction | Right-hand |
| AASA | Thread Length | 0.378 inches minimum and 0.428 inches maximum |
| AASB | Fastener Length | 0.763 inches minimum and 0.793 inches maximum |
| AASK | Head Style | Flat countersunk |
| AASL | Head Diameter | 0.350 inches minimum and 0.399 inches maximum |
| AAUR | Grip Diameter | 0.2485 inches minimum and 0.2495 inches maximum |
| ABQZ | Internal Drive Style | Offset cruciform (torque set) |
| AHYM | Nominal Thread Diameter | 0.250 inches |
| ANEE | Grip Length | 0.365 inches minimum and 0.385 inches maximum |
| CMLP | Thread Quantity per Inch | 28 |
| CQBC | Minimum Tensile Strength | 160000 pounds per square inch |
| CQFM | Hardness Rating | 36.0 rockwell C minimum overall and 40.0 rockwell C maximum overall |
| CRSQ | Countersink Angle | 100.0 degrees nominal |
| CSYM | Surface Finish | 32.0 microinches grip |
| CSYM | Surface Finish | 32.0 microinches threads |
| MATT | Material | Steel comp E4340 overall or steel comp 4140 overall or steel comp 8740 overall or steel comp 8735 overall or steel comp 6150 overall |
| SFTT | Surface Treatment | Cadmium overall and chromate overall |
| STDC | Surface Treatment Document and Classification | QQ-P-416 TY2 CL2 fed spec single treatment response overall |
| THSD | Thread Series Designator | UNJF |
| ZZZK | Specification/Standard Data | 80205-NAS1581 professional/industrial association standar |
| 02 | F | Aircraft, Phantom F-4 |
| 19 | F | Aircraft, Eagle F-15 |
| 24 | F | Aircraft, Thunderbolt Ii, A-10 |
| 26 | F | Aircraft, F-16 |
| 32 | N | FA18 Aircraft Armament |
| 36 | F | Missile, Air Launch Cruise (Alcm) AGM-86B |
| 42 | F | Aircraft, T-38 |
| 43 | N | Aircraft, Hornet F/A-18 |
| AD | F | Missile, Advanced Medium Range Air-to-Air (AMRAAM)/AIM120A |
| DL | F | Engine, Aircraft, F100 PW220 (F-15C/D/E) |
| VM | N | F4S Aircraft |
| VU | N | Aircraft, Hornet F/A-18 (E/F) |
| Z5 | N | EA-18G (Growler) |
| Z9 | N | Aircraft, FA-18, a - D, E/F, G (Growler) |