| MRC |
Requirement Statement |
Characteristics |
| AAJD |
THREAD CLASS |
3B SINGLE END |
| AAGT |
WALL THICKNESS |
0.035 INCHES NOMINAL |
| AJFY |
SEAT ANGLE IN DEG |
45.0 SINGLE END |
| AGAV |
III END ITEM IDENTIFICATION |
AIRCRAFT, GALAXY C-5 |
| ARJD |
DESIGN FORM |
PREBENT |
| AJFX |
END CONNECTION STYLE |
SWIVEL NUT WITH COMPRESSION SLEEVE SINGLE END |
| AHSA |
TUBING MATERIAL |
STEEL, CORROSION RESISTING |
| AFQW |
MATING END QUANTITY |
2 SINGLE END |
| CRTL |
CRITICALITY CODE JUSTIFICATION |
FEAT |
| FEAT |
SPECIAL FEATURES |
WEAPON SYSTEM ESSENTIAL; ASSEMBLY CONSISTS OF: TUBE P/N C5P27900-1, NUT,SLEEVE COUPLING P/N MS21921-4K, SLEEVE, COUPLING P/N MS21922-4C; NEXT HIGHER ASSEMBLY P/N 5900-105J |
| THSD |
THREAD SERIES DESIGNATOR |
UNJF SINGLE END |
| ABHP |
OVERALL LENGTH |
8.150 INCHES NOMINAL |
| AAJF |
THREAD DIRECTION |
RIGHT-HAND SINGLE END |
| BBYQ |
TUBE OUTSIDE DIAMETER |
0.250 INCHES NOMINAL |
| CQJX |
NOMINAL THREAD SIZE |
0.438 INCHES SINGLE END |
| MATL |
MATERIAL |
STEEL, CORROSION RESISTING SINGLE END |
