| MRC |
Requirement Statement |
Characteristics |
| MEDA |
MEDIA FOR WHICH DESIGNED |
HYDRAULIC FLUID, MIL-H-5606 SINGLE RESPONSE |
| FEAT |
SPECIAL FEATURES |
WEAPON SYSTEM ESSENTIAL |
| AARX |
INSIDE DIAMETER |
1.220 INCHES MINIMUM |
| SR-1 |
SPEC/STD CONTROLLING DATA |
|
| SR-1 |
MANUFACTURERS CODE |
82918 |
| CRJM |
OUTER COVERING ENVIRONMENTAL PROTECTION |
FIRE RESISTANT |
| CRTL |
CRITICALITY CODE JUSTIFICATION |
FEAT |
| AGAV |
END ITEM IDENTIFICATION |
KC-135 AIRCRAFT ENGINE |
| AAGR |
CROSS-SECTIONAL SHAPE STYLE |
ROUND |
| ABJH |
TEMP RATING |
-65.0 DEG FAHRENHEIT AND 400.0 DEG FAHRENHEIT SINGLE RESPONSE |
| CRXX |
MEASURING METHOD AND LENGTH |
21.250 INCHES NOMINAL WORKING |
| ABKV |
OUTSIDE DIAMETER |
1.558 INCHES MAXIMUM |
| CQGM |
MAXIMUM OPERATING PRESSURE |
1000.0 POUNDS PER SQUARE INCH |
| CRDW |
HYDROSTATIC TEST PRESSURE |
1800.0 POUNDS PER SQUARE INCH |
| SR-1 |
MFR SOURCE CONTROLLING REFERENCE |
458-50019-15 |
| CQBD |
BURST TEST PRESSURE |
3600.0 POUNDS PER SQUARE INCH |
| CRWL |
INSIDE SURFACE CONDITION |
CONVOLUTED |
