MRC | Criteria | Characteristic |
---|---|---|
AGAV | END ITEM IDENTIFICATION | F-404 ENGINE, F/A-18 HORNET AIRCRAFT |
CQQN | (NON-CORE DATA) EXTERNAL PROTECTION TYPE AND LOCATION | BOTH ENDS CHAFE GUARD, SPIRALLY WRAPPED POLYTETRAFLUOROETHYLENE |
MEDA | MEDIA FOR WHICH DESIGNED | FUEL/OIL, HYDROCARBON SINGLE RESPONSE |
SR-1 | SPEC/STD CONTROLLING DATA | |
CBBL | FEATURES PROVIDED | IDENTICAL ENDS |
CRXX | MEASURING METHOD AND LENGTH | 7.350 INCHES MINIMUM WORKING AND 7.470 INCHES MAXIMUM WORKING |
ADJM | (NON-CORE DATA) INNER CONVEYING TUBE MATERIAL | STEEL, CORROSION RESISTING |
SR-1 | MANUFACTURERS CODE | 99207 |
CRJM | OUTER COVERING ENVIRONMENTAL PROTECTION | ABRASION RESISTANT |
SR-1 | MFR SOURCE CONTROLLING REFERENCE | 4058T62 |
CRDW | HYDROSTATIC TEST PRESSURE | 2400.0 POUNDS PER SQUARE INCH |
CRTL | CRITICALITY CODE JUSTIFICATION | FEAT |
FEAT | SPECIAL FEATURES | WEAPON SYSTEM ESSENTIAL |
AAGR | CROSS-SECTIONAL SHAPE STYLE | ROUND |
CQGM | MAXIMUM OPERATING PRESSURE | 1200.0 POUNDS PER SQUARE INCH |
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